TITLE OF INVENTION "MACHINES RUNNING ON SECRET FUEL"

My invention is completely new, novel, and not obvious and of the greatest strategic importance, since it will make us all self-sufficient, not dependant on anyone abroad and since it can be made bullet proof, shell proof and even bomb proof, can be made to be undetectable on even the most sensitive radar and will have extremely low exhaust temperature, will be highly manoeuvrable and will never run out of fuel when flying over the sea, it will be impossible to shoot down, so high speed is not critical yet high speed versions are available (detailed later in this application).

WHOEVER MAKES THIS INVENTION IN ALL ITS MANIFESTATIONS WILL HAVE THE GREATEST ADVANTAGE?

There will be no real defence against anybody possessing this invention.

This invention is completely non-polluting and when running on fuel detailed later in this application will reverse the greenhouse effect and enable full employment. SO BECAUSE OF MY INVENTION ALL WIN THERE IS NO LOSS.

Anything is highly complex, this invention is particularly complex and really cannot be summarized since there are so many aspects of it that must be contained in this Patent to guarantee absolute security, to ALL, that is most absolutely necessary.

To give the best understanding of my invention, I will gradually add more and more detail. I am sure that all of my invention qualifies as one invention that is completely new and not obvious.

One of the more widely applicable aspects of my invention is the fact that it makes energy extremely low cost. The very core of a thriving economy is low cost energy so this invention could not be more vitally important.

Ever since planet Earth was first created water has been washing a vast amount of elements into the sea including gold, silver, platinum, copper, tin, iron, salt, aluminium and a great deal more.

The energy my invention makes available is so inexpensive that more than 1,000,000,000 tons of gold, silver and platinum dissolved in the sea is now recoverable at

extremely low cost, and so is much else so that we can and must now be self sufficient. Even when the price per ton of recovered material diminishes such vast tonnages are available via my invention that vast profits will be made that must be immediately invested in making my invention as big as possible to gain the economy of really big size, thus saving ALL. This will make vast amounts of extremely inexpensive energy available to all without pollution. Thus saving all the World. I wish to use the profits from this invention to create a vast charity to create most lasting valid jobs to help All the World out of trouble via maximum security. This is the best method of saving all. We can and will spread self-sufficiency throughout the World thus spreading lasting peace solely via absolute security.

Recovering elements from the sea without pollution will produce vast amounts of pure water as a by-product at very little expense so solving the Worlds fresh pure water problem, and also replacing conventional surface mining so saving the World.

Deep coal mines can be re-opened since the low cost energy from my invention can power them and be used to fractionally distil coal to a vast range of products including pharmaceuticals, plastics, soaps, petrol, diesel fuel, lubrication oil, aviation kerosine, paraffin, gas and much more. Long term my invention can easily supply all energy needs, at extremely low cost, on Earth until the sun absorbs the Earth in about 3,000,000,000 years time. Also low cost energy from my machine can help flush out the oil in remain¬ ing oil fields and fractionally distil it to useful valuable products rather than wastefully burning it, this way all benefit the most. So all our precious fossil fuels that would run out soon can now be conserved and converted to raw materials and finished products at extremely low cost and not burnt to waste and pollution, and be endlessly re¬ cycled, thus greatly increasing the value of all we have already.

It is most important that there is no pollution, this will be achieved by using vast amounts of energy available without pollution from my machine to close and balance the elements into harmony from open cycle pollution to closed cycle recycling that eliminates toxic waste and will produce useful inexpensive non polluting durable products.

Inexpensive energy from my machine can be used to make a lot of hydrogen and oxygen from electrolysis of water. Amongst many uses the hydrogen can be heated and passed through

oxidized ores to convert them to the ore plus water vapour. For instance, FE.3 0.4 (iron ore) + heat + 4 H.2 (hydrogen) ^■ FE.3 (pure iron) + 4 H.20 (pure water).

