From: Subject: Practical Guide to Free-Energy Devices - Chapter 8 Date: Sun, 28 Mar 2010 16:29:48 +0200 MIME-Version: 1.0 Content-Type: multipart/related; type="text/html"; boundary="----=_NextPart_000_0000_01CACE93.E2558410" X-MimeOLE: Produced By Microsoft MimeOLE V6.00.2900.5579 This is a multi-part message in MIME format. ------=_NextPart_000_0000_01CACE93.E2558410 Content-Type: text/html; charset="Windows-1252" Content-Transfer-Encoding: quoted-printable Content-Location: http://free-energy-info.co.uk/Chapt8.html Practical Guide to Free-Energy Devices - Chapter = 8
A Practical Guide to = Free-Energy=20 = Devices           =             &= nbsp;    =20 =             &= nbsp;           &n= bsp;           &nb= sp;           Auth= or:=20 Patrick J. Kelly

Chapter 8:=20 Self-Powered Engines

We have been raised = with the idea=20 that it is necessary to burn a fuel to produce power which we can = use.=20   We are sold coal, coke, timber, paraffin/kerosene, = petrol/gasoline,=20 diesel, propane, etc. for us to burn in order to =93get=94 energy. =  =20 While it is perfectly true that burning these things will indeed = result in=20 energy in a form which we find convenient to use in heating, = cooling,=20 powering engines, etc. what is carefully avoided is the fact that = it is=20 not at all necessary to burn a fuel in order to run the things = which we=20 want to power.   This =91inconvenient=92 fact has been = concealed and=20 denied for more than fifty years now (very surprisingly, by the = people who=20 want to sell us these fuels to burn =96 do you perhaps think that = they may=20 have some motive for this, other than our best interests which = they no=20 doubt are very concerned about?).

This chapter is about=20 =91fuel-less=92 motors.   Strictly speaking, they are not = =91self-powered=92=20 but as they don=92t burn a fuel of any kind, in everyday language = they can=20 be described as =91self-powered=92.   In the same way that a = solar panel=20 in sunlight uses no fuel and yet puts out electrical power, these = motors=20 draw energy from the environment and provide us with mechanical = power.=20   In actual fact, power is never =93used up=94 but just = converted from=20 one form into another.   In the case of our trusty solar = panel, some=20 17% of the radiation from the sun (mainly ultraviolet) is = converted into=20 electrical power and 83% goes in heating and other losses, but as = we don=92t=20 have to supply the sunlight, and the solar panel pours out the = electricity=20 which we want without us having to do anything to make it happen, = we=20 really don=92t care very much about its extremely low efficiency. =   As=20 far as we are concerned, the electricity flowing from the panel is = =93free-energy=94.

It is really amazing that we have been = persuaded=20 that we must burn a fuel in order to get power.   Take the = case of a=20 heavy-displacement sailing yacht.   The skipper can voyage = using his=20 inboard diesel engine:



This = matches perfectly with the thinking that you need to burn a fuel = in order=20 to get power as the yacht is moving along, pushed by the engine = which is=20 powered by burning diesel fuel.   But, what if the skipper = decides to=20 switch the engine off and set the sails?:


Now, = the=20 same boat, weighing exactly the same with the same crew, is now = continuing=20 the voyage at the same speed, but no fuel is being burnt.   = The=20 really interesting thing is that while we know this perfectly = well, and we=20 are aware that people have sailed right around the world in boats = which do=20 not have engines, it does not seem to occur to us that this shows=20 conclusively that it is not necessary to burn a fuel to power some = item of=20 equipment or form of transport.

In the case of our yacht, = the=20 energy comes from the sun which heats the atmosphere unevenly, = causing=20 winds to blow and the yachtsman uses the sails to make those winds = power=20 his boat through the water.   So, a sailing boat is actually = powered=20 by the sun although we don=92t usually think about it that way.=20

There are many hydro-electric =93power stations=94 where = electricity=20 is =91generated=92 by machines driven by water pressure.   In = actual=20 fact, no power is =91generated=92 at all, but instead, the = potential energy of=20 the body of water is converted into electricity by having = the water=20 fall and spin the shaft of a machine.   So, how did the water = get up=20 there in the first place?   Well, it came from rain.   = And how=20 did the rain get up there?  It rose up there due to = evaporation=20 caused by the heat of the sun.   So, the bottom line again is = that=20 hydro-electric =91power=92 stations are powered by the sun. =

Windmills=20 are also powered by the sun.   But, and here is the really=20 interesting thing, if I state that it is perfectly possible for a=20 compressed-air engine to produce mechanical power with burning any = fuel,=20 then there is an immediate and strong reaction where people will = say=20 =93Impossible =96 that is perpetual motion !!=94   They imply = that=20 perpetual motion is impossible but never supply any rational = evidence to=20 support that implication.   The Earth has been spinning on = its axis=20 for millions of years, so when exactly do they expect it to stop? =  =20 All the planets in the Solar System have been orbiting for = millions of=20 years, how long do they have to orbit before they can be = considered to be=20 in perpetual motion?   Why then are people so opposed to the = idea of=20 perpetual motion?   Presumably, because perpetual motion = shows=20 clearly that a fuel does not have to be burned to =91produce=92 = power and that=20 would not be good for people who sell fuels, and so, we are all = told from=20 an early age that perpetual motion is =93impossible=94. =

Well, that=20 does not matter here as we are going to look at compressed-air = engines=20 which run off the heat of the sun.   That is, they are = heat-pumps=20 which are a well accepted engineering fact and they work on wholly = accepted standard scientific principles.   An ordinary = refrigerator=20 outputs three or four times as much heat power as the electrical = power=20 driving it, and it could be twice that efficient if it were used = properly.=20   This is a Coefficient Of Performance (COP) of 3 or 4, which = is=20 supposed to be =93impossible=94 but unfortunately, all = refrigerators work like=20 this and you can=92t exactly say that refrigerators don=92t exist, = just=20 because their performance does not appear to fit in with some = theories.=20

Actually, there is no magic involved here as the extra = energy is=20 being drawn from the heat content of the air in the immediate = locality.=20   The refrigerator is not operating in isolation and there is = a heat=20 exchange with the air surrounding it.   This outside energy = causes=20 the COP>1 performance.   In passing, all COP>1 devices = operate=20 by drawing energy in from an external source (usually the = zero-point=20 energy field) and none of them actually break the =91rules=92 of = science.=20   But, enough of that.

The people who don=92t want = self-powered=20 engines used in the world today, pin their hopes on a continued = ignorance=20 of Engineering facts relating to heat pumps.   A = self-sustaining=20 compressed-air engine is actually running off power from the sun = just as=20 sailboats, windmills and hydro-electric power stations do.   = Sorry=20 folks, no magic here, just bog-standard Engineering.   = Admittedly,=20 very few people know or realise the implications of this standard=20 Engineering:
  1. All work done in compressing air into a storage tank is = converted=20 into heat and then lost to the atmosphere, so the energy in the=20 compressed air inside the tank is the same as that produced by=20 atmospheric heating of that air, but as more of it is now in the = tank,=20 there is additional potential for work to be done.   This = extra=20 energy was fed into the air by atmospheric heating before the = air was=20 compressed.

    The First Law of Thermodynamics states that = where=20 heat is converted into mechanical energy, or mechanical energy = is=20 converted into heat, the quantity of heat is exactly equivalent = to the=20 amount of mechanical energy.   We then have the intriguing=20 situation where all of the mechanical energy put into = compressing air=20 into a storage tank is lost as heat, and yet, the tank contents = now has=20 a higher potential for doing work.   This information comes = from=20 Engineering textbooks.
  2. If the expanded cold air leaving the engine is used to cool = the=20 intake air of the compressor, then there will be an added gain = when it=20 warms up inside the cylinder, pulling heat in from the local=20 environment.
  3. If the heat of compression is transferred to the air = container=20 feeding the engine and not given time to dissipate, then there = is a=20 further power gain for the engine.
  4. If compressed air is allowed to expand rapidly, there is a = marked=20 drop in temperature.   The Leroy Rogers engine design, = shown later=20 in this chapter, uses this fact to create air-conditioning for a = car=20 driven by a compressed-air engine.
OK then, in broad = outline,=20 the energy available from a tank of compressed air comes directly = from the=20 heat contained in the atmosphere, in spite of the fact that we = always=20 imagine that the energy in the tank was put there by our energetic = pumping.

Let=92s check this out by taking a look at some = of the=20 engines which use these principle to provide fuel-less operation, = starting=20 with the design of Bob Neal specified in his (slightly re-worded) = patent:=20

US Patent 2,030,759		       	      11th Feb. 1936			      Inventor:  Bob =
Neal 

COMPRESSOR=20 UNIT


This invention relates to the=20 construction of a compressor, and more particularly to a combined=20 fluid-operated engine and compressor.

The primary object = of the=20 invention, is the provision of a compressor of this character, = wherein=20 there is arranged an automatically counterbalanced crankshaft and = fluid=20 equalisers within a storage tank, which makes it possible for the = engine=20 to operate on constant reserve tank pressure, so as to actuate = additional=20 equipment, the pistons for the engine also being automatically = balanced=20 and suspended when the engine is operating.

Another object = of the=20 invention is the provision of an engine which is operated by air = under=20 pressure, the air being supplied by compressors which are in a = bank with=20 the engine construction.

A further object of this = invention is the=20 provision of an engine of this type of novel construction as the = engine=20 and the compressors are operated from the same crankshaft, which = is of the=20 automatically balanced type, so that high efficiency is attained.=20

A still further object of the invention is the provision = of an=20 engine of this character which is comparatively simple in = construction,=20 thoroughly reliable and efficient in its operation, strong, = durable, and=20 inexpensive to manufacture.

With these and other objects = in view,=20 the invention consists in the features of construction, = combination and=20 arrangement of parts as will be described more fully here, = illustrated in=20 the accompanying drawings which disclose the preferred embodiment = of the=20 invention, and pointed out in the appended Claim.


In the=20 drawings, Fig.1 is a perspective view of the engine = constructed in=20 accordance with the invention.



Fig.2= =20 is a vertical transverse cross-section view through the compressor = part of=20 the engine.



Fig.3= =20 is a vertical cross-sectional view through the power part of the=20 engine.



Fig.4= =20 is a detail elevation of the crankshaft of the engine.



Fig.5= =20 is an enlarged cross-sectional view through one of the electric = heaters=20 for the engine.



Fig.6= =20 is a vertical, longitudinal, cross-sectional view through the air = storage=20 tank, including the equaliser.


The same reference = numbers are=20 used for each individual part in every view in every drawing. =


Referrin= g=20 to the drawings in detail, the engine in its entirety, composes a = cylinder=20 block 10 having inside it, the series of compressor = cylinders=20 11 and the power cylinders 12.   The block = 10 is=20 of the V-type and the upper ends of the cylinders are closed off = by the=20 removable heads 13 and 14 which are held in place by = conventional head bolts 15.   Beneath block 10 = is the=20 crank case 16, which has detachable plates 17 at = opposite=20 sides, held in place by fasteners 18, and seated so as to = be leak=20 proof.   The block 10 is chambered to provide a water = jacket=20 19 surrounding the cylinders, while at the forward end of = the block=20 are water pumps 20, circulating water through the inlet = pipe=20 21 which leads into the jacket and the water exits from the = jacket=20 through the outlet pipe 22.   Beside the pumps = 20, is a=20 fan 23 which is operated from the same belt 24 which = drives=20 the pumps.

Working inside the cylinders 11,are the=20 reciprocating pistons 25, their rods 26 sliding = through=20 packing glands 27 and fixed to crossheads 28 which = slide on=20 their mounting guides 29 which are secured to the walls of = the=20 crank case 16.   These crossheads 28 are fitted = with=20 wrist pins 30, forming a pivoting connection with the = connecting=20 rods 31, which are connected to their cranks 33 by = their=20 bearings 32.   The cranks 33 form part of a = counter=20 balanced crankshaft 34, which is mounted in supports = 35=20 attached to the crank case 16, the shaft being provided = with the=20 required bearings 36.


The = inner=20 ends of the cylinders 11 are fitted with inner end heads = 37,=20 which are provided with air intake ports 38 fitted with = spring ball=20 inlet checks 39, the air entering through passages = 40 which=20 open outside the block 10.   Glands 27 are = mounted in=20 the heads 37.

The heads 13 and 37 are = provided with the compressed air outlets 41 and 42, = which=20 are fitted with spring ball checks 43.   The heads = 13=20 are also provided with the central air inlets 44, which are = fitted=20 with spring checks 45.   Couplings 46 attach = the air=20 outlets 41 and 42 to their outlet feed pipes = 47 and=20 48.   These pipes lead to a main conduit 49 = which is=20 located in the centre channel 50 of the block 10. =


At the = rear=20 end of the block 10, mounted on shaft 36, there is a = conventional flywheel 51.



Working = inside the cylinders 12 are the pistons 52, with = their=20 piston rods 53 sliding through packing glands 54 and = fixed=20 in crossheads 55 which slide along their mounting guides = 56,=20 mounted on the inner walls of the crank case 16.   The = crossheads=20 55 have wrist pins 57 which provide a pivoting joint = for the=20 connecting rods 58 which are connected by their bearings = 59=20 to their cranks 60 of the crank shaft 34, the inner = ends of=20 the cylinders 12 being closed by the inner heads 61 = and=20 their associated glands 54.

On the cylinders = 12 are=20 slide valve chests 62 in which are the slide valves = 63,=20 these being operated by throw rods 64 actuated by cams = 65=20 and the valves controlling the admission and exhaust of air into = and out=20 of the cylinders 12, through the ports 66 and = 67, and=20 these valves 63 are provided with ports 68 for the = delivery=20 of air under pressure from the inlet passages 69 common to = a pipe=20 70 coming from a compressed air storage tank 71. =

The=20 bottom of the crank case 16 is fitted with a removable = plate=20 72 which is secured in place by fasteners 73, and = when this=20 plate is removed, it provides access to the crank shaft 34 = and the=20 bearings for the engine, as well as other parts inside the crank = case.=20


Leading = into the cylinders 11 are the passages 74 of a = lubricating=20 system (not shown).   The compressed air storage tank = 71 has=20 inside it a double-check discharge nozzle 75, supported by = member=20 76.   Leading to this equaliser is an air inlet pipe = 77=20 which connects through its valved section 78 to the = compressed air=20 reservoir 79.   In the equaliser 75, are the = spaced=20 spring ball checks 80 and 81, one being for the = inlet side=20 and the other for the outlet side of the equaliser.   This = pipe=20 77 is connected with the main conduit 49, while a = pipe=20 82 connects to pipe 70.   The tank is also = fitted with=20 an automatic relief valve 83 and this valve can be of any = approved=20 type.


Placed=20 around the pipes 70 which connect to the air passages = 69=20 (Fig.3) are electric heating units 84 to heat the=20 pressurised air to above freezing temperature when delivered from = tank=20 71 to the cylinders 12.   Supported on the = block=20 10 is an electric generator 85 which is driven from = the=20 shaft 34 (Fig.2) through a belt 24 = (Fig.1) and=20 this generator is included in an electric circuit which also has = the=20 heaters 84 so that these will operate from current supplied = by the=20 generator.

The compressed air storage tank 71 with = the=20 equaliser is constructed so that it is possible to pump air into = it while=20 it contains an air pressure of 200 pounds per square inch while = the=20 compressors are only pumping against 15 pounds per square inch of=20 (atmospheric) pressure.   An outside air pressure source can = be=20 coupled with the tank to augment that pressure derived from the = cylinders=20 11 of the engine.

CLAIMS

What = is=20 claimed is:
In a structure of the kind described, a V-shaped = cylinder=20 block provided with upwardly divergent cylinders, end heads fitted = to said=20 cylinders at opposite ends thereof, each head having valved inlets = and=20 outlets, a main outlet lead between the cylinders of the block for = a=20 storage tank and having lateral branches to the outlets at the = inner sides=20 of said heads, one inlet being located at the centre of each head = at the=20 outer ends of said cylinders while the remaining inlets are at the = outer=20 sides of the heads at the inner ends of said cylinders, a = substantially=20 V-shaped crank case fitted to the block beneath the cylinders, a=20 counterbalanced crank shaft journaled in the crank case, pistons = operating=20 in the cylinders and having rods extended into the crank case, = crosshead=20 guides fitted to the interior sides of said case, crossheads = connecting=20 the rods with the guides and sliding on them and connecting rods = operated=20 by the crank shaft and pivoted at the crossheads in order to allow = reciprocation of the pistons.


************************


You will = notice=20 that Bob has avoided any direct mention of the fact that his = engine design=20 is fuel-less.   That sort of statement is not popular with = Patent=20 Examiners even if it is perfectly true.

This system could = do with=20 some further explanation, so here is an idea from Scott = Robertson's web site, for a = possible=20 working compressor system using a leaf-blower:



Whil= e=20 this looks rather complicated, in reality it really isn=92t. =   Let=92s=20 take the different sections in order:




Firs= t,=20 you have an ordinary air engine, supplied with compressed air from = a=20 pressure tank.   This engine exhausts its (cold, expanded) = air to the=20 atmosphere.   The engine powers two compressors which between = them=20 keep the tank full of compressed air.



The = first compressor is a simple =91leaf-blower=92 type which produces = a large=20 volume of low-pressure air.   The big question is =93how do = you get=20 this large volume of low-pressure air into a tank which has = high-pressure=20 compressed air inside it?=94.   Well this seemingly = impossible task is=20 performed by the second compressor aided by a cunning, = ultra-simple=20 design:



Here= ,=20 low-pressure air is fed into the low-pressure area marked in pink. =  =20 Separating it from the high-pressure area is a metal plug marked = in green.=20   Set into this plug is a ring of five one-way air valves = marked in=20 red.   These one-way valves let the low-pressure air into the = high-pressure area because of a high-speed jet of air produced by = the=20 =91jet-drive compressor=92.   At first glance, this seems = impossible, but=20 it is actually just an application of a standard Engineering = technique.=20   The high-speed air jet is directed through a specially = shaped=20 nozzle, creating a local low-pressure zone around the jet: =


The=20 low-pressure air at point =93A=94 flows through the ring of = five=20 one-way valves into the disc-shaped low pressure area = =93B=94 and is=20 blasted into the high-pressure area =93C=94 by the = high-power air jet=20 ripping through the doughnut-shaped ring marked in yellow.   = The=20 high-speed air jet causes the low pressure ring =93B=94 by = its rapid=20 movement which creates a vortex due to the shape and positioning = of the=20 doughnut-shaped ring marked in yellow.   This clever = arrangement=20 allows large volumes of low-pressure air to be drawn into a tank = which=20 contains high-pressure air.

You will also note that the = two-stage=20 compressor which generates this high-speed jet of air, has its = working=20 area actually inside the tank.   This means that the heat of=20 compression is used to heat the air inside the tank and raise its=20 pressure, enhancing the operation further.   It should be = borne in=20 mind that the new air entering the system has been heated by the = sun and=20 contains the energy which powers the system. =



The Leroy Rogers Engine.
This=20 engine is driven by compressed air.   This principle is very = easily=20 understood and is not a long way from the operation of = steam-powered=20 railway engines of years gone by.   What is not generally = realised is=20 that more energy is available from compressed air than the energy = required=20 to compress the air in the first place.   Another detail not=20 generally realised is that simple heat energy can be drawn from = the local=20 environment and used to help power the air compressor in a design = of this=20 type.

The Rogers motor shown here makes no claims to = spectacular=20 operation, but in spite of that, Leroy did admit in an interview = that this=20 motor does indeed have a greater output than the applied input, = provided=20 that the motor is not left just ticking over.   This motor is = like=20 the US patent 3,744,252 =93Closed Motive Power System Utilising = Compressed=20 Fluids=94 by Eber Van Valkinburg shown below.   However, the = Rogers=20 patent shown here has the distinct advantage that it uses = off-the-shelf=20 motors and readily available hardware and there is nothing really = exotic=20 or difficult about the Rogers engine that a person couldn=92t get = from a=20 valve supplier or get a metal fabrication company to construct.=20

Present day vehicle engines are under-geared and run at = fairly low=20 revs.   These same engines operate much more efficiently at = higher=20 revs, if they are given different gearing.   With the Rogers = motor,=20 the air contained in the high-pressure tank is sufficient to drive = the=20 pistons up and down.   The exhaust air can be captured in a = buffer=20 tank and pumped back into the high-pressure tank by a compressor = with much=20 higher gearing and much lower capacity per piston stroke.   = The=20 expanded air exiting from the engine is at much lower temperature = than the=20 surrounding air.   This gives it higher density and so the=20 re-compression efficiency is raised and in addition, once back in = the=20 storage tank it=92s temperature rises again which boosts the = pressure in the=20 storage tank, courtesy of the heat from the local environment.=20

Here is a slightly re-worded copy of the Lee Rogers = patent:=20

Patent  US 4,292,804 		       6th October 1980  		 =
      Inventor: Leroy K. Rogers

METHOD=20 AND APPARATUS FOR OPERATING AN ENGINE ON COMPRESSED GAS=20


ABSTRACT

The present invention = relates to a=20 method and apparatus for operating an engine having a cylinder = containing=20 a reciprocating piston driven by a compressed gas.   The = apparatus=20 comprises a source of compressed gas connected to a distributor = which=20 conveys the compressed gas to the cylinder.   A valve is = provided to=20 admit compressed gas to the cylinder when the piston is in an=20 approximately Top Dead Centre position.

In one embodiment = of the=20 present invention, the timing of the opening of the valve is = advanced so=20 that the compressed gas is admitted to the cylinder progressively = further=20 before the Top Dead Centre position of the piston as the speed of = the=20 engine increases.

In a further embodiment of the present=20 invention, a valve actuator is provided which increases the length = of time=20 over which the valve remains open to admit compressed gas to the = cylinder=20 as the speed of the engine increases.

A still further = embodiment=20 of the present invention relates to an apparatus for adapting a=20 conventional internal combustion engine for operation on = compressed gas.=20

US Patent References:
3,881,399	May., 1975	=
Sagi et al.            91/187.
3,885,387	May., 1975	Simington            60/407.
4,018,050	Apr., 1977	 Murphy	                60/412.

DESCRIPTION

BACKGROUND AND SUMMARY OF THE = PRESENT INVENTION


The present invention is a = method and=20 apparatus for operating an engine using a compressed gas as the = motive=20 fluid.   More particularly, the present invention relates to = a=20 apparatus for adapting a pre-existing internal combustion engine = for=20 operation on a compressed gas.

Air pollution is one of the = most=20 serious problems facing the world today.   One of the major=20 contributors to air pollution is the ordinary internal combustion = engine=20 which is used in most motor vehicles today.   Various = devices,=20 including many items required by legislation, have been proposed = in an=20 attempt to limit the pollutants which an internal combustion = engine=20 exhausts to the air.   However, most of these devices have = met with=20 limited success and are often both prohibitively expensive and = complex.=20   A clean alternative to the internal combustion engine is = needed to=20 power vehicles and other machinery.

A compressed gas, = preferably=20 air, would provide an ideal motive fluid for an engine, since it = would=20 eliminate the usual pollutants exhausted from an internal = combustion=20 engine.   An apparatus for converting an internal combustion = engine=20 for operation on compressed air is disclosed in U.S. Pat. No. = 3,885,387=20 issued May 27, 1975 to Simington.   The Simington patent = discloses an=20 apparatus including a source of compressed air and a rotating = valve=20 actuator which opens and closes a plurality of mechanical poppet = valves.=20   The valves deliver compressed air in timed sequence to the=20 cylinders of an engine through adapters located in the spark plug = holes.=20   However, the output speed of an engine of this type is = limited by=20 the speed of the mechanical valves and the fact that the length of = time=20 over which each of the valves remains open cannot be varied as the = speed=20 of the engine increases.

Another apparatus for converting = an=20 internal combustion engine for operation on steam or compressed = air is=20 disclosed in U.S. Pat. No. 4,102,130 issued July 25, 1978 to = Stricklin.=20   The Stricklin patent discloses a device which changes the = valve=20 timing of a conventional four stroke engine such that the intake = and=20 exhaust valves open once for every revolution of the engine = instead of=20 once every other revolution of the engine.   A reversing = valve is=20 provided which delivers live steam or compressed air to the intake = valves=20 and is subsequently reversed to allow the exhaust valves to = deliver the=20 expanded steam or air to the atmosphere.   A reversing valve = of this=20 type however does not provide a reliable apparatus for varying the = amount=20 of motive fluid injected into the cylinders when it is desired to = increase=20 the speed of the engine.   Further, a device of the type = disclosed in=20 the Stricklin patent requires the use of multiple reversing valves = if the=20 cylinders in a multi-cylinder engine were to be fired = sequentially.=20

Therefore, it is an object of the present invention to = provide a=20 reliable method and apparatus for operating an engine or = converting an=20 engine for operation with a compressed gas.

A further = object of=20 the present invention is to provide a method and apparatus which = is=20 effective to deliver a constantly increasing amount of compressed = gas to=20 an engine as the speed of the engine increases.

A still = further=20 object of the present invention is to provide a method and = apparatus which=20 will operate an engine using compressed gas at a speed sufficient = to drive=20 a conventional automobile at highway speeds.

It is still a = further=20 object of the present invention to provide a method and apparatus = which is=20 readily adaptable to a standard internal combustion engine, to = convert the=20 internal combustion engine for operation with a compressed gas.=20

Another object of the invention is to provide a method and = apparatus which utilises cool expanded gas, exhausted from a = compressed=20 gas engine, to operate an air-conditioning unit and/or an = oil-cooler.=20

These and other objects are realised by the method and = apparatus=20 of the present invention for operating an engine having at least = one=20 cylinder containing a reciprocating piston and using compressed = gas as the=20 motive fluid.   The apparatus includes a source of compressed = gas, a=20 distributor connected it for conveying the compressed gas to the = cylinder=20 or cylinders.   A valve is provided for admitting the = compressed gas=20 to the cylinder when the piston is in an approximately Top Dead = Centre=20 position within the cylinder.   An exhaust is provided for = exhausting=20 the expanded gas from the cylinder as the piston returns to = approximately=20 the Top Dead Centre position.

In a preferred embodiment of = the=20 present invention, a device is provided for varying the duration = of each=20 engine cycle over which the valve remains open to admit compressed = gas to=20 the cylinder, dependent upon the speed of the engine.   In a = further=20 preferred embodiment of the present invention, an apparatus for = advancing=20 the timing of the opening of the valve is arranged to admit the = compressed=20 gas to the cylinder progressively further and further before the = Top Dead=20 Centre position of the piston, as the speed of the engine = increases.=20

Further features of the present invention include a valve = for=20 controlling the amount of compressed gas admitted to the = distributor.=20   Also, a portion of the gas which has been expanded in the = cylinder=20 and exhausted through the exhaust valve, is delivered to a = compressor to=20 be compressed again and returned to the source of compressed gas. =   A=20 gear train can be engaged to drive the compressor selectively at = different=20 operating speeds, depending upon the pressure maintained at the = source of=20 compressed air and/or the speed of the engine.   Still = further, a=20 second portion of the exhaust gas is used to cool a lubricating = fluid for=20 the engine or to operate an air-conditioning unit.

In a = preferred=20 embodiment of the present invention, the valve for admitting = compressed=20 gas to the cylinder is operated electrically.   The device = for=20 varying the duration of each engine cycle, over which the intake = valve=20 remains open, as the speed of the engine increases, comprises a = rotating=20 element whose effective length increases as the speed of the = engine=20 increases, causing a first contact on the rotating element to be=20 electrically connected to a second contact on the rotating = element, for a=20 longer period of each engine cycle.   The second contact = operates the=20 valve causing it to remain in an open position for a longer period = of each=20 engine cycle, as the speed of the engine increases.

Still = further=20 features of the present invention include an adaptor plate for = supporting=20 the distributor above the intake manifold of a conventional = internal=20 combustion engine after a carburettor has been removed to allow = air to=20 enter the cylinders of the engine through the intake manifold and=20 conventional intake valves.   Another adaptor plate is = arranged over=20 an exhaust passageway of the internal combustion engine to reduce = the=20 cross-sectional area of the exhaust passageway. =

BRIEF=20 DESCRIPTION OF THE DRAWINGS
Preferred embodiments of a = method=20 and apparatus for operating an engine according to the present = invention=20 will be described with reference to the accompanying drawings in = which=20 components have the same reference numbers in each drawing.=20

Fig.1 is a schematic representation of an apparatus = according to the present invention arranged on an engine:




<= B>Fig.2=20 is a side view of one embodiment of a valve actuator according to = the=20 present invention.


Fi= g.3=20 is a cross-sectional view taken along the line 3--3 in=20 Fig.2.




<= B>Fig.4=20 is a cross-sectional view of a second embodiment of a valve = actuator=20 according to the present invention.



<= B>Fig.5=20 is a view taken along the line 5--5 in Fig.4.



<= B>Fig.6=20 is a cross-sectional view of a third embodiment of a valve = actuator=20 according to the present invention;



<= B>Fig.7=20 is a view taken along the line 7--7 in Fig.6.



<= B>Fig.8=20 is a cross-sectional view of a gearing unit to drive a compressor=20 according to the present invention.



<= BR>DETAILED=20 DESCRIPTION OF THE PREFERRED EMBODIMENTS

With = reference to=20 Fig.1, an engine block 21 (shown in phantom) having = two=20 banks of cylinders with each bank including cylinders 20 = having=20 pistons 22 which reciprocate in them in a conventional = manner (only=20 one of which is shown in phantom).   While the illustrated = engine is=20 a V-8 engine, it will be apparent that the present invention is = applicable=20 to an engine having any number of pistons and cylinders with the = V-8=20 engine being utilised for illustration purposes only.   A = compressed=20 gas tank 23 is provided to store a compressed gas at high = pressure.=20   It may also be desirable to include a small electric or gas = compressor to provide compressed gas to supplement the compressed = gas held=20 in the tank 23.   In a preferred embodiment, the = compressed=20 gas is air which can be obtained from any suitable source. =




A= =20 line 25 transports the gas withdrawn from the tank = 23 when a=20 conventional shut-off valve 27 is open.   In addition, = a=20 solenoid valve 29 preferably operated by a suitable = key-operated=20 engine switch (not shown) is also placed in the line 25. =   In=20 normal operation, the valve 27 is maintained open at all = times with=20 the solenoid valve 29 operating as a selective shut off = valve to=20 start and stop the engine 21.

A suitable regulating = valve=20 31 is arranged downstream of the solenoid valve 29 = and is=20 connected by a linkage 33 to a throttle linkage 35 = which is=20 operator-actuated by any suitable apparatus such as a foot pedal = (not=20 shown).   The line 25 enters an end of a distributor = 33=20 and is connected to an end of a pipe 35 which is closed at = the=20 other end.   A plurality of holes, which are equal to the = number of=20 cylinders in the engine 21, are provided on either side of = the pipe=20 35 along the length of the pipe 35.

When the = present=20 invention is used to adapt a conventional internal combustion = engine for=20 operation on compressed gas, an adaptor plate 36 is = provided to=20 support the distributor 33 in spaced relation from the = usual intake=20 opening in the intake manifold of the engine after a conventional=20 carburettor has been removed.   In this way, air is permitted = to=20 enter the internal combustion engine through the usual passageways = and to=20 be admitted to the cylinders through suitable intake valves (not = shown).=20   The adaptor plate 36 is attached to the engine block = 21 and the distributor 33 by any suitable apparatus, = e.g.,=20 bolts.

Each of the holes in the pipe 35 is = connected in=20 fluid-tight manner to a single line 37.   Each line = 37=20 carries the compressed gas to a single cylinder 20.   = In a=20 preferred embodiment, each of the lines 37 is 1/2 inch high = pressure plastic tubing attached through suitable connectors to = the=20 distributor 33 and the pipe 35.   Each of the = lines=20 37 is connected to a valve 39 which is secured in an = opening=20 provided near the top of each of the cylinders 20.   = In the=20 case of a conversion of a standard internal combustion engine, the = valves=20 39 can be conveniently screwed into a tapped hole in the = cylinder=20 20 typically provided for a spark plug of the internal = combustion=20 engine.   In a preferred embodiment, the valves 39 are = solenoid actuated valves in order to provide a fast and reliable = opening=20 and closing of the valves 39.

Each of the valves = 39=20 is energised by a valve actuator 41 through one of a = plurality of=20 wires 43.   The valve actuator 41 is driven by = a shaft=20 of the engine similar to the drive for a conventional distributor = of an=20 internal combustion engine.   That is, a shaft 55 of = the valve=20 actuator 41 is driven in synchronism with the engine = 21 at=20 one half the speed of the engine 21.


A = first=20 embodiment of the valve actuator 41 (Fig.2 and=20 Fig.3), receives electrical power through a wire 45 = which is=20 energised in a suitable manner by a battery, and a coil if = necessary (not=20 shown) as is conventional in an internal combustion engine.   = The=20 wire 45 is attached to a central post 47 by a nut = 49.=20   The post 47 is connected to a conducting plate = 51=20 arranged in a housing 53 for the valve actuator 41. =  =20 Within the housing 53, the shaft 55 has an = insulating=20 element 57 secured to an end of the shaft 55 and = rotates=20 with it when the shaft 55 is driven by the engine = 21.  =20 A first end of a flexible contact 59 is continuously biased = against=20 the conducting plate 51 to receive electricity from the = battery or=20 other suitable source.   The other end of the contact = 59 is=20 connected to a conducting sleeve 60 which is in constant = contact=20 with a spring biased contact 61 which is arranged within = the sleeve=20 60.   The contact 61 is pressed by a spring = 63=20 which pushes contact 61 towards a side wall of the housing=20 53.



With = reference to Fig.3, a plurality of contacts 65 are = spaced=20 from one another and are arranged around the periphery of the = housing=20 53 at the same level as the spring biased contact = 61.  =20 Each contact 65 is electrically connected to a post = 67 which=20 extends outside of the housing 53.   The number of = contacts=20 65 is equal to the number of cylinders in the engine = 21.=20   One of the wires 43, which actuate the valves = 39, is=20 secured to each of the posts 67.

In operation, as = the shaft=20 55 rotates in synchronism with the engine 21, the = insulating=20 element 57 rotates and electricity is ultimately delivered = to=20 successive pairs of the contacts 65 and wires 43 = through the=20 spring loaded contact 61 and the flexible contact = 59.  =20 In this way, each of the electrical valves 39 is activated = and=20 opened in the proper timed sequence to admit compressed gas to = each of the=20 cylinders 20 to drive the pistons 22 on a downward = stroke.=20

The embodiment illustrated in Fig.2 and = Fig.3 is=20 effective in causing each of the valves 39 to remain open = for a=20 long enough period of time to admit sufficient compressed gas to = each of=20 the cylinders 20 of the engine 21 to drive the = engine=20 21.   The length of each of the contacts 65 = around the=20 periphery of the housing 53 is sufficient to permit the = speed of=20 the engine to be increased when desired by the operator by moving = the=20 throttle linkage 35 which actuates the linkage 33 to = further=20 open the regulating valve 31 to admit more compressed gas = from the=20 tank 23 to the distributor 33.   However, it = has been=20 found that the amount of air admitted by the valves 39 when = using=20 the first embodiment of the valve actuator 41 (Fig.2 = and=20 Fig.3) is substantially more than required to operate the = engine=20 21 at an idling speed.   Therefore, it may be = desirable to=20 provide a valve actuator 41 which is capable of varying the = duration of each engine cycle over which the solenoid valves = 39 are=20 actuated, i.e., remain open to admit compressed gas, as the speed = of the=20 engine 21 is varied.



A = second=20 embodiment of a valve actuator 41 which is capable of = varying the=20 duration of each engine cycle over which each of the valves = 39=20 remains open to admit compressed gas to the cylinders 20 = dependent=20 upon the speed of the engine 21 will be described with = reference to=20 Fig.4 and Fig.5 wherein members corresponding to = those of=20 Fig.2 and Fig.3 bear like reference numbers.   = The wire=20 45 from the electricity source is attached to the post = 47 by=20 the nut 49.   The post 47 has a annular contact = ring=20 69 electrically connected to an end of the post 47 = and=20 arranged within the housing 53.   The shaft 55 = rotates=20 at one half the speed of the engine as in the embodiment of = Fig.2=20 and Fig.3.