The oxygen from the electrolysis can be used to run the bessemer converter converting impure ore to pure ore then one can pass the hydrogen through the remaining pure ore to remove any excess oxygen thus producing the pure element.

Collecting all the heat and products produced via catalysts will make pure elements out of the original ore.

All this means extremely low cost stainless steel 316 that will endure forever.

Low cost energy makes many viable materials at low cost available. Re-cycled materials can be retrieved via fractional distillation in an inert gas (for example H.20 (steam) CO.2 or nitrogen) so non renewable wood will be saved, thus saving our trees that are our lungs.

The low cost energy from my invention makes it most economic to make pure water from sea water so existing water systems can be continuously topped up so no new reservoirs will be needed thus further saving the environment and cost.

3,500 kw hours per ton are need to make aluminium from bauxite, extremely low cost energy from my machine will make this immensely important substance plentiful and a perfect substitute for wood both in its own right (on its own) and since plastic simulations of wood do not like stress, aluminium is an ideal reinforcing material to combine with plastic, thus making it totally uneconomic to use wood so saving trees from ever being hurt. EXTREMELY LOW COST ENERGY FROM MY MACHINE WILL ENABLE FULL EMPLOYMENT AND SELF- SUFFICIENCY. l/12th of the Earths crust is aluminium, so there is a vast amount of it that can now be economically retrieved from the sea. With low cost energy good glass can be made from sand inexpensively. So we can build low cost greenhouses on set aside land heated and lighted by low cost energy from my invention and save the vast amount of money and resources we spend importing food.

Some of the gold we retrieve from the sea we can build up our gold reserves with and the beauty of self-sufficiency is that our currency will never need support because we will not be importing anything except free sea water.

With some of the precious metal retrieved from the sea we can pay of the debts of the very poorest countries directly thus eliminating corruption and help them grow their own food (rather than cash crops for export that do not really help them).

With low cost energy from my machine deserts can be irrigated and cultivated, pollution eliminated and there can easily be more than enough for everybody enabling us to plant many millions of trees and other plants further reducing our CO.2 levels in the air.

Using inexpensive heat from my machine and the correct catalyst CO.2 from the atmosphere can be separated out to carbon and oxygen. The oxygen can be released to atmosphere to enrich the air and for many other uses.

The carbon can be used to make carbon fibre as a structural material, carbon brakes, electrical brushes, carbon black for tyre manufacture, safe black paint, and many other uses, for instance in arc lamps. Thus the Greenhouse effect of CO.2 in the atmosphere will be reversed. CO.2 can be concentrated in Greenhouses to aid food production.

One of the most efficient uses of my machine is to convert salt water to inexpensive, plentiful convenient energy, plus essential raw materials, and pure water. THIS IS UNIQUE, NOVEL, NEW, NOT OBVIOUS AND THERE IS NO TECHNICAL PRECEDENT YET I HAVE PROVED IT WORKS.

One of the most accessible sources of salt water is the sea that covers approximately 4/5ths of the surface of planet Earth. If one evaporated all the water from the sea the solids remaining would be of a mass greater than the whole of Europe to a depth of one mile. That is all extremely valuable material. The ratio of salt to water around Britain is between 35 and 36 parts of salt to 1,000 parts of water. To remove the pure water to concentrate the salt for use in my machine one has to pass the salt water through a vessel in which the pressure is greatly reduced thus greatly reducing the boiling point of the salt water, heat from the exhaust of my machine via a refrigeration circuit and heat exchangers is used to assist the evaporation of the pure water from the salt. More detail is given later in this Application.

I have successfully burnt salt (sodium chloride) in air at atmospheric pressure that gives off a lot of useful heat and no pollution.

At higher pressure and temperature the combustion is even more efficient. The process of this part of my machine is air + sodium chloride useful heat + oxidized sodium chloride. The beauty of this reaction is no CO.2 is produced.