At = an=20 upper end of the shaft 55, a splined section 71 = receives a=20 sliding insulating member 73.   The splined section = 71=20 of the shaft 55 holds the insulating member 73 = securely as=20 it rotates with shaft 55 but permits the insulating member=20 73 to slide axially along the length of the splined section = 71.   Near the shaft 55, a conductive sleeve = 72=20 is arranged in a bore 81 in an upper surface of the = insulating=20 element 73 generally parallel to the splined section = 71.=20   A contact 75, biased towards the annular contact = ring=20 69 by a spring 77, is arranged within the conductive = sleeve=20 72 and in contact with it.   The conductive sleeve = 72=20 also contacts a conductor 79 at a base of the bore = 81.=20

The conductor 79 extends to the upper surface of = the=20 insulating element 73 near an outer periphery of the = insulating=20 element 73 where the conductor 79 is electrically = connected=20 to a flexible contact 83.   The flexible contact = 83=20 connects, one after the other, with a series of radial contacts = 85=20 which are positioned on an upper inside surface of the housing = 53.=20   A weak spring 87 arranged around the splined section = 71 engages a stop member 89 secured on the shaft = 55=20 and the insulating element 73 to slightly bias the = insulating=20 element 73 towards the upper inside surface of the housing=20 53 to ensure contact between the flexible contact 83 = and the=20 upper inside surface of the housing 53.   As best seen = in=20 Fig.5, the radial contacts 85 on the upper inside = surface of=20 the housing 53 are arranged generally in the form of radial = spokes=20 extending from the centre of the housing 53 with the number = of=20 contacts being equal to the number of cylinders 20 in the = engine=20 21.   The number of degrees covered by each of the = radial=20 contacts 85 gradually increases as the distance from the = centre of=20 the upper inside surface of the housing 53 increases. =

In=20 operation of the device of Fig.4 and Fig.5, as the = shaft=20 55 rotates, electricity flows along a path through the wire = 45 down through post 47 to the annular contact = member=20 69 which is in constant contact with the spring biased = contact=20 75.   The electrical current passes through the = conductive=20 sleeve 72 to the conductor 79 and then to the = flexible=20 contact 83.   As the flexible contact 83 = rotates along=20 with the insulating member 73 and the shaft 55, the = tip of=20 the flexible contact 83 successively engages each of the = radial=20 contacts 85 on the upper inside of the housing 53. =   As=20 the speed of the shaft 55 increases, the insulating member=20 73 and the flexible contact 83 attached to it, move = upwards=20 along the splined section 71 of the shaft 55 due to = the=20 radial component of the splines in the direction of rotation under = the=20 influence of centrifugal force.   As the insulating member = 73=20 moves upwards, the flexible contact 83 is bent so that the = tip of=20 the contact 83 extends further outwards radially from the = centre of=20 the housing 53 (as seen in phantom lines in Fig.4). =  =20 In other words, the effective length of the flexible contact = 83=20 increases as the speed of the engine 21 increases. =

As the=20 flexible contact 83 is bent and the tip of the contact = 83=20 moves outwards, the tip remains in contact with each of the radial = contacts 85 for a longer period of each engine cycle due to = the=20 increased angular width of the radial contacts with increasing = distance=20 from the centre of the housing 53.   In this way, the = length=20 of time over which each of the valves 39 remains open is = increased=20 as the speed of the engine is increased.   Thus, a larger = quantity of=20 compressed gas or air is injected into the cylinders as the speed=20 increases.   Conversely, as the speed decreases and the = insulating=20 member 73 moves downwards along the splined section = 71, a=20 minimum quantity of air is injected into the cylinder due to the = shorter=20 length of the individual radial contact 85 which is in = contact with=20 the flexible contact 83.   In this way, the amount of=20 compressed gas that is used during idling of the engine 21 = is at a=20 minimum whereas the amount of compressed gas which is required to = increase=20 the speed of the engine 21 to a level suitable to drive a = vehicle=20 on a highway is readily available.



Shown= in=20 Fig.6 and Fig.7, is a third embodiment of a valve = actuator=20 41 according to the present invention.   This = embodiment=20 includes a curved insulating element 91 having it=92s first = end able=20 to pivot, being secured by any suitable device such as screw = 92 to=20 the shaft 55 for co-rotation with the shaft 55. =   The=20 screw 92 is screwed into a tapped hole in the insulating = element=20 91 so that a tab 94 at an end of the screw 92 = engages=20 a groove 96 provided in the shaft 55.   In this = way,=20 the insulating element 91 rotates positively with the shaft = 55.   However, as the shaft 55 rotates faster, = the=20 other end 98 of the insulating element 91 is = permitted to=20 pivot outwards under the influence of centrifugal force because of = the=20 groove 96 provided in the shaft 55.   A spring=20 93, connected between the second end 98 of the = element=20 91 and the shaft 55 urges the second end of the = element=20 91 towards the centre of the housing 53.



A=20 contact 99 similar to the contact 59 (Fig.2) = is=20 arranged so that one end of the contact piece 99 is in = constant=20 contact with the conducting plate 51 located centrally = within the=20 housing 53.   The other end of the contact 99 = engages a=20 conductive sleeve 101 arranged in bore 102.   A = contact=20 element 95 is arranged in the conductive sleeve 101 = in=20 constant contact with the sleeve 101.   The bore = 102 is=20 arranged generally parallel to the shaft 55 near the second = end of=20 the curved insulating element 91.   The contact = 95 is=20 biased by a spring 97 towards the upper inside surface of = the=20 housing 53 for selective contact with each of the plurality = of=20 radial contacts 85 which increase in arc length towards the = outer=20 peripheral surface of the housing 53 (Fig.6). =

When=20 the device shown in Fig.6 and Fig.7 is operating, as = the=20 shaft 55 rotates the curved insulating element 91 = rotates=20 with the shaft 55 and the second end 98 of the = insulating=20 element 91 tends to pivot about the shaft 55 due to=20 centrifugal force.   Thus, as the effective length of the = contact=20 95 increases, i.e., as the curved insulating element = 91=20 pivots further outwards, the number of degrees of rotation over = which the=20 contact 95 is in contact with each of the radial contacts = 85=20 on the upper inside surface of the housing 53 increases = thereby=20 allowing each of the valves 39 to remain open for a longer = period=20 of each engine cycle, which in turn, allows more compressed gas = enter the=20 respective cylinder 20 to further increase the speed of the = engine=20 21.

With reference to Fig.1, a mechanical = advance=20 linkage 104 which is connected to the throttle linkage = 35,=20 advances the initiation of the opening of each valve 39 = such that=20 compressed gas is injected into the respective cylinder further = before the=20 piston 22 in the respective cylinder 20 reaches a = Top Dead=20 Centre position as the speed of the engine is increased by moving = the=20 throttle linkage 35.   The advance linkage 104 = is=20 similar to a conventional standard mechanical advance employed on = an=20 internal combustion engine.   In other words, the linkage = 104=20 varies the relationship between the angular positions of a point = on the=20 shaft 55 and a point on the housing 53 containing = the=20 contacts.   Alternatively, a conventional vacuum advance = could also=20 be employed.   By advancing the timing of the opening of the = valves=20 39, the speed of the engine can more easily be increased.=20

The operation of the engine cycle according to the present = invention will now be described.   The compressed gas = injected into=20 each cylinder of the engine 21 drives the respective piston = 22 downwards to rotate a conventional crankshaft (not = shown).=20   The movement of the piston downwards causes the compressed = gas to=20 expand rapidly and cool.   As the piston 22 begins to = move=20 upwards in the cylinder 20 a suitable exhaust valve (not = shown),=20 arranged to close an exhaust passageway, is opened by any suitable = apparatus.   The expanded gas is then expelled through the = exhaust=20 passageway.   As the piston 22 begins to move = downwards again,=20 a suitable intake valve opens to admit ambient air to the = cylinder.  =20 The intake valve closes and the ambient air is compressed on the=20 subsequent upward movement of the piston until the piston reaches=20 approximately the Top Dead Centre position at which time the = compressed=20 gas is again injected into the cylinder 20 to drive the = piston=20 22 downwards and the cycle begins again.

In the = case of=20 adapting a conventional internal combustion engine for operation = on=20 compressed gas, a plurality of plates 103 are arranged, = preferably=20 over an end of the exhaust passageways, in order to reduce the = outlet size=20 of the exhaust passageways of the conventional internal combustion = engine.=20   In the illustrated embodiment, a single plate having an = opening in=20 the centre is bolted to the outside exhaust passageway on each = bank of the=20 V-8 engine, while another single plate having two openings in it, = is=20 arranged with one opening over each of the interior exhaust = passageways on=20 each bank of the V-8 engine.   A line 105 is suitably = attached=20 to each of the adaptor plates to carry the exhaust to an = appropriate=20 location.   In a preferred embodiment, the exhaust lines = 105=20 are made from 1.5" plastic tubing.

In a preferred = embodiment, the=20 exhaust lines 105 of one bank of the V-8 engine are = collected in a=20 line 107 and fed to an inlet of a compressor 109. =   The=20 pressure of the exhaust gas emanating from the engine 21 = according=20 to the present invention is approximately 25 p.s.i.   In this = way,=20 the compressor 109 does not have to pull the exhaust into = the=20 compressor since the gas exhausted from the engine 21 is at = a=20 positive pressure.   The positive pressure of the incoming = fluid=20 increases the efficiency and reduces wear on the compressor = 109.=20   The exhaust gas is compressed in the compressor 109 = and=20 returned through a line 111 and a check valve 113 to = the=20 compressed gas storage tank 23.   The check valve = 113=20 prevents the flow of compressed gas stored in the tank 23 = back=20 towards the compressor 109.

A suitable pressure = sensor=20 115 is arranged at an upper end of the tank 23 and = sends a=20 signal along a line 117 when the pressure exceeds a = predetermined=20 level and when the pressure drops below a predetermined level. =   The=20 line 117 controls an electrically activated clutch = 119=20 positioned at the front end of the compressor 109.   = The=20 clutch 119 is operated to engage and disengage the = compressor=20 109 from a drive pulley 121.   Also, the signal = carried=20 by the line 117 activates a suitable valve 123 = arranged on=20 compressor housing 125 to exhaust the air entering the = compressor=20 housing 125 from the line 107 when the clutch = 119 has=20 disengaged the compressor 109 from the drive pulley = 121.=20

In a preferred embodiment, when the pressure is the tank = 23=20 reaches approximately 600 p.s.i., the clutch 119 is = disengaged and=20 the compressor 109 is deactivated and the valve 123 = is=20 opened to exhaust the expanded gas delivered to the compressor = 109=20 from the line 107 to the atmosphere.   When the = pressure=20 within the tank 23 drops below approximately 500 p.s.i., = the sensor=20 115 sends a signal to engage the clutch 119 and = close the=20 valve 123, thereby operating the compressor 109 for=20 supplying the tank 23 with compressed gas.

The = pulley=20 121 which drives the compressor 109 through the = clutch=20 119 is driven by a belt 127 which is driven by a = pulley=20 129 which operates through a gear box 131.   = With=20 reference to Fig.1 and Fig.8, a second pulley = 133 on=20 the gear box is driven by a belt 135 from a pulley = 137=20 arranged on a drive shaft 139 of the engine 21. The = pulley=20 137 drives a splined shaft 140 which has a first = gear=20 141 and a second larger gear 143 placed on it, which = rotates=20 with the splined shaft 140.   The splined shaft = 140=20 permits axial movement of the gears 141 and 143 = along the=20 shaft 140.



In=20 normal operation (as seen in Fig.8), the first gear = 141=20 engages a third gear 145 arranged on a shaft 147 = which=20 drives the pulley 129.   The shafts 140 and = 147=20 are arranged in suitable bearings 149 positioned at each = end of it.=20   When the speed of the engine 21 drops below a = predetermined=20 level, a suitable sensor 151 responsive to the speed of the = drive=20 shaft 139 of the engine 21 generates a signal which = is=20 transmitted through a line 153 to a solenoid actuator = 155=20 arranged within the gear box 131.   The solenoid = actuator=20 155 moves the first and second gears 141, 143 = axially along=20 the splined shaft 140 to the right as seen in Fig.8 = so that=20 the second, larger gear 143 engages a fourth smaller gear=20 157 which is arranged on the shaft 147.   The = ratio of=20 the second gear 143 to the fourth gear 157 is = preferably=20 approximately 3 to 1.

In this way, when the speed of the = engine=20 21 drops below the predetermined level as sensed by the = sensor=20 151 (which predetermined level is insufficient to drive the = compressor 109 at a speed sufficient to generate the = 500-600 pounds=20 of pressure which is preferably in the tank 23), the = solenoid=20 actuator 155 is energised to slide the gears 143, = 141=20 axially along the splined shaft 140 so that the second, = larger gear=20 143 engages the fourth, smaller gear 157 to drive = the pulley=20 129 and hence the compressor 109 at a higher rate, = to=20 generate the desired pressure.   When the speed of the engine = increases above the predetermined level, which, in a preferred = embodiment=20 is approximately 1500 rpm, the solenoid actuator 155 is = deactivated=20 by the sensor 151 thereby moving the gears 143 and=20 141 to the left as seen in Fig.8 so that the first = gear=20 141, engages again with the third gear 145 to = effectuate a 1=20 to 1 ratio between the output shaft 139 of the engine = 21 and=20 the pulley 129.

The other bank of the V-8 engine = has its=20 exhaust ports arranged with adapter plates 103 similar to = those on=20 the first bank.   However, the exhaust from this bank of the = engine=20 21 is not collected and circulated through the compressor=20 109.   In a preferred embodiment, a portion of the = exhaust is=20 collected in a line 159 and fed to an enlarged chamber = 161.=20   A second fluid is fed through a line 163 into the = chamber=20 161 to be cooled by the cool exhaust emanating from the = engine=20 21 in the line 159.   The second fluid in the = line=20 163 may be either transmission fluid contained in a = transmission=20 associated with the engine 21 or a portion of the oil used = to=20 lubricate the engine 21.   A second portion of the = exhaust=20 from the second bank of the V-8 engine is removed from the line = 159=20 in a line 165 and used as a working fluid in an air = conditioning=20 system or for any other suitable use.

It should be noted = that the=20 particular arrangement utilised for collecting and distributing = the gas=20 exhausted from the engine 21 would be determined by the use = for=20 which the engine is employed.   In other words, it may be=20 advantageous to rearrange the exhaust tubing such that a larger or = smaller=20 percentage of the exhaust is routed through the compressor = 109.=20   It should also be noted that since the exhaust lines = 105 are=20 plastic tubing, a rearrangement of the lines for a different = purpose is=20 both simple and inexpensive.

In operation of the engine of = the=20 present invention, the engine 21 is started by energising = the=20 solenoid valve 29 and any suitable starting device (not = shown),=20 e.g., a conventional electric starter as used on an internal = combustion=20 engine.   Compressed gas from the full tank 23 flows = through=20 the line 25 and a variable amount of the compressed gas is = admitted=20 to the distributor 33 by controlling the regulator valve = 31=20 through the linkage 33 and the operator actuated throttle = linkage=20 35.   The compressed gas is distributed to each of the = lines=20 37 which lead to the individual cylinders 20.   = The=20 compressed gas is admitted to each of the cylinders 20 in = timed=20 relationship to the position of the pistons within the cylinders = by=20 opening the valves 39 with the valve actuator 41.=20

When it is desired to increase the speed of the engine, = the=20 operator moves the throttle linkage 35 which simultaneously = admits=20 a larger quantity of compressed gas to the distributor 33 = from the=20 tank 23 by further opening the regulator valve 31. =  =20 The timing of the valve actuator 41 is also advanced = through the=20 linkage 104.   Still further, as the speed of the = engine=20 21 increases, the effective length of the rotating contact=20 83 (Fig.4) or 95 (Fig.6) increases = thereby=20 electrically contacting a wider portion of one of the stationary = radial=20 contacts 85 to cause each of the valves 39 to remain = open=20 for a longer period of each engine cycle to admit a larger = quantity of=20 compressed gas to each of the cylinders 20.

As can = be seen,=20 the combination of the regulating valve 31, the mechanical = advance=20 104, and the valve actuator 41, combine to produce a = compressed gas engine which is quickly and efficiently adaptable = to=20 various operating speeds.   However, all three of the = controls need=20 not be employed simultaneously.   For example, the mechanical = advance=20 104 could be utilised without the benefit of one of the = varying=20 valve actuators 41 but the high speed operation of the = engine may=20 not be as efficient.   By increasing the duration of each = engine=20 cycle over which each of the valves 39 remains open to = admit=20 compressed gas to each of the cylinders 20 as the speed = increases,=20 conservation of compressed gas during low speed operation and = efficient=20 high speed operation are both possible.

After the = compressed gas=20 admitted to the cylinder 20 has forced the piston 22 = downwards within the cylinder to drive the shaft 139 of the = engine,=20 the piston 22 moves upwards within the cylinder 20 = and=20 forces the expanded gas out through a suitable exhaust valve (not = shown)=20 through the adapter plate 103 (if employed) and into the = exhaust=20 line 105.   The cool exhaust can then be collected in = any=20 suitable arrangement to be compressed and returned to the tank = 23=20 or used for any desired purpose including use as a working fluid = in an air=20 conditioning system or as a coolant for oil.

When using = the=20 apparatus and method of the present invention to adapt a ordinary = internal=20 combustion engine for operation with compressed gas it can be seen = that=20 considerable savings in weight are achieved.   For example, = the=20 ordinary cooling system including a radiator, fan, hoses, etc. can = be=20 eliminated since the compressed gas is cooled as it expands in the = cylinder.   In addition, there are no explosions within the = cylinder=20 to generate heat.   Further reductions in weight are obtained = by=20 employing plastic tubing for the lines which carry the compressed = gas=20 between the distributor and the cylinders and for the exhaust = lines.=20   Once again, heavy tubing is not required since there is = little or=20 no heat generated by the engine of the present invention.   = In=20 addition, the noise generated by an engine according to the = present=20 invention is considerably less than that generated by an ordinary = internal=20 combustion engine since there are no explosions taking place = within the=20 cylinders.

The principles of preferred embodiments of the = present=20 invention have been described in the foregoing specification. =  =20 However, the invention which is intended to be protected is not to = be=20 construed as limited to the particular embodiments disclosed. =   The=20 embodiments are to be regarded as illustrative rather than = restrictive.=20   Variations and changes may be made by others without = departing from=20 the spirit of the invention.   Accordingly, it is expressly = intended=20 that all such variations and changes which fall within the spirit = and the=20 scope of the present invention as defined in the appended claims = be=20 embraced thereby.

**********************


This patent shows = how the=20 practical details of running an engine on compressed air can be = dealt=20 with.   What it does not show is background details of the = actual=20 energy flows and the effects of compressing air and then letting = it=20 expand.   These things are not normally encountered in our = daily=20 lives and so we do not have an immediate intuitive feel for how a = system=20 like these will operate.   Take the effects of expansion. =  =20 While it is quite well known that letting a compressed gas expand = causes=20 cooling, the practical effect is seldom realised.

This web = site show the details of a =93vortex tube=94 which is a = completely passive=20 device with no moving parts:




This= =20 device does things which you would not expect.   Compressed = air at a=20 normal temperature of, say, seventy degrees Centigrade is fed into = the=20 circular chamber where the shape of the chamber causes it to = spiral=20 rapidly as it exits the tube:



Ther= e=20 is an energy gain in a vortex, as can be seen in a hurricane or = tornado,=20 but the really interesting thing here is the dramatic change in=20 temperature caused by the change in pressure as the air expands. =  =20 The ratio of heat gain to heat loss is controlled by the ratio of = the=20 sizes of the openings, which is why there is an adjustable nozzle = on the=20 small opening.

The air exiting through the large opening = is much=20 higher volume than the air exiting through the small opening and = it=20 expands very rapidly, producing a massive drop in temperature. =   The=20 density of this cold air is now much higher than the air entering = the=20 vortex chamber.   So there has been both a drop in = temperature and an=20 increase in density.   These features of the expansion are = made use=20 of in the Leroy Rogers engine design, where some of the expanded = air=20 exhaust of the engine is compressed and passed back to the main = air=20 storage tank.   While the compressor does raise the air = temperature=20 as it pumps the air back into the tank, it does not reach its = original=20 temperature instantly.

This results in the air temperature = inside=20 the tank dropping as the engine operates.   But, the lowered = tank=20 temperature causes an inflow of heat from its immediate = environment,=20 raising the overall tank temperature again.   This warming of = the=20 chilled air causes the tank pressure to increase further, giving = an energy=20 gain, courtesy of the local environment.   It is important to = understand that it takes less energy to compress air than the = kinetic=20 energy which can be generated by letting that compressed air = expand again.=20   This is a practical situation, courtesy of the local = environment=20 and is not a breach of the law of Conservation of Energy.   = It is=20 also a feature which has not yet been exploited to any great = degree and=20 which is just waiting to be used by any adventurous inventor or=20 experimenter.



The Eber Van = Valkinburg=20 Engine.
Eber presents a custom engine = based on=20 these principles.   His engine uses both compressed air and=20 compressed oil to manipulate pressures within the system and = provide an=20 engine which is self-powered.   Here is a slightly re-worded = copy of=20 the Eber Van Valkinburg patent:

Patent  US 3,744,252                            =
10th July 1973                            Inventor: Eber Van =
Valkinburg

CLOSED=20 MOTIVE POWER SYSTEM UTILISING COMPRESSED=20 FLUIDS


ABSTRACT

Stored energy in = a=20 compressed elastic fluid is utilised in a controlled manner to = pressurise=20 an inelastic fluid and to maintain such pressurisation.   The = pressurised inelastic fluid is throttled to the impeller of a = prime mover.=20   Only a portion of the output energy from the prime mover is = utilised to circulate the inelastic fluid so as to maintain a = nearly=20 constant volumetric balance in the system.=20

DESCRIPTION
The objective of the = invention is to=20 provide a closed-loop power system which utilises the expansive = energy of=20 a compressed elastic fluid, such as air, to pressurise and = maintain=20 pressurised throughout the operational cycle of the system a = second=20 non-elastic and non-compressible fluid, such as oil.   The=20 pressurised non-elastic fluid is released in a controlled manner = by a=20 throttle to the rotary impeller of a turbine or the like, having = an output=20 shaft.   This shaft is coupled to a pump for the non-elastic = fluid=20 which automatically maintains the necessary circulation needed for = the=20 operation of the prime mover, and maintains a near volumetric = balance in=20 the system between the two fluids which are separated by = self-adjusting=20 free piston devices.   The pump for the non-elastic fluid = includes an=20 automatic by-pass for the non-elastic fluid which eliminates the=20 possibility of starving the pump which depends on the discharge of = the=20 non-elastic fluid at low pressure from the exhaust of the turbine. =  =20 Other features and advantages of the invention will become = apparent during=20 the course of the following detailed description. =


BRIEF=20 DESCRIPTION OF DRAWING FIGURES
Fig.1
is a partly = schematic=20 cross-sectional view of a closed motive power system embodying the = invention.



F= ig.2=20 is a fragmentary perspective view of a rotary prime mover utilised = in the=20 system. Fig.3 is an enlarged fragmentary vertical section = through=20 the prime mover taken at right angles to its rotational axis. = Fig.4=20 is an enlarged fragmentary vertical section taken on line = 4--4 of=20 Fig.1. Fig.5 is a similar section taken on line = 5--5=20 of Fig.4.


DETAILED DESCRIPTION




Refe= rring=20 to the drawings in detail, in which the same numbers refer to the = same=20 parts in each drawing, the numeral 10 designates a supply = bottle or=20 tank for a compressed elastic fluid, such as air.   = Preferably, the=20 air in the bottle 10 is compressed to approximately 1,500 = p.s.i.=20   The compressed air from the bottle 10 is delivered = through a=20 suitable pressure regulating valve 11 to the chamber = 12 of a=20 high pressure tank 13 on one side of a free piston = 14 in the=20 bore of such tank.   The free piston 14 separates the = chamber=20 12 for compressed air from a second chamber 15 for = an=20 inelastic fluid, such as oil, on the opposite side of the free = piston.=20   The free piston 14 can move axially within the bore = of the=20 cylindrical tank 13 and is constantly self-adjusting there = to=20 maintain a proper volumetric balance between the two separated = fluids of=20 the system.   The free piston has the ability to maintain the = two=20 fluids, air and oil, completely separated during the operation of = the=20 system.

The regulator valve 11 delivers compressed = air to=20 the chamber 12 under a pressure of approximately 500 p.s.i. =  =20 The working inelastic fluid, oil, which fills the chamber = 15 of=20 high pressure tank 13 is maintained under 500 p.s.i. = pressure by=20 the expansive force of the elastic compressed air in the chamber = 12=20 on the free piston 14.   The oil in the chamber = 15 is=20 delivered to a prime mover 16, such as an oil turbine, = through a=20 suitable supply regulating or throttle valve 17 which = controls the=20 volume of pressurised oil delivered to the prime mover. =

The=20 turbine 16 embodies a stator consisting of a casing ring = 18=20 and end cover plates 19 joined to it in a fluid- tight = manner.=20   It further embodies a single or plural stage impeller or = rotor=20 having bladed wheels 20, 21 and 22 in the = illustrated=20 embodiment.   The peripheral blades 23 of these = turbine wheels=20 receive the motive fluid from the pressurised chamber 15 = through=20 serially connected nozzles 24, 25 and 26, connected=20 generally tangentially through the stator ring 18, as shown = in=20 Fig.3.   The first nozzle 24 shown = schematically in=20 Fig.1 is connected directly with the outlet of the throttle = valve=20 17.   The successive nozzles 25 and 26 = deliver=20 the pressurised working fluid serially to the blades 23 of = the=20 turbine wheels 21 and 22, all of the turbine wheels = being=20 suitably coupled to a central axial output or working shaft = 27 of=20 the turbine 16.



Back= -pressure=20 sealing blocks 28, made of fibre, are contained within = recesses=20 29 of casing ring 18 to prevent co-mingling of the = working=20 fluid and exhaust at each stage of the turbine.   A = back-pressure=20 sealing block 28 is actually only required in the third = stage=20 between inlet 26 and exhaust 31, because of the = pressure=20 distribution, but such a block can be included in each stage as = shown in=20 Fig.1.   The top surface, including a sloping face = portion=20 30 on each block 28, reacts with the pressurised = fluid to=20 keep the fibre block sealed against the adjacent, bladed turbine = wheel;=20 and the longer the slope on the block to increase it=92s top = surface area,=20 the greater will be the sealing pressure pushing it against the = periphery=20 of the wheel.

Leading from the final stage of the turbine=20 16 is a low-pressure working fluid exhaust nozzle 31 = which=20 delivers the working fluid, oil, into an oil supply chamber or = reservoir=20 32 of a low pressure tank 33 which may be bolted to = the=20 adjacent end cover plate 19 of the turbine, as indicated at = 34.   The oil entering the reservoir chamber 32 = from=20 the exhaust stage of the turbine is at a pressure of about 3-5 = p.s.i.=20   In a second chamber 35 of the low pressure tank = 33=20 separated from the chamber 32 by an automatically moving or = self-adjusting free piston 36, compressed air at a = balancing=20 pressure of from 3-5 p.s.i. is maintained by a second pressure = regulating=20 valve 37.   The pressure regulating valve 37 is = connected with the compressed air supply line 38 which = extends from=20 the regulating valve 11 to the high pressure chamber = 12 for=20 compressed air.

Within the chamber 32 is a gear = pump=20 39 or the like having its input shaft connected by a = coupling=20 40 with the turbine shaft 27.   Suitable = reduction=20 gearing 41 for the pump may be provided internally, as = shown, or in=20 any other conventional manner, to gear down the rotational speed = derived=20 from the turbine shaft.   The pump 39 is supplied with = the oil=20 in the filled chamber 32 delivered by the exhaust nozzle or = conduit=20 31 from the turbine.   The pump, as illustrated, has = twin=20 outlet or delivery conduits 42 each having a back-pressure = check=20 valve 43 connected therein and each delivering a like = volume of=20 pressurised oil back to the high pressure chamber 15 at a = pressure=20 of about 500 p.s.i.   The pump 39 also has twin fluid = inlets.=20   The pump employed is preferably of the type known on the = market as=20 "Hydreco Tandem Gear Pump," Model No. 151515, L12BL, or = equivalent.  =20 In some models, other types of pumps could be employed including = pumps=20 having a single inlet and outlet.   The illustrated pump will = operate=20 clockwise or counter-clockwise and will deliver 14.1 g.p.m. at = 1,800=20 r.p.m. and 1,500 p.s.i.   Therefore, in the present = application of=20 the pump 39, it will be operating at considerably less than = capacity and will be under no undue stress.




=


Sinc= e=20 the pump depends for its supply of fluid on the delivery of oil at = low=20 pressure from the turbine 16 into the chamber 32, an = automatically operating by-pass sleeve valve device 44 for = oil is=20 provided as indicated in Fig.1, Fig.4 and Fig.5. =   This=20 device comprises an exterior sleeve or tube 45 having one = end=20 directly rigidly secured as at 46 to the movable free = piston=20 36.   This sleeve 45 is provided with slots = 47=20 intermediate its ends.   A co-acting interior sleeve = 48=20 engages telescopically and slidably within the sleeve 45 = and has a=20 closed end wall 49 and ports or slots 50 = intermediate its=20 ends, as shown.   The sleeve 48 communicates with one = of the=20 delivery conduits 42 by way of an elbow 51, and the = sleeve=20 48 is also connected with the adjacent end of the pump = 39,=20 as shown.

As long as the chamber 32 is filled with = low=20 pressure oil sufficient to balance the low air pressure in the = chamber=20 35 on the opposite side of free piston 36, such = piston will=20 be positioned as shown in Fig.1 and Fig.4 so that = the slots=20 47 and 50 of the two sleeves 45 and 48 = are out=20 of registration and therefore no flow path exists through them. =  =20 Under such circumstances, the oil from the chamber 32 will = enter=20 the pump and will be delivered by the two conduits 42 at = the=20 required pressure to the chamber 15.   Should the = supply of=20 oil from the turbine 16 to the chamber 32 diminish = so that=20 pump 39 might not be adequately supplied, then the = resulting drop=20 in pressure in the chamber 32 will cause the free piston = 36=20 to move to the left in Fig.1 and bring the slots 47 = into=20 registration or partial registration with the slots 50, as = depicted=20 in Fig.5.   This will instantly establish a by-pass = for oil=20 from one conduit 42 back through the elbow 51 and = tubes=20 48 and 45 and their registering slots to the oil = chamber=20 32 to maintain this chamber filled and properly pressurised = at all=20 times.   The by-pass arrangement is completely automatic and = responds=20 to a diminished supply of oil from the turbine into the chamber = 32,=20 so long as the required compressed air pressure of 3-5 p.s.i. is=20 maintained in the chamber 35.

Briefly, in summary, = the=20 system operates as follows.   The pressurised inelastic and=20 non-compressible fluid, oil, from the chamber 15 is = throttled into=20 the turbine 16 by utilising the throttle valve 17 in = a=20 control station.   The resulting rotation of the shaft = 27=20 produces the required mechanical energy or work to power a given=20 instrumentality, such as a propeller.   A relatively small = component=20 of this work energy is utilised through the coupling 40 to drive = the pump=20 39 which maintains the necessary volumetric flow of oil = from the=20 turbine back into the high pressure chamber 15, with the = automatic=20 by-pass 44 coming into operation whenever needed. =

The=20 ultimate source of energy for the closed power system is the = compressed=20 elastic fluid, air, in the tank or bottle 10 which through the = regulating=20 valves 11 and 37 maintains a constant air pressure = in the=20 required degree in each of the chambers 12 and 35. =   As=20 described, the air pressure in the high pressure chamber 12 = will be=20 approximately 500 p.s.i. and in the low pressure chamber 35 = will be=20 approximately 3-5 p.s.i.

It may be observed in = Fig.1 that=20 the tank 33 is enlarged relative to the tank 13 to=20 compensate for the space occupied by the pump and associated = components.=20   The usable volumes of the two tanks are approximately = equal.=20

In an operative embodiment of the invention, the two free = pistons=20 14 and 36 and the tank bores receiving them are 8 = inches in=20 diameter.   The approximate diameters of the bladed turbine = wheels=20 are 18 inches.   The pump 39 is approximately 10 = inches long=20 and 5 inches in diameter.   The tank 13 is about 21 = inches=20 long between its crowned end walls.   The tank 33 is = 10 inches=20 in diameter adjacent to the pump 39.

The terms and=20 expressions which have been employed herein are used as terms of=20 description and not of limitation, and there is no intention, in = the use=20 of such terms and expressions, of excluding any equivalents of the = features shown and described or portions thereof but it is = recognised that=20 various modifications are possible within the scope of the = invention=20 claimed.



The Clem = Engine.
This engine is based on an entirely different = principle,=20 and one which is not spoken about very often.   Hurricanes or = =93twisters=94 as they are sometimes called, are large rotating = air masses of=20 incredible power which develop in hot areas which are more than = eight=20 degrees North or South of the equator.   The distance from = the=20 equator is essential as the rotation of the Earth is needed to = give them=20 their initial spin.   They usually develop over water which = is at a=20 temperature of twenty-eight degrees Centigrade or higher as that = allows=20 the air to absorb enough heat energy to get started.   That = is why=20 there is a distinct =93hurricane season=94 in these areas, since = at certain=20 times of the year the ocean temperature is just not high enough to = trigger=20 a hurricane.

What is not generally realised is that a = hurricane=20 develops excess energy due to its swirling circular movement. =   The=20 generation of this extra power was observed and documented by = Viktor=20 Schauberger of Austria, who also used his observations to great = effect.=20   I think that what Schauberger says makes some people = uncomfortable=20 as they seem to think that anything =93unorthodox=94 has to be = weird and too=20 peculiar to be mentioned.   This is rather strange as all = that is=20 involved here is a simple observation of how our environment = actually=20 works.   A hurricane is wider at the top than at the bottom = and this=20 concentrates power at the base of the swirling mass of air.   = This=20 tapered rotation is called a =93vortex=94 which is just a simple = name to=20 describe the shape, but any mention of =93vortex power=94 (the = power at the=20 base of this rotation) seems to make many people uncomfortable = which is=20 most peculiar.

Leaving that aside, the question is =93can = we use=20 this energy gain from the environment for our own purposes?=94. =   The=20 answer may well be =93Yes=94.   Perhaps this principle is = utilised by=20 Richard Clem.   In 1992, Richard Clem of Texas, demonstrated = a=20 self-powered engine of an unusual type.   This engine, which = he had=20 been developing for twenty years or more, weighs about 200 pounds = (90=20 kilos) and generated a measured 350 horsepower continuously over = the full=20 period of a nine-day self-powered test.   Although this = engine which=20 runs from 1,800 to 2,300 rpm is especially suited to powering an=20 electrical generator, Richard did install one in a car, and = estimated that=20 it would run for 150,000 miles without any need for attention and = without=20 any kind of fuel.   Richard said that his prototype car had = reached a=20 speed of 105 mph.   Just after receiving funding to produce = his=20 engine, Richard died suddenly and unexpectedly at about 48 years = of age,=20 the death certificate having =93heart attack=94 written on it as = the cause of=20 death.   Remarkably convenient timing for the oil companies = who would=20 have lost major amounts of money through reduced fuel sales if = Richard=92s=20 motor had gone into production.

The motor is unusual in = that it is=20 a rotary turbine style design which runs at a temperature of=20 3000F (1400C) and because of that high = temperature,=20 uses cooking oil as its operational fluid, rather than water as = the oil=20 has a much higher boiling point.   To a quick glance, this = looks like=20 an impossible device as it appears to be a purely mechanical = engine, which=20 will definitely have an operating efficiency which is less than = 100%.=20

In broad outline, the oil is pumped through a pipe and = into the=20 narrow end of the cone-shaped rotor.   The engine is started = by being=20 rotated by an external starter motor until it reaches the speed at = which=20 it generates enough power to be sustain its own operation.   = The=20 rapid spinning of the cone, causes the oil to run along spiral = grooves cut=20 in the inner face of the cone and exit through angled nozzles = placed at=20 the large end of the cone:




=


The = operating pressure produced by the pump is 300 to 500 psi. Richard = did not=20 attempt to patent his engine as US Patent 3,697,190 =93Truncated = Conical=20 Drag Pump=94 granted in 1972 as a liquid-asphalt pump is so close = in detail=20 that Richard felt that there was insufficient difference for him = to be=20 granted a patent:



Ther= e=20 appears to be considerable scope for anyone who wishes to build or = manufacture this engine and it is capable of acting as a heater as = well as=20 device for producing mechanical power.   This suggests that = water=20 purification could be an additional =93extra=94 option for this = engine.=20



Prof. Alfred Evert of Germany has produced = an=20 analysis of the operation of the Clem Engine and turbines in this = general=20 category.   His = website has=20 this to say:

07.05.=20 Centrifugal-Thrust-Engine=20

Objectives

Several different versions of = air-drive=20 engines have been described in the previous chapters.   One = which is=20 particularly powerful, is the =93Suction-Cylinder-Engine=94 when = driven by=20 compressed air.   Water-drive engines require a much more = complex=20 arrangement of closed circuits due to the strong centrifugal = forces caused=20 by using such a dense working-medium.

This new concept of = the=20 =93Centrifugal-Thrust-Engine=94 shows that centrifugal forces can = contribute=20 to turning momentum.   Initially, however, we need to discuss = some=20 general points of view concerning the inertia of rotating systems. =

Gravity and Centrifugal Forces
First, = consider=20 the movement of a mass (a sphere or body of water) moving in a = circular=20 path around the inside wall of a hollow cylinder.   = Centrifugal=20 forces always press radially outwards while Gravitational forces = always=20 act straight downwards. Fig 07.05.01 shows diagrams of three situations.   A = partial plan=20 view of such a cylinder is shown in grey.   This cylinder has = a=20 radius of 100 cm (R100).  =20 Along its inner wall, mass M is=20 moving at a speed of 3.13 m/s (see arrow V3.13).   This mass = is=20 continuously pushed inwards by the cylinder.   This inward=20 acceleration A can = be=20 calculated by the formula Speed squared divided by Radius, in this case, with 3.13 m/s at a radius of 1 = m,=20 acceleration   A =3D=20 (3.13)2 / 1 =3D 9.8 m/s2.


Matching= =20 that inward acceleration is the outward centrifugal force of that = mass.=20   That centrifugal force (A9.8) is shown as the red vector in the diagram.  =20 Gravitational acceleration is also about 9.8 m/s2, and = is shown=20 here as the green vector ( G9.8)=20 in the diagram, acting vertically downwards.   The resulting = force is=20 shown as the blue line in the diagram.   If the cylinder wall = were=20 replaced by the inside surface of a cone with a 45 degree = inclination,=20 then the mass would rotate at the same speed, maintaining a = constant=20 height.

Now, consider the middle diagram.   Here, the = radius=20 distance to the wall is only 24 cm (R24) and the mass is only moving at 1.5 m/s (V1.5).   The inward, = or=20 =93centripetal=94 acceleration produced is A =3D 1.52 / 0.24 which is 9.8 m/s2 so, here again, = the=20 centrifugal force (A9.8)=20 corresponds to acceleration under gravity (G9.8).   = Consequently, the=20 diagram of the resolution of forces matches that of the previous = diagram.=20

So whenever a mass completes one rotation in exactly one = second,=20 the centripetal (inward) acceleration is the same as acceleration = under=20 gravity.   At a radius of 1 m, the circumference is about = 3.13 m and=20 so the speed is about 3.13 m/s for one rotation per second.   = At a=20 radius of 0.24 m, the circumference is about 1.5 m and so one = rotation per=20 second requires a speed of 1.5 m/s, and so identical results are = produced.=20   Whether this happens to be a pure coincidence or due to = some other=20 cause, is discussed later in the section entitled =93Aether = Physics=94.=20

In the lowest section of Fig = 07.05.01, a rotation at this same speed of 1.5 m/s (V1.5), but this time at = the shorter=20 radius of, say, 16 cm (R16)=20 produces a stronger inward acceleration given by A =3D 1.52 / 0.16 which = works out at=20 about 14 m/s2.   As the force diagram shows, this = results=20 in the mass rotating along a circular track which is higher up = than the=20 previous tracks.   This can be seen in action when coffee in = a cup is=20 being stirred vigourously. =


Lifting-Force
Now=20 consider Fig 07.05.02 which=20 illustrates the effects of imposing higher rotational speeds on a = mass.=20   The radius of 24 cm (R24)=20 and of 16 cm (R16) = are now each=20 propelled at the higher rate of 6 m/s (V6).   The inward =93centripetal=94 acceleration = is=20 correspondingly greater and is given by the equation A =3D 62 / = 0.24 which=20 works out at about 150 m/s2 (A150) and about 225 m/s2 (=20 A225 ) respectively.

In both = of=20 these cases, the centrifugal force is substantially greater than = the=20 gravitational force (shown as the short green near-vertical vector = marked=20 as G9.8) and so the = resulting=20 net forces (shown in blue in the diagram) are much closer to the=20 horizontal than before.   These masses will therefore rotate = at a=20 constant height when moving along the inner face of a cone which = has much=20 steeper walls (shown in grey).

The lowest diagram of Fig 07.05.02 shows the = situation where=20 these forces press against a less steeply sloping wall (shown in = grey).=20   The wall resists this pressure by pressing back at right = angles to=20 its surface (dark green vectors).   Consequently, the = remainder of=20 the nearly horizontal centrifugal force produces an upward = component=20 (H20 and H30, shown in red), = parallel to the=20 sloping face of the wall.   Depending on the speed of the = mass and=20 the angle of inclination of the wall, this upward force causes an=20 acceleration of the mass, upwards along the wall.   In these=20 examples, that acceleration is about 20 to 30 m/s2. =   In=20 our example of coffee being stirred in a cup, the faster the = stirring and=20 the more angled the sides of the cup, the larger the amount of = coffee=20 which spills over the lip of the cup.   Notice that part of = this=20 centrifugal force becomes a component which acts in a direction = opposite=20 to gravity. In our example, the 6 m/s (six revolutions per second = or 360=20 rpm), produces a lifting-force which is much greater than the = force of=20 gravity.

Spiral Tracks
In Fig=20 07.05.03, the diagrams on the left hand = side show=20 sphere A, which = might be a=20 bowling ball, rolling in a straight line from right to left on a = flat,=20 horizontal surface.   The plan view presented immediately = below,=20 shows that the movement of the sphere is a straight line.   = However,=20 as shown at the bottom left of the Figure, if the sphere is = projected at=20 an angle, into a vertical cylinder, then it follows an upward = helical=20 track from E to = F in the diagram.   = The path=20 followed is similar to a screw thread inside a nut or on the = outside of a=20 bolt.   This same path would be followed if the moving object = were a=20 jet of water rather than a solid sphere.


The=20 corresponding three diagrams on the right hand side of Fig 07.05.03 show the = situation for=20 the sphere if instead of a vertical cylinder, it is projected into = an=20 inverted cone shape.   In this instance, the path followed is = a=20 spiral curve starting at point K=20 and continuing to point L.=20   When this movement is shown on a flat surface, you will = notice that=20 the sphere rolls in a curve towards point D.

This shows clearly that there is an = additional=20 sideways force C = acting on the=20 sphere, causing this curved path.   This has the effect that = when the=20 sphere is projected into the cone shape, it exits at point L with a greater upward = angle than=20 that with which it enters the cone at point K.   This effect is also seen if a jet of water = is used=20 rather than a sphere or bowling ball. It should also be realised = that as=20 the sphere runs upwards along the inside surface of the cone, that = it=92s=20 path gets progressively steeper the further it rolls.=20

Steeper, Shorter and Faster
In Fig 07.05.04 the inner = surface of the=20 cone of Fig 07.05.03 = is shown=20 opened out to form a flat surface.   The cross-lines shown = are=20 positioned to indicate each 30 degree strip of the conical = surface.  =20 If a jet of water is projected into the lower edge of the cone at = point=20 A, at an angle of 30 = degrees,=20 then it will exit from the top of the cone at point B some 150 degrees later = (sector S150).   The angle of = exit is=20 also 30 degrees and the spiral track C, shown in blue, is the path followed during it=92s = constant,=20 steady rise though the cone.

The = blue=20 line D shows what = happens when a=20 jet of water is projected into the cone.   It enters the = lower edge=20 of the cone at an angle of 30 degrees as before, but this time the = water=20 velocity is greater.   As a result of this higher velocity, = the water=20 now exits from the upper edge of the cone at a steeper angle of = about 35=20 degrees.   That track D=20 runs within a sector of the cone which spans only 120 degrees = (S120) and so the track = followed is=20 shorter, steeper and covered more quickly than the jet of water = flowing=20 along the previous track C.=20

The diagram at the bottom right hand side of Fig 07.05.02, shows the = cone as seen=20 from the top.   Track C=20 with its constant rate of rise is shown, as is the steeper and = shorter=20 track D.   The = far side of=20 the cone, shows several paths which indicate how the water flows = if the=20 angle of entry at the bottom of the cone, is increased in steps.=20

The diagram at the bottom left shows the cross-sectional = view of=20 the section of cone used in this discussion.   It shows how = the water=20 enters at the bottom edge, moves along the inner wall and exits = from the=20 upper edge of the cone.   The vector M shows the diagonal thrust of the water against the = wall of=20 the cone.   This is the direct equivalent of the two forces = G (against the wall) and = H (upwards along the = wall).  =20 Force H is much = greater here=20 than with the earlier example where the rate of upward movement = was=20 constant.

Provisional Result
In this = first=20 section, only well-known facts have been mentioned. However, an=20 understanding of these examples and their points of view will be = important=20 during the following discussion:

We have noted that:=20
  • Centrifugal force equals that of gravity for one rotation = per=20 second.
  • A mass at this velocity maintains a constant height on a = wall=20 inclined at 45 degrees.
  • If the mass moves faster than that, it rises up the inner = wall.
  • The lifting force increases with increased velocity and/or = wall slop=20 and
  • The track along the inner wall surface becomes increasingly=20 steeper.
  • The mass moves with increasing speed as it progresses = towards the=20 outer edge of the cone.
The = =93Centrifugal-Thrust-Engine=94 is=20 based on the principle that a hollow cone-shaped cylinder is a = =91passive element=92.   = Additionally, a=20 working medium flowing along it=92s stationary inner wall, is an = =91active element=92.   These = key properties=20 are now discussed in the following section:=20


Rotor-Cylinder
Fig=20 07.05.05 shows a representation of a = turbine T.   Initially, this = is shown as=20 a round cylinder.   At the top left hand side of the diagram, = a=20 vertical cross-section is shown, and to the right of that is the = view from=20 above.   The diagram at the bottom of the Figure shows the = inside=20 wall of the cylinder opened out and laid on a flat surface.   = The=20 cylinder in this example has a radius of 16 cm (R16) and a circumference = of 1 metre.=20   Circular pipes are positioned vertically around the = circumference=20 to act in a similar way to turbine-blades (TS shown in blue).   Here, twelve of these pipes = are shown,=20 each parallel to the system axis and running in a straight line = from=20 bottom to top.

A = 6 m/s jet=20 of water enters the bottom of these pipes at an upward angle of 30 = degrees.   Due to the rotation of the cylinder drum, the = water moves=20 along the diagonal path A to=20 B.   As = explained earlier,=20 the water has a horizontal velocity component marked in red in the = diagram=20 as V6, and because = of the angle=20 of entry of the water, there is a vertical speed of about 3.5 m/s = (shown=20 in green and marked as V3.5).=20   The water flowing in these pipes actually flows in a spiral = path=20 diagonally upwards, following the path shown by the blue line = running from=20 A to B.   If the height of = the=20 cylinder is 24 cm (H24), then=20 the water moves around through the whole of sector S150 during its upward = flow through=20 the vertical pipes.

Rotor-Cone
At the top = left=20 hand side of Fig 07.05.06 a=20 conical cylinder turbine T is=20 shown.   The pipes running up the inside of the cone are set = with a=20 16 cm radius at the lower edge of the cone (R16) and a 24 cm radius = (R24) at the top of the = cone.  =20 These pipes therefore have a curved shape as they run up the = inside face=20 of the cone.   These pipes can be thought of as performing = the same=20 function as turbine blades in a jet engine.


In the = same=20 way as before, a jet of water is fed at an upward angle of 30 = degrees into=20 the bottom of the pipes.   Unlike the previous case, the jet = of water=20 does not strike the walls of the pipes at their lowest point = because the=20 water is entering parallel to a diagonal wall.   In this = case, as=20 before, the overall height of the cylinder is 24 cm.   The = track=20 taken by the water will be exactly the same as the previous track, = running=20 from A to B shown in the previous = diagram, and=20 again spanning a sector of 150 degrees (S150).

The central diagram of Fig=20 07.05.06 shows the conical cylinder = surface laid out=20 flat.   The dark blue curve C shows the path taken by the jet of water as it = spirals=20 upwards and outwards from A to=20 B, within the sector = S150 shaded in blue. =  =20 Interestingly, since the cone circumference at the outlet level is = longer=20 than at the inlet level (having 24 cm and 16 cm lengths = respectively), the=20 cone actually rotates at a greater speed than the speed of the = water.=20   This means that the water accelerates as it passes up = through the=20 curved pipes inside the cone (although that is not the intended = job of any=20 turbine).

As shown in the top right hand diagram, the = pipes inside=20 this conical turbine need to be curved backwards in the opposite = direction=20 to that in which the turbine rotates.   These pipes are = curved to=20 follow the path shown in red and marked G which is contained within the 50 degree sector = S50.

As stated = earlier, the=20 water flowing in these pipes presses against the outer wall, due = to=20 centrifugal force.   Once the water speed is great enough, = the water=20 gets lifted upwards by its own motion.   If the pipes allow = that=20 additional upward motion, then the water will exit from the top of = the=20 pipes at a more acute angle than the angle of entry at the bottom = of the=20 pipes.

The bottom diagram shows a design arrangement where = the=20 water enters at an angle of 30 degrees (point E), and exits at the same = 30 degree=20 angle (at point F). =   With=20 this arrangement, the water travels along a shorter, steeper path = D in a narrower sector of = just 120=20 degrees (S120). =   Due to=20 this shorter path, the pipe follows a different curve, such as the = one=20 shown in red and marked H in the diagram.   The pipe itself, = is=20 contained in a sector of just 40 degrees (S40).

The diagram at the top right hand side of = the=20 Figure, show this short pipe run.   The water enters at point = A and flows upwards = through the pipe=20 marked G, to exit at = point B.

Notice that the = pipe curves=20 away from the direction of rotation.   This is because the = pipe acts=20 something like a jet engine and the direction of thrust is in the = opposite=20 direction to the direction of the jet of water coming out of the = pipe.=20   The pipe shown in this illustration covers a sector of 50 = degrees.=20   However, remember that the water flowing in that pipe = covers a=20 sector of 150 degrees due to the rotation of the turbine cone. =   The=20 lower pipe H shows = the other=20 design and it spans just 40 degrees.   Water in that pipe = flows=20 upwards from E to = F and passes through 120 = degrees due=20 to the rotation of the turbine cone, and it also flows faster and = reaches=20 its outlet earlier.   These different pipes are only shown on = a=20 single turbine cone for illustration purposes, as any turbine = construction=20 will have all of its pipes constructed to one design or the other = and not=20 a mix of the two shapes. =


Turbine-Blades
On=20 the left hand side of Figure = 07.05.07, shown in red, is the =91neutral=92 track H of the actual water flow = when=20 crossing a cylindrical sector of 40 degrees (S40).   Also shown in = the top=20 left hand diagram, (shown in dark blue) is the corresponding steep = track=20 D followed by the = water when it=20 flows across a cylindrical sector of 120 degrees (S120).   In the lower = left hand=20 diagram, the corresponding paths for the flows across a conical = turbine=20 surface are shown.


However,= if=20 the flowing water is to be used to generate a driving force on the = turbine=20 cylinder or cone, then the diagrams on the right hand side of the = Figure=20 show the necessary arrangement.   To achieve this aim, the = pipes=20 carrying the water need to be curved to a greater degree.   = Here, the=20 curve of the pipes is increased by, say, an arbitrary additional = 50=20 degrees to give a total of 90 degrees, as indicated by the curves = marked=20 L (shown in red) = within sector=20 S90. =

Correspondingly,=20 track K (shown in = blue) is=20 curved more sharply upwards with its sector reduced to a width of = just 70=20 degrees (S70). =   This=20 amount is the previous 120 degrees, reduced by our arbitrary 50 = degrees.=20   The upper right hand side diagram shows the design for a=20 cylindrical turbine while the diagram below it shows the design = for a=20 conical turbine.   The thin lines H and D = show the=20 original curves which would not apply any turning force to the = turbine=20 pipes were the water to flow through them.   These paths = could be=20 called the =91neutral=92 tracks as they do not impart any thrust, = and it takes=20 the greater curvature shown by the thick lines to actually drive = the=20 turbine.


Cone-Wall and = Cone-Turbine
The lower=20 section of Fig 07.05.08 shows=20 the cross-section of turbine T=20 which has a radius of 24 cm (R24) at its upper edge and a radius of 16 cm (R16) at its lower edge and = which has a=20 height of about 24 cm (H24).=20   Below the main conical turbine (shown below the dotted = line) there=20 is an inlet section marked as TE=20 and which has an additional height of 12 cm (H12), and which tapers = down to a=20 radius of 12 cm (R12).

In the=20 previous example, the general arrangement of the turbine-blades = TS (shown in red), being = curved pipes=20 inside the turbine, was discussed.   In this example, grooves = are=20 formed in the outer surface of the turbine cone.   These = grooves, or=20 indentations, are open on the outside and the turbine cone is = housed=20 inside a cylindrical outer housing shown in grey and designated as = KW.   This outer wall = supports an=20 inner conical housing (not shown) and the turbine rotor revolves = inside=20 that conical housing.   Water (shown as light blue) fills the = space=20 between the turbine rotor and the outer conical housing.   = The water=20 is bounded on one side by the smooth wall of the outer housing and = on the=20 other by the saw tooth shaped vertical grooves which form the = turbine=20 =93blades=94.

This example is needed to explain the = curvature of the=20 grooves at the surface of the cone.   Unlike standard = turbines, the=20 water flows from a short radius inlet, to a much larger radius = outlet.=20   Water can=92t accelerate to reach the greater speed needed = at the=20 longer radius, so normal turbines have the water flowing from the = longer=20 radius inward towards the shorter radius.   This causes = deceleration=20 of the water flow to generate torque.   Consequently, our = design here=20 appears =91wrong=92 in conventional terms, and seems to make no = sense in=20 normal applications.   This =91wrong=92 design only makes = sense when=20 using a cone-like rotor with its saw tooth-like blades.=20

Sawtooth-Blades
Mechanical turning = momentum=20 (torque) is generated by flows which press against one side of the = turbine=20 blades.   Commonly, turbines have blades where a groove is=20 effectively created between two successive blades.   In = effect, the=20 driving pressure of a turbine is applied to one face of this = virtual=20 groove.   With this arrangement, the leading face represents = the=20 =93pressure=94 side and the trailing face represents the = =93suction=94 side.=20   The generation of torque is based on the difference of = pressure=20 between these two wall faces.   This pressure difference is = maximised=20 if there is no suction side at all, that is, when there is no = pressure at=20 all on the =93suction=94 side.   This is possible along the = surfaces of a=20 cone-shaped turbine which has saw tooth-like grooves as already = described.=20

These turbine =93blades=94 have a pressure-side which = faces in a=20 radial direction relative to the direction of rotation.   = Each groove=20 has a =91bottom=92 or inner side which faces in a tangential = direction.  =20 Water flow which moves diagonally outwards effectively flows = parallel to=20 that inner face.   The pressure-side plus the inner-side, = form the=20 contours of an asymmetric saw tooth shaped groove.   Each = inner-side=20 extends from the inner edge of the pressure-side to the outer edge = of the=20 following pressure-side.   These triangular shaped grooves=20 effectively have no backside wall.

In Fig=20 07.05.08, the cross-sectional view shows = several=20 axial levels marked with the dotted lines A to H. =   The=20 plan-view diagram shown at the top of the Figure indicates where = these=20 levels extend horizontally.   At inlet level A, the radius is 12 cm and = a=20 ring-shaped cross-sectional surface is available for water to = enter=20 between the round turbine face and the round cone-shaped wall of = the=20 housing (drawn here across a sector of 30 degrees). =

Further up,=20 these tooth-shaped blades extend further out of the surface of the = turbine=20 cone.   At point B, the=20 inner edge still has a radius of nearly 12 cm, while the outer = edge=20 extends further out into the ring-shaped groove.   Here for = example,=20 twelve turbine =93blades=94 are shown, and in the 60 degree sector = B, there are two of these = =93saw-teeth=94.=20

Level C = marks the=20 junction between the turbine-inlet area (TE) to the main body of the turbine (T).   The turbine = =93teeth=94 at this=20 level have a radius of 16 cm and this level has the deepest = grooves.=20   This sector of 60 degrees has two of these teeth TS.

Further up, = the outer=20 circumference becomes greater and the notches become longer. =   If the=20 cross-sectional area for water flow were to remain constant, then = the=20 notches would need to be correspondingly shallower.   In = sectors=20 D, E and F, which again span a 60 = degree=20 sector, two turbine-blades are shown in each sector.

As = sector=20 H covers only 30 = degrees, it=20 contains just one tooth.   At this top level, which has a = radius of=20 24 cm, is located the turbine outlet, where water should exit, = forming a=20 homogenous flat jet.   Consequently, the contours of the = turbine=20 rotor grooves should be ring-shaped.   Also, the water which = previous=20 ran along the inner side of a cone-shaped wall, now is contained = in a=20 space between that wall and the inner turbine cone.   These = surfaces=20 can effectively be a nozzle and this long groove can have = additional=20 divider walls (shown as thick red lines), to enlarge the = pressure-surfaces=20 in this area.


Winding Staircase
Fig 07.05.09 attempts to = give the=20 impression of the spiral arrangement of the previously described=20 tooth-shaped notches running around the surface of the turbine = cone.=20   The cone-like mountain shape has faces A running all around it. =   These=20 faces start at a low angle and then become steeper as they rise = higher.=20   Each of these has a vertical wall B alongside it, formed by the side of the next = innermost face.=20   These faces are not visible at the right hand side of the = diagram=20 as their downward slopes are hidden from view.


For=20 clarity, in this diagram the cone is shown inverted, and so the = direction=20 of rotation appears clockwise, but in reality, when in its correct = position, the rotation will be counter-clockwise.   Notice in = the=20 upper diagram, that the incoming water D hits these faces at nearly a right-angle, providing = substantial thrust in the direction of the arrows.

As the = lower=20 diagram shows the top view of the inverted cone it has the = appearance of a=20 conical hill. At points E and=20 F, lines are marked = which=20 indicate the height of the saw tooth shaped indentations in the = surface of=20 the cone.   The lines at E=20 represent the pressure-side, while at F the inner side indicates only the slope surface and = thus no=20 =91suction-side=92 exists.

Now these indentations are not = arranged to=20 run straight down but are shifted as shown in the diagram at point = G.   Previous = vertical=20 indentations E now = create the=20 pressure-wall H, = which=20 corresponds to the previous indentation A in its spiral path.   The inner-walls F of the earlier = indentations thus=20 create the surface M = through=20 their vertical walls B.  =20 In effect, the whole hill is built from these successive = =91winding=20 staircases=92, which admittedly actually don=92t have any steps. =   These=20 paths spiral upwards with progressively smaller radius and = increasing=20 steepness.

At point N in=20 the diagram, part of several of these spiral pathways is shown. =  =20 Here, the vertical walls between them are visible only as small = blue=20 curves.   The whole of the surface area of this turbine cone = is a=20 pressure-side because of these spiral surfaces running all around = it.=20   Like diagonally falling rain, water flows all around the = surfaces=20 of that hill in its downward flow, and anywhere it is forced to = turn right=20 it generates a rotational force on the turbine cone.   = Remember that=20 this machine has a cone-shaped housing which ensures that the = water flows=20 exactly in its intended path.


Crossing=20 Flows
To summarise, in Fig=20 07.05.10 the complete 360 degree surface = of the cone=20 is shown four times one below the other.   Since the wide = part of the=20 cone has a radius of 24 cm it has a circumference of about 150 cm = (R24 and U150), while the narrow = part has a=20 radius of 16 cm and hence a circumference of about 100 cm (R16 and U100).   The length = of the=20 side-surface is about 24 cm (H24).   Using this example with these dimensions, = the upward=20 flow is along the indentations in the cone and along the walls of = the=20 cone.


The = angle=20 of entry of the water at the narrow circumference was assumed to = be 30=20 degrees.   Maintaining this steady angle would cause the = water flow=20 to cover an angular sector of about 150 degrees, exiting at that = same=20 angle.   Due to the centrifugal force of water striking the = wall at=20 an angle, an upward force is generated which causes the water to = follow a=20 steeper track and exit after crossing a sector which spans only = 120=20 degrees or so (S120) = and exit at=20 an increased angle of about 35 degrees.   That track D (drawn in blue) is shown = several=20 times in the top diagram.

Water flowing in indentations = will=20 follow this track.   However, this water can=92t follow the = faster=20 moving wider circumference at the top of the cone.   In order = to=20 achieve the =91neutral-force=92 track for the complete path across = the cone,=20 the indentations need to have an increased backward curvature of = one=20 third.   This indentation track H is shown in red and is contained within a sector of = 40=20 degrees (S40) and = this path is=20 also drawn several times in the top diagram.

In order to = have the=20 turbine generate a mechanical turning force, the indentations need = to be=20 curved backwards more strongly.   Here, for example, that = sector was=20 extended to cover 90 degrees (S90) so water is channelled outwards faster, and exits = after=20 covering only 70 degrees (S70).=20   In the second diagram that indentation L (shown in red) and = water=20 track K (shown in = blue) are=20 drawn several times.

The indentations of the turbine are = shown=20 here as saw tooth-like notches which are open on their outer side. =  =20 This arrangement results in two separate flows: on the one hand, = there is=20 forced flow within the indentations and on the other hand there is = the=20 free flow of water on the wall of the cone.   In the third = diagram,=20 these indentations L = (shown in=20 red) are drawn several times as are the tracks of the free-flowing = water=20 D (shown in blue). =   These=20 two paths cross each other at an angle of about 90 degrees.=20

Because free-flowing water projected upwards is too slow = for the=20 turbine-surface which is moving rather fast, but the water = movement will=20 be fast enough if it flows along the indentations L which are curved = backwards as shown=20 in the bottom diagram.   In this diagram, both track D (shown in blue) taken by = the=20 free-flowing water and the indentation-forced track K (shown in red) are = shown.  =20 Again, both flows are drawn several times and it can be seen = clearly that=20 these paths cross each other at an acute angle.   The = free-flowing=20 water =91brushes=92 across the water which is flowing forwards in = the=20 indentations.   It does this in the direction of rotation and = this=20 causes the water flowing in the indentations to start revolving.=20

Water within the indentations becomes redirected backwards = and=20 transfers it=92s inertia to the pressure-sides of the = indentations, thus=20 decelerating it=92s forward motion.   This water still has = centrifugal=20 force, but the further out it progresses, the faster the = pressure-sides=20 run away ahead of it.   This water which is flowing =91too = slowly=92 can=20 only apply pressure to the walls if they were much more strongly = curved=20 backwards, and even in that case it would only be by a small angle = which=20 would impart practically no additional turning momentum. =

Also,=20 free-flowing water can=92t keep up with the faster movement of the = turbine=20 at its larger exit circumference.   However, the outward = water flow=20 is easily fast enough to fill the grooves with water and produce=20 additional rotation around its longitudinal axis.   This=20 revolving-water-cylinder effectively works like a gear wheel as it = applies=20 the pressure of the free flowing water on to the pressure-sides of = the=20 grooves.   The water flowing along the cone-wall is not = pressed into=20 the grooves, and so it is not redirected and its forward motion is = not=20 decelerated.   So the centrifugal forces of that free-flowing = water=20 can go on contributing to the turning momentum of the turbine, but = only=20 indirectly, by driving that water-cylinder within the grooves.=20


Spin inside the Grooves
Fig 07.05.11 shows = sections of the=20 area between the cone wall KW (shown in grey) and the turbine cone = T.   Free-flowing = water moves=20 alongside the cone wall, moving upwards and outwards.   At = the=20 surface of the turbine, the turbine blades TS (light shading) are arranged in the shape of saw = tooth-like=20 notches.   Water flowing within these grooves is guided = outwards=20 along the ever steepening track.   Turning momentum is = generated by=20 the redirection of this part of the water flow.


On the=20 pressure-sides of these grooves, there is also the additional = pressure of=20 the free flowing water B.  =20 This component of the water flows along a path which is not so = steep and=20 so it moves faster in the direction of rotation, i.e. it sweeps = over the=20 grooves.   This generates a revolving movement C, in the water flowing = inside the=20 grooves.   This increases the pressure on the pressure-sides = of the=20 grooves. So, this free-flowing component of the water flow, = contributes=20 indirectly to the turning momentum of the turbine.

The = diagram at=20 the lower left hand side of the Figure is a sketch of the outlet = at the=20 top of the turbine.   The inner wall of the cone is curved = slightly=20 inwards as shown.   This guides the free-flowing component of = the=20 water flow into the grooves.   It should also be noted that = as this=20 part of the water is redirected, it is also decelerated which = contributes=20 further to the turning momentum of the turbine.

At the = lower right=20 hand side of the Figure, both the cross-sectional and longitudinal = views=20 of the outlet are shown.   Here, the groove is no longer saw=20 tooth-like but instead it has a constant width, and this causes = the water=20 to exit in a continuous jet.   The groove here is rather wide = and=20 could well be divided by the introduction of additional blades = ZS, which would allow the = water=20 pressure to be applied to a greater surface area.

To = summarise;=20 with this arrangement, not all of the water flow is forced into = the=20 grooves and immediately redirected and decelerated.   The=20 free-flowing parts of the water are allowed to move in its natural = direction and under the influence of the centrifugal forces they = follow a=20 steeper path as they flow outwards and upwards.   Moving = along this=20 track causes the water to cross over the water flowing in the = grooves.=20   This in turn, causes the water in the grooves to rotate as = it flows=20 upwards and this additional revolving movement add to the torque = being=20 generated by the water flow.   Finally, as it nears the = outlet, the=20 free-flowing component of the water is directed into the grooves = and this=20 redirection causes a deceleration which adds even further to the=20 rotational drive of the turbine.

One further beneficial = effect=20 which is easily overlooked, is the fact that the water in each = groove=20 forms a long stretch of rotating water.   This length of = rotating=20 water rotates faster in the upper sections of the groove and a = twisting=20 vortex of this type generates a strong suction which pulls the = water=20 entering the turbine inlet, strongly upwards towards the outlet of = the=20 turbine.   This has been described in detail in earlier = chapters and=20 is further discussed later on in this document.=20


Cross-Sectional Surfaces
The lower = diagram of=20 Figure 07.05.12 = shows a=20 cross-sectional view through a cone-shaped turbine T, which has it=92s intake = extended=20 downwards by an additional section TE.   Between the turbine and the conical wall = KW (shown in grey), water = flows from=20 the intake at the bottom E and=20 exits at the upper outlet A.=20   This flow has two components.   The first, which is = shown in=20 dark blue, flows freely along the conical wall.   The second, = which=20 is shown in light blue, flows in the grooves or indentations = formed by the=20 saw tooth-like turbine =93blades=94.


The = upper=20 diagram in the Figure shows a schematic cross-sectional = representation of=20 the plan view of this turbine.   The ring-shaped water outlet = A is shown in light-blue. =   This=20 outlet is formed between the inside of the conical housing, which = has a 24=20 cm radius at this level, and the cone which has a 22 cm radius. =  =20 These are marked as R24 and=20 R22 respectively, = and between=20 them a 2 cm wide outlet is formed, with a cross-sectional surface = area of=20 about 290 cm2 (F250).=20   Also shown in light blue, is the ring-shaped inlet E, formed between a radius = of 16 cm=20 and one of 12 cm (R16 and R12), and so is 4 cm wide, = with a=20 cross-sectional area of about 350 cm2 (F350).

On the = right hand side=20 of the Figure is shown the previous curve D (shown in dark blue), which represents the track of = the water=20 flowing in the grooves.   Water enters the turbine along its = lower=20 edge, at an angle of about 30 degrees and exits from the top of = the=20 turbine at an angle of about 60 degrees.   Free-flowing water = also=20 enters the underside of the turbine at a very low angle and flows = upwards=20 until near the outlet it is directed into the grooves where it = also exits=20 the turbine at that same steep angle.

In the example = above, it was=20 assumed that the inlet water speed was about 7 m/s (V7), i.e. = entering at=20 an angle of 30 degrees while moving in the horizontal direction at = about 6=20 m/s (V6), the same = speed that=20 the turbine is moving at that level.   The inlet, water has a = vertical rate of movement of about 3.5 m/s (V3.5).   If we were = to assume=20 that the water speed at the outlet is also 7 m/s, due to it=92s = steep exit=20 angle of 60 degrees, it=92s horizontal velocity will be only 3.5 = m/s.  =20 However, it actually exits at a vertical speed of 6 m/s (see the=20 vector-graphs).

Within pipes, the linear speed of flow is=20 inversely proportional to the cross-sectional area of the pipe. =   In=20 our particular case, due to the rotational component of motion, = the flow=20 also depends on the =91gradient=92 of the flows, and not just the = speed of=20 movement in the axial direction.   If water exits at the top = at 6 m/s=20 through an opening with a cross-sectional area of 250 = cm2, then=20 if the inlet flow has a vertical speed of only 3.5 m/s, then it = would=20 require an inlet cross-sectional area of about 430 cm2, = so our=20 cross-sectional area of only 390 cm2 is a little too = small.=20


Suction Effect through Centrifugal = Force
It=20 was mentioned above, that centripetal (inward) acceleration is = stronger=20 than the acceleration under gravity at relatively low speeds = within a=20 radius as narrow as this.   Since centrifugal force increases = with=20 the square of the speed, the outward pressure is a multiple of the = weight=20 of the water.   With the inclination of the conical housing = wall=20 shown here, about one third of this force results in an upward = push along=20 that wall.

Because of this, the upward water flow gets = shifted on=20 to an increasingly steeper track and consequently it exits from = the=20 turbine outlet at a rather acute angle.   But if the = cross-sectional=20 area of the intake is too small, then a sufficient mass of water = is=20 prevented from flowing into the turbine and the upward movement is = hindered.   This causes the free-flowing component of the = water to=20 move along a flatter track, which again results in increased = centrifugal=20 forces.   So, finally, an inlet with too small a = cross-sectional area=20 creates enormous suction forces and the inlet water is pulled = upwards very=20 strongly.

The turbines described in previous chapters, = could only=20 use the flows generated by pumps.   With an air-driven = machine, it is=20 possible to generate areas of relative void into which air = particles move=20 through their own normal molecular movements.   Autonomous=20 acceleration up to the speed of sound is possible with a minimum = of input=20 energy.   Water is not compressible, so pressure is = transmitted=20 through water immediately.   Suction pressure also acts = immediately=20 with no delay.   Consequently, if the water in the upper = areas of the=20 turbine is pushed upwards by centrifugal forces, these forces also = exert=20 an upward pull on the water lower down in the turbine.   So = unlike=20 all of the machines described earlier, in this turbine, flows are=20 generated based on the effects of centrifugal force alone.  =20 Experiments with similar machines has confirmed that more water = was pulled=20 upwards than gravity would have been able to move downwards when = acting on=20 the same mass of water, even when just simple cones with plane = surfaces=20 were used.


Pump-Turbine = Hybrid
Turbines of=20 this type can also work as a pump.   If the cone is driven = around,=20 then it will cause the surrounding water to rotate.   At the=20 housing=92s conical wall, water gets lifted through the = centrifugal force.=20   That =91pump=92 has no forward-facing surfaces and so it = can=92t affect=20 the pressure.   The water is presented with vertical walls in = close=20 proximity to =91winding staircases=92 which move continuously = dragging the=20 water into rotation.   The higher that the water is lifted, = the=20 greater the cone radius encountered, and the greater the = centrifugal=20 forces which it experiences.

As the rotational motion = increases,=20 the lifting force-component become stronger and the water gets = pressed=20 into the diagonal surfaces of the grooves, and the turning = momentum is=20 achieved which allows the pump to become self-powering and no = longer=20 needing any input power to continue operating.   If the speed = of=20 rotation continues increasing, and turbine-mode is achieved, then, = if the=20 turbine is not loaded it will accelerate automatically until the = water=20 can=92t enter the inlet any faster or alternatively, until the = turbine=20 self-destructs.