Over a few years the oxidized, sodium chloride, by virtue of being exposed to radiation from the Sun, will release the oxygen into the air and revert to sodium chloride and be washed to the sea by rain and thus be able to flow to my machine.

The level of salt in the air will never be high and on Guernsey surrounded by sea I have proof plants have good resistance to salt in the air. This is really a long term use of solar energy that will never run out. The pure water from my invention will be the lowest cost pure water, ideal for drinking, domestic use, irrigation, and a vast number of industrial uses.

The extremely low cost and endless plentiful energy from my machine makes tanks that can fly overseas for rapid deployment and over obstacles certain, also my machine can manifest itself as aircraft that can keep deployed and airborne over the sea forever, crews could be transferred in the air by virtue of my aircraft applications hovering ability, detailed later, similarly surface ships and submarines could remain deployed forever providing formidable ability. This will make it safe to build floating cities out of material retrieved from the sea. These would be immune from earthquakes, and be streamlined (of low wind drag) with many examples of my machine providing vast amounts of power to propel them through any wind and big enough to more than withstand any weather conditions, security comes first so any fabrics can be made from fire proof woven glass fibre from sand energised by my machine. So the whole of my machine will be quite safe, the only fire will be in its combustion chambers.

Large quantities of slightly refrigerated water can be pumped over the surface of any structure curved for uniform distribution using extremely low cost energy from my machine thus causing any heat seeking missile to veer away to a warmer background.

Page 2 of Drawings, Fig. 2, shows how the external surface of my machine is best protected by making a sandwich of different materials. Outermost is a layer of the most absorptive rubber, it must be thick enough to absorb all

light and radar and laser and ultra-sound signals and not so thick that bullets "dig in". The next layer in is a high resilience rubber to deflect bullets, shells and bombs. The next layer in is the hardest available steel which must be flexible. The next layer in is high resilience rubber to eliminate shock waves and cope with differential expansion. The next layer in is a thick layer of aluminium to spread the stress most efficiently. Thick (foamed or honeycomb) aluminium is ideal, carbon fibre is not suitable for this because it shatters on impact.

If a high velocity armour piercing shell is incident on the structure (Page 2 of Drawings, Fig. 3) the rubber layers will absorb its shock waves and deflect its energy as much as possible, if despite this the shell penetrates the steel layer, because the next layer in is much softer aluminium (Page 2 of Drawings - Fig. 4) the shell will experience an instantaneous turning couple (higher resistance steel on top side of shell) (lower resistance aluminium on bottom side of shell) so the shell will exit without going further into the structure (Page 2 of Drawings - Fig. 5) thus eliminating suffering.

The overall structure should be so arranged that ordinance incident on it can only exert a glancing blow (low angle of approach) as in Page 3 of Drawings - Fig. 6a.

Fig. 6a on Page 3 of Drawings also minimises radar and other reflections. Fig 6b, Page 3 of Drawings, is aircraft head on. (as this description progresses I will add progressively more detail).

All the following are on Page 3 of Drawings: Fig. 7 is a tank side on, the rearward inclining tube from the turret is the only air inlet to minimise the angle of incidence to the vents of any incoming ordinance with a spring steel wire mesh screen covering it to bounce away molotov cocktails without breaking them. The gun will tend to be facing the origin of any incoming ordinance so the air vent will incline away from the incoming ordinance. Fig. 8 is a tank head on. Fig. 9 is a submarine side on. Fig. 10 is a submarine head on. It is important to always face the enemy to minimise frontal area. Fig. 11 is a ship side on. Fig. 12 is a ship head on.

All air inlets must be horizontal louvres at the highest points of the structures. All exhausts are horizontal under the structures with very strong flap valves to withstand blast except the ship and submarine which have the exhaust

on top behind the inlet. More details later.