Safety first: Avoiding=20 Liability
In Figure = 07.05.13, the previous discussed elements are shown = installed in=20 housing G (shown in = grey) along=20 with some additional elements.   The most important new = component is=20 the =91sluice-valve=92 B (shown in=20 yellow).   This is a ring-shaped device which can be raised = or=20 lowered (as shown on the right hand side of the diagram), to = control the=20 water flow, and if necessary, bring the device to a complete = standstill in=20 the event of uncontrolled self-acceleration.


If=20 preferred, that control valve can be of different construction and = installed elsewhere.   A definite requirement of any piece of = equipment of this type is the ability to guarantee complete safety = during=20 operation.   It should be remembered that centrifugal forces = increase=20 with the square of the speed, which means that the rapid rotation = of a=20 mass of just one kilogram can generate a loading on the housing = wall of=20 several tons.   Part of this enormously enlarged force is = converted=20 into turning momentum.

I have only = described=20 movement principles in general, and how some constructional = elements could=20 be designed.   However, it must be made completely clear, = that I=20 accept no responsibility or liability for the actual construction = or use=20 of any such machines.   The complete responsibility for all = risks,=20 rests solely with whoever decides to actually construct or operate = any=20 such machine. =


Circuit

As described in detail above, water (shown in light = blue) is=20 sucked in through inlet E into=20 the area of the turbine-inlet designated TE.   This water then flows both upwards and = outwards,=20 flowing inside saw-tooth-like turbine-grooves positioned close to = the=20 conical wall of the outer housing KW.   Approaching the exit point, the water is = deflected=20 into a groove which runs all around the turbine cone, so that at = outlet=20 A, in Figure=20 07.05.13 a steady, flat jet of water is = ejected=20 outwards.   This water flies into the air-filled area shown = shaded=20 light yellow, and falls under gravity as indicated by the blue = points.=20   The level of the water in that backflow area R, is only a few = centimetres below the=20 level of outlet A, = so water is=20 lifted against gravity through only a small height.

The = water flow=20 exiting the turbine does so at a relatively steep angle, and that = flow=20 moves relatively slowly relative to the already spinning turbine = cone.=20   When flowing downwards, the water should generate some = faster=20 rotational movement, guided by correctly curved fins, marked here = as=20 =91backflow-stator=92 RS (shown in=20 dark blue).   The conical wall is attached to the housing by = these=20 cross-beams.

In the lower diagram, at the backflow-area, = an=20 =91inlet-stator=92 ES (shown shaded=20 in dark blue) is marked and through these fins water is directed = again=20 into the turbine intake area.   As explained earlier, = suction,=20 generated by centrifugal forces, pulls the water upwards.   = That=20 water does not flow straight upwards but rotates as it moves = upwards and=20 so rotational acceleration forces are generated.

The inlet = area is=20 divided by six appropriately curved fins, as indicated in the = plan-view=20 schematic diagram at the bottom of the Figure.   These = conduit=20 sections could have vertical dividers if so desired.   The = shape (or=20 any equivalent design of conduit) produces the necessary rotation = and=20 angle of water flow needed at the turbine inlet. =

Example:=20 Mazenauer and Clem
Experienced readers will be familiar = with=20 the engine of Hans Mazenauer and the working engine of Richard = Clem.=20   These are detailed in my =93Ether-Physics=94 book in = chapter 05.10:=20 =91Tornado-Motor=92 and in my 2005 chapter entitled = =91Auto-Motor=92.   In=20 these, I concentrate on working out the suction-effect of twisting = flow=20 within the indentations, while here in this design of the=20 =91Centrifugal-Thrust-Engine=92, enormous centrifugal forces are = used.=20

Mazenauer did use air-driven double-cones as shown in the = upper=20 illustration of Figure 07.05.14.=20   This did accelerate unaided from a stationary start right = up to a=20 speed which caused it to self-destruct.   Most unfortunately, = Mazenauer was financially ruined by these experiments, and so was = unable=20 to complete his work successfully.   Mazenauer used a = double-cone,=20 where the large part (shown on the left hand side of the = illustration)=20 worked as a turbine while the small part functioned as a pump. =  =20 During operation, air got moved in inward-turning and = outward-turning=20 vortices, overlaid by twist flows within the grooves.


However,= a=20 pump of this type which has the driving medium flowing from the = outside=20 towards the inside will not be very effective.   What is = needed is a=20 turning vortex which moves towards the turbine intake and this is = better=20 generated by stationary fins of the previously shown inlet-stator = (at=20 least when using water as working medium).   Clem based his = engine=20 design on an asphalt-pump, and without the slightest doubt, he ran = his car=20 without consuming any common fuel.   Based on known sketches = and=20 pictures, he did use a cone with grooves arranged with rather = small=20 gradients (see the lower diagram).   However a working-medium = which=20 flows in grooves is =91stirred=92 by the pattern of its own = movements.  =20 While that is an advantage for heating asphalt, it meant that Clem = had to=20 dissipate surplus heat, and because of the high temperatures = generated he=20 used oil as his working medium.   As shown by my analysis = above, much=20 steeper indentations combined with much better angles, generate = far=20 greater torque.   In addition, Clem=92s grooves were rather = small and=20 did not present large surfaces with strong resistance to the = driving=20 medium.

As is the case here, the centrifugal forces of = water=20 movement is utilised, and the turning momentum is achieved by = pressure=20 applied to the turbine surfaces.   For this reason, the = grooves need=20 to expose only their pressure-sides, on which flows can produce = the best=20 effect.   So, unlike these examples from Mazenauer and Clem, = my=20 analysis indicates that =91grooves without suction-sides=92 shaped = by these=20 saw tooth-like turbine-paths, are very advantageous.=20


Horizontal Shaft
When using a = horizontal=20 shaft version of an engine of this type, some additional = components and=20 details are needed to implement the design.   This = arrangement is an=20 interesting variation and it can be in the form shown in Figure 07.05.15.   = Here, the=20 conical wall KW = (shown shaded in=20 grey), turbine T and = the turbine=20 inlet TE are similar = to those=20 already discussed.   At the outlet A however, water now falls downwards (as indicated by = the blue=20 dots) through the air-filled area (shaded in light yellow) into = the=20 reservoir.   As in the previous example, at the outlet there = is a=20 safety-valve B = (shown in yellow)=20 which is installed to control the flow.


Water = flows=20 into the backflow tank R (shaded=20 light blue).   From there, it is guided towards inlet E via pump P (shown shaded green) and = the=20 snail-conduit C. =   This=20 inlet-conduit is arranged diagonally, so that water enters the = space=20 between the conical housing wall and the turbine cone at the angle = required for the operation of the turbine.

The pump is = installed=20 fairly low down in the water tank as it is only used when starting = the=20 turbine from standstill.   Once the turbine is running, the = turbine=20 creates sufficient suction to maintain the water flow without the = need for=20 the application of any external power.   The water pump just = turns=20 idly when the turbine is running, rotated by the water flow caused = by the=20 suction created by the rotation of water inside the conical = turbine=20 section.   It is actually possible to boost the rotational = speed of=20 the turbine by powering the pump and thus boosting the mass flow = through=20 the turbine.

In principle, any pump could be used in this=20 position.   In this example, the schematic shows a = =91slide-pump=92 P with its eccentric shaft = and=20 radial-moving pump blades PS=20 (shown in dark green).   The advantage of this kind of pump = is that=20 it has a precisely known volume contained within it=92s chambers = and that=20 exact volume is transported during each revolution.   Hence, = the=20 pumped volume is exactly proportional to the pump revolutions.=20


Small Constructional Volumes
A = turbine engine=20 of this type with a horizontal shaft, could be installed in = vehicles to=20 provide the mechanical drive via a standard clutch and gear = transmission.=20   On the other hand, since electricity has so many different = uses,=20 this engine could readily be used to drive an electrical = generator.  =20 The electricity produced by such an arrangement could readily be = used for=20 both powering a pump and it=92s control units.   Mind you, = electrical=20 generation can also be achieved quite easily with a vertical shaft = turbine.   In general, we tend to think that a larger = throughput=20 volume will be needed to produce a greater level of performance. =  =20 Here, however, the performance is based on centrifugal forces and = inward=20 acceleration and since these are inversely proportional to the = radius, the=20 usual idea that performance increases with increasing size, just = does not=20 apply.   At any given speed, the centrifugal force at a small = radius=20 is much greater than at a large radius, and the vertical lifting = component=20 is also correspondingly stronger in smaller turbines.

The = turbine=20 T shown in Figure 07.05.16, has a = wide exit-level=20 radius of only 18 cm. The conical inner surface of the housing = KW (shown in grey) angles = downwards in=20 a straight line to a snail-like inlet-area E.   Water exits from the top of the turbine = through=20 outlet A and flows = back down=20 through the backflow-conduit R.=20   This backflow winds spirally downwards and enters pump = P (shaded green) which = pushes it=20 through conduit C = back into the=20 snail-like inlet at the base of the turbine.


The = path of=20 the water through the turbine and subsequent backflow conduit is = shown=20 here shaded in light blue, while the water path within the pump = and the=20 turbine inlet is shaded in dark blue.   The pump shown in = this=20 schematic diagram is an impeller type of pump which operates in a = similar=20 way to the previously mentioned slide-pump where each revolution = of the=20 pump represents a known volume of water throughput.   This = turbine is=20 controlled by the revolutions of the pump.   When the pump is = stationary it operates very nearly the same as a stop-valve. =   In=20 addition, the suction produced by flow at the conical wall has an = effect=20 back through the inlet to the pump.   When the turbine is = running,=20 the pump effectively acts as a =91moderator=92 which does not = require much in=20 the way of energy input.

It is also possible for all of = the=20 internal space of the turbine to be filled with water, including = the area=20 at outlet A, thus = producing a=20 completely closed circuit of water.   This design of turbine = could=20 also be arranged to have a horizontal shaft.   In addition, = this=20 general principle of combined movements can be applied to most = variations=20 of turbine design.


Impossible?
We now = come to=20 the question which is often asked, namely, =93why does this = machine work at=20 all?=94.   Without any shadow of doubt, when spun at a high = rate of=20 revolutions per minute, a one-kilogram mass produces literally = tons of=20 pressure on the inner walls of a surrounding cylinder.   = Given=20 cone-shaped inner walls, there is not the slightest doubt that a = flowing=20 mass of water will press outwards from a narrow radius towards a = wider=20 radius.   Also, without question, is the fact that this flow = can=20 generate mechanical turning momentum via turbine-blades as a = side-effect.=20   What needs to be determined through experiment, is the = optimum=20 energy draw-off and distance between the turbine cone and the = conical=20 inner wall of the housing.   What is absolutely certain is = that the=20 turbine will not require the entire kinetic energy produced to = power=20 itself.

Because water has =91cohesive consistency=92, any = flow along=20 the conical wall produces a suction effect on the water below it. =  =20 This means that the flow-pressure is like flow-suction and so = produces a=20 closed flow-circuit.   Backflow must be organized with the = lowest=20 level of friction losses and should be =91force-neutral=92, = requiring no=20 energy input to function as required. It is important that the = water being=20 channelled to the narrow radius inlet does not oppose the = centrifugal=20 forces operating the turbine.

When these design parameters = are=20 applied, a steady circuit flow with excess energy generation is = possible.=20   The dynamic pressure of the =91water-fall=92 of the water = (which has=20 considerable weight) is converted into mechanical turning = momentum, and=20 after that the water must continue its flow in an = =91energy-neutral=92 way as=20 it is guided inwards to the inlet-area.   Various = constructional=20 measurements were given in the above example of how this motion = principle=20 operates.   However, it should be realised that those = measurements=20 were just presented as an illustration of the principles involved = and many=20 alternative dimensions may be used when a turbine of this type is = being=20 constructed.   The following design also illustrates an = effective=20 working design.


Outlet and = Water-Cylinder
In=20 Figure 07.05.17, a = horizontal=20 axis turbine T is = shown which=20 has tooth-like turbine-blades TS=20 as part of the cone.   The main cone of the turbine is = extended by=20 the turbine inlet section TE.=20   Opposite these surfaces is the hollow-cone of the conical = housing=20 wall KW (shown in = grey) and it=20 is attached to the main housing G (also shown shaded in grey).   Water, (shown = in light=20 blue) flows between these surfaces in a rotating motion.   = This=20 physical construction and operational movement is the same as in = the=20 previous examples.


In the=20 previous examples of construction, it was suggested that the flow = along=20 the side cone-wall was directed into the turbine grooves just = before=20 exiting from the turbine cone.   For this to be effective, it = is=20 necessary to have an adequate flow in the outlet region.   = Only=20 practical experiments can determine what percentage of the = free-flowing=20 water is the most effective to directed into the turbine grooves = at this=20 point.   For example, this diagram shows a design of outlet = A where all of the water = at the cone=20 wall can flow off freely.   Here, cone ridges produce a = smoothly=20 curving water flow across the surface of the turbine cone. =

A new=20 constructional element in this design is shown as ring B which runs all the way = around the=20 upper edge of the turbine cone.   Water enters this =91round = pipe=92=20 tangentially and does a U-turn of some 180 degrees.   = Previously, it=20 was shown that water left the outlet at an angle of about 60 = degrees, so=20 water will enter this pipe by a spiral track.   No matter = what the=20 angle of entry is, the water will exit from the =91round = half-pipe=92=20 tangentially because of it=92s own motion generating centrifugal = force (so,=20 as drawn here, it will move towards the right hand side). =

Sharp=20 redirections like these ones, normally produce turbulent flows = with=20 corresponding major friction losses.   This is because within = any=20 normal pipe bend, the inner flow path around the bend is much = shorter than=20 the outer flow path around the bend.   But, in this case, = there is no=20 inner part of any such narrow bend, and the water keeps rotating = in a=20 cylindrical movement as it flows.   Within these = water-cylinders,=20 flow layers of different radius and different turning-speeds = balance out=20 without friction.   This =91all-around=92 pipe with the water = rotating=20 inside it, acts like a ball-bearing, so the flow from the outlet = and the=20 redirection of water towards the inlet is achieved with the = minimum of=20 frictional losses.


Axial Backflow
The = conical=20 inner wall KW = (shaded in grey)=20 needs to be attached to the outer parts of the housing G (also shown shaded grey) = with=20 spike-rods C (shown = in dark=20 blue).   The backflow-conduit is positioned all the way = around the=20 turbine, and it has a ring-shaped cross-sectional area.   The = water=20 in this conduit flows with a rotational angle of about 60 degrees, = so=20 these cross-beams should be shaped like fins to push the flow into = a=20 somewhat greater angular flow of about 75 degrees, towards the = right.=20

The cross-sectional area of the ring-shaped = backflow-conduit D (light blue) is = relatively large, so=20 there is little friction at it=92s surface.   Water will move = relatively slowly towards the right when in that conduit.   = This area=20 represents a =91buffer=92 for the water flow as water there can = move towards=20 the right, adjusting it=92s rate of rotation as it flows along.=20

Another new constructional element here are the fins E (shown in dark blue), = which function=20 like a stator.   Unlike the previous examples, here the flow = is=20 directed into a straight axial flow direction (from left to right = without=20 any rotation).   In the backflow-conduit D, the water is still = moving with a=20 more or less spiral track.   Consequently, the left hand ends = of fins=20 E should be rounded = to avoid any=20 frictional losses, while the right hand edges of these fins should = end=20 sharply.

Unlike the few cross-beams C, about 12 to 18 cross-beams E should be installed.   The cross-sectional = area of the=20 conduits becomes less, so the water accelerates accordingly. =   Unlike=20 the previous enlargement of the cross-sectional area, this = narrowing does=20 not affect resistance.   Water is now directed parallel to = the system=20 axis by these fins E.   The=20 water there is not rotating around the system axis and so does not = have=20 any centrifugal force acting radially outwards from the system = axis.=20


Centripetal Backflow
Like ring B which runs all the way = around, we=20 now have ring F = (shaded in light=20 blue).   Water enters tangentially into this ring, flows = radially=20 inwards towards the system axis and then leaves this ring via = conduit H=20 (shaded in dark blue) towards the turbine cone.   As within = ring=20 B, here too, the = water flow in=20 ring F is = rotational, and here=20 again, the relatively sharp redirection occurs without significant = frictional losses, practically like a ball-bearing.

As the = water=20 moves, at all times it=92s centrifugal force is directed on to the = wall at=20 right angles to the wall.   Because of the direction of this=20 centrifugal force, the water flows off ring F in a tangentially inward direction.   The = volume of the=20 ring reduces the further inwards it goes but it opens further as = it=20 approaches conduit H = allowing=20 additional space for movement.   Thus, water is directed = inwards to=20 the smaller radius at the system axis and this motion is not = opposed to=20 the direction of the centrifugal forces which are radial to the = system=20 axis.

Water from ring F=20 now runs in an axial direction towards the turbine inlet.   = However,=20 the inlet water needs to be rotating around the system axis when = it=20 reaches the inlet to enable the necessary centrifugal forces to be = produced.   Consequently, the water needs to enter the space = between=20 the turbine cone and the inside wall at an angle of about 30 = degrees=20 through the turbine inlet.   That redirection of flow, = (inwards and=20 towards right side of the diagram) to become a rotational flow = (around the=20 system axis and towards the right) is achieved by conduit H.   Fins are = installed in this=20 section, directing the water from ring F radially inwards.   These fins are gently = curved in the=20 direction of system rotation, so water is guided by slight angular = deflections towards the turbine inlet E, ending up with the required 30 degree angle.=20


Pump and Control
Before water reaches = the=20 turbine intake area, it flows through pump P (shaded green).   It=92s pump-blades PS (dark blue) are = arranged at right=20 angles to the previously mentioned fins, to produce an angle of 60 = degrees=20 opposite to the direction on rotation of the turbine.   = During normal=20 operation, this pump =91idles=92 within that diagonal flow.   = Suction of=20 the water at conical wall reaches back diagonally through the pump = to=20 conduit H, and from = there,=20 radially into ring F = and so to=20 it=92s inlet E. =

So because=20 of the resulting thrust-forces along the cone-wall, water is = pushed from=20 the turbine outlet A = into=20 backflow-conduit D. =   On=20 the other hand, because of the general flow within the closed = circuit,=20 water is dragged into turbine-inlet E.   Because the water within fins E and ring F and first part of fins = H, is not rotating around = the system=20 axis, no centrifugal forces hinder that radially inward movement. =  =20 So this redirection of water exhibits almost no resistance to the = flow.=20

The pump has important control-functions.   Under = normal=20 operation, the pump turns at the same speed as the water flow. =   If=20 greater performance is required, then the pump is powered up and = it=20 accelerates the water flow, speeding up the water jet feeding the = turbine=20 inlet which immediately creates an enhanced level of thrust.=20

Alternatively, if the rate of rotation of the pump is = reduced, the=20 intake water jet is reduced in effectiveness, reducing the = centrifugal=20 forces, which reduces the performance of the turbine. If the pump = is=20 stopped completely, then water flows into the turbine in the = reverse=20 direction, thus lowering the turning momentum to zero. =

That pump=20 is therefore in effect, a =91control=92 device which starts the = system,=20 controls it=92s running mode, deals with brief additional = performance=20 demands and can be used to bring the system to a halt.   Once = more,=20 let me point out that the system is self-accelerating provided = that it is=20 not loaded excessively.   It is absolutely vital to establish = the=20 maximum rate of revolution of the turbine and to prevent this = value from=20 being exceeded.   Let me again point out that this document = only=20 presents the theoretical considerations needed for the general = design of=20 such machines, however, all responsibility for any risks involved = in=20 actually producing or using any such machines resides exclusively = with the=20 people who construct or operate them.


Compact = and=20 Perfect
A turbine of the type described here might have = the=20 following dimensions:   A cylinder with an outer diameter of = about 60=20 cm.   A turbine-outlet which has a radius between 18.5 cm and = 20 cm=20 and a cross-sectional area of about 180 cm2.   If = water=20 exits from this outlet at 6 m/s in the axial direction, then the=20 mass-throughput will be about 100 Kg per second (with a pipe of 15 = cm=20 diameter and water flow of 100 litres per second - about 20 Km/h). =  =20 Pump-blades at the turbine inlet having a radius between 10 cm and = 15 cm=20 giving a cross-sectional area of about 360 cm2 = producing an=20 axial water flow of 3.5 m/s.   This throughput is achieved by = a=20 rotational rate of only 600 rpm.

Anybody can make = calculations=20 estimating the performance of this compact engine.   Unlike = any other=20 known machine and unlike any of the other designs presented, this=20 =91Centrifugal-Thrust-Engine=92 utilises these enormous = centrifugal forces,=20 not only for generating mechanical turning momentum but also for=20 automatically creating a continuous, steady circulation of the = working=20 medium.

Naturally these general design principles need to = be=20 optimised until perfectly designed versions become available = commercially.=20   It is possible that all of the internal combustion engines=20 currently in use in vehicles, will be replaced by this = zero-consumption=20 engine and, of course, a wide range of other power requirements = will also=20 be met by this design of turbine.



The Papp Engine.
The=20 Hungarian, Josef Papp, invented an unusual engine system which = genuinely=20 appears to be very nearly =93fuel-less=94.   His design = modifies an=20 existing vehicle engine to operate on a fixed amount of gas. =   That=20 is to say, the engine has no air intake and no exhaust and = consequently,=20 no inlet or exhaust valves.   The engine cylinders contain a = mixture=20 of gases which have an Atomic Number below 19, specifically, 36% = helium,=20 26% neon, 17% argon, 13% krypton, and 8% xenon by volume.   = The=20 control system causes the contained gas to expand to drive the = pistons=20 down the cylinders and then contract to suck the pistons back up = the=20 cylinders.   This effectively converts the engine into a = one-stroke=20 version where there are two power strokes per revolution from = every=20 cylinder.

A small amount of radioactive material is used = in the=20 engine, and I have seen it suggested that the engine should be = screened to=20 protect the user from radiation.   I=92m not sure that this = is correct,=20 but if it is, then it suggests that a matter to energy conversion = is=20 indeed taking place.   It seems most unlikely that the minor = amount=20 of radioactive material in the engine itself could cause any = significant=20 radiation.   The patent describes the material as = =93low-level=94 which=20 suggests to me, material no more dangerous that the luminous paint = that=20 used to be used on the hands of clocks and watches. =

Suitable=20 engines must have an even number of cylinders as they operate in = pairs.=20   Josef=92s first prototype was a four-cylinder, 90 = horsepower Volvo=20 engine.   He removed the intake and exhaust components and = replaced=20 the engine head with his own design.   During a thirty-five = minute=20 test in a closed room, the engine generated a constant 300 = horsepower=20 output at 4,000 rpm.   The electrical power needed to run the = engine=20 was produced by the standard engine alternator, which was also = able to=20 charge the car battery at the same time.   Interestingly, an = engine=20 of this type, quite apart from having zero pollution emissions = (other than=20 heat), is quite capable of operating under water.

Josef, a = draftsman and ex-pilot, emigrated from Hungary to Canada in 1957 = where he=20 lived until his death in April 1989.   There is solid = evidence that=20 Josef built an engine of over 100 horsepower (75 kilowatts) that = was=20 "fuelled" by a mixture of inert (or =93noble=94) gases.   = With no exhaust=20 or cooling system, it had huge torque even at low rpm (776 = foot-pounds at=20 only 726 rpm in one certified test).   Dozens of engineers,=20 scientists, investors and a Federal judge with an engineering = background=20 saw the engine working in closed rooms for hours.   This = would not=20 have been possible if the engine had been using fossil fuel. =   There=20 was absolutely no exhaust and no visible provision for any = exhaust.  =20 The engine ran cool at about 60=B0C (140=B0F) on its surface, as = witnessed by=20 several reliable observers.   All these people became = convinced of=20 the engine's performance.   They all failed to discover a = hoax.=20   Ongoing research in the United States (totally independent = of Papp)=20 has proved conclusively that inert gases, electrically triggered = in=20 various ways, can indeed explode with fantastic violence and = energy=20 release, melting metal parts and pushing pistons with large = pressure=20 pulses.   Some of the people performing this work, or who = have=20 evaluated it, are experienced plasma physicists.   = Contemporary=20 laboratory work has established that inert gases can be made to = explode=20

In a demonstration on 27th October 1968 in the Californian = desert,=20 Cecil Baumgartner, representing the top management of the TRW = aerospace=20 corporation and others witnessed the detonation of one of the = engine=20 cylinders.   In full public view, just a few cubic = centimetres of the=20 inert gas mixture was injected into the cylinder using a = hypodermic=20 needle.   When the gas was electrically triggered, the thick = steel=20 walls of the cylinder were burst open in a dramatic way.   = William=20 White, Edmund Karig, and James Green, observers from the Naval = Underseas=20 Warfare Laboratory had earlier sealed the chamber so that Papp or = others=20 could not insert explosives as part of a hoax.   In 1983, an=20 independent certification test was carried out on one of the Papp = engines.=20

Joseph Papp was issued three United States patents for his = process=20 and engines:

US 3,680,431 on 1st August 1972 = "Method and=20 Means for Generating Explosive Forces" in which he states the = general=20 nature of the inert gas mixture necessary to produce explosive = release of=20 energy.   He also suggests several of the triggering sources = that may=20 be involved.   It appears that Papp is not offering full = disclosure=20 here, but there is no doubt that others who have examined this = patent and=20 followed its outline have already been able to obtain explosive=20 detonations in inert gases.   Caution: = Anyone who=20 tries to duplicate this process must be very careful about safety=20 issues.

US 3,670,494 on = 20th June=20 1972 "Method and Means of Converting Atomic Energy into Utilisable = Kinetic=20 Energy" and

US 4,428,193 on 31st January 1984 = "Inert Gas=20 Fuel, Fuel Preparation Apparatus and System for Extracting Useful = Work=20 from the Fuel".   This patent shown here, is very detailed = and=20 provides information on building and operating engines of this = type.=20   It also gives considerable detail on apparatus for = producing the=20 optimum mixture of the necessary gasses.

At the time of = writing, a=20 web-based video of one of the Papp prototype engines running on a = test=20 bed, can be found h= ere=20 although it must be said that a good deal of the footage is of = very poor=20 quality, having been taken many years ago.   The video is=20 particularly interesting in that some of the demonstrations = include=20 instances where a transparent cylinder is used to show the energy=20 explosion.   Frame-by-frame operation on the original video = shows=20 energy being developed outside the cylinder as well as inside the=20 cylinder, which does seem to suggest that the zero-point energy = field is=20 involved.   I have recently been contacted by one man who = attended=20 some of the engine demonstrations run by Papp and he vouches for = the fact=20 that the engine performed exactly as described.


US Patent 4,428,193    =
                       31st January 1984                            =
Inventor: Josef Papp

INERT=20 GAS FUEL, FUEL PREPARATION APPARATUS AND SYSTEM
FOR EXTRACTING = USEFUL=20 WORK FROM THE FUEL


ABSTRACT =
An=20 inert gas fuel consisting essentially of a precise, homogeneous = mixture of=20 helium, neon, argon, krypton and xenon.   Apparatus for = preparing the=20 fuel includes a mixing chamber, tubing to allow movement of each = inert gas=20 into and through the various stages of the apparatus, a plurality = of=20 electric coils for producing magnetic fields, an ion gauge, = ionises,=20 cathode ray tubes, filters, a polarise and a high frequency = generator.=20   An engine for extracting useful work from the fuel has at = least two=20 closed cylinders for fuel, each cylinder being defined by a head = and a=20 piston.   A plurality of electrodes extend into each chamber, = some=20 containing low level radioactive material.   The head has a = generally=20 concave depression facing a generally semi-toroidal depression in = the=20 surface of the piston.   The piston is axially movable with = respect=20 to the head from a first position to a second position and back, = which=20 linear motion is converted to rotary motion by a crankshaft. =   The=20 engine's electrical system includes coils and condensers which = circle each=20 cylinder, an electric generator, and circuitry for controlling the = flow of=20 current within the system.

BACKGROUND OF THE=20 INVENTION
This invention relates to closed = reciprocating=20 engines, i.e., ones which do not require an air supply and do not = emit=20 exhaust gases, and more particularly to such engines which use = inert gases=20 as fuel.   It also concerns such inert gas fuels and = apparatus for=20 preparing same.

Currently available internal combustion = engines=20 suffer from several disadvantages.   They are inefficient in = their=20 utilisation of the energy present in their fuels.   The fuel = itself=20 is generally a petroleum derivative with an ever-increasing price = and=20 sometimes limited availability.   The burning of such fuel = normally=20 results in pollutants which are emitted into the atmosphere. =   These=20 engines require oxygen and, therefore, are particularly unsuitable = in=20 environments, such as underwater or outer space, in which gaseous = oxygen=20 is relatively unavailable.   Present internal combustion = engines are,=20 furthermore, relatively complex with a great number of moving = parts.=20   Larger units, such as fossil-fuel electric power plants, = escape=20 some of the disadvantages of the present internal combustion = engine, but=20 not, inter alia, those of pollution, price of fuel and = availability of=20 fuel.

Several alternative energy sources have been = proposed, such=20 as the sun (through direct solar power devices), nuclear fission = and=20 nuclear fusion.   Due to the lack of public acceptance, cost, = other=20 pollutants, technical problems, and/or lack of development, these = sources=20 have not wholly solved the problem.   Moreover, the = preparation of=20 fuel for nuclear fission and nuclear fusion reactors has = heretofore been a=20 complicated process requiring expensive apparatus.=20


SUMMARY OF THE INVENTION
Among the = several=20 objects of the present invention may be noted the provision of an = engine=20 which is efficient; the provision of an engine which does not = require=20 frequent refuelling; the provision of an engine which develops no=20 pollutants in operation; the provision of an engine which is = particularly=20 suited for use in environments devoid of free oxygen; the = provision of an=20 engine which requires no oxygen in operation; the provision of an = engine=20 having a relatively small number of moving parts; the provision of = an=20 engine of a relatively simple construction; the provision of an = engine=20 which can be used in light and heavy-duty applications; the = provision of=20 an engine which is relatively inexpensive to make and operate; the = provision of a fuel which uses widely available components; the = provision=20 of a fuel which is relatively inexpensive; the provision of a fuel = which=20 is not a petroleum derivative; the provision of relatively simple = and=20 inexpensive apparatus for preparing inert gases for use as a fuel; = the=20 provision of such apparatus which mixes inert gases in precise,=20 predetermined ratios; and the provision of such apparatus which = eliminates=20 contaminants from the inert gas mixture.   Other objects and = features=20 will be in part apparent and in part pointed out hereinafter.=20

Briefly, in one aspect the engine of the present invention = includes a head having a generally concave depression in it, the = head=20 defining one end of a chamber, a piston having a generally = semi-toroidal=20 depression in its upper surface, the piston defining the other end = of the=20 chamber, and a plurality of electrodes extending into the chamber = for=20 exciting and igniting the working fluid.   The piston can = move along=20 its axis towards and away from the head, causing the volume of the = chamber=20 to alter, depending on the position of the piston relative to the = head.=20

In another aspect, the engine of the present invention = includes a=20 head which defines one end of the chamber, a piston which defines = the=20 other end of the chamber, a plurality of magnetic coils wound = around the=20 chamber for generating magnetic fields inside the chamber, and at = least=20 four electrodes extending into the chamber for exciting and = igniting the=20 working fluid.   The magnetic coils are generally coaxial = with the=20 chamber.   The electrodes are generally equidistantly spaced = from the=20 axis of the chamber and are each normally positioned 90 degrees = from the=20 adjacent electrodes.   Lines between opposed pairs of = electrodes=20 intersect generally on the axis of the chamber to define a focal = point.=20

In a further aspect, the engine of the present invention = includes=20 a head which defines one end of a chamber, a piston which defines = the=20 other end of the chamber, at least two electric coils wound around = the=20 chamber for generating magnetic fields inside the chamber, and a = plurality=20 of electrodes extending into the chamber for exciting and igniting = the=20 working fluid.   The electric coils are generally coaxial = with the=20 chamber, and the working fluid includes a mixture of inert gases.=20

The apparatus of the present invention for preparing a = mixture of=20 inert gases for use as a fuel includes a chamber, electric coils = for=20 generating predetermined magnetic fields inside the chamber, = tubing=20 adapted to be connected to sources of preselected inert gases for = flow of=20 the gases from the sources to the chamber, and ionisers for = ionising the=20 gases.

The fuel of the present invention includes a = mixture of=20 inert gases including approximately 36% helium, approximately 26% = neon,=20 approximately 17% argon, approximately 13% krypton, and = approximately 8%=20 xenon by volume.


BRIEF DESCRIPTION OF THE=20 DRAWINGS

Fig.1 is a side elevation of an = engine of=20 this invention:
Fig.2 is a rear elevation of an engine = of this=20 invention:





= Fig.3=20 is a top view of an engine of this invention:



F= ig.4=20 is a cross-sectional view generally along line 4--4 of Fig.3 of an = engine=20 of this invention:



F= ig.5=20 is a cross-sectional view of a cylinder of an engine of this = invention:=20



F= ig.6=20 is a plan of the base of a cylinder head of an engine of this = invention:=20



F= ig.7=20 is an elevation of an electrode rod of an engine of this = invention:=20



F= ig.8=20 is an elevation, with parts broken away, of one type of electrode = used in=20 an engine of this invention:



F= ig.9=20 is a view taken generally along line 9--9 of Fig.8:



F= ig.10=20 is a cross-sectional view of a second type of electrode used in an = engine=20 of this invention:



F= ig.11=20 is a cross-sectional view similar to Fig.5 showing the piston in = its=20 uppermost position:



F= ig.12=20 is a cross-sectional view similar to Fig.5 showing an alternative = cylinder=20 used in an engine of this invention:



F= ig.12A=20 is a cross-sectional view similar to Fig.5 and Fig.12, but on a = reduced=20 scale and with parts broken away, showing an additional embodiment = of a=20 cylinder head used in an engine of this invention:



F= ig.13A=20 and Fig.13B are schematic diagrams of the electrical = circuitry for=20 an engine of this invention:



F= ig.14=20 is a schematic diagram of an alternative high-voltage ignition = system for=20 an engine of this invention:



F= ig.15=20 is a schematic diagram of an electronic switching unit for an = engine of=20 this invention: Fig.16 is a schematic diagram of a=20 regulator/electronic switching unit for an engine of this = invention:=20



F= igs.17A-17D=20 are schematic diagrams of a fuel mixer of the present invention: =
















= Fig.18=20 is a schematic diagram of the mixing chamber portion of the fuel = mixer=20 shown in Figs.17A-17D:



F= igs.19A-19E=20 are schematic diagrams of a portion of the electrical circuitry of = the=20 fuel mixer shown in Figs.17A-17D:



















F= igs.20A-20F=20 are schematic diagrams of the rest of the electrical circuitry of = the fuel=20 mixer shown in Figs.17A-17D:























N= ote:=20 Corresponding reference characters indicate corresponding parts = throughout=20 all of the views of the drawings.