Extremely low cost energy from my invention makes re-cycling economic and sewage can be combusted in hot air giving useful heat via heat exchangers and no pollution since the CO.2 from the combusted sewage can be re-cycled via a catalyst to carbon and separate oxygen so the overall effect of my machine is no pollution.

It is most important to realize that externally thermally insulating my invention is most necessary in order to make maximum use of the energy my invention makes available.

In addition, all drag in the system must be minimised by having a smooth finish in all the tubes, vessels and heat exchangers must be as big a bore and size as possible. All the pumps must be most efficient. If the highest practical efficiency of insulation and operation is not achieved this machine will not function at its best. The highest pract¬ ical immediate efficiency of insulation and operation will be achieved. This machine correctly utilized will get us all out of trouble to a pure future forever. It could not be more important.

There is a vast amount of detail to come in this Application. I will start as simply as I can to give the best overall understanding of my machine. Thank you in advance for your patience, it is most worth it.

With reference to Page 1 of Drawings in this Application shows the overall arrangement of some of one of the versions of my invention. I will illustrate and describe each section in more detail later. Starting at the bottom right- hand side of Page 1 of Drawings:- Any water base fuel extra to the water base fuel in Tank 13 (bottom centre of same page) comes in at 1 (bottom right-hand side of Page 1 of Drawings).

My machine will accept any water base fuel as water containing flammable particles that must be individually small enough to be transported through my machine to combustion to provide overall power and there must be more than enough particles per unit volume of water to provide surplus power.

My machine will run on any combustible substance of more than adequate quantity. So if a tank version of my machine was surrounded it could run on surrounding vegetation fluidized in any available water and thus escape and win by

vertical take off. Any available water base fuel that contains particles small enough to make it to combustion in my machine and with more than enough particles per unit volume of water they are in to provide surplus power will go into 1, bottom right-hand corner of Fig. 1, Page 1 of Drawings included in this Application.

The most ideal fuel to pass into 1 (bottom right-hand side of Page 1 of Drawings, Fig. 1) IS SALT WATER. We will trace it through my machine. The salt water next passes vertically up to 2, the inlet port of the vane pump that greatly pressurises the salt water through Port 26, rising from 26 through (Condenser 28, 27, 44, 43) to 45, 46, 47 and 48 the salt water gains heat that has come from combustion of the salt in Turbine Rotor 62, 62 (centre of Page 1 of Drawings). The hot exhaust gas leaves Rotor 62, 62 horizontally in ducting that is cooled by refrigerant. To the right of Rotor 62 hot exhaust gas passes in ducting cooled by refrigerant by the hot gas passing from 35 to 34. To the left of Rotor 62 hot exhaust gas passes from 37 to 36 in ducting cooled by refrigerant. The refrigerant comes in coldest at 34 (right-hand side - middle of Page 1 of Drawings) then moves peripherally around the exhaust ducting to 36 (left-hand side) and then spirals in the ducting into 37 and then around Rotor 62 to 35. The now hot refrigerant passes from 35 (on the immediate right of Rotor 62) up to 38 into inlet port of the vane pump at 39 then sucked by the Rotor moving in direction 41 to be pressurised through Exhaust Port 42 which pushes the hot refrigerant up to 43. From 43 the hot refrigerant gives its heat to the pressurised salt water flowing from 1 to 46 (bottom right- hand side of Page 1 of Drawings to top right-hand side) by the refrigerant flowing from 43 via 44 to 28 and 27, then the now cold high pressure refrigerant flows to 29, (the inlet port of the next vane pump that uses the high pressure cold refrigerant to push vane 32 about Rotor 31 in direction 30 to Port 33).

Rotor 31 helps to drive the rest of the pump system, the mechanism for this is not shown on this page, it is shown later in this Application. The refrigerant leaving exhaust Port 33 goes to very low pressure, this makes it extremely cold whereupon it flows up to 34 which takes us to where I started describing this really important refrigeration circuit. This refrigeration circuit guarantees the exhaust from my machines will be colder than surrounding air, so any heat seeking missiles aimed at my machines will veer away to warmer background.

This refrigeration circuit described above gives us hot high pressure salt water at the Inlet Port 48 of the vane pump at the top left-hand side of Page 1 of Drawings.

The salt water must be highly pressurised between the first pump it meets and the second pump to prevent it boiling and to keep all its contents in the water. When the high pressure salt water enters Inlet Port 48 (top left-hand side - Page 1 of Drawings) it pushes Rotor 49 in direction 50 helping to drive the other pumps (method shown later in this Application). At Exhaust Port 51 Evaporators 52, 53 (big chamber to immediate right of 51) must be immediately next to Exhaust Port 51 so that when the pressure drops at Exhaust Port 51 no elements precipitate out but are immediately carried away by the salt water whilst it rapidly evaporates surplus water because of the extremely low pressure in Evaporator 52, 53.

The salinity of sea water around Britain is about 35 parts of salt to 1000 parts of water, so a lot of water has to be evaporated from the salt water in the Evaporator using minimal amounts of energy. This is done by keeping the pressure in the Evaporator as low as possible. The lower the pressure the greater the evaporation. So via low pressure in the Evaporator 52, 53 maximum heat obtained from the exhaust from Rotor 62 is used to evaporate large amounts of water. In Evaporator 52 the salt water flows from 51 to 73 getting stronger concentration as pure water evaporates through the communicating oraface, (with a raised rim around it to stop pure water flowing back) up to 53. From 53 the pure water flows mainly as vapour to the vane pump responsible for the extremely low pressure in 52, 53 by flowing through Inlet Port 54 and then by flowing around Rotor 55 in direction 56 it is greatly compressed through Exhaust Port 57. This compresses the water vapour to a liquid at high temperature that is forced down the tube 58, 59. Just where tube 59 meets tube 60 there is a T-junction allowing the pure water to flow both to tube 80 and down tube 60, following the flow along tube 80:- Do not be distracted by Tube 92 crossing it, Tube 92 does not communicate with tube 80. Follow Tube 80 to where it feeds the water to a Valve 161 controlled by ballcock 162 that maintains the level of the fresh water around Anode 81 and via Flap Valve 104 (to prevent hydrogen meeting Oxygen outside combustion chamber in Rotor 62) to Cathode 89. Catalyst (never used up) diluted sulphuric acid is used between 81 and 89 to aid electrolysis.

Other than through the pure water plus sulphuric acid, any

path between Anode 81 and Cathode 89 must be electrically insulating (tough glass/ceramic/plastic/glass fibre is ideal) to maximize the electrical flow between 81 and 89 to generate as much Oxygen and Hydrogen as possible to guarantee the hottest flame in Rotor 62, (more details later in this Application).

Dealing with Anode 81, oxygen rises from it, as oxygen pressure builds up the water/sulphuric acid level at Float 94 will sink so slide Valve 82 will slide to the right to open position shown on Fig. 1 (Page 1 of Drawings). When oxygen pressure falls water/sulphuric acid level will rise so Float 94 will rise, shutting Slide 82 by it moving to the left until the oxygen pressure rises again.

When oxygen is passing through the hole shown in Slide 82 it goes into Port 84 above Slide 82 with air direct from atmos¬ phere coming from 83 (just to the right of and below 84). Just above 84 Rotor 85 rotates in direction 86 causing the Vane near 86 to compress the Oxygen + air through Outlet Port 87 and then up to Tube 88 into the centre of the co- axil tubes going up into Rotor 62. (More details later in this Application). Above Cathode 89, (to the left of Anode 81), a similar process to that already described for the oxygen from Anode 81 happens to the Hydrogen from Cathode 89. The Hydrogen rises causing Float 95 to go down causing Slide Valve 90 to open causing Hydrogen to rise in Tube 91 into Rotor 62. (