DESCRIPTION OF = A=20 PREFERRED EMBODIMENT
Referring = to=20 the drawings, there is shown in Fig.1 a two-cylinder engine = 11 comprising a block 13 preferably of a nonmagnetic = material such as aluminium, a nonmagnetic head 15, and a = pair of=20 cylinder heads 17A and 17B of a magnetisable = material such=20 as 0.1-0.3% carbon steel.   Also shown in Fig.1 is a = flywheel=20 19 attached to a crankshaft 21, a generator = 23, a=20 high-voltage coil 25, a distributor 27 attached by a = gear=20 arrangement shown in part at 29 to the crankshaft, and an=20 electrical cable 31 which is connected to the distributor = and to=20 both cylinders.   Cable 31 (see Fig.2) is also=20 electrically connected to a switching unit 33 which = preferably=20 comprises a plurality of silicon controlled rectifiers (SCRs) or=20 transistors.   Also shown in Fig.2 is a second = electrical=20 connection of the cable to the cylinders, which connection is = indicated=20 generally at 35.   Turning to Fig.3, there is = shown a=20 starter motor 37 as well as a clearer view of the = connections=20 35 to each cylinder.
A=20 cross section of the engine is shown in Fig.4.   The = cylinder=20 heads have associated with them, pistons marked 39A and = 39B,=20 respectively, the heads and pistons define opposite ends of a pair = of=20 chambers or cylinders 41A and 41B respectively. =   The=20 pistons are made of a magnetisable material.   Although only = two=20 chambers are shown, the engine can include any number.   It = is=20 preferred, however, for reasons set forth below, that there be an = even=20 number of cylinders.   Pistons 39A and 39B move = axially=20 with respect to their corresponding heads from a first position = (the=20 position of piston 39A in Fig.4) to a second = position (the=20 position of piston 39B) and back, each piston being = suitably=20 connected to crankshaft 21.   As shown in = Fig.4, this=20 suitable connection can include a connecting rod CR, a = wrist pin=20 WP, and a lower piston portion or power piston LP. =  =20 The connecting rods and/or power pistons must be of = non-magnetisable=20 material.   When a split piston is used, pistons 39A = and=20 39B are suitably connected to lower piston portions = LP by=20 bolting, spring-loaded press fitting, or the like.   Pistons=20 39A and 39B are attached 180 degrees apart from each = other=20 with respect to the crankshaft so that when one piston is at top = dead=20 centre (TDC) the other will be at bottom dead centre (BDC) and = vice versa.=20   Additional pairs of cylinders may be added as desired but = the=20 pistons of each pair should be attached to the crankshaft 180 = degrees from=20 each other.   Of course, the relative position of each piston = with=20 respect to its respective head determines the volume of its = chamber.=20

Integral with the piston bodies are walls 43 which = form the=20 walls of the chambers.   Preferably, a set of air-tight = bellows=20 45, of similar construction to that sold under the = designation ME=20 197-0009-001 by the Belfab Company of Daytona Beach, Fla., are = suitably=20 secured between walls 43 and cylinder heads 17A and=20 17B respectively to form an air-tight seal between each = piston and=20 its cylinder head.   While walls 43 and piston = 39 can=20 be made of one magnetisable piece, a preferable and more efficient = construction has walls 43 separate from piston 39 = and made=20 of a non-magnetisable material.   The length of time that a = given=20 engine will run is a function of the efficacy of its sealing = system.=20   Means, such as bellows 45, for hermetically sealing = the=20 cylinders will optimise said length of time.   Such a = hermetic seal=20 should be secured between walls 43 and cylinder heads = 17 to=20 form an air-tight seal between them.   This seal could be the = airtight bellows system shown or some other sealing system such as = an oil=20 sealing system.

Cylinder bodies 47 (see = Fig.4), made=20 of nonmagnetic material such as stainless steel, extend from the = point of=20 attachment of each bellows to its cylinder head to the base of the = corresponding pistons, forming sleeves for each piston in which = each=20 piston moves.   Three sets of electric coils 49A, 49B, = 51A,=20 51B, and 53A, 53B, are wound around sleeves 47, = and=20 hence around chambers 41A and 41B, respectively, for = generating magnetic fields in the chambers, those coils being = generally=20 coaxial with their respective chambers.   Each of these coils = has an=20 inductance of approximately 100 mH.   It is preferred that = 14-19=20 gauge wire be used to wind these coils and that the coils be = coated with a=20 suitable coating, such as #9615 hardener from Furane Plastics, = Inc., of=20 Los Angeles, California, or the coating sold by the Epoxylite = Corp. of=20 South El Monte, California under the trade designation Epoxylite = 8683.=20   Each chamber is also surrounded by a pair of capacitors, = C1A,=20 C1B and C2A, C2B wound around it, capacitors C1A, = C1B=20 having a capacitance of approximately 1.3 microfarads and = capacitors=20 C2A, C2B having a capacitance of approximately 2.2 = microfarads.=20   The coils and capacitors are potted in hardened epoxy of = fibreglass=20 material 55.   The epoxy resin and hardener sold under the=20 designations EPI Bond 121 and #9615 hardener by Furane Plastics, = supra,=20 are satisfactory, but other epoxy material which will remain = stable at=20 temperatures up to 200 degrees F would probably also be = acceptable.  =20 It is preferred that a small amount of graphite such as that sold = under=20 the trade designation Asbury 225 by Asbury Graphite, Inc. of = Rodeo,=20 Calif., be included in the epoxy potting to prevent nuclear = particles=20 formed in the chamber from escaping from the apparatus.   Ten = to 15%=20 graphite to epoxy by weight is more than enough.

A=20 typical cylinder is shown in section in Fig.5, showing the = piston=20 in its fully extended position with respect to the head and = showing many=20 details on a somewhat larger scale than that of Fig.4. =   A set=20 of seals 57, made of a material such as that sold under the = trade=20 designation Teflon by the DuPont Company of Delaware, is = positioned=20 between the cylinder head and wall 43 to prevent escape of = the=20 working fluid from chamber 41.   A filler tube = 59 with=20 a ball valve at its lower end is used in filling the chamber with = the=20 working fluid but is closed during operation of the engine. =

The=20 cylinder head has a generally concave depression in it, indicated = at=20 61, which defines the top end of the chamber.   A = plurality of=20 electrodes for exciting and igniting the working fluid extend = through the=20 cylinder head into the chamber.   Two of those electrodes, = shown in=20 section in Fig.5 and labelled 63 and 65, have = tungsten points 75, while the other two, labelled 67 = and=20 69 (see Fig.6 for electrode 69) are = containers=20 called, respectively, the anode and the cathode.   The = electrodes are=20 generally equidistantly spaced from the axes of their chambers and = are=20 generally coplanar to each other, their mutual plane being = perpendicular=20 to the axes of their chambers.   Each electrode is positioned = 90=20 degrees from adjacent electrodes in this embodiment and are = generally=20 positioned so that a line from the anode to the cathode and a line = between=20 the other two electrodes intersect at a focal point generally on = the axis=20 of the chamber.   The radial distance of each electrode from = the=20 focal point is fixed for a reason discussed below.   The = general=20 construction of electrodes 63 and 65 is shown in=20 Fig.6 to Fig.9. These electrodes include a = conductive rod=20 71 (see Fig.7) preferably of brass or copper; a = conductive,=20 generally rectangular plate 73 (see Fig.6, Fig.8 and = Fig.9); and tungsten point 75 mounted in a = conductive base=20 77 generally at right angles to the plate (see Fig.8 = and=20 Fig.9).


The=20 construction of the anode and cathode is shown in Fig.10. = Each=20 includes a conductive rod 79 and a container 81. =   The=20 cathode container is substantially pure aluminium.   If = desired,=20 aluminium alloys with, e.g., less than 5% copper, 1% manganese and = 2%=20 magnesium may be used.   In one embodiment, the cathode = container=20 contains approximately four grams of thorium-232 and is filled = with argon.=20 In this same embodiment the anode container is copper or brass and = contains approximately two grams of rubidium-37 and approximately = three=20 grams of phosphorus-15 hermetically sealed in mineral oil.   = In a=20 second embodiment, the cathode is still aluminium, but it contains = at=20 least two grams of rubidium-37 in addition to the approximately = four grams=20 of thorium-232 in either argon or mineral oil.   In this = second=20 embodiment, the anode is also aluminium and contains at least 4 = grams of=20 phosphorus-15 and at least 2 grams of thorium-232 in argon or = mineral oil.=20   Alternatively, mesothorium may be used for the thorium,=20 strontium-38 may be used for the rubidium, and sulphur-16 may be = used for=20 the phosphorus.   Rods 71 and 79 extend through = cylinder head 17 to the exterior where electrical = connections are=20 made to the electrodes.   Each rod is surrounded by one of = four=20 insulating sleeves 83, the lower portion of each of which = being=20 flared outwards to seat firmly in the cylinder head.


The = piston=20 has a generally semi-toroidal depression in its upper surface (see = Fig.4, Fig.5 and Fig.11) and carries a conductive = discharge=20 point 85 of copper, brass or bronze generally along the = axis of the=20 chamber.   When the piston is generally extended, the = discharge point=20 is a substantial distance from the electrodes.   But when the = piston=20 is in its upper position (see Fig.11), the discharge point = is=20 positioned generally between all four electrodes and close to = them, there=20 being gaps between the electrodes and the discharge point.   = When the=20 piston is in this upper position, the electrodes extend somewhat = into the=20 semi-toroidal depression in the piston's upper surface and the = chamber is=20 generally toroidal in shape.   The volume of the chamber = shown in=20 Fig.11 can be from approximately 6.0 cubic inches (100 cc) = or=20 larger.   Given the present state of the art, 1500 cubic = inches=20 (25,000 cc) appears to be the upper limit.   A plurality of = ports=20 87 and one-way valves 89 return working fluid which = escapes=20 from the chamber back into it, so long as a sealing system such as = bellows=20 45 is used.


An=20 alternative cylinder head/piston arrangement is shown in = Fig.12.=20   The main difference between this arrangement and that of=20 Fig.5 is that the chamber walls, here labelled 43' = are=20 integrally formed with the head.   As a result seals = 57 are=20 carried by the piston rather than by the head, the attachment of = bellows=20 45 is somewhat different, and the fluid-returning valves = and ports=20 are part of the piston rather than of the head.   Otherwise = these=20 arrangements are substantially the same.   Preferably, the = cylinders=20 of both arrangements are hermetically sealed.


An=20 additional embodiment of a cylinder head/piston arrangement used = in the=20 present invention is shown in Fig.12A.   In this = arrangement,=20 a tapered sleeve 17C mates between cylinder head 17 = and=20 piston 39, a plurality of seals 57 are provided, and = electrodes 67 and 69 have a somewhat different = shape.  =20 Also, in this embodiment, a chamber 90 is provided in = cylinder head=20 17 for storing additional working fluid, i.e., the purpose = of=20 chamber 90 is to extend the operating time between = refuelling by=20 circulating the working fluid, viz. the mixture of inert gases = described,=20 between cylinder 41 and chamber 90 as needed so that = the=20 reactions in cylinder 41 are not adversely affected.   = To=20 accomplish this, this embodiment further includes a two-way = circulation=20 valve 90B, a relief valve 90C, and duct or = passageway=20 90D for evacuating and filling chamber 90, a duct or = passageway 90E for evacuating and filling cylinder = 41, a=20 passageway 90F between chamber 90 and cylinder = 41 in=20 which two-way valve 90B is disposed, a sensor 90G = and a=20 plurality of small pressure relief holes 90H.   Relief = holes=20 90H serve to relieve the pressure on bellows 45 as = the=20 piston moves from BDC to TDC.

In larger engines holes = 90H=20 should be replaced with one way valves.   Two-way valve = 90B is=20 either controlled by sensor 90G or is manually operated, as = desired, to allow the circulation of gases between chamber = 90 and=20 cylinder 41.   The sensor itself detects a condition = requiring=20 the opening or closing of valve 90B and signals that = condition to=20 the valve.   For example, sensor 90G can measure = pressure in=20 cylinder 41 while the piston is at top dead centre.   = A=20 predetermined cylinder pressure can cause a spring to compress, = causing=20 the valve to open or close as appropriate.   A subsequent = change in=20 the cylinder pressure would then cause another change in the = valve.  =20 Another sensor (not shown) could measure the physical location of = the=20 piston by a physical trip switch or an electric eye, or it could = measure=20 angular distance from top dead centre on the distributor or the=20 crankshaft.   The sensor must keep the gas pressure in = chamber=20 90 at one atmosphere, plus or minus 5%, and at top dead = centre,=20 cylinder 41 should also be at that pressure.   If gas = is lost=20 from the system, it is more important to maintain the proper = pressure in=20 cylinder 41.   Alternatively, a small passage between = cylinder=20 41 and chamber 90 could function in a passive manner = to=20 satisfactorily accomplish the same result.   From the above, = it can=20 be seen that this embodiment utilises the hollowed out centre of = the=20 cylinder head for storing additional working fluid, which fluid is = circulated between chamber 90 and cylinder 41 through a valve = system=20 comprising valve 90B and sensor 90G with the moving = piston=20 causing the gases to circulate.

The electrical circuitry = for=20 engine 11 includes (see Fig.13A) a 24 V battery = B1,=20 an ignition switch SW1, a starter switch SW2, = starter motor=20 37, a main circuit switch SW4, a step-down = transformer=20 93 (e.g., a 24 V to 3.5 V transformer), a switch SW6 = for=20 supplying power to ignition coil 25 (shown in = Fig.13A and=20 Fig.13B as two separate ignition coils 25A and = 25B),=20 and various decoupling diodes.


The=20 circuitry of Fig.13A also includes a high frequency voltage = source=20 or oscillator 95 for supplying rapidly varying voltage = through two=20 electronic current regulators 97A, 97B (see Fig.13B = for=20 regulator 97B) to the anode and cathode electrodes of each=20 cylinder, and a high-voltage distributor 99 for = distributing 40,000=20 volt pulses to the cylinders. Distributor 99 has two wipers = 99A and 99B and supplies three pulses to each = cylinder per=20 cycle.   Wipers 99A and 99B are 180 degrees out = of=20 phase with each other and each operates to supply pulses to its = respective=20 cylinder from TDC to 120 degrees thereafter.   More pulses = are=20 desirable and therefore a better distributor arrangement (shown in = Fig.14) may be used.   The arrangement shown in = Fig.14=20 includes two ignition coils 101, 103, a simple distributor=20 105 and a pair of magnetic ignition circuits 107 and = 109, described below.   Of course many other ignition = systems=20 could also be developed. For example, a single circuit might be = used in=20 place of circuits 107, 109, additional induction coils = might be=20 added to the ignition coils to assist in starting or a resistor = could be=20 added to the ignition coils to ensure a constant 40,000 volt = output=20 regardless of engine rpm.   Also, a solid-state distributor = could be=20 used instead of the mechanical distributor labelled 99.=20

Referring back to Fig.13A, for engines of more than = 1000 hp=20 a high frequency source 95 could be used to control engine = RPM.=20   The output frequency is controlled by a foot pedal similar = to an=20 accelerator pedal in a conventional vehicle.   The output = frequency=20 varies through a range of from approximately 2.057 MHz to = approximately=20 27.120 MHz with an output current of approximately 8.4 amps. =   The=20 speed of engine 11 is controlled by the output frequency of = source=20 95.   The high frequency current, as described below, = is=20 directed to each cylinder in turn by circuitry described below. =   For=20 engines producing from 300 to 1000 hp (not shown), a high = frequency source=20 having a constant output of 27.120 MHz with a constant current of = 3.4 amps=20 which is continually supplied to all cylinders could be used. =   In=20 this case an autotransformer, such as that sold under the trade=20 designation Variac by the General Radio Company, controlled by a = foot=20 pedal varies the voltage to each cylinder from 5 to 24 volts DC at = 4.5=20 amps, using power from the batteries or the alternator.   The = DC=20 current from the Variac is switched from cylinder to cylinder by = two small=20 electronic switching units which in turn are controlled by larger=20 electronic switching units.   For the smallest engines (not = shown), a=20 high frequency generator could supply a constant output of 27.120 = MHz with=20 a constant current of 4.2 amps to the cylinders during starting = only.=20   Speed control would be achieved by a Variac as described = above=20 which controls the DC voltage supplied to the cylinders in turn = within a=20 range of from 5 to 24 volts at a current of 5.2 amps.   In = this case,=20 once the engine is running, the full voltage needed to ignite the=20 (smaller) quantity of gases is obtained from the electrodes in the = other=20 cylinder of the pair.

The circuitry of Fig.13A also = includes the generator, a voltage regulator and relay 111, = five=20 electronic switching units 113, 115, 117, 119 and = 121,=20 electrodes 63 and 65 associated with chamber = 41A=20 (hereinafter chamber 41A is sometimes referred to as the = "A"=20 cylinder and chamber 41B is sometimes referred to as the = "B"=20 cylinder), anode 67, cathode 69, magnetic coils = 49A,=20 51A and 53A, capacitors C1A and C2A, = and=20 various decoupling diodes.   The electronic switching units = can take=20 a variety of forms.   For example, one simple form (see=20 Fig.15) includes a pair of SCRs 123 and 125. = The=20 switching unit is connected at terminal IN to the = corresponding=20 line on the input side and at terminal OUT to the = corresponding=20 line on the output side.   When a voltage of 3.5 volts is = supplied=20 from the battery through a distributor, for example, to the = ON=20 terminal, SCR 125 conducts, thereby completing a circuit = through=20 the switching unit.   Conversely, when 3.5 volts is applied = to the=20 OFF terminal, SCR 123 conducts and the circuit is = broken.=20   Likewise, the circuit for regulators 97A and = 97B (see=20 Fig.16) includes two SCRs 127 and 129 and a = PNP=20 transistor 131.   In this circuit when SCR 127 = is gated=20 on, it forces transistor 131 into conduction, thereby = completing=20 the circuit through the regulator.   When SCR 129 is = gated on,=20 the circuit through transistor 131 is broken.   A = number of=20 other configurations may be used in place of those of = Fig.15 and=20 Fig.16 and not all would use SCRs.   For example, one = triode=20 could be used to replace two main SCRs, or transistors could be = used=20 instead of SCRs.

A pair of low-voltage distributors = 135 and=20 137 are also shown in Fig.13A.   Distributors=20 135 and 137 provide gating pulses for the electronic = switching units of Fig.13A and Fig.13B.   Of = course,=20 solid-state distributors could also replace mechanical = distributors=20 135 and 137.

In addition, the engine = circuitry=20 includes (see Fig.13B) five electronic switching units = 143, 145,=20 147, 149 and 151 corresponding to units 113, 115, = 117,=20 119 and 121 of Fig.13A, electrodes 63 and = 65 of the "B" cylinder, anode 67, cathode = 69,=20 electric coils 49B, 51B and 53B, capacitors = C1B and=20 C2B, and various decoupling diodes.   The circuitry of = Fig.13B is generally the same as the corresponding portions = of=20 Fig.13A, so the description of one for the most part = applies to=20 both.   Of course, if more than two cylinders are used, each = pair of=20 cylinders would have associated with them, circuitry such as that = shown in=20 Fig.13A and Fig.13B.   The circuitry of = Fig.13A=20 is connected to that of Fig.13B by the lines L1- = L17.=20

The working fluid and the fuel for the engine are one and = the same=20 and consist of a mixture of inert gases, which mixture consists=20 essentially of helium, neon, argon, krypton and xenon.   It = is=20 preferred that the mixture contain 35.6% helium, 26.3% neon, 16.9% = argon,=20 12.7% krypton, and 8.5% xenon by volume, it having been calculated = that=20 this particular mixture gives the maximum operation time without=20 refuelling.   Generally, the initial mixture may contain, by = volume,=20 approximately 36% helium, approximately 26% neon, approximately = 17% argon,=20 approximately 13% krypton, and approximately 8% xenon.   This = mixture=20 results from a calculation that equalises the total charge for = each of the=20 gases used after compensating for the fact that one inert gas, = viz. radon,=20 is not used.   The foregoing is confirmed by a spectroscopic=20 flashing, described below, that occurs during the mixing process. =  =20 If one of the gases in the mixture has less than the prescribed=20 percentage, it will become over-excited.   Similarly, if one = of the=20 gases has more than the prescribed percentage, that gas will be=20 under-excited.   These percentages do not vary with the size = of the=20 cylinder.

Operation of the engine is as follows:   At = room=20 temperature, each cylinder is filled with a one atmosphere charge = of the=20 fuel mixture of approximately 6 cubic inches (100 cc) /cylinder = (in the=20 case of the smallest engine) by means of filler tube 59. =   The=20 filler tubes are then plugged and the cylinders are installed in = the=20 engine as shown in Fig.4, one piston being in the fully = extended=20 position and the other being in the fully retracted position. =   To=20 start the engine, the ignition and starter switches are closed, as = is=20 switch SW6.   This causes the starter motor to crank = the=20 engine, which in turn causes the wiper arms of the distributors to = rotate.=20   The starting process begins, for example, when the pistons = are in=20 the positions shown in Fig.4.   Ignition coil = 25 and=20 distributor 99 (see Fig.13A) generate a 40,000 volt = pulse=20 which is supplied to electrode 65 of chamber 41A. =  =20 Therefore, a momentary high potential exists between electrodes = 63=20 and 65 and the plates on each.   The discharge point = on piston=20 39A is adjacent these electrodes at this time and sparks = occur=20 between one or more of the electrodes and the discharge point to = partially=20 excite, e.g. ionise, the gaseous fuel mixture.

The gaseous = fuel=20 mixture in cylinder 41A is further excited by magnetic = fields set=20 up in the chamber by coil 49A.   This coil is = connected to the=20 output side of electronic switching unit 121 and, through = switching=20 unit 113, to the battery and the generator.   At this = time,=20 i.e., between approximately 5 degrees before TDC and TDC, = distributor=20 135 is supplying a gating signal to unit 121.   = Any=20 current present on the input side of unit 121, therefore, = passes=20 through unit 121 to energise coil 49A.   = Moreover, high=20 frequency current from oscillator 95 is supplied via = regulator=20 97A to coil 49A.   This current passes through=20 regulator and relay 97A because the gating signal supplied = from=20 distributor 135 to unit 121 is also supplied to = relay=20 97A.   The current from switching unit 121 and = from=20 oscillator 95 is also supplied to the anode and the = cathode. It is=20 calculated that this causes radioactive rays (x-rays) to flow = between the=20 anode and the cathode, thereby further exciting the gaseous = mixture.=20

As the starter motor continues cranking, piston 39A = begins=20 moving downward, piston 39B begins moving upward, and the wiper = arms of=20 the distributors rotate. (Needless to say, a solid-state = distributor would=20 not rotate.   The distributor could utilise photo cells, = either light=20 or reflected light, rather than contact points).   After 45 = degrees=20 of rotation, distributor 135 supplies a gating pulse to = electronic=20 switching unit 119, thereby completing a circuit through = unit=20 119.   The input to unit 119 is connected to = the same=20 lines that supply current to coil 49A.   The = completion of the=20 circuit through unit 119, therefore, causes coil 51A = to be=20 energised in the same manner as coil 49A.   After an=20 additional 45 degrees of rotation, distributor 135 gates on = electronic switching unit 117 which completes a circuit to = the same=20 lines.   The output terminal of unit 117 is connected = to coil=20 53A, and so this coil is energised when unit 117 is = gated=20 on. All three coils of the "A" cylinder remain energised = and,=20 therefore, generating magnetic fields in chamber 41A until = piston=20 39A reaches BDC.


As = piston=20 39A moves from TDC to BDC, two additional 40,000 volt = pulses (for a=20 total of three) are supplied from distributor 99 to the = "A"=20 cylinder. These pulses are spaced approximately 60 degrees apart. =  =20 If more pulses are desired, the apparatus shown in Fig.14 = may be=20 used. In that case, the solenoids indicated generally at 107A, = 107B=20 and 109A, 109B are energised to create a number of rapid,=20 high-voltage pulses which are supplied as indicated in = Fig.14 to=20 the cylinders, distributor 105 operating to supply pulses = to only=20 one of the pair of cylinders at a time.

As piston = 39A=20 reaches BDC, distributor 135 sends a pulse to the OFF = terminals of=20 electronic switching units 121, 117 and 119, = respectively,=20 causing all three coils 49A, 51A and 53A to = be=20 de-energised.   At about the same time, i.e., between = approximately 5=20 degrees before TDC and TDC for piston 39B, distributor = 137=20 supplies a gating pulse to the ON terminals of electronic = switching units=20 113 and 115. The power inputs to units 113 = and=20 115 come from the generator through regulator 111 = and from=20 the battery, and the outputs are directly connected to coils = 49A=20 and 53A.   Therefore, when units 113 and = 115 are=20 gated on, coils 49A and 53A are re-energised.   = But in=20 this part of the cycle, the coils are energised with the opposite=20 polarity, causing a reversal in the magnetic field in chamber = 41A.=20   Note that coil 51A is not energised at all during = this=20 portion of the cycle. Capacitors C1A and C2A are = also=20 charged during the BDC to TDC portion of the cycle. (During the = TDC to BDC=20 portion of the cycle, these capacitors are charged and/or = discharged by=20 the same currents as are supplied to the anode and cathode since = they are=20 directly connected to them).

As piston 39A moves = upwards,=20 electrodes 63 and 65 serve as pick-up points in = order to=20 conduct some of the current out of chamber 41A, this = current being=20 generated by the excited gases in the chamber.   This current = is=20 transferred via line L7 to electronic switching unit = 151.=20   The same gating pulse which gated on units 113 and=20 115 was also supplied from distributor 137 via line=20 L12 to gate on switching unit 151, so the current = from the=20 electrodes of chamber 41A passes through unit 151 to = the=20 anode, cathode and capacitors of chamber 41B, as well as = through=20 switching units 147 and 149 to coils 49B, 51B = and=20 53B.   Thus it can be seen that electricity generated = in one=20 cylinder during a portion of the cycle is transferred to the other = cylinder to assist in the excitation of the gaseous mixture in the = latter.=20   Note that this electricity is regulated to maintain a = constant=20 in-engine current. It should be noted, that twenty four volts from = the=20 generator is always present on electrodes 63 and 65 = during=20 operation to provide for pre-excitement of the gases.

From = the=20 above it can be seen that distributors 135 and 137 = in=20 conjunction with electronic switching units 113, 115, 117, 119, = 121,=20 143, 145, 147, 149 and 151 constitute the means for=20 individually energising coils 49A, 49B, 51A, 51B, 53A and=20 53B.   More particularly, they constitute the means to = energise all the coils of a given cylinder from the other cylinder = when=20 the first cylinder's piston is moving from TDC to BDC and operate = to=20 energise only two (i.e., less than all) of the coils from the = alternator=20 when that piston is moving from BDC to TDC.   Additionally, = these=20 components constitute the means for energising the coils with a = given=20 polarity when the piston of that cylinder is moving from TDC to = BDC and=20 for energising the first and third coils with the opposite = polarity when=20 that piston is moving from BDC to TDC.

As can also be = seen,=20 switching units 121 and 151 together with = distributors=20 135 and 137 constitute the means for closing a = circuit for=20 flow of current from chamber 41A to chamber 41B = during the=20 BDC to TDC portion of the cycle of chamber 41A and for = closing a=20 circuit for flow of current from chamber 41B to chamber = 41A=20 during the TDC to BDC portion of the cycle of chamber 41A. =  =20 Oscillator 95 constitutes the means for supplying a time = varying=20 electrical voltage to the electrodes of each cylinder, and = oscillator=20 95, distributors 135 and 137, and regulators=20 97A and 97B together constitute the means for = supplying the=20 time varying voltage during a predetermined portion of the cycle = of each=20 piston.   Moreover, distributor 99 together with = ignition=20 coils 25A and 25B constitute the means for supplying = high-voltage pulses to the cylinders at predetermined times during = the=20 cycle of each piston.

The cycle of piston 39B is = exactly=20 the same as that of piston 39A except for the 180 degree = phase=20 difference.   For each cylinder, it is calculated that the = excitation=20 as described above causes the gases to separate into layers, the = lowest=20 atomic weight gas in the mixture, namely helium, being disposed = generally=20 in the centre of each chamber, neon forming the next layer, and so = on=20 until we reach xenon which is in physical contact with the chamber = walls.=20   The input current (power) to do this is the calculated = potential of=20 the gas mixture.   Since helium is located in the centre of = the=20 chamber, the focal point of the electrode discharges and the = discharges=20 between the anode and cathode is in the helium layer when the = piston is=20 near TDC.   As the piston moves slightly below TDC, the = electrons=20 from electrodes 63 and 65 will no longer strike the = tip of=20 the piston, but rather will intersect in the centre of the = cylinder (this=20 is called "focal point electron and particle collision") as will = the=20 alpha, beta and gamma rays from the anode and cathode.   Of = course,=20 the helium is in this exact spot and is heavily ionised at that = time.=20   Thus the electrodes together with the source of electrical = power=20 connected thereto constitute the means for ionising the inert gas. =

It is calculated that as a result of all the = aforementioned=20 interactions, an ignition discharge occurs in which the helium = splits into=20 hydrogen in a volume not larger than 2 or 3 x 10-6 = cubic=20 millimetres at a temperature of approximately 100,000,000 degrees = F.=20   Of course this temperature is confined to a very small = space and=20 the layering of the gases insulates the cylinder walls from it. =  =20 Such heat excites the adjacent helium so that a plasma occurs. =  =20 Consequently, there is a minute fusion reaction in the helium = consisting=20 of the energy conversion of a single helium atom, which releases=20 sufficient energy to drive the piston in that chamber toward BDC = with a=20 force similar in magnitude to that generated in a cylinder of a=20 conventional internal combustion engine.   Electrodes = 63 and=20 65 extend into the argon layer while each piston is in its = BDC to=20 TDC stroke so as to pick up some of the current flowing in that = layer. It=20 may take a cycle or two for the gases in the cylinders to become=20 sufficiently excited for ignition to occur.

Once ignition = does=20 occur, the electrical operation of the engine continues as before, = without=20 the operation of the starter motor.   Distributor 99 = supplies=20 three pulses per cycle (or more if the magnetic ignition system of = Fig.14 is used) to each cylinder; and distributors = 135 and=20 137 continue to supply "on" and "off" gating pulses to the=20 electronic switching units.   The rpm of the engine is, as = explained=20 above, governed by the frequency of the current from oscillator = 95=20 (or in the case of smaller horsepower units, by the DC voltage = supplied to=20 the cylinders from the Variac).

Because of the minute = amount of=20 fuel consumed in each cycle, it is calculated that a cylinder can = run at=20 1200 rpm approximately 1000 hours, if not more, on a single charge = of gas.=20   Note that even at 1200 rpm, there will be intense heat = occurring=20 only 0.002% of the time.   This means that input power need = be=20 applied only sporadically.   This power can be supplied to a = cylinder=20 from the other cylinder of its pair by means of electronic = switching units=20 which, in the case of SCRs, are themselves triggered by low = voltage (e.g.=20 3.5 V) current.   Thus, since electrical power generated in = one=20 cylinder is used to excite the gases in the other cylinder of a = pair, it=20 is practical that the cylinders be paired as discussed above. =  =20 Capacitors are, of course, used to store such energy for use = during the=20 proper portion of the cycle of each cylinder.

From the = above, it=20 should be appreciated that the engine of this invention has = several=20 advantages over presently proposed fusion reactors, such as = smaller size,=20 lower energy requirements, etc.   But what are the bases of = these=20 advantages?   For one, presently proposed fusion reactors use = hydrogen and its isotopes as a fuel instead of inert gases.   = Presumably this is because hydrogen requires less excitement = power.  =20 While this is true, the input power that is required in order to = make=20 hydrogen reactors operate makes the excitation power almost = insignificant.=20   For example, to keep a hydrogen reactor from short = circuiting, the=20 hydrogen gas has to be separated from the reactor walls while it = is in the=20 plasma state. This separation is accomplished by the maintenance = of a near=20 vacuum in the reactor and by the concentration of the gas in the = centre of=20 the reactor (typically a toroid) by a continuous, intense magnetic = field.=20   Accordingly, separation requires a large amount of input = energy.=20

In the present invention, on the other hand, the greater=20 excitation energy of the fuel is more than compensated for by the = fact=20 that the input energy for operation can be minimised by = manipulation of=20 the unique characteristics of the inert gases.   First, = helium is the=20 inert gas used for fusion in the present invention.   The = helium is=20 primarily isolated from the walls of the container by the layering = of the=20 other inert gases, which layering is caused by the different = excitation=20 potential (because of the different atomic weights) of the = different inert=20 gases, said excitation being caused by the action of the = electrodes, anode=20 and cathode in a magnetic field.   This excitation causes the = gases=20 each to be excited in inverse proportion to their atomic numbers, = the=20 lighter gases being excited correspondingly more.   Helium,=20 therefore, forms the central core with the other four gases = forming=20 layers, in order, around the helium.   The helium is = secondarily=20 isolated from the walls of the container by a modest vacuum (in = comparison=20 to the vacuum in hydrogen reactors) which is caused partially by = the=20 "choking" effect of the coils and partially by the enlargement of = the=20 combustion chamber as the piston moves from TDC to BDC.   = (Unexcited,=20 the gases are at one atmosphere at TDC).   Second, argon, the = middle=20 gas of the five, is a good electrical conductor and becomes an = excellent=20 conductor when (as explained below) it is polarised during the = mixing=20 process.   By placing the electrodes such that they are in = the argon=20 layer, electrical energy can be tapped from one cylinder for use = in the=20 other.   During a piston's movement from BDC to TDC, the = gases are=20 caused to circulate in the cylinder by the change in the polarity = of the=20 coils, which occurs at BDC.

During such circulation, the = gases=20 remain layered, causing the argon atoms to be relatively close to = each=20 other, thereby optimising the conductivity of the argon.   = This=20 conductivity optimisation is further enhanced by a mild choking = effect=20 that is due to the magnetic fields.   The circulation of the = highly=20 conductive argon results in a continuous cutting of the magnetic = lines of=20 force so that the current flows through the electrodes.   = This=20 production of electricity is similar to the rotating copper wire = cutting=20 the magnetic lines of force in a conventional generator except = that the=20 rotating copper wire is replaced by the rotating, highly = conductive argon.=20   The amount of electricity that can be produced in this = manner is a=20 function of how many magnetic field lines are available to be cut. =  =20 If one of the coils, or all three of the coils or two adjacent = coils were=20 energised, there would be only one field with electricity produced = at each=20 end.   By energising the top and the bottom coil, two = separate fields=20 are produced, with electricity produced at four points.

A = five=20 coil system, if there were sufficient space, would produce three = fields=20 with the top, bottom and middle coils energised.   Six points = for=20 electricity production would result.   The number of coils = that can=20 be installed on a given cylinder is a function of space = limitations.=20   The recombination of gas atoms during the BDC to TDC phase = causes=20 the radiation of electrical energy which also provides a minor = portion of=20 the electricity that the electrode picks up.   Additional=20 non-grounded electrodes in each cylinder would result in more = electricity=20 being tapped off. It should be noted that during the BDC to TDC = phase, the=20 anode and the cathode are also in the argon layer and, like the=20 electrodes, they pick up electricity, which charges the capacitors = around=20 the cylinder.   Third, inert gases remain a mixture and do = not=20 combine because of the completeness of the electron shells.   = They=20 are therefore well suited to a cycle whereby they are continually=20 organised and reorganised.   Fourth, as the helium atoms are=20 consumed, the other gases have the capacity to absorb the charge = of the=20 consumed gas so that the total charge of the mixture remains the = same.=20

The second basis of these advantages of the present engine = over=20 proposed fusion reactors concerns the fact that hydrogen reactors = develop=20 heat which generates steam to turn turbines in order to generate=20 electrical power.   This requires tremendous input energy on = a=20 continuous basis.   The present invention operates on a = closed cycle,=20 utilising pistons and a crankshaft which does not require a = continuous=20 plasma but rather an infrequent, short duration (10-6 = second)=20 plasma that therefore requires much less input energy.   In = the=20 present invention, a plasma lasting longer than 10-6 = second is=20 not necessary because sufficient pressure is generated in that = time to=20 turn the engine.   A plasma of longer duration could damage = the=20 engine if the heat were sufficiently intense to be transmitted = through the=20 inert gas layers to the cylinder walls.   A similar heat = build-up in=20 the engine can occur if the repetition rate is increased.   = Such an=20 increase can be used to increase the horsepower per engine size = but at the=20 cost of adding a cooling system, using more expensive engine = components,=20 and increasing fuel consumption.   Note that even though = layers of=20 inert gases insulate the cylinder walls, there might be some = slight=20 increase in the temperature of the gas layers after a number of = cycles,=20 i.e., after a number of ignitions.

Whereas hydrogen fusion = reactors cannot directly produce power by driving a piston = (because of the=20 required vacuum), the present invention uses the layered inert = gases to=20 transmit the power from the plasma to each gas in turn until the = power is=20 applied to a piston, which can easily be translated into rotary = motion.=20   The layered gases also cushion the piston from the full = force of=20 the ignition.   Moreover, the fields inside the cylinder = undergoing=20 expansion cause the gases to shrink, thereby taking up some of the = pressure generated by the explosion and preventing rupturing of = the=20 cylinder walls.

Turning now to Fig.17A to Fig.17D, = there is=20 shown apparatus 201 for preparing the fuel mixture for = engine=20 11.   For convenience apparatus 201 is called a = mixer=20 although it should be understood that the apparatus not only mixes = the=20 gases which form the fuel but also performs many other vital = functions as=20 well.   The five constituent inert gases are introduced in = precise,=20 predetermined proportions.   The mixer extracts, filters and=20 neutralises the non-inert gases and other contaminants which may = be found=20 in the gas mixture.   It also increases the potential = capacity of gas=20 atoms, discharges the krypton and xenon gases, polarises the argon = gases,=20 ionises the gases in a manner such that the ionisation is = maintained until=20 the gas has been utilised and otherwise prepares them for use as a = fuel in=20 engine 11.   In particular, the mixer makes the gases = easier=20 to excite during operation of the engine.   Mixing does not = mean an=20 atomic or molecular combination or unification of gases because = inert=20 gases cannot chemically combine, in general, due to the = completeness of=20 the outer shell of electrons.   During mixing, the various = gases form=20 a homogeneous mixture.   The mixing of the five inert gases = in=20 apparatus 201 is somewhat analogous to preparing a five = part liquid=20 chemical mixture by titration.   In such a mixture, the = proportions=20 of the different chemicals are accurately determined by visually = observing=20 the end point of each reaction during titration.   In = apparatus=20 201, a visible, spectroscopic flash of light accompanies = the=20 desired end point of the introduction of each new gas as it = reaches its=20 proper, precalculated proportion.   (Each gas has its own=20 distinctive, characteristic, spectroscopic display).   The = ends=20 points are theoretically calculated and are determined by pre-set = voltages=20 on each of a group of ionising heads in the apparatus, as = described below.=20


Mixer=20 201 includes (see Fig.17A) an intake port, indicated = generally at 203, which during operation is connected to a = source=20 205 of helium gas, a gauge 206, glass tubing = 207=20 comprising a plurality of branches B10-B25 for flow of the = gases=20 through the mixer, a plurality of valves V1-V11 in the = branches,=20 which valves may be opened or closed as necessary, three gas = reservoirs=20 209, 211 and 213 for storing small quantities of = helium,=20 argon and neon gas respectively, an ionising and filtering unit = 215=20 for filtering undesired non-inert gases and contaminants out of = the fuel=20 mixture, for regulating the gas atom electron charge and to absorb = the=20 free flowing electrons, a gas flow circulation pump 217, = two=20 ionising heads 219 and 221, and three quality = control and=20 exhaust valves V12-V14.   The mixer also comprises = (see=20 Fig.17B) a high frequency discharge tube 225, a = non-directed=20 cathode ray tube 227, two more ionising heads 229 = and=20 231, two additional gas reservoirs 233 and = 235 for=20 storing small quantities of xenon and krypton, a quadruple = magnetic coil=20 237, a group of valves V15-V24, valves V23 = and=20 V24 being quality control and exhaust valves, and a = plurality of=20 additional glass tubing branches B26-B32.

Turning = to=20 Fig.17C, mixer 201 also includes additional ionising = heads=20 239, 240 and 241, additional valves V25-V46, = V39A and=20 V40A, valves V29 and V32 being quality = control and=20 exhaust valves and valve V39A being a check valve, a vacuum = and=20 pressure gauge 242 between valves V35 and = V36, tubing=20 branches B34-B49 (branch B39 consisting of two parts = B39A and B39B), a pair of intake ports 243 = and=20 245 which during operation are connected to sources = 247 and=20 249 of argon and neon gas respectively, gauges 250A = and=20 250B, a spark chamber 251, a hydrogen and oxygen = retention=20 chamber 253 containing No. 650 steel dust in a silk filter, = an ion=20 gauge 255 (which can be an RG 75K type Ion Gauge from Glass = Instruments, Inc. of Pasadena, Calif.) for removing excess inert = gases=20 from the mixture, inner and outer coils of glass tubing 257 = and=20 259 surrounding a mixing chamber 261, a focused = x-ray tube=20 263 for subjecting the mixture flowing through it to 15-20 = millirem=20 alpha radiation and 120-125 millirem beta radiation, a = directed=20 cathode ray tube 265, two twin parallel magnetic coils = 266=20 and 267, and a focusing magnetic coil 269.   It = is=20 important that coils 266 and 267 be immediately = adjacent=20 mixing chamber 261.   And (see Fig.17D) the = mixer also=20 comprises three more ionising heads 271, 273 and = 275, two=20 entry ports 277 and 279 which during operation are = connected=20 to sources 281 and 283 of krypton and xenon = respectively,=20 gauges 284A and 284B, a high frequency discharge = tube=20 285, a twin parallel magnetic coil 287 surrounding a = polariser 289 for polarising the argon, said polarise = containing=20 fine steel particles which are polarised by coils 287 and = which in=20 turn polarise argon, a second hydrogen retention chamber = 291, a=20 pair of tubing branches B50 and B51, two filters = 293=20 and 295 and a plurality of valves V47-V59, valves = V57=20 and V59 being quality control and exhaust valves. =

Inner and=20 outer glass tubing coils 257 and 259 and mixing = chamber=20 261 are shown in cross section in Fig.18.  =20 Intermediate glass coils 257 and 259 are two = magnetic coils=20 297 and 299 having an inductance of approximately = 130 mH.=20   A yoke coil 301 is positioned in a semi-circle = around mixing=20 chamber 261.   Inside mixing chamber 261 are = located a=20 pair of screens 303 and 305, insulators 307 = and=20 309, and a pair of spark gaps indicated generally at = 311 and=20 313.   A high frequency amplitude modulated source = 27,=20 provides 120 V AC, 60 Hz, 8.4 amp, 560 watt,120 to 40,000 MHz plus = or=20 minus 160 KHz current via heavily insulated wires 315 and=20 317 to the chamber.   These wires are about twelve = gauge, like=20 those used as spark plug wires on internal combustion engines. =  =20 Additionally 95 volt Direct Current is supplied via a smaller = (e.g.=20 sixteen to eighteen gauge) insulated wire 319.   As = described=20 below, the gases to be mixed and prepared flow through chamber = 261=20 and are suitably treated therein by the action of the various = fields=20 present in the chamber.

The magnetic coils, ionisation = heads, and=20 pump 217, along with the required electrical = interconnections, are=20 schematically shown in Fig.19A to Fig.19E.   More=20 particularly, heads 239 and 241 are shown in = Fig.19A,=20 as is pump 217.   Each ionising head has two = electrodes with a=20 gap between them to cause ionisation of gases flowing through the = head,=20 the electrodes being connected to a source of electrical power. =  =20 Pump 217 is directly connected to a source of power (either = AC or=20 DC as required by the particular pump being used).   The = connections=20 between the circuitry on Fig.19A and that on Fig.19B = are=20 shown as a plug 321, it being understood that this plug = represents=20 a suitable one-to-one connection between the lines of = Fig.19A and=20 those of Fig.19B.


The=20 remaining ionising heads and all the magnetic coils are shown in=20 Fig.19B.   For clarity, the coils are shown in an=20 unconventional form.   Quadruple coil 237 (shown at = the top of=20 Fig.19B) has one side of each winding connected in common = but the=20 other sides are connected to different lines.   Coil = 223=20 consists of two windings in parallel.   Coils 297 and=20 299, the ones around the mixing chamber, are shown = overlapping, it=20 being understood that coil 297 is actually interior of coil = 299.   Yoke coil 301, as shown, extends = half-way from=20 the bottom to the top of coils 297 and 299.   = Twin=20 parallel magnetic coils 267 are connected in parallel with = each=20 other, both sides of focusing coil 269 being connected to = one node=20 of coils 267.   Likewise coils 287 are = connected in=20 parallel.   The connections between the lines of = Fig.19B and=20 those of Fig.19C and Fig.19D are shown as plugs = 323=20 and 325, although other suitable one-to-one connections = could=20 certainly be made.   Fig.19C shows the interconnecting = lines=20 between Fig.19B and Fig.19E.   A plug = 327 or=20 other suitable one-to-one connections connects the lines of = Fig.19C=20 and Fig.19E.

A plurality of power sources, like the = above-mentioned Variacs, of suitable voltages and currents as well = as a=20 plurality of relays 329, and plugs 331 are shown on=20 Fig.19D and Fig.19E.   The connections between = these=20 two Figures is shown as a plug 333.   It should be = appreciated=20 that the Variacs can be adjusted by the operator as necessary to = supply=20 the desired voltages to the aforementioned coils and ionising = heads.=20   It should also be realised that the desired relays can be = closed or=20 opened as needed by connecting or disconnecting the two parts of = the=20 corresponding plug 331.   That is, by use of plugs = 331,=20 the operator can control the energising of the ionising heads and = magnetic=20 coils as desired.   Plugs 331 are also an aid in = checking to=20 ensure that each component is in operating condition just prior to = its=20 use.   Of course, the manipulation of the power sources and = the=20 relays need not be performed manually; it could be automated. =

The=20 remaining circuitry for the mixer is shown on Fig.20A to=20 Fig.20F.   For convenience, plugs 335, 337, 339, = 341, 343,=20 345 and 347 are shown as connecting the circuitry shown = in the=20 various Figures, although other suitable one-to-one connections = may be=20 used.   The chassis of the apparatus is shown on these = Figures in=20 phantom and is grounded.   The power supply for the apparatus = is=20 shown in part on Fig.20A and Fig.20D and includes an = input=20 349 (see Fig.20D) which is connected to 120 volt, 60 = Hz=20 power during operation and an input 351 which is connected = to the=20 aforementioned high frequency generator or some other suitable = source of=20 approximately 27,120 MHz current.   The power supply includes = a pair=20 of tuners 353, numerous RLC circuits, a triode 355, = a=20 pentode 357 with a ZnS screen, a variable transformer = 359,=20 an input control 361, a second variable transformer = 363 (see=20 Fig.20A) which together with a filter 365 forms a = 2.0 volts=20 (peak-to-peak) power supply 367, a pentode 369, a = variable=20 transformer 371, and a resistor network indicated generally = at=20 373.   Exemplary voltages in the power supply during = operation=20 are as follows:   The anode of triode 355 is at 145 V, = the=20 control grid at 135 V and the cathode at -25 V.   The voltage = at the=20 top of the right-hand winding of transformer 359 is -5 V. =  =20 The anode of pentode 357 is at 143 V, the top grid is = grounded (as=20 is the ZnS screen), the bottom grid is connected to transformer=20 359, and the control electrode is at 143 V.   The = input to=20 supply 367 is 143 volts AC while its output, as stated = above, is 2=20 V (peak-to-peak).   The anode of pentode 369 is at 60 = V, the=20 grids at -1.5 V, the control electrode at 130 V, and the cathode = is=20 substantially at ground.   The output of resistor network = 373,=20 labelled 375, is at 45 V.


Also = shown=20 on Fig.20D is spark chamber 251.   Spark = chamber=20 251 includes a small amount of thorium, indicated at = 377,=20 and a plurality of parallel brass plates 379.   When = the gases=20 in the mixer reach the proper ionisation, the alpha particles = emitted by=20 the thorium shown up as flashes of light in the spark chamber.=20

Turning now to Fig.20B, ionising and filtering unit = 215 includes a pair of conductive supports 381 for a = plurality of conductors 383, said supports and conductors = being=20 connected to a voltage source, an insulating support 385 = for=20 additional conductors 387, and a ZnS screen 388 = which emits=20 light when impurities are removed from the gaseous fuel mixture. =  =20 Unit 215 also includes a second set of interleaved = conductors=20 indicated generally at 389, a cold-cathode tube 391, = and an=20 x-ray tube indicated generally at 393.   Also shown on = Fig.20B is an RLC network 395 which has an output on = a line=20 397 which is at 35 V, this voltage being supplied to the = x-ray=20 tube.

High frequency discharge tube 255 (see=20 Fig.20C) has a conductive electrode 399 at one end = to which=20 high frequency current is applied to excite the gases in the = mixer, and an=20 electrode/heater arrangement 401 at the other, a voltage of = 45 V=20 being applied to an input 402 of the tube.   It is = desirable=20 that a small quantity of mercury, indicated at 403, be = included in=20 tube 225 to promote discharge of the helium gas.   = Magnetic=20 coils 237 have disposed therein a pair of generally = parallel=20 conductors 405 to which a high frequency signal is applied. =  =20 When gas flows through coils 237 and between parallel = conductors=20 405, therefore, it is subjected to the combination of a DC = magnetic=20 field from the coil and high frequency waves from the conductors, = which=20 conductors act as transmitting antennas.   The resulting high = frequency magnetic field causes the atoms to become unstable, = which allows=20 the engine to change a given atom's quantum level with much less = input=20 power than would normally be required.   The volume of each = gas atom=20 will also be smaller.   Also shown on Fig.20C is = non-directed=20 cathode ray tube 227.   The grids of tube 227 = are at=20 145 V, the control electrode is at ground, while the anode is at = 35 V to=20 80 V (peak-to-peak).   The purpose of non-directed cathode = ray tube=20 227 is to add photons to the gas mixture.   To = generate these=20 photons, tube 227 has a two layer ZnS coating indicated = generally=20 at 407.   Chamber 261, described above, is also = shown=20 schematically on Fig.20C, along with an RLC network = 409.=20

The power supply for the mixer (see the lower halves of=20 Fig.20E and Fig.20F) also includes two pentodes = 411=20 and 413, a transformer 415, and a diode tube = 417.=20   The control electrode of pentode 411 is at 5 V to 40 = V=20 (peak-to-peak), the grids are at 145 V, the anode is at 100 V, and = the=20 cathode is at 8 V to 30 V (peak-to-peak).   The control = electrode of=20 pentode 413 is at 115 V, while its grids and cathode are at = -33 V.=20   The anode of tube 413 is connected to transformer=20 415.   Also shown on Fig.20E are a relay = 419=20 associated with ion gauge 255, and focused x-ray tube = 263=20 associated with ionisation head 240.   The upper input = to tube=20 263 is at 45 V to 80 V (peak-to-peak).

Turning to=20 Fig.20F, there is shown tubes 265 and 285. =  =20 Directed cathode ray tube 265 is a pentode connected like = tube=20 227.   High frequency discharge tube 285 = includes a=20 phosphor screen and is connected to a high frequency source. =   Also=20 shown on Fig.20F is a triode 421 with its anode at = 30 V, its=20 cathode at ground, and its control grid at -60 V; a pentode = 423=20 with its anode at 135 V to 1000 V peak to peak, its cathode at = ground, its=20 control electrode at 143 V, its grids at 20 V; and a transformer=20 425.   It should be understood that various = arrangements of=20 electrical components other than those described above could be = designed=20 to perform the same functions.

The operation of the mixer = is best=20 understood with reference to Fig.17A to Fig.17D and = is as=20 follows:   Before and during operation, the mixer, and = particularly=20 chamber 261 is kept hermetically sealed and evacuated. =   To=20 begin the mixing process, helium is admitted into the mixer via = intake=20 port 203.   Then a vacuum is again drawn, by a vacuum = pump=20 (not shown) connected to valve V38, to flush the chamber. =  =20 This flushing is repeated several times to completely cleanse the = tubing=20 branches of the mixer.   The mixer is now ready.   The=20 ionisation heads next to mixing chamber 261 are connected = to a=20 voltage corresponding to approximately 36% of the calculated total = ionising voltage, DC current is allowed to flow through magnetic = coils=20 297 and 299 around chamber 261, and high = frequency=20 current is allowed to pass through the mixing chamber.   = Helium is=20 then slowly admitted, via port 203, into the mixer.   = From=20 port 203, the helium passes through ionisation head = 219 into=20 glass tubing coil 259.   This glass coil, being = outside=20 magnetic coils 297 and 299, is in the diverging = portion of a=20 magnetic field.   The helium slowly flowing through glass = coil=20 259 is gently excited.   From coil 259, the = helium=20 flows through branch B45 to ionisation head 275 and = from=20 there, via branch B28, to ionisation head 229 (see=20 Fig.17B).   From head 229, the gas flows = through=20 non-directed cathode ray tube 227 to high-frequency = discharger=20 225.   The high frequency discharger 225, with = heating=20 element, discharges, separates or completely neutralises the = charge of any=20 radioactive and/or cosmic particles that are in the helium atom in = addition to the protons, neutrons and electrons.

The gas = exits=20 discharger 225 via branch B26 and passes to = high-frequency=20 discharger 285.   The high frequency discharger = 285,=20 without heating element, disturbs the frequency of oscillation = which binds=20 the gas atoms together.   This prepares the helium atoms so = that the=20 electrons can more easily be split from the nucleus during the = excitation=20 and ignition process in the engine.   Discharger 285 = includes=20 a phosphorus screen or deposit (similar to the coating on a = cathode ray=20 tube) which makes discharges in the tube visible.   From = discharger=20 285, the helium passes through directed cathode ray tube = 265=20 and focused x-ray tube 263.   Directed cathode ray = tube=20 265 produces cathode rays which oscillate back and forth=20 longitudinally underneath and along the gas carrying tube.   = After=20 that, the helium passes successively through branch B21, = ionisation=20 head 221, branch B23, twin parallel magnetic coil=20 266, and branch B25 into mixing chamber 261. =  =20 Helium flows slowly into and through apparatus 201.   = The=20 helium atoms become ionised as a result of excitation by magnetic = force,=20 high frequency vibrations and charge acquired from the ionisation = heads.=20   When sufficient helium has entered the apparatus, the = ionisation=20 energy (which is approximately 36% of the total) is totally = absorbed.=20   A spectroscopic flash of light in the mixing chamber = signals that=20 the precise, proper quantity of helium has been allowed to enter. =  =20 The entry of helium is then immediately halted by the closing of = valve=20 V3.

The next step in preparing the fuel is to add = neon to=20 the mixture.   The potential on the relevant ionisation = heads,=20 particularly head 241 (see Fig.17C), is raised by = the=20 addition of approximately 26% which results in a total of = approximately=20 62% of the total calculated potential and valve V31 is = opened,=20 thereby allowing neon to slowly enter the mixer via port = 245.=20   This gas passes through branch B36, ionisation head=20 241, and branch B35 directly into the mixing = chamber.  =20 Since the previously admitted helium is fully charged, the neon = absorbs=20 all of the increased ionisation potential.   As soon as the = neon=20 acquires the additional charge, a spectroscopic flash of light = occurs and=20 the operator closes valve V31.

In the same manner, = the=20 potential on the ionisation heads is increased by the addition of=20 approximately 17% for a total of approximately 79% of the total = calculated=20 potential and then valve V30 is opened to admit argon into = the=20 mixer via port 243.   This gas passes through branch=20 B34, ionisation head 239, and branch B33 into = mixing=20 chamber 261.   Again, when the proper amount of argon = has been=20 admitted, it emits a spectroscopic flash of light and the operator = closes=20 valve V30.   Next, the potential on the ionisation = heads is=20 increased by the addition of approximately 13% to result in a = total of=20 approximately 92% of the total calculated potential and valve = V58=20 (see Fig.17D) is opened to admit krypton into the system. =  =20 The krypton gas passes through branch B51, ionisation head=20 271 and branch B48 into chamber 261.   = Upon the=20 emission of a spectroscopic flash of light by the gas, the = operator closes=20 valve V58.   Finally, the potential on the ionisation = heads is=20 increased by the addition of approximately 8% which brings the = ionisation=20 potential to the full 100% of the calculated ionisation voltage = and valve=20 V56 is opened to admit xenon into the mixer via port = 279.=20   This gas passes through branch B50, ionisation head=20 273 and branch B47 to the mixing chamber.   = When the=20 proper amount of gas has been admitted, a spectroscopic flash of = light=20 occurs signalling the operator to close valve V56.   = Note that=20 there are two filter/absorber units, labelled 253 and = 291.=20     Unit 253 is connected to the neon and argon = inlet=20 branches B33 and B35 while unit 291 is = connected to=20 the krypton and xenon inlet branches B47 and B48. =  =20 These two units absorb hydrogen residue and immobilise the water = vapour=20 created when the pump circulates the gases and generates vacuum = states.=20

After all the gases are admitted in the desired = proportions, all=20 the valves are closed.   (The mixture in the mixing chamber = and in=20 the adjacent tubing is at one atmosphere pressure at this time). =  =20 Once this is done, the interval valves of the system are all = opened (but=20 the inlet and outlet valves remain closed) to allow the mixture to = circulate throughout the tubing as follows: branch B44, = magnetic=20 coils 267 and 269, ionisation head 240, = branch=20 B29, ionisation head 231, branch B24, = ionisation head=20 219, pump 217, branches B15 and B39A,=20 ionisation gauge 255, branches B38 and B42,=20 ionisation head 275, branch B28, ionisation head = 229,=20 non-directed cathode ray tube 227, quadruple magnetic coil=20 272, ionisation head 221, branch B23, twin = parallel=20 magnetic coil 266, branch B25 and mixing chamber = 261.=20   When this circuit is initially opened, the pressure of the = mixture=20 drops 40-50% because some of the tubing had previously been under = vacuum.=20   Pump 217 is then started to cause the gases to be = slowly and=20 evenly mixed.

Because of dead space in the tubing and the = reaction=20 time of the operator, it may occur that the proportions of the = gases are=20 not exactly those set forth above.   This is remedied during = the=20 circulation step.   As the gas flows through ionisation gauge = 255, excess gas is removed from the mixture so that the = correct=20 proportions are obtained.   To do this the grid of gauge = 255=20 is subjected to 100% ionisation energy and is heated to = approximately 165=20 degrees F.   This temperature of 165 degrees F is related to = xenon's=20 boiling point of -165 degrees F in magnitude but is opposite in = sign.=20   Xenon is the heaviest of the five inert gases in the = mixture.=20   As the gas mixture flows through ionisation gauge = 255, the=20 gas atoms that are in excess of their prescribed percentages are = burned=20 out of the mixture and their charge is acquired by the remaining = gas atoms=20 from the grid of the ionisation gauge.   Because the gases = are under=20 a partial vacuum, the ionisation gauge is able to adjust the gas=20 percentages very precisely.   (Note: The steps described in = the last=20 two paragraphs are repeated if the finished gases are rejected in = the=20 final quality control step described below).

The next step = involves purifying the mixture so that only the five inert gases = remain,=20 absorbing any free electrons and regulating the electrical charge = in the=20 mixture.   To do this, the circuit consisting of the = following=20 components is opened:   Branch B44, magnetic coil = 267,=20 magnetic coil 269, ionisation head 240, branch = B29,=20 ionisation head 231, branch B24, ionisation head = 219,=20 pump 217, branches B15 and B39, magnetic coil = 287 (see Fig.17D) polariser 289, branch = B17,=20 ionising and filtering unit 215, branches B16, B42, = and=20 B41, x-ray tube 263, branch B21, ionisation = head=20 221, branch B23, magnetic coil 266, branch=20 B25, and mixing chamber 261.   The gases should = complete this circuit at least three times.

The last step = required=20 to prepare the mixture for bottling is polarisation of the argon. =  =20 The circuit required to do this consists of the following = components:=20 mixing chamber 261, branch B44, magnetic coil = 267,=20 magnetic coil 269, ionisation head 240, cathode ray = tube=20 265, branch B40, tubing coil 257, branches = B49=20 and B30, ionisation head 231, branch B24, = ionisation=20 head 219, pump 217, branches B15 and = B39, twin=20 parallel magnetic coil 287 (see Fig.17D), polariser=20 289, branch B17, ionising and filtering unit = 215,=20 branches B16, B42 and B20, ionisation head = 229,=20 cathode ray tube 227, magnetic coil 237, ionisation = head=20 221, branch B23 and magnetic coil 266.   = This=20 too is repeated at least three times.   The key to the = polarisation=20 of argon is polariser 289 and twin parallel magnetic coil=20 287 that encircles it.   Polariser 289 is a = glass=20 bottle which is filled with finely powdered soft iron which can be = easily=20 magnetised.   The filled bottle is, in effect, the iron core = of the=20 coils.   The iron particles align themselves with the = magnetic lines=20 of force, which lines radiate from the centre toward the north and = south=20 poles.   The ionised gas mixture is forced through the = magnetised=20 iron powder by means of pump pressure and vacuum, thereby = polarising the=20 argon gas.   Filters 293 and 295 are disposed = as shown=20 in order to filter metallic particles out of the gas.

The = mixture=20 is now double-checked by means of spark chamber 251 at = atmospheric=20 pressure since the fusion reaction in the engine is started at one = atmosphere.   Because the gases in mixing apparatus = 201 are at=20 a partial vacuum, sufficient gases must be pumped into spark = chamber=20 251 to attain atmospheric pressure.   To do this = valves=20 V33, V36 and V40A are closed and circulating pump = 217=20 pumps the gases in the mixing apparatus via branches B15 = and=20 B39A, through check valve V39A into spark chamber = 251=20 until the vacuum and pressure gauge 242 indicates that the = gases=20 within spark chamber 251 are at atmospheric pressure. =   Valve=20 V34 is then closed.   The spark chamber is similar to = a cloud=20 chamber.   Six or more high capacity brass capacitor plates = are=20 spaced 1/8" to 1/4" apart in the chamber.   A small plastic = container=20 holds the thorium 232.   One side of the chamber is = equipped=20 with a thick glass window through which sparks in the chamber may = be=20 observed.   A potential is placed on the brass plates in the = chamber=20 and the current flowing between the plates is measured.   If = this=20 current exactly corresponds to the ionisation current, the mixture = is=20 acceptable.   A difference of greater than 5% is not = acceptable.=20   A lesser difference can be corrected by recirculating the = gas in=20 the mixer and particularly through ionisation gauge 255 as=20 previously described in the circulation step.   A second test = is then=20 given the gases that pass the first test.   A calculated high = frequency current is gradually imposed on the spark chamber = capacitor=20 plates.   This excitation causes neutrons to be emitted from = the=20 thorium 232 which, if the mixture is satisfactory, can be = easily=20 seen as a thin thread of light in the chamber.   If the = mixture is=20 not satisfactory, light discharges cannot be seen and the high = frequency=20 circuit will short out and turn off before the desired frequency = is=20 reached.

To bottle the mixture, valve V33 is opened = and=20 valves V36 and V40 are closed.   During = bottling,=20 polariser 289, twin parallel magnetic coil 287, = ionisation=20 unit 215 and ion gauge 255 are electrically = energised (all=20 electrical circuits are previously de-energised) to improve the = stability=20 of the mixture.   The prepared gases are withdrawn from the = mixing=20 apparatus via branches B24 and B16, ionisation unit=20 215, branch B17, filters 293 and 295,=20 polariser 289, twin parallel magnetic coil 287, = branch=20 B39, ion gauge 255, check valve V39A, branch=20 B38 and spark chamber 251.   If desired, after = bottling=20 the mixer may be exhausted by opening valves V12, V13, V14, = V23, V24,=20 V29, V32, V57 and V59.   Of course, one can also = automate=20 the fuel preparation process to be continuous so that it would = never be=20 necessary to exhaust the gas.

In operation of mixing = apparatus=20 201, certain operational factors must be considered.   = For=20 one, no electrical devices can be on without the pump being in = operation=20 because an electrical device that is on can damage adjacent gas = that is=20 not circulating.   For another, it should be noted that = directed=20 cathode ray tube 265, non-directed cathode ray tube = 227 and=20 focused x-ray tube 263 serve different functions at = different=20 points in the mixing process.   In one mode, they provide hot = cathode=20 radiation, which can occur only in a vacuum.   When gases are = flowing=20 through these devices, they provide a cold cathode discharge. =   For=20 example, during argon polarisation and the circulation step, = focused x-ray=20 tube 263 is under vacuum and affects the gases flowing = through=20 ionisation head 240 by way of hot cathode radiation.   = During=20 the introduction of the different gases into mixing apparatus = 201=20 and during the recirculation step, the gases are flowing through = focused=20 x-ray tube 263, which affects the gases by way of a cold = cathode=20 discharge.

It is preferred that each switchable electrical = component in mixing apparatus 201 be wired into a separate = circuit=20 despite the fact that one of the poles of each could be commonly = wired.=20   In a common ground circuit if one device is turned on, all = of the=20 other units may also turn on because the gases in the device are=20 conductive. In addition, if one unit on a common circuit were = energised=20 with high frequency current, the others would also be affected. In = the=20 same vein, the high frequency current cannot be used when the = cathode ray=20 tubes, the x-ray tubes or the dischargers are heated and under = vacuum=20 because the heater filaments will burn out.

Finally, the = current=20 source, the variable rectifiers and the electrical measuring = instruments=20 must be located more than ten feet from mixing apparatus = 201=20 because the high frequency current is harmful to the rectifiers, = causing=20 them to burn out or short out.

It is hoped that a brief = summary of=20 the concepts used by the inventor in developing the above = invention will=20 be helpful to the reader, it being understood that this summary is = in no=20 way intended to limit the claims which follow or to affect their = validity.=20   The first concept is that of using an inert gas mixture at=20 approximately one atmosphere at TDC (at ignition) as a fuel in a=20 thermonuclear energy production process.   The second concept = is the=20 layering of the various inert gases, which layering is designed to = confine=20 the input energy in the innermost layers during pre-excitement and = ignition, to provide thermal insulation for the container walls = during and=20 after ignition, to transmit power resulting from the ignition = through the=20 layers in turn to the piston, to absorb the pressure generated = during=20 ignition to protect the cylinder walls, and to provide an orderly, = predictable positioning of the argon layer during the BDC to TDC = portion=20 of the engine cycle.   The third concept of this invention = involves=20 utilising electric current produced in one cylinder of a pair to = perform=20 functions in the other cylinder of that pair.   This concept = includes=20 the sub-concepts of generating electric current by atomic = recombination=20 and of electric generation in place resulting from the rotation of = layered=20 inert gases within each cylinder because of the changed polarity = of the=20 encircling coils at BDC, from judicious placement of coils which = produce=20 magnetic field lines which are cut by a near perfect conductor = (polarised=20 argon), and from movement of said near perfect conductor through = the=20 magnetic field.

The fourth and fifth concepts of this = invention=20 are the transformation of rapid, intense, but short duration = thermonuclear=20 reactions into pressure that is transmitted from inert gas to = inert gas=20 until it creates linear kinetic energy at the piston, which energy = is=20 converted into rotary kinetic energy by a crankshaft, and the use = of a=20 shaft-driven generator to provide power to spaced field coils = during the=20 BDC to TDC portion of the cycle of each cylinder.

The = sixth=20 concept concerns adequate pre-excitement of the inert gas fuel and = more=20 particularly involves the sub-concepts of pre-exciting the fuel in = the=20 mixing process, of manipulation of the currents in the coils = surrounding=20 each cylinder, of discharging the capacitors surrounding each = cylinder at=20 predetermined times in the cycles, of causing a stream of = electrical=20 particles to flow between electrodes and a conductive discharge = point on=20 the piston, of emitting alpha, beta and gamma rays from an anode = and a=20 cathode containing low level radioactive material to the piston's=20 discharge point, of accelerating the alpha, beta and gamma rays by = the=20 application of a high-voltage field, and of situating capacitor = plates 90=20 degrees from the anode and cathode to slow and reflect neutrons = generated=20 during ignition.   The seventh concept involves the provision = of a=20 minute, pellet-type fission ignition, the heat from which causes a = minute=20 fusion as the result of the ignition chamber shape and = arrangement, as a=20 result of the collision of the alpha, beta and gamma rays and the=20 electrical particles at a focal point in conjunction with the = discharge of=20 the capacitors that surround the cylinder through the electrodes, = and as a=20 result of increasing the magnetic field in the direction of the = movement=20 of each piston.


The Robert = Britt=20 Engine.
Robert Britt designed a = very similar=20 engine to that of Josef Papp, and he was also awarded a US patent = for an=20 engine operating on inert gasses.   William Lyne remarks that = this=20 engine design may be replicated using a Chevy =93Monza=94 = 6-cylinder engine or=20 a VolksWagen 4-cylinder engine.   The heads are removed and = the new=20 heads cast using the =93pot metal=94 used for =93pseudo chrome=94 = automotive trim.=20   That alloy contains aluminium, tin, zinc and possibly = antimony and=20 is particularly suitable as the insides of the cavities can be = polished to=20 the high reflectivity specified in the patents.


  US Patent 3,977,191  =
                  31st August 1976                      Inventor: Robert =
G. Britt

ATOMIC=20 EXPANSION REFLEX OPTICS POWER SOURCE (AEROPS) ENGINE=20


ABSTRACT
An engine is = provided which=20 will greatly reduce atmospheric pollution and noise by providing a = sealed=20 system engine power source which has no exhaust nor intake ports. =  =20 The engine includes a spherical hollow pressure chamber which is = provided=20 with a reflecting mirror surface.   A noble gas mixture = within the=20 chamber is energised by electrodes and work is derived from the = expansion=20 of the gas mixture against a piston.


SUMMARY OF = THE=20 INVENTION
An atomic expansion reflex optics power = source=20 (AEROPS) engine, having a central crankshaft surrounded by a = crankcase.=20   The crankcase has a number of cylinders and a number of = pistons=20 located within the cylinders.  The pistons are connected to = the=20 crankshaft by a number of connecting rods.   As the = crankshaft turns,=20 the pistons move in a reciprocating motion within the cylinders. =   An=20 assembly consisting of a number of hollow spherical pressure = chambers,=20 having a number of electrodes and hollow tubes, with air-cooling = fins, is=20 mounted on the top of each cylinder.   The necessary gaskets = are=20 provided as needed to seal the complete engine assemblies from = atmospheric=20 pressure.   A means is provided to charge the hollow = spherical=20 pressure chamber assembly and the engine crankcase with noble gas = mixtures=20 through a series of valves and tubes.   A source of = medium-voltage=20 pulses is applied to two of the electrodes extending into each of = the=20 hollow spherical pressure chambers.

When a source of = high-voltage=20 pulses is applied from an electrical rotary distributor switch to = other=20 electrodes extending into each of the hollow spherical pressure = chambers=20 in a continuous firing order, electrical discharges take place=20 periodically in the various hollow spherical pressure chambers. =  =20 When the electrical discharges take place, high energy photons are = released on many different electromagnetic frequencies.   The = photons=20 strike the atoms of the various mixed gases, e.g., xenon, krypton, = helium=20 and mercury, at different electromagnetic frequencies to which = each is=20 selectively sensitive, and the atoms become excited.   The = first=20 photons emitted are reflected back into the mass of excited atoms = by a=20 reflecting mirror surface on the inside wall of any particular = hollow=20 spherical pressure chamber, and this triggers more photons to be = released=20 by these atoms.   They are reflected likewise and strike = other atoms=20 into excitation and photon energy release.   The electrons = orbiting=20 around the protons of each excited atom in any hollow spherical = pressure=20 chamber increase in speed and expand outward from centre via = centrifugal=20 force causing the atoms to enlarge in size.   Consequently, a = pressure wave is developed, the gases expand and the pressure of = the gas=20 increases.

As the gases expand, the increased pressure is = applied=20 to the top of the pistons in the various cylinders fired = selectively by=20 the electrical distributor.   The force periodically applied = to the=20 pistons is transmitted to the connecting rods which turn the = crankshaft to=20 produce rotary power.   Throttle control valves and = connecting tubes=20 form a bypass between opposing hollow spherical pressure chambers = of each=20 engine section thereby providing a means of controlling engine = speed and=20 power.   The means whereby the excited atoms are returned to = normal=20 minimum energy ground-state and minimum pressure level, is = provided by=20 disrupting the electrical discharge between the medium-voltage = electrodes,=20 by cooling the atoms as they pass through a heat transfer = assembly, and by=20 the increase in the volume area above the pistons at the bottom of = their=20 power stroke.   The AEROPS engine as described above provides = a=20 sealed unit power source which has no atmospheric air intake nor = exhaust=20 emission.   The AEROPS engine is therefore pollution free.=20


BRIEF OBJECTIVE OF THE INVENTION
This = invention relates to the development of an atomic expansion reflex = optics=20 power source (AEROPS) engine, having the advantages of greater = safety,=20 economy and efficiency over those disclosed in the prior art. =   The=20 principal object of this invention is to provide a new engine = power=20 technology which will greatly reduce atmospheric pollution and = noise, by=20 providing a sealed system engine power source which has no exhaust = nor=20 intake ports.

Engine power is provided by expanding the = atoms of=20 various noble gas mixtures.   The pressure of the gases = increases=20 periodically to drive the pistons and crankshaft in the engine to = produce=20 safe rotary power.   The objects and other advantages of this = invention will become better understood to those skilled in the = art when=20 viewed in light of the accompanying drawings. =


BRIEF=20 DESCRIPTION OF THE DRAWINGS
Fig.1 is an = elevational view=20 of the hollow spherical pressure chamber assembly, including = sources of=20 gas mixtures and electrical supply:




=
Fig.2=20 is an elevational view of the primary engine power stroke: =




=
Fig.3=20 is an elevational view of the primary engine compression stroke:=20





=
Fig.4=20 is a rear elevational view of a six cylinder AEROPS engine: =




=
Fig.5=20 is a top view of the six cylinder AEROPS engine:




= Fig.6=20 is an electrical schematic of the source of medium-voltage: =




= Fig.7=20 is an electrical schematic of the source of high-voltage:




= DETAILED=20 DESCRIPTION



Refe= rring=20 to Fig.1 of the drawings, the AEROPS engine comprises a = hollow=20 spherical pressure chamber 1 having an insulated = high-voltage=20 electrode 2 mounted on the top, an insulated medium-voltage = electrode 3 mounted on the right, and an insulated common = ground=20 electrode 4 mounted on the left, as shown in this = particular view.=20   Electrodes 2, 3 and 4 extend through the wall = of the=20 hollow spherical pressure chamber 1 and each electrode = forms a=20 pressure seal.   A plurality of hollow tubes 5 = arranged in a=20 cylindrical pattern extend through the wall of the hollow = spherical=20 pressure chamber 1, and each hollow tube is welded to the = pressure=20 chamber to form a pressure seal.   The opposite ends of = hollow tubes=20 5 extend through the mounting plate MP and are = welded=20 likewise to form a pressure seal.   A plurality of heat = transfer fins=20 6 are welded at intervals along the length of said hollow = tubes=20 5.   A bright reflecting mirror surface 7 is = provided=20 on the inner wall of the hollow spherical pressure chamber = 1.=20   A source of high-voltage 8 is periodically connected = to the=20 insulated high-voltage electrodes 2 and 4.   A = source=20 of medium-voltage 9 from a discharge capacitor is connected = to the=20 insulated medium-voltage electrodes 3 and 4.   = A source=20 of noble gas mixtures 10, e.g., xenon, krypton, helium and = mercury=20 is applied under pressure into the hollow spherical pressure = chamber=20 1 through pressure regulator valve 11 and check = valve=20 12.




= Referring=20 now to Fig.2 of the drawings, the complete assembly = 13 shown=20 in Fig.1 is mounted on the top of the cylinder 14 = via=20 mounting plate MP.   The necessary gaskets or other = means are=20 provided to seal the engine and prevent loss of gases into the = atmosphere.=20   The piston 15 located within cylinder 14 has = several=20 rings 16 which seal against the inner wall of the cylinder. =  =20 The piston 15 is connected to the crankshaft 17 by=20 connecting rod 18.   The source of noble gas mixtures=20 10 is applied under pressure into the crankcase 21 = through=20 pressure regulator valve 11, check valve 12 and = capillary=20 tube 19.   The piston 15 is now balanced = between equal=20 gas pressures.   Assuming that the engine is running and the = piston=20 15 is just passing Top-Dead-Centre (TDC), a source of=20 medium-voltage from a capacitor discharge system 9 = (Fig.6, a=20 single typical capacitor section) is applied to electrodes = 3 and=20 4.   A source of high-voltage pulses from a standard = ignition=20 coil 8 (such as shown in Fig.7) is applied to = electrodes=20 2 and 4 and the gases within the hollow spherical = pressure=20 chamber 1 are ionised and made electrically conductive. =   An=20 electrical discharge takes place between electrodes 3 and = 4=20 through the gases in the hollow spherical pressure chamber = 1.=20

The electrical discharge releases high energy photons on = many=20 different electromagnetic frequencies.   The photons strike = the atoms=20 of the various gases, e.g., xenon, krypton, helium and mercury at=20 different electromagnetic frequencies to which each atom is = selectively=20 sensitive and the atoms of each gas become excited.   The = first=20 photons emitted are reflected back into the mass of excited atoms = by the=20 reflecting mirror surface 7.   This triggers more = photons to=20 be released by these atoms, and they are reflected likewise from = the=20 mirror surface 7 and strike other atoms into excitation and = more=20 photons are released as the chain reaction progresses.   The=20 electrons orbiting around the protons of each excited atom = increase in=20 speed and expand outward in a new orbital pattern due to an = increase in=20 centrifugal force.   Consequently, a pressure wave is = developed in=20 the gases as the atoms expand and the overall pressure of the = gases within=20 the hollow spherical pressure chamber 1 increases.   = As the=20 gases expand they pass through the hollow tubes 5 and apply = pressure on the top of piston 15.   The pressure = pushes the=20 piston 15 and the force and motion of the piston is = transmitted=20 through the connecting rod 18 to the crankshaft 17 = rotating=20 it in a clockwise direction.   At this point of operation, = the power=20 stroke is completed and the capacitor in the medium-voltage = capacitor=20 discharge system 9 is discharged.   The excited atoms = return=20 to normal ground state and the gases return to normal pressure = level.=20   The capacitor in the medium-voltage capacitor discharge = system=20 9 is recharged during the time period between (TDC) power = strokes.=20




= Referring=20 now to Fig.3 of the drawings, the compression stroke of the = engine=20 is shown.   In this engine cycle the gases above the piston = are=20 forced back into the hollow spherical pressure chamber through the = tubes=20 of the heat transfer assembly.   The gases are cooled as the = heat is=20 conducted into the fins of the heat transfer assembly and carried = away by=20 an air blast passing through the fins.   An example is shown = in=20 Fig.4, the centrifugal air pump P providing an air = blast=20 upon like fins.


Some of = the=20 basic elements of the invention as set forth in Fig.1, = Fig.2, and=20 Fig.3 are now shown in Fig.4 and Fig.5 which = show=20 complete details of a six-cylinder horizontally-opposed AEROPS = engine.=20

Referring now to Fig.4 and Fig.5 of the = drawings.=20   Fig.4 is a view of the rear section of the engine = showing=20 the crankshaft, centre axis and two of the horizontally-opposed = cylinders.=20   In as much as the rear R, middle M and front = F=20 sections of the engine possess identical features, only the rear = R=20 engine section will be elaborated upon in detail in order to = prevent=20 repetition and in the interest of simplification.   The = crankshaft=20 17A consists of three cranks spaced 120 degrees apart in a = 360=20 degree circle as shown.   Both connecting rods 18A and = 18B are connected to the same crank.   Their opposite = ends=20 connect to pistons 15A and 15B, located in cylinders = 14A and 14B respectively.   Each piston has = pressure=20 sealing rings 16A and 16B.   The hollow = spherical=20 pressure chamber assemblies consisting of 1A and 1D = are=20 mounted on cylinders 14A and 14B via mounting plates = MP.   The necessary gaskets are provided as needed to = seal the=20 complete engine assemblies from atmospheric pressure.



The = source=20 of gas mixtures 10A is applied under pressure to pressure = regulator=20 valve 11A and flows through check valve 12A, through = check=20 valve 12B to the hollow spherical pressure chamber = 1A, and=20 through check valve 12C to the hollow spherical pressure = chamber=20 1D.   The gas flow network consisting of capillary = tubes below=20 point 19A represents the flow of gases to the rear section = R=20 of the engine.   The middle section M and the front = section=20 F both have gas flow networks identical to that consisting = of=20 capillary tubes below point 19A, while the gas flow network = above=20 is common to all engine sections.   Throttle valve 20A = and the=20 connecting tubing form a variable bypass between hollow spherical = pressure=20 chambers 1A and 1D to control engine speed and = power.  =20 Engine sections R, M and F each have this bypass = throttle=20 network.   The three throttle valves have their control = shafts ganged=20 together.   A source of medium-voltage pulses 9A is = connected=20 to medium-voltage electrodes 3A and 3D.   In = one=20 particular embodiment the medium-voltage is 500 volts.   A = source of=20 high-voltage pulses 8A is connected to electrode 2A = through=20 the distributor as shown.   Electrode 4A is connected = to=20 common ground.   Centrifugal air pumps P force air = through=20 heat transfer fins 6A and 6B to cool the gases = flowing in=20 the tubes 5A and 5B.

Fig.5 is a top = view of=20 the AEROPS engine showing the six cylinders and crankshaft = arrangement=20 consisting of the rear R, middle M and front = F=20 sections.   The crankshaft 17A is mounted on bearings=20 B, and a multiple shaft seal S is provided as well = as the=20 necessary seals at other points to prevent loss of gases into the=20 atmosphere.   The hollow spherical pressure chambers 1A, = 1B, 1C,=20 1D, 1E and 1F are shown in detail with high-voltage = electrodes=20 2A, 2B, 2C, 2D, 2E, 2F and medium-voltage electrodes 3A, = 3B, 3C,=20 3E and 3F.   The common ground electrodes 4A, = 4B, 4C,=20 4D, 4E, 4F are not shown in Fig.5 but are typical of = the common=20 ground electrodes 4A and 4D shown in Fig.4. =   It=20 should be noted that the cranks on crankshaft 17A are so = arranged=20 to provide directly opposing cylinders rather than a conventional=20 staggered cylinder design.


Fig.6= =20 is an electrical schematic of the source of medium-voltage = 9A.=20   The complete operation of the converter is explained as = follows:=20   The battery voltage 12 VDC is applied to transformer = T1,=20 which causes currents to pass through resistors R1, R2, R3 = and=20 R4.   Since it is not possible for these two paths to = be=20 exactly equal in resistance, one-half of the primary winding of = T1=20 will have a somewhat higher current flow.   Assuming that the = current=20 through the upper half of the primary winding is slightly higher = than the=20 current through the lower half, the voltages developed in the two = feedback=20 windings (the ends connected to R3 and R2) tend to = turn=20 transistor Q2 on and transistor Q1 off.   The = increased=20 conduction of Q2 causes additional current to flow through = the=20 lower half of the transformer primary winding.   The increase = in=20 current induces voltages in the feedback windings which further = drives=20 Q2 into conduction and Q1 into cut-off, = simultaneously=20 transferring energy to the secondary of T1.   When the = current=20 through the lower half of the primary winding of T1 reaches = a point=20 where it can no longer increase due to the resistance of the = primary=20 circuit and saturation of the transformer core, the signal applied = to the=20 transistor from the feedback winding drops to zero, thereby = turning=20 Q2 off.   The current in this portion of the primary = winding=20 drops immediately, causing a collapse of the field about the = windings of=20 T1.   This collapse in field flux, cutting across all = of the=20 windings in the transformer, develops voltages in the transformer = windings=20 that are opposite in polarity to the voltages developed by the = original=20 field.   This new voltage now drives Q2 into cut-off = and=20 drives Q1 into conduction.   The collapsing field=20 simultaneously delivers power to the secondary windings L1, L2, = L3, L4,=20 L5 and L6.   The output voltage of each winding is = connected through resistors R5, R6 and R7 and diode=20 rectifiers D1, D2, D3, D4, D5 and D6, respectively, = whereby=20 capacitors C1, C2, C3, C4, C5 and C6 are charged = with a=20 medium-voltage potential of the polarity shown.   The output = voltage=20 is made available at points 3A, 3B, 3C, 3D, 3E and = 3F which=20 are connected to the respective medium-voltage electrodes on the = engine=20 shown in Fig.4 and Fig.5.


Referrin= g=20 now to Fig.7 of the drawings, a conventional "Kettering" = ignition=20 system provides a source of high-voltage pulses 8A of = approximately=20 40,000 volts to a distributor, which provides selective voltage = output at=20 2A, 2B, 2C, 2D, 2E and 2F, which are connected to = the=20 respective high-voltage electrodes on the engine shown in = Fig.4 and=20 Fig.5.   The distributor is driven by the engine = crankshaft=20 17A (Fig.5) at a one to one mechanical gear ratio.=20

Referring again to Fig.4 and Fig.5 of the = drawings,=20 the operation of the engine is as follows:   Assuming that a = source=20 of noble gas mixtures, e.g., xenon, krypton, helium and mercury is = applied=20 under pressure to the hollow spherical pressure chambers 1A, = 1B, 1C,=20 1D, 1E and 1F and internally to the crankcase = 21A=20 through pressure regulator valve 11A and check valves = 12A,=20 12B and 12C; and the source of medium-voltage 9A = is=20 applied to electrodes 3A, 3B, 3C, 3D, 3E and 3F; and = a=20 source of high-voltage pulse 8A is applied to electrode = 2A=20 through the timing distributor, the gas mixtures in the hollow = spherical=20 pressure chamber 1A is ionised and an electrical discharge = occurs=20 immediately between electrodes 3A and 4A.=20

High-energy photons are released on many different = electromagnetic=20 frequencies.   The photons strike the atoms of the various = gases,=20 e.g., xenon, krypton, helium and mercury at different = electromagnetic=20 frequencies to which each is particularly sensitive and the atoms = of each=20 gas become excited.   The first photons emitted are reflected = back=20 into the mass of excited atoms by the internal reflecting mirror = surface=20 on the inside wall of the hollow spherical pressure chamber = 1A.=20   This triggers more photons to be released by these atoms = and they=20 are reflected likewise from the mirror surface and strike other = atoms into=20 excitation and more photons are released as the chain reaction = progresses.=20   The electrons orbiting around the protons of each excited = atom in=20 the hollow spherical pressure chamber 1A increase in speed = and=20 expand outward in a new orbital pattern due to an increase in = centrifugal=20 force.   Consequently, a pressure wave is developed in the = gases as=20 the atoms expand and the overall pressure of the gases within the = hollow=20 spherical pressure chamber 1A increases.

As the = gases=20 expand they pass through the hollow tubes 5A applying = pressure on=20 the top of piston 15A.   The pressure applied to = piston=20 15A is transmitted through connecting rod 18A to the = crankshaft 17A rotating it in a clockwise direction.   = As the=20 crankshaft 17A rotates it pushes piston 15B via = connecting=20 rod 18B in the direction of a compression stroke, forcing = the gases=20 on the top of the piston through hollow tubes 5B into the = hollow=20 spherical pressure chamber 1D.   As the gases pass = through the=20 hollow tubes 5A and 5B the heat contained in the = gases is=20 conducted into the heat transfer fins 6A and 6B, = where it is=20 dissipated by a blast of air passing through the fins from the = centrifugal=20 air pumps P.   At this point of operation the power = stroke of=20 piston 15A is completed and the capacitor in the = medium-voltage=20 capacitor discharge system 9A is discharged.   The = excited=20 atoms return to normal ground state and the gases return to normal = pressure level.   The capacitor in the medium-voltage = capacitor=20 discharge system 9A is recharged during the time period = between the=20 power strokes of piston 15A.

The above power stroke = cycle=20 occurs exactly the same in the remaining cylinders as the = high-voltage=20 firing order progresses in respect to the position of the = distributor=20 switch.   In as much as the AEROPS engine delivers six power = strokes=20 per single crankshaft revolution, the crankshaft drives the = distributor=20 rotor at a one to one shaft ratio.   The complete = high-voltage firing=20 order is 1, 4, 5, 2, 3, 6, whereas, the high-voltage is applied to = electrodes 2A, 2B, 2C, 2D, 2E and 2F respectively. =   A=20 means of controlling engine speed and power is provided by a = plurality of=20 throttle control valves and connecting tubes which form a bypass = between=20 opposing hollow spherical pressure chambers of each engine = section.=20

The AEROPS engine as described above provides a sealed = unit power=20 source which has no atmospheric air intake nor exhaust emission = and is=20 therefore pollution free.


The = Michael=20 Eskeli Turbine.
In April 1989, = Michael Eskeli=20 was annoyed by a newspaper article published in the Dallas Times = Herald=20 which commented on the failure of science to come up with = alternative=20 power systems which do not rely on petroleum products to operate. =  =20 Michael responded in a letter to the Editor, stating that he holds = patents=20 for fuel-less power generators, work-free heat pumps, and other = related=20 items, 56 patents issued in the mid-70s.

Michael does hold = many=20 patents, one of which is shown in Chapter 14, as a work-free = fuel-less=20 heater.   However, as I am not aware of any working prototype = being=20 shown, I must recommend that you consider the following = information as =93an=20 idea=94 rather than a proven fact.   As far as I am aware, in = the=20 1970s, the US Patent Office did not demand to see a working = prototype=20 before granting a patent, especially if the patent related to a = device=20 based on accepted Engineering principles.

However, as = Michael=92s=20 claim is for self-powered devices, his claim seems too important = to be=20 ignored, prototype or no prototype, as competent people reading = this may=20 well understand the principles suggested and be in a position to = build a=20 self-powered device as a result.   If that is the case, then = I should=20 really appreciate feedback information on any successful = replications and=20 the construction methods used.

As I understand it, = Michael=92s=20 self-powered devices are Heat Pumps where the additional energy is = flowing=20 from the heat contained in the air, courtesy of the heating = effects of=20 sunshine.   Standard engineering, but with a design which = utilises=20 this available energy to provide practical mechanical output power = for=20 vehicles and electrical generators.

The Eskeli patents = which I=20 have been able to locate are:

3,650,636 Rotary Gas=20 Compressor
3,719,434 Rotary Ejector Compressor
3,748,054 = Reaction=20 Turbine
3,748,057 Rotary Compressor with Cooling
3,758,223 = Reaction=20 Rotor Turbine
3,761,195 Compressing Centrifuge
3,795,461 = Compressor=20 with Cooling
3,809,017 Heat and Steam Generator
3,834,179 = Turbine=20 with Heating and Cooling
3,854,841 Turbine
3,861,147 Sealed=20 Single-rotor Turbine
3,874,190 Sealed Single-rotor = Turbine
3,879,152=20 Turbine
3,889,471 Dual-rotor Dual-fluid Turbine
3,895,491 = Turbine=20 with Dual Rotors
3,919,845 Dual-fluid Single-rotor = Turbine
3,926,010=20 Rotary Heat Exchanger
3,931,713 Turbine with = Regeneration
3,933,007=20 Compressing Centrifuge
3,933,008 Multi-stage Heat=20 Exchanger
3,937,034 Gas Compressor-Expander
3,938,336 = Turbine with=20 Heating and Cooling
3,939,661 Power Generator
3,949,557=20 Turbine
3,961,485 Turbine with Heat Intensifier
3,962,888 = Heat=20 Exchanger
3,972,194 Thermodynamic Machine of the Vane = Type
3,972,203=20 Rotary Heat Exchanger
3,981,702 Heat Exchanger
3,986,361 = Turbine=20 with Regeneration
4,003,673 Fluid Pressuriser
4,005,587 = Rotary Heat=20 Exchanger with Cooling and Regeneration *
4,012,164 Rotor with=20 Recirculation
4,012,912 Turbine
4,030,856 Rotor with Jet=20 Nozzles
4,044,824 Heat Exchanger
4,047,392 Dual Rotor Heat = Exchanger=20 *
4,050,253 Thermodynamic Machine
4,057,965 Thermodynamic = Machine=20 with Step-type Heat Addition
4,060,989 Thermodynamic Machine = with=20 Step-type Heat Exchangers
4,068,975 Fluid = Pressuriser
4,077,230=20 Rotary Heat Exchanger with Cooling
4,106,304 Thermodynamic=20 Compressor
4,107,944 Heat Pump with Two Rotors *
4,107,945=20 Thermodynamic Compressor
4,124,993 Refrigeration = Machine
4,167,371=20 Method of Fluid Pressurisation
4,178,766 Thermodynamic = Compressor=20 Method
4,574,592 Heat Pump with Liquid-Gas working = Fluid


And=20 there are presumably 7 others not listed here, to raise the total = to the=20 56 mentioned by Michael.   I do not have the expertise to = tell which=20 of these may be self-powered just by reading the patent = information, which=20 generally does not mention anything along those lines, (the Patent = Office=20 staff not believing that COP>1 exists).   Practically any = of these=20 patents might fit Michael=92s description, so I will pick the = following=20 patents to reproduce here:

4,107,944 Heat Pump with Two = Rotors=20 (continuing 4,005,587 and 4,047,392)
4,012,912 Turbine,=20 and
3,931,713 Turbine with Regeneration


*********************


 US Patent 4,107,944   =
                 22nd August 1978                      Inventor: Michael =
Eskeli


HEAT PUMP WITH TWO = ROTORS



ABSTRACT

A=20 method and apparatus for generating heating and cooling by = circulating a=20 working fluid within passageways carried by rotors, compressing = the=20 working fluid in them and removing heat from the working fluid in = a=20 heat-removal heat exchanger and adding heat into the working fluid = in a=20 heat-addition heat exchanger, all carried within the rotors. =   The=20 working fluid is sealed in, and may be a suitable gas, such as = nitrogen.=20   A working fluid heat exchanger is also provided to exchange = heat=20 within the rotor between two streams of working fluid.   In = one=20 arrangement, the unit uses two rotors, both rotating; in an = alternate=20 arrangement, one of the rotors may be held stationary.   = Applications=20 include air conditioning and heating applications.

US = Patent=20 References:
2,490,064 Thermodynamic Machine - Dec 1949 -=20 Kollsman
2,490,065 Thermodynamic Machine - Dec 1949 -=20 Kollsman
2,520,729 Machine for producing Heat Energy - Aug 1950 = -=20 Kollsman
2,597,249 Thermodynamic Engine - May 1952 -=20 Kollsman
3,470,704 Thermodynamic Apparatus and Method - Oct = 1969 -=20 Kantor
3,834,179 Turbine with Heating and Cooling - Sep 1974 -=20 Eskeli
3,861,147 Sealed Single-rotor Turbine - Jan 1975 -=20 Eskeli
3,889,471 Dual-rotor Dual-fluid Turbine - Jun 1975 -=20 Eskeli
3,895,491 Turbine with Dual Rotors - Jul 1975 -=20 Eskeli
3,919,845 Dual-fluid Single-rotor Turbine - Nov 1975=20 Eskeli
3,931,713 Turbine with Regeneration - Jan 1976=20 Eskeli
4,005,587 Rotary Heat Exchanger with Cooling & = Regeneration=20 - Feb 1977 - Eskeli
4,044,824 Heat Exchanger - Aug 1977 -=20 Eskeli


Cross References to Related = Applications
This=20 application is a continuation-in-part application of "Dual Rotor = Heat=20 Exchanger" filed Nov. 18, 1973, Ser. No. 407,665, now U.S. Pat. = No.=20 4,047,392.   This application also is a continuation-in-part = of "Heat=20 Pump" filed June 30, 1975, Ser. No. 591,881, now abandoned. =

And=20 this application also is a continuation-in-part of "Rotary Heat = Exchanger=20 with Cooling and Regeneration" filed Oct. 1, 1975, Ser. No. = 618,456, now=20 U.S. Pat. No. 4,005,587.


BACKGROUND OF THE = INVENTION=20
This invention relates generally to devices for heat = transfer=20 from a lower temperature to a higher temperature by using a = working fluid=20 enclosed within a centrifuge rotor as an intermediate fluid to = transport=20 the heat.

Heat pumps have been known in the past but are = complex=20 and costly, and usually use a working fluid that is evaporated and = condensed, which results in poor efficiency, and so, high energy = cost.=20


SUMMARY OF THE INVENTION
It is an = object of=20 this invention to provide apparatus that is low in initial cost = and has=20 high thermal efficiency thus reducing cost of the power required = to run=20 it.   It is further the object of this invention to provide a = device=20 and process wherein the losses that normally occur in bearings and = seals,=20 due to friction, are applied to the working fluid for its = circulation,=20 thus in effect eliminating the power loss due to such friction = losses.=20   Also, it is an object of this invention to provide the = rotor with a=20 working fluid heat exchanger to reduce needed rotor speeds.=20


BRIEF DESCRIPTION OF THE DRAWINGS =


Fig.1= =20 is a cross section of the device.




F= ig.2=20 is an end view of the device.




F= ig.3=20 is an axial cross section of another form of the device.=20


DESCRIPTION OF PREFERRED EMBODIMENTS =


Fig.1= =20 shows an axial cross section of the device, where 10 is the = base,=20 11 is the first rotor, 12 is the second rotor, = 13 is=20 a seal and 14 is the bearing which supports shaft = 15,=20 16 is a fluid passage in the second rotor, 17 is = working=20 fluid opening which may be a nozzle, 18 is the first heat = exchanger=20 for heat removal from the working fluid, 19 is first heat = transfer=20 fluid conduit, 20 is the working fluid heat exchanger, in = this=20 instance formed from sheet metal like bellows, 21 are = vanes,=20 22 is the second heat exchanger for heat addition to the = working=20 fluid, 23 is a bearing which supports shaft 24, = 25=20 and 26 are the entry and the exit for the second heat = transfer=20 fluid, 27 and 28 are the entry and exit points for = the first=20 heat transfer fluid, and 29 is a vane in the peripheral = passage.=20



F= ig.2=20 is an end view of the unit shown in Fig.1, where 10 = is the=20 base, 11 is the first rotor, 17 are fluid openings,=20 12 is the second rotor, 16 are the second rotor = fluid=20 passages with vanes, 30 indicates the direction of = rotation,=20 24 is the first rotor shaft, and 21 are vanes. =



In=20 Fig.3, the rotors are arranged differently, but perform=20 approximately the same functions as in the unit of Fig.1, = where=20 40 is first rotor, 41 is first heat exchanger for = heat=20 removal from first fluid, 42 is first rotor shaft, = 43 and=20 44 are entry and exit for first heat transfer fluid, = 45 is=20 conduit, 46 is working fluid heat exchanger, 47 are = fluid=20 openings which may be nozzles, 48 is second rotor, = 49 is=20 second heat exchanger for adding heat to the working fluid, = 50 is=20 bearing and seal, 51 is second rotor shaft, 52 and = 53=20 are entry and exit for second heat transfer fluid.

In = operation,=20 the rotors are caused to rotate and the rotor cavities are filled = with a=20 suitable working fluid, which is usually a gas, such as nitrogen, = air or=20 other gaseous or vapour substance.   Referring to = Fig.1, the=20 second rotor rotates usually faster than the first rotor, and the = working=20 fluid is compressed by centrifugal force in passages 16, = and in the=20 first rotor to some extent, after which heat is removed in heat = exchanger=20 18, with such heat then being transported by the first heat = transfer fluid out of the device.   The working fluid then = passes=20 along the peripheral passage 29 and releases heat in heat = exchanger=20 20, after which the fluid is expanded against centrifugal = force in=20 vanes 21 and in heat exchanger 22 where heat is = added to the=20 working fluid.   After expansion, the working fluid passes = along=20 centre passage and receives heat from heat exchanger 20, = thus=20 completing its work cycle.

The operation of the unit in=20 Fig.3 is similar, except that the second rotor usually = rotates=20 slower than the first rotor, and the second rotor may be kept = stationary,=20 if desired.   Note that if the second rotor is held = stationary, one=20 may use dirty water as the second heat transfer fluid; normally, = in=20 rotating heat exchangers, the heat transfer fluid must be free of = solids,=20 which will collect in the heat exchanger due to centrifugal force, = and=20 block the heat exchanger, and by having a stationary heat = exchanger,=20 ordinary water may be used, such as water from a cooling tower. =

In=20 the unit of Fig.1, the power input is normally to the = second rotor,=20 and the first rotor is allowed to rotate freely.   In such = usage, the=20 rotor diameters are selected to provide, together with the = friction loss=20 in bearings, for the needed speed differential between the two = rotors.=20   With the second rotor rotating faster, necessary push for = the=20 working fluid is provided to keep the working fluid circulating. =  =20 Alternately, the speed differential may be maintained by using a = power=20 transmission between the two rotors, such as a gearbox.   In = the unit=20 of Fig.3, the second rotor speed is slower than the speed = of the=20 first rotor, and where the rotor diameters are suitable, the = second rotor=20 may be held stationary, providing needed push for the working = fluid for=20 its circulation.

The working fluid heat exchanger = 20 and=20 46, employ centrifugal force and varying gas density to = obtain heat=20 exchange between the two working fluid streams.   Hot gas in = the=20 peripheral passage is lighter, and colder gas between the folds of = the=20 heat exchanger is colder, thus the cold gas is displaced by = lighter gas by=20 centrifugal force.   Similarly, at the centre passage, cold = gas at=20 centre displaces hot gas between folds.   Other types of heat = exchangers may be used for the heat exchanger 20, including = heat=20 pipes, sheet metal discs, and finned tubing filled with a liquid.=20

The rotor may be encased within a vacuum tank, if desired, = to=20 reduce friction on rotor outer surfaces.   The use of the = working=20 fluid heat exchanger 20 will reduce required rotor speeds = to obtain=20 required temperature differentials between the two heat transfer = fluids,=20 which then reduces friction losses on the rotor, which may = eliminate the=20 need for a vacuum tank.

Various modifications of this = device may=20 be made, and different types of heat exchangers used.   Also, = working=20 fluid radial passages may be curved in various directions, one = being the=20 slope for vanes shown as item 21 in Fig.2.   By = using=20 vane slopes and sloped passages, one can adjust the amount of work = exchange between the working fluid and the rotor.   Nozzles = 47=20 are usually positioned so as to discharge backwards, in order to = generate=20 some torque on the first rotor, and similar nozzles may also be = used in=20 passages 21 of the unit shown in Fig.1.   = Further, the=20 heat exchanger 22, of Fig.1, may be mounted on a = stationary=20 member, if desired, in the manner shown in Fig.3, and heat = exchanger 18 may be mounted within rotor 12, if = desired.=20   The various components of the units may be interchanged, as = desired.


CLAIMS
1. In a heat = pump=20 wherein a compressible working fluid is circulated radially = outwardly in a=20 first fluid passage, said first passage contained in a first = member, and=20 radially inwardly towards centre of rotation in a second fluid = passage,=20 the second passage contained in at least one of the first and = second=20 members, the first and second members coaxially arranged, at least = one of=20 the members being supported by a shaft for rotation; the first and = the=20 second radial working fluid passages communicatingly connected at = their=20 respective outward ends by an outer passage and at their = respective inward=20 ends by an inner passage, the radial and outer and inner passages = forming=20 a closed loop extending at least partially through both of the = members, a=20 working fluid adapted to be circulating through the loop, means = for=20 compressing the working fluid by centrifugal force within the loop = with=20 accompanying temperature increase, first heat exchange means for = cooling=20 the working fluid after compression, the first heat exchange means = being=20 carried by one of the members, a second heat exchange means, = carried by=20 one of the members, for regeneratively exchanging heat between the = working=20 fluid within the inner and outer passages, and a third heat = exchange means=20 carried by one of the members for heating the working fluid after = the heat=20 exchange between the working fluid within the inner and outer = passages.=20

2. The heat pump of claim 1 wherein a first heat = transfer=20 fluid is circulated within the first heat exchange means to remove = heat=20 with the first heat exchange fluid entering and leaving via = conduits near=20 the centre of rotation of the members.

3. The heat = pump of=20 claim 1 wherein a second heat transfer fluid is circulated within = the=20 third heat exchange means entering and leaving via conduits near = the=20 centre of rotation of the members.

4. The heat pump = of=20 claim 1 wherein both of the members are rotors.

5. = The heat=20 pump of claim 4 wherein the two rotors rotate at different angular = speeds.=20

6. The heat pump of claim 1 wherein at least one of = the=20 members is a rotor.

7. The heat pump of claim 6 = wherein the=20 second heat exchange means includes a plurality of folds.=20

8. The heat pump of claim 7 wherein the second heat = exchange means is of bellows configuration.


*********************
 US Patent =
4,012,912                    22nd March 1977                      =
Inventor: Michael Eskeli
TURBINE
ABSTRACT

A method = and=20 apparatus for the generation of power wherein a working fluid is=20 compressed within outward extending rotor passages, and then = passed inward=20 in other rotor passages with accompanying expansion and = deceleration, with=20 work being generated by the decelerating fluid.   Heat may be = added=20 into the working fluid near the rotor periphery, and in closed = rotors,=20 heat is removed from the working fluid after expansion.   A=20 regenerator may also be used, mounted on the rotor, exchanging = heat=20 between two streams of the working fluid.   During the = deceleration,=20 the working fluid passages are curved backwards, while the working = fluid=20 passages for acceleration are usually radial.   The working = fluid may=20 be either a liquid or a gas, and the heating fluid and the cooling = fluid=20 may also be either a liquid or a gas.


US Patent=20 References:
3,761,195 Compressing Centrifuge - Sept 1973 -=20 Eskeli
3,834,179 Turbine with Heating and Cooling - Sept 1974 - = Eskeli
3,926,010 Rotary Heat Exchanger - Dec 1975 -=20 Eskeli



Cross References to Related=20 Applications:
This application is a continuation-in-part=20 application of "Turbine," Ser. No. 566,373, filed 4-9-75 now U.S. = Pat. No.=20 3,949,557.


BACKGROUND OF THE = INVENTION
This=20 invention relates to power generators where a working fluid is = circulated=20 from a higher energy level to lower energy level, generating = power.=20

In my earlier U.S. Pat. Nos. 3,874,190 and 3,854,841, I = described=20 a closed and open type turbines, and using centrifuge design. =   These=20 turbines used forward facing nozzles within the rotor; in the = apparatus=20 disclosed here, such nozzles have been replaced by other methods.=20


SUMMARY OF THE INVENTION
It is an = object of=20 this invention to provide a single rotor centrifuge type turbine = stage,=20 where vanes or fins, with suitable contours, are used to extract = power=20 from the working fluid, using either an open type or a closed type = rotor.=20


BRIEF DESCRIPTION OF THE = DRAWINGS




F= ig.1=20 is a cross section and



F= ig.2=20 is an end view of a closed type rotor.



F= ig.3=20 is a cross section and



F= ig.4=20 is an end view of an open type rotor.



F= ig.5=20 is a cross section of a unit using a closed type rotor and also = using a=20 regenerator.


DESCRIPTION OF PREFERRED = EMBODIMENTS=20




Refe= rring=20 to Fig.1, there is shown a cross section of one form of the = unit,=20 where 10 is the rotor which is supported by bearings = 16 and=20 22, shaft 17 and base 21, 12 is a heat = supply=20 heat exchanger and 15 is cooling heat exchanger, 14 = and=20 11 are vanes or fins, 18 and 19 are coolant = entry and=20 exit, 20 is a dividing wall, 23 and 24 are = heating=20 fluid entry and exit, and 13 is a working fluid passage = which may=20 be used to regulate the flow of working fluid within the rotor. =



F= ig.2=20 is an end view of the unit shown in Fig.1. Where 10 = is the=20 rotor, 17 the shaft, 19 is a coolant passage, = 21 is=20 the base, 14 are vanes positioned so that they slope away = from the=20 direction of rotation as indicated by arrow 25, while=20 simultaneously passing the working fluid inwards, 12 is the = heating=20 heat exchanger, and 15 is the cooling heat exchanger. =



In=20 Fig.3, a rotor for a unit using open cycle is used, where = the=20 working fluid enters and leaves the rotor.   Here, 30 = is the=20 rotor, 31 is the vane situated in a passage which extends = outwards,=20 32 is the fluid passage, 33 is a vane in the passage = for=20 inward bound working fluid, 34 is the working fluid exit, = 35=20 is the rotor shaft, 36 is a rotor internal divider and = 37 is=20 the working fluid entry into the rotor.



F= ig.4=20 shows an end view of the unit of Fig.3 where 30 is = the=20 rotor, 35 is the shaft, 31 are vanes in the passages = for=20 outward bound fluid, and are shown here to be curved backwards, = when the=20 rotor rotates in the direction shown by arrow 38.   = After=20 passing openings 32, the working fluid passes inwards = guided by=20 vanes 33rotation, so the working fluid provides thrust = against the=20 rotor components as it decelerates when passing inwards toward the = centre=20 of the rotor.



In=20 Fig.5, a rotor with a regenerator is shown, and also the = rotor=20 shaft is arranged so that it can be kept stationary if desired. =  =20 50 is the rotor which is supported by bearings 56 = and=20 63 and shaft 57.   Vanes 51 may be = radial or=20 curved as desired, and vanes 54 are curved in a manner = similar to=20 vanes 33 in Fig.4.   52 is a = regenerative heat=20 exchanger, exchanging heat between the working fluid streams = flowing in=20 passages 53 and 61.   Heat supply heat = exchanger=20 55 and cooling heat exchanger 62 are attached to the = shaft,=20 so that the shaft may be kept stationary or rotated at a different = speed=20 than the rotor 50.   58 and 59 are the = entry and=20 exit points for the heating fluid while 64 and 65 = are the=20 entry and exit points for the cooling fluid, and 66 is an = opening.=20

When operating, the rotor rotates, and a working fluid = within the=20 rotor passes outwards in passage 11, and is compressed by=20 centrifugal force, and accelerated to a tangential speed that may = be the=20 same as that for the rotor periphery.   In a closed rotor = such as is=20 shown in Fig.1, heat is added into the working fluid near = the rotor=20 periphery, and then the working fluid decelerated in the fluid = passages=20 14 extending inwards toward rotor centre, with the passages = being=20 curved backwards away from the direction of rotation as shown in=20 Fig.2.   As the working fluid is decelerated in the = inward=20 extending passages, the work associated by such deceleration is=20 transferred into the rotor and this provides the thrust and torque = to=20 rotate the rotor.   After deceleration and expansion, the = working=20 fluid is cooled in heat exchanger 15 and then passed to the = outward=20 extending passages thus completing its working cycle.

The=20 operation of the unit of Fig.3 is similar, except that the = working=20 fluid enters the rotor via opening 37 from external = sources.  =20 For the unit shown in Fig.3, the heat addition heat = exchanger is=20 omitted; for this unit, there is a pressure drop between entry = 37=20 and exit 34.   A heat exchanger similar to that shown = in=20 Fig.1, item 12, may be used in the unit of = Fig.3, and=20 then the entry and exit pressure for the working fluid may be the = same, if=20 desired.

The operation of the unit shown in Fig.5, = is=20 similar to that described for the other units.   The rotor = rotates,=20 and by centrifugal force, compresses the working fluid in passages = 51, and then the working fluid gains heat in the = regenerative heat=20 exchanger, with the heat being supplied by another working fluid = stream=20 returning from the high temperature end of the unit.   The = working=20 fluid is expanded and decelerated in passages 54 and heat = is added=20 in the heat exchanger 55.   Then the working fluid = passes=20 through the regenerative heat exchanger and then is cooled in the = cooling=20 heat exchanger and then is passed into passages 51 thus = completing=20 its cycle.

The various components of the units shown can = be=20 exchanged to make additional forms of the apparatus.   As = noted, the=20 unit of Fig.3 may be provided with a heat exchanger similar = to that=20 shown in Fig.1 for adding heat into the working fluid near = the=20 rotor periphery.   Further, a regenerator may be provided = with the=20 units of Fig.1 and Fig.3, if desired, between the = outward=20 extending and the inward extending working fluid passages.   = Also,=20 the cooling coil of Fig.5, item 62 may be = eliminated, and=20 the working fluid taken into the unit from outside the unit, if = desired.=20

The openings 32, 13 and 66 may be made into = nozzles,=20 if desired, and the nozzle oriented in different directions as = desired.=20   In particular, these nozzles may be positioned so as to = discharge=20 the working fluid tangentially backwards, if desired.

The=20 regenerator of Fig.5 is shown to be tapered.   This = taper may=20 be as shown, or the taper may be made such that the regenerator = portion=20 diameter is smaller at the end which has the heat exchanger = 55,=20 than the end which has the heat exchanger 62.   Also, = the=20 regenerator may be made without a taper.

Passages = 53 and=20 61 are usually provided with vanes, as indicated in = Fig.5,=20 to prevent tangential movement of the working fluid. =

Applications=20 for this power generator are those normally encountered in power=20 generation.

The working fluid is usually a gas for units = such as=20 those shown in Fig.1 and Fig.5, but the working = fluid may=20 also be a liquid for a unit such as shown in Fig.3.   = The=20 heating and cooling fluids may be either gases or liquids, as = desired.=20

The heat exchangers for heating and cooling are shown to = be made=20 of finned tubing.   Other forms of heat exchangers for adding = heat=20 and for removing heat may be used.   The regenerative heat = exchanger=20 is shown to be made of sheet metal; other forms of heat exchangers = may be=20 also used.


CLAIMS
  1. In a power generating turbine, wherein a working fluid is=20 accelerated and pressurized within a rotating rotor first = outwardly=20 extending passages, and wherein a working fluid is expanded = within a=20 rotating rotor inwardly extending second passages, with the = first and=20 the second passages being connected at their outward ends by a = passage=20 means to allow said working fluid to flow outwardly within the = first=20 passage and through said passage means and inwardly within the = second=20 passage, the improvement comprising:
    a. a curved = inwardly=20 extending second passage, for the generation of thrust and = torque on=20 said rotating rotor, with the curvature of said curved inwardly=20 extending passage being backward and away from the direction of=20 rotation.
  2. The turbine of claim 1 wherein a heating heat exchanger is = provided=20 to add heat into said working fluid near said passage means. =
  3. The turbine of claim 2 wherein the rotor of the turbine is = closed=20 and said working fluid is sealed therein, and wherein a cooling = heat=20 exchanger is provided within the rotor to remove heat from the = working=20 fluid near rotor centre, and where the inner ends of the first = passages=20 and the second passages are connected and adapted for = circulation of=20 said working fluid.
  4. The turbine of claim 3 wherein a regenerative heat exchanger = is=20 provided to exchange heat between two streams of the working = fluid, one=20 of the streams being before the heat addition heat exchanger and = another=20 being after the heat addition heat exchanger, and where said=20 regenerative heat exchanger is carried by the rotor.
  5. The turbine of claim 4 wherein said heating heat exchanger = is=20 mounted on the rotor shaft, and said shaft is held stationary.=20



*********************


 US Patent =
3,931,713                    13th January 1976                      =
Inventor: Michael Eskeli


TURBINE WITH REGENERATION=20

ABSTRACT
A method and apparatus for=20 generating power by passing a motivating fluid from a higher = energy level=20 to a lower energy level by compressing the fluid in a = centrifuge-type=20 first rotor and discharging the fluid via nozzles near the = periphery of=20 the first rotor, forwards in the direction of rotation to a second = rotor=20 which is an inward flow type reaction turbine, then passing the = fluid=20 through a regeneration type heat exchanger to transfer heat from = the=20 inward bound fluid into the outward bound fluid, after which the = fluid is=20 cooled in a heat exchanger to its original temperature and is = passed=20 outward again thus completing its cycle.   Heat is added to = the fluid=20 near the periphery of the second rotor, or the heat may be added = near the=20 periphery of the first rotor, or both.   Additionally, the = fluid may=20 be supplied to the unit from outside source, and returned to such = outside=20 source, and the cooling may thus be eliminated from the unit. =  =20 Further, the fluid entering from an outside source may be at an = elevated=20 pressure.   The fluids used may be gaseous, which is normal = for a=20 closed type unit, or they may be liquids at entry for the open = type unit.=20


US Patent References:
2,490,064 = Thermodynamic=20 Machine - Dec 1949 - Kollsman
2,514,875 U-passage Gas Turbine - = July=20 1950 - Kollsman
2,597,249 Thermodynamic Engine - May 1952 -=20 Kollsman
3,236,052 Closed-cycle Gas Turbines - Feb 1966 -=20 Guin
3,530,671 Regenerative Air Turbines - Sep 1970 -=20 Kolodziej


This application is a continuation-in-part=20 application of "Turbine with Dual Rotors," Ser. No. 405,628, filed = 10/11/73, and uses material of a previous U.S. Pat. No. 3,834,179, = "Turbine with Heating and Cooling".


BACKGROUND = OF THE=20 INVENTION
This invention relates generally to devices = for=20 generating power in response to a fluid flowing from a higher = energy level=20 to a lower energy level passing through a turbine for generating = the=20 power.

There have been various types of turbines = previously, in=20 some of which a fluid is accelerated in a single or multiple = stationary=20 nozzles and then passed to vanes mounted on a rotating rotor = wheel, where=20 the kinetic energy contained by the moving fluid is converted to = power by=20 deceleration of the fluid.

These conventional turbines = normally=20 have a high energy loss due to fluid friction, especially between = rotor=20 vanes and the fluid where the velocity differential is usually = large.=20 Also, these turbines often require complex shaped turbine vanes = making the=20 unit costly.


SUMMARY OF THE = INVENTION
It is=20 an object of this invention to provide a turbine for power = generation in=20 which heat is converted to power, in an efficient and economical = manner,=20 and with high thermal efficiency.   It is also an object of = this=20 invention to provide a means for transferring heat from the = motivating or=20 working fluid, which is the first fluid, during its passage from = rotor=20 periphery to rotor centre into the first fluid which is passing = from the=20 rotor centre towards the rotor periphery.   This heat = transfer=20 improves the efficiency of the turbine, and reduces the necessary=20 rotational speed of the rotor, allowing less costly rotor = construction.=20


BRIEF DESCRIPTION OF THE = DRAWINGS




F= ig.1=20 is a cross section of one form of the device, and



F= ig.2=20 is an end view of the unit shown in Fig.1



F= ig.3=20 is a cross section of another form of the device.



F= ig.4=20 is a detail of rotor nozzles.



F= ig.5=20 is a pressure-enthalpy diagram of the first fluid with working = cycle=20 illustrated for the first fluid.



DESCRIPTION = OF THE=20 PREFERRED EMBODIMENTS



F= ig.1=20 shows a cross section of one form of the turbine. In this form, = the first=20 fluid is sealed within the rotor with a second fluid which = supplies heat=20 to the first fluid, and a third fluid which cools the first fluid, = being=20 circulated from external sources.

The first fluid is = accelerated=20 and compressed within the first rotor, and after discharge from = the=20 nozzles of the first rotor, into the second rotor, where it = receives heat=20 from the second fluid, and after deceleration and expansion the = first=20 fluid passes in heat exchange relationship with the first fluid = flowing=20 outward so that heat is transferred from the inward bound first = fluid to=20 the outward bound first fluid.   Cooling is then provided for = the=20 first fluid to bring the first fluid temperature to an initial=20 predetermined value.

In Fig.1, 10 is the casing, = 11=20 is the first rotor, 12 is the third fluid heat exchanger, = 13=20 is the vane which also serves as a heat exchange member, 14 = is a=20 heat-conductive wall, 15 is a vane, 16 is a nozzle,=20 17 is the second rotor, 18 is the second fluid=20 heat-exchanger, 19 is a vane, 20 is the second-fluid = conduit, 21 is a combined bearing and seal, 22 is a = combined=20 bearing and seal, 23 is a second rotor shaft for the = delivery of=20 power, and for support of the second rotor, 24 and = 25 are=20 supply and return for the third-fluid, 26 is a vent opening = in the=20 casing into which a vacuum source may be connected, 34 is a = dividing wall, 27 are vanes serving also as heat-exchange = members,=20 28 is a first-fluid passage, 30 is a combined = bearing and=20 seal, 31 and 32 are the second-fluid entry and exit = points,=20 and 33 is the first rotor shaft.



F= ig.2=20 shows an end view of the unit of Fig.1 where 10 is = the=20 casing, 11 is the first rotor, 17 is the second = rotor,=20 16 are the first-fluid nozzles, 18 is a heat = exchanger,=20 19 are vanes, 20 is a conduit, 13, 14 and = 27=20 form a heat exchanger for the first-fluid and 23 is the = second=20 rotor shaft.



F= ig.3=20 shows another form of the turbine, where the first-fluid is = supplied to=20 the turbine from outside sources thus eliminating the third-fluid = heat=20 exchanger.   50 is the first rotor, 51, 52 and=20 53 form a heat exchanger for the first-fluid, 55 and = 58 are heating heat exchangers for adding heat to the = first-fluid=20 and may use a second- fluid at the same temperature or at a = different=20 temperature as the heating fluid, 54 are vanes within first = rotor,=20 56 are first-fluid nozzles oriented to discharge forwards,=20 57 is the second rotor, 59 are vanes, 60 is a = conduit=20 for the second-fluid, 61, 62 and 72 are bearings, = 64, 65,=20 69 and 70 are entries and exits for the second-fluid, = 63=20 is the second rotor shaft, 71 is first rotor shaft, = 66 is=20 the base, while 67 and 68 are the exit and entry = points for=20 the first-fluid.



F= ig.4=20 shows a detail of the first-fluid nozzles where 34 is wall = on which=20 nozzles 16 are mounted, 35 is the approximate = direction of=20 leaving of the first-fluid, and 36 indicates direction of = rotation=20 of first rotor.



In=20 Fig.5, a pressure-enthalpy diagram for the first fluid is shown, = with the=20 working cycle for the first-fluid where 80 is the pressure axis = and 81 is=20 enthalpy axis, 82 are constant entropy lines, 83 are constant = pressure=20 lines, and for the cycle, compression with heat removal, or = without heat=20 removal, occurs from 84 to 85, heat is added from returning = first-fluid=20 from 85 to 86, further compression is from 86 to 87, then = expansion from=20 87 to 88 and 89, and heat removal to the first-fluid from 89 to = 84, thus=20 completing the cycle. Heat is normally added between 87 and 88, = from the=20 second-fluid. The heat addition between 85 and 86, and heat = removal=20 between 89 and 84 may be at constant or varying pressure as = desired;=20 pressure may be varied conveniently by increasing or decreasing = the=20 diameter of the first-fluid to first-fluid heat exchanger, making = the heat=20 exchanger tapered.

In operation, the rotors are filled to = a=20 desired pressure with a suitable first-fluid, and the first rotor = is=20 caused to rotate. The first-fluid is first compressed with heat = removal,=20 and then is passed in heat exchange relationship with the inward = bound=20 first-fluid with addition of heat, and after this the first-fluid = is=20 further compressed and accelerated and after this compression, the = first-fluid is passed via nozzles mounted on the first rotor = forwards in=20 the direction of rotation, after which the first fluid enters the = second=20 rotor=92s inward extending passages for deceleration, with heat = being added=20 to the first-fluid in the second rotor inward passages for = reduction of=20 density of the first-fluid. After passing inwards and = decelerating, the=20 first-fluid is passed in heat exchange relationship with the = outward bound=20 first-fluid, and after that, the first-fluid may be further = decelerated,=20 and then the first-fluid enters the outward extending passages of = the=20 first rotor thus completing the cycle.

The operation of = the open=20 turbine of Fig.3 is similar to that described, except that the = first-fluid=20 is supplied from external sources, and is then returned to said = external=20 source, with cooling then being deleted.

The work input to = the=20 first rotor is the work required to accelerate the first-fluid, = and the=20 work output by the second rotor is the work of deceleration = received by=20 the second rotor. The work output by the turbine is the work = differential=20 of these two rotors.

The rotational speed of the second = rotor may=20 be higher than the rotational speed of the first rotor. To provide = for=20 inward flow of the first fluid within the second rotor, the fluid = density=20 is reduced by adding heat to the first fluid either within the = second=20 rotor, or also within the first rotor.

The addition of = heat from=20 the inward bound first fluid to the outward bound first fluid = increases=20 the temperature of the first fluid during latter part of = compression and=20 during expansion, and thus has the effect of improving the thermal = efficiency of the turbine. Also, another effect is the reduction = in the=20 needed rotational speed for the turbine rotors, thus reducing the = required=20 strength for the rotors, and making the rotors more economical to = make and=20 operate.

Working fluids for this turbine are usually gases = for the=20 first-fluid, and liquids for the second and third fluids. Gaseous = second=20 and third fluids may be also used, and the first-fluid may be a = liquid in=20 some instances. Also, the first fluid may undergo a phase change = within=20 the turbine, if so desired, when using a suitable fluid. = Applications for=20 this turbine include normal power generation service using various = heat=20 sources.

The first rotor shaft and the second rotor shaft = are=20 normally connected via a power transmission device so that a part = of the=20 power produced by the second rotor is used to rotate the first = rotor.=20 Starting of the unit is by a starting device. The vanes of the = rotors may=20 be made curved if desired. In many instances, the first rotor = vanes may be=20 curved backward to increase compression of the first-fluid, and = the vanes=20 of the second rotor may be also curved, to improve performance, = and to=20 suit the design and fluid selected. In this connection, the fins = for the=20 heat exchangers are considered to be vanes.

The = pressure-enthalpy=20 diagram shown in Fig.5, is approximate only. This diagram may be = varied,=20 depending of the amount of heat added in the second rotor, or in = the first=20 rotor, and depending on the specific location of the second fluid = and=20 third fluid heat exchangers. In particular, heat may be added to = the=20 first-fluid during expansion to make the first-fluid actually = increase in=20 temperature; this will normally improve the overall thermal = efficiency of=20 the turbine. Also, heat removal by the third fluid may be = conducted in=20 places other than that shown in Fig.1, as desired.

It = should be=20 also noted that the heat addition to the first-fluid may be from = sources=20 other than the second fluid, and similarly, some other means may = be used=20 to cool the first-fluid other than the third fluid. Such heating = sources=20 may include electricity, or other rotors mounted in proximity to = this=20 turbine; these will not change the spirit of this invention. =

The=20 heat exchanger mechanism for transferring heat from the inward = bound=20 first-fluid to the outward bound first-fluid can also be located = within=20 the second rotor, and also the entry and exit for the first-fluid = into the=20 turbine may be within the second rotor. Such arrangements are not = shown=20 specifically in the drawings since they are considered to be = within the=20 capabilities of a skilled designer, in view of the descriptions = given=20 herein.


CLAIMS
  1. A turbine for generating power and comprising:=20
    1. means for rotatably supporting first and second rotors;=20
    2. first and second rotor shafts journaled in said support = means for=20 rotation;=20
    3. first rotor means provided said first shaft for rotation=20 therewith, said first rotor means having a first passageway = for an=20 outward bound first fluid, with said first passageway = communicating at=20 its downstream end with means for accelerating said first = fluid=20 forwardly in the direction of rotation of said first rotor = means and=20 for passing said first fluid into said second rotor means, = said first=20 rotor means further having a second passageway for inbound = first fluid=20 in close proximity to said first passageway and in = communication=20 therewith near the downstream end of said second passageway, = and heat=20 exchanger means intermediate said first and second passageways = for=20 adding heat to said outward bound first fluid from said inward = bound=20 first fluid;=20
    4. second rotor means mounted on said second shaft for = rotation=20 therewith, said second rotor having further passageway means = for said=20 first fluid, said further passageway means being in fluid=20 communication at its upstream end with said first rotor = accelerating=20 means, and in fluid communication at its downstream end with = said=20 first rotor second passageway.

  2. The turbine of claim 1 wherein a heating heat exchanger is = provided=20 for adding heat to said first fluid downstream of said first = passageway.=20
  3. The turbine of claim 1 and including heat removal heat = exchanger=20 means provided downstream of said first rotor second passageway = means.=20
  4. A method of generating power comprising the following steps: =
    1. compressing a outward bound motivating fluid within a = first=20 passageway of a rotating first rotor;=20
    2. accelerating and discharging said motivating fluid into a=20 passageway of an independently rotating second rotor;=20
    3. passing said motivating fluid from said second rotor = passageway=20 into a second passageway of said first rotor; and=20
    4. effecting heat transfer from said motivating fluid in said = first=20 rotor second passageway to said motivating fluid in said first = rotor=20 first passageway.

  5. The method of claim 4 and including the following additional = step:=20 returning said motivating fluid from the downstream end of said = first=20 rotor second passageway to the upstream end of said first rotor = first=20 passageway.
  6. A method of transferring heat within a rotor, comprising the = following steps:=20
    1. driving an outward bound motivating fluid within a first=20 passageway of said rotor;=20
    2. effecting a heat transfer between an outside source and = said=20 motivating fluid;=20
    3. causing said motivating fluid to be inbound within a = second=20 passageway of said rotor, proximate to said first passageway; = and=20
    4. effecting heat transfer between said motivating fluid in = said=20 second passageway and said motivating fluid in said first = passageway.=20


Much of this Michael Eskeli = information is=20 taken from the web = site, of=20 Scott Robertson, with his kind permission. =



Self-Powered=20 Water-pump Generator.
Repeated here from Chapter 2, a = device which=20 needs to be in this list of self-powered devices is the ultra = simple=20 water-jet generator. There is a video on Google which shows a = self-powered=20 electrical water-pump driven, electrical generator here.=20

This is a very simple device where the jet of water from = the pump=20 is directed at a simple water-wheel which in turn, spins an = electrical=20 alternator, powering both the pump and an electric light bulb,=20 demonstrating free-energy. What is of particular note is the utter = simplicity of this device. It uses off-the-shelf parts almost = exclusively=20 and can be constructed by almost anyone.

It should be = noted that=20 the implementation shown in this video uses the most basic of = turbine=20 blades which must have a very low efficiency, and yet the output = power=20 generated is well above the level needed to sustain its own = operation.=20 Given well shaped conventional turbine blades of much higher = efficiency=20 would appear to raise the performance further, while one would = think that=20 using a Tesla Turbine with its simple discs should give a really=20 spectacular performance. However, this may very well not be the = case a the=20 irregular, pulsed drive of the wheel will be leading-out = additional energy=20 as in the case of the Chas Campbell flywheel and the John Bedini = flywheel.=20 As it is, with its present form of construction, this device is = already=20 capable of producing additional power able to run other pieces of = standard=20 mains equipment.



This= is=20 clearly a development platform and it would benefit from having = the areas=20 which contain water, fully enclosed, and the electrical diversion = from=20 mains power to the output alternator operated by a switch. =




Init= ially,=20 the generator is got up to speed, driven by the mains electrical = supply.=20 Then, when it is running normally, the mains connection is removed = and the=20 motor/generator sustains itself and is also able to power at least = one=20 light bulb. The generator output is normal mains current from a = standard=20 off-the-shelf alternator. Power generation could hardly get any = more=20 simple than this.


Arthur Cahill and John Scott =  =20 have patented a heat-pump system which draws heat energy from the=20 surrounding environment and uses that energy to produce mechanical = and/or=20 electrical energy for powering a household. Why most people have a = refrigerator they are generally not aware that it is a heat-pump = and moves=20 three times as much heat from inside the refrigerator compared to = the=20 necessary input power (COP=3D3 but could be up to COP=3D11 when = used=20 differently).

This heat-pump system appears to run without = any=20 form of energy input, but the energy comes indirectly from the sun = heating=20 the surrounding environment and there is no magic involved. Mind = you, when=20 the system runs and provides power, generally, without the need = for any=20 fuel, the user can be forgiven for thinking of it as a fuel-less = or=20 self-powered system even though strictly speaking, that is not the = case.=20 The inventors have made allowances for unusual conditions where=20 environmental conditions can't provide the temperature difference = needed=20 to make the system operate as intended. A liquid or gaseous fuel = is=20 provided along with a burner to provide the heat difference if = those=20 conditions are encountered.

Here is an extract from their = patent:=20
 
Patent US 4,309,619 5th January 1982 Inventors: = Arthur Cahill & John Scott
SOLAR ENERGY = SYSTEM=20


ABSTRACT
A dynamic, = self-sustaining and=20 self-perpetuating device for the production of motive force by = combining=20 cryogenic and thermodynamic principles into one system, keeping = the=20 systems separated, two open to atmosphere, the other closed, = sealed,=20 pressurised and using special compounded fluids, which when = alternately=20 exposed to the heat of atmospheric temperature, then, to the = coldness of a=20 liquid or air-cooled condensor, first evaporates, then condenses. = Rapid=20 expansion during evaporation produces a high pressure vapour which = operates an engine and a generator, which are an integral part of = the=20 closed system. Rapid condensation drastically reduces back = pressure on the=20 aft side of the engine, and the engine operates on the difference = between=20 the two pressures, producing electricity, or, the engine can be = used as a=20 direct drive for vehicles or equipment. Built-in safeguards and=20 alternatives are a part of the systems, assuring continued = operation=20 despite adverse conditions.


US Patent = References:
2,969,637	Converting solar to mechanical energy				=
Jan 1961  Rowekamp
3,495,402	Power system							Feb 1970  Yates
3,995,429	Generating power using environmental temperature differentials	=
Dec 1976  Peters
4,110,986	Using solar energy carried by a fluid				Sep 1978  Tacchi
4,214,170	Power generation-refrigeration system				Jul 1980  Leonard


BACKGROUND OF THE INVENTION

1.=20 Field of the Invention
This invention relates to a = closed-cycle,=20 sealed, pressurised, energy producing system, utilising the = sciences of=20 thermodynamics and cryogenics to convert liquid into gas, then = back to=20 liquid.

2. Description of the Prior Art
There = is no=20 exact prior art, as cryogenics have been used primarily for air=20 conditioning and refrigeration purposes, and thermodynamic efforts = have=20 been directed in the area of low efficiency ocean thermal energy=20 conversion systems. A few attempts have been made to combine some = form of=20 cryogenics and thermodynamics, without notable success, mainly = using sea=20 water for evaporation and condensing. While using no fuel and = requiring=20 little in the area of labour, these ocean thermal energy = conversion=20 systems are of necessity, low pressure systems and require large = sea going=20 platforms to support the huge turbines and heat exchangers which = are=20 necessary to produce reasonable electrical power, resulting in = excessive=20 capital costs for minimal electrical output, since such stations = only have=20 the ability to service a small portion of the populace along the=20 seaboards. None of these contrivances serve or benefit the = populace as a=20 whole, while the whole bears the burden of financing through = taxes, or=20 government grants.

Proposals to heat gases and cool gases = in an=20 endeavour to improve the efficiency of home heating and cooling = systems,=20 have been previously advanced, some operating on the heat pump = principle.=20 All such previous proposals and inventions have had one thing in = common,=20 they all plug into the Utility Company's electric line to obtain = the=20 electricity necessary to run the system.

In cryogenics the = knowledge that certain liquids, when heated, change into a high = pressure=20 vapour, which is the heart of all air conditioning and = refrigeration=20 systems, has been known for many years. Thermodynamics were = pioneered by=20 the 19th century French physicist Nicholas Carnot. Attempts have = been=20 advanced during the years to harness one or the other and = sometimes both,=20 for the purpose of heating and cooling, resulting in the invention = of the=20 heat pump in a much earlier year, but none of the systems yet = devised for=20 use by the general public have been able to operate without the = use of an=20 outside source of electricity, or, fuel, such as oil, or gas fired = boilers, resulting in a considerable consumption of fuel and a = cataclysmic=20 effect on the earth's environment.


SUMMARY OF = THE=20 INVENTION
In accordance with the present invention, = the device=20 will operate in hot sunshine; on cloudy days without sunshine; = during=20 rainstorms; during snowstorms; during changes in temperature from = day to=20 night; during changes in seasons from winter, to spring, to = summer, to=20 fall; when it's cold, even below zero; for the power generated is = that=20 energy produced when a compounded fluid changes form, first to = vapour,=20 then back to liquid, by application of controlled temperatures = within the=20 sealed cycle. Thus, by combining cryogenics and thermodynamics = into one=20 system, keeping the two separated, one open to atmosphere and the = other=20 closed, sealed and pressurised, and by using fluids specifically=20 compounded for the given area, or climate, these fluids, when = exposed to=20 atmospheric temperatures, in accordance with the kinetic theories = of=20 matter, gases and heat, provide the kinetic energy to operate an = engine.=20

The condenser can be either liquid or air cooled, although = for the=20 embodiment shown here, the condenser is air cooled. Generally = speaking,=20 there is up to an approximate 2.5 psi increase associated with = each degree=20 F. of temperature rise in most cryogenic fluids and gasses. = However, using=20 commercially available fluids, here are a few examples:


You = will=20 notice that R-13 at 80=B0 F. produces 521 psi., or 35.4 times = atmospheric=20 pressure and at 125=B0 F. would produce thousands of psi. At 95=B0 = F. R-22=20 produces 185 psi., or a thrust on a five inch diameter piston of = 3,633.4=20 pounds. Even at 30=B0 F., with R-22 a thrust of 583.2 pounds is = obtained.=20 R-13 at 30=B0 F. produces 263 psi. or 5,112.7 pounds of thrust on = a five=20 inch diameter piston. The pressures are there by using the Casco=20 Perpetuating Energy System, utilising proprietary formulated = liquids for=20 the area and temperatures to be encountered. It is not intended = that any=20 of these mentioned fluids will be used in the present invention; = the=20 comparisons being made herein with popular and well known liquids, = for=20 comparison purposes only.


THE = INVENTION
The=20 present invention relates to a device to supply pollution free = power to=20 operate a generator for the producing of electrical power, or, to = supply=20 power as a direct drive to a shaft, transmission, clutch, = differential or=20 the such, the invention being independent of outside sources of = power such=20 as electricity supplied by a Public Utility Company. This is not = to be=20 considered perpetual motion, as will be explained later in the = text.=20



Prop= rietary=20 liquids, specifically compounded to produce the desired results in = a given=20 area, or climate, under pressure in the reservoir to keep them in = a liquid=20 state, will, when directed through tubes exposed to atmospheric=20 temperature, change from a liquid state into a gaseous state (from = here on=20 referred to as steam), such conversion resulting in tremendous = expansion,=20 thus producing high pressure steam with which to drive the engine, = or=20 turbine.

It is a general object of this invention to = provide a=20 pollution free device for public utilisation, that will produce = electrical=20 power or, direct drive power. One object is to produce electrical = power=20 with which to heat, cool, cook, run electrical appliances and = light a=20 home. Another object of the invention is to provide industry with = a=20 pollution free means to not only heat, cool and light factories, = but to=20 supply electrical or direct drive power with which to operate = factory=20 equipment. A still further object of the invention is to provide a = pollution free source of power to propel cars, trains, trucks, = buses,=20 equipment, steamships, aeroplanes, and other forms of = transportation,=20 without the use of fossil fuels as the primary power source. It is = also an=20 object of the present invention to provide the means whereby = individuals=20 can produce electrical power for their own use, and as a small = power=20 production, sell their surplus electrical power to the local = electricity=20 utility company. A further object of the invention is to provide a = self-sustaining, small apparatus, that provides ample power from = the=20 engine to operate a car or other conveyance, or to supply = sufficient=20 electrical power to a home or factory, without having to plug the=20 apparatus into a Public Utility electrical supply. =


BRIEF=20 DESCRIPTION OF THE DRAWING



Fig.1= =20 is a partially sectioned schematic view of the system:=20

DETAILED DESCRIPTION OF A PREFERRED = EMBODIMENT
In=20 the drawing, Fig.1, the invention is shown in a preferred=20 embodiment for home use. The liquid pump 39, pumps the = cryogenic=20 fluid from the pressurised liquid reservoir 38, into liquid = line=20 40, where the fluid gravity feeds into flash boiler = 8.=20   Pump 39 also prevents back pressure from flash = boiler=20 8 from entering the pressurised liquid reservoir 38, = and=20 since the pressure within steam line 10 and liquid line = 40=20 are equal, the cryogenic fluid gravity feeds down liquid line = 40=20 into steam line 10. The fins on flash boiler 8 are = heated to=20 atmospheric temperature by air stream 4, which converts the = fluid=20 within steam line 10, inside flash boiler 8 into = high=20 pressure steam. To maintain the pressure during the passage of = steam to=20 the engine 15, steam line 10 from flash boiler = 10 is=20 housed inside the oven 9, which is exhausted when necessary = by=20 discharge 12 from centrifugal blower 11. Constant=20 temperature within oven 9 and flash boiler 8 is = maintained=20 by the admission of fresh atmosphere via air stream 4 = passing=20 through the finned flash boiler 8 and up through oven = 9.=20 Centrifugal blower 11 is thermostatically controlled to = exhaust air=20 within oven 9 which has cooled below a predetermined = temperature.=20 Any excess pressure within steam line 10 is by-passed = through check=20 valve 13 and bleed line 14 into the exhaust = collector box=20 18, thus, a pressurised, closed system is maintained, = which, once=20 charged, unless an accident damages or ruptures a line, should not = have to=20 be replenished. Pressure within the exhaust collection box = 18 will=20 be less than the inlet pressure from steam line 10 to = engine=20 15, because the condensor 24 is at a lower pressure, = as is=20 steam return tube 19, than psi. input to engine 15 = from=20 steam line 10, thereby creating a suction on the back of = the=20 exhaust collector box 18.

Airstream 29, = which has=20 been cooled by evaporator cooler 27, flows over the finned = surfaces=20 of condensor 24, instantly lowering the temperature of the = steam=20 within condenser 24 below a predetermined condensation = point, thus=20 turning the steam back to a liquid, such conversion and instant = reduction=20 of volume within condenser 24 causing a pressure reduction = at the=20 back of engine 15. This condensed liquid drains down into = liquid=20 coil return 35, where it is immediately pumped into the = pressurised=20 liquid reservoir 38 by liquid pump 36.

While = under=20 pressure in pressurised liquid reservoir 38, the fluid is=20 maintained in a liquid state regardless of exterior temperature, = until it=20 is re-circulated back into the system by liquid pump 39, = through=20 liquid line 40 to flash boiler 8, where it again = converts=20 into steam.

The capacity of evaporator cooler 27 = and=20 packing 28 is sufficient to cool intake air stream = 29 to a=20 predetermined temperature below atmospheric temperature at any = given time,=20 even with humidity rise at night, or during rainstorms, or just = during=20 high humidity weather. This temperature differential is maintained = as the=20 atmospheric temperature rises and falls, with an anti-freeze = liquid being=20 added to the water in the evaporator cooler when temperatures drop = below=20 32=B0 F., to keep it from freezing.

Additional warm air to = augment=20 air stream 4 is obtained by directing the warm air exhaust=20 collected in hot exhaust air collector 26, by centrifugal = blower=20 41, through T-assembly 42. Air flow through = T-assembly=20 42 is directed and controlled by the warm air control = mechanism=20 44, which regulates flow-damper 43 to either exhaust = through=20 exit 45 into the atmosphere, or alternatively, recirculate = air flow=20 29 through restricted-T 42, thereby compressing and = further=20 heating air flow 29 before injecting it through flash = boiler=20 8. Warm air control mechanism 44 also controls fan = 1=20 and louvers 3, selecting the optimum heat from either = T-assembly=20 42 or variable-Venturi 2, to perpetuate the system.=20

The evaporator cooler 27 has an inlet water pipe = 34=20 which supplies cold water from the normal house water supply, or = well,=20 (neither shown). The bottom water reservoir 33 is kept at a = constant level of water by float valve 32. The water is = pumped by=20 pump 31 up tube 30 into the top water reservoir = 25,=20 where it runs through the perforated bottom of reservoir 25 = down on=20 to the packing 28, keeping packing 28 constantly = wet, which=20 cools air flow 29 as it is drawn through packing 28 = and over=20 the fins of condenser 24 by the partial vacuum in the hot = air=20 exhaust collector 26, such partial vacuum being created by=20 centrifugal blower 41 exhausting the air from the hot = exhaust air=20 collector 26 slightly faster than air flow 29 can = replace=20 it.

As long as there is warmer air on the flash boiler = 8=20 side of the system than the cooler condensor 24 side of the = system,=20 this device will continue to operate and produce electricity = and/or power.=20 The heat recirculating system and the use of three separate, = distinct=20 sub-systems within the system, one sealed, permits the system to=20 perpetuate itself. As mentioned above, this device is not to be = considered=20 perpetual motion, for somewhere in the ranges of temperature = differentials=20 and weather conditions, there may be a no-man's land where the = system=20 could shut down, then the variable venturi 2, in = conjunction with=20 motor and fan 1 and louvers 3, will come into use=20 automatically upon a signal from warm air controller 44 and = 12 voltage controller 23, and be used for a period = of time.=20 Motor and fan 1 forces an air stream 4 upward = through the=20 variable Venturi 2, with air stream 4 controlled by = warm air=20 controller 44 and 12 volt controller 23, adjusting = louvers=20 3. As air stream 4 is forced through the restriction = of=20 variable Venturi 2, air stream 4 is compressed as it = funnels=20 up the narrowing walls of the variable Venturi 2, such = compression=20 causing the air to heat, thus overcoming possible deadlocked or = identical=20 temperatures between the condensor 24 and air flow 4. This slight=20 temperature rise in air stream 4 will enable the system to = perpetuate=20 itself until the atmospheric temperature itself changes enough to = permit a=20 continued operation. Since fan and motor 1 is run by = battery power=20 from 12-volt supply 23, even though the batteries are = constantly=20 being charged during operation, the batteries may become exhausted = because=20 of an extended time the fan and motor 1 are run, then, or, = if for=20 any other reason the system starts to run down, a small burner = 7,=20 operating on liquid or gaseous fuel 6, through line = 5 and=20 valve 48, is ignited by spark mechanism 47 and = supplies the=20 heat necessary to support and perpetuate the system until = atmospheric=20 temperature and condensing temperature permits the system to = operate=20 normally. Fired clay heat retainers 46 are arranged on the = grate=20 within burner 7, to retain heat.

The cryogenic = system is=20 charged by filling with liquid under pressure through fill pipe = 37.=20 Re-charging, if necessary, is done the same way. Engine 15 = turns=20 drive shaft 16, which turns generator 17, producing=20 electrical power (110V or 220V) via electric control system = 20=20 which passes the electricity into three channels: =

One: To=20 12-volt controller 23, to run the electrical parts of the system = and keep=20 the batteries charged.
Two: To the house 22, to supply = the=20 electricity with which to cook, run appliances, light, heat and = cool the=20 home.
Three: All remaining electricity is channelled = through=20 utility meter 21 into a local utility company's electrical line = for sale=20 and use elsewhere.



Patrick Kelly
engpjk@yahoo.co.uk
http://www.free-energy-info.c= o.uk/=20 =

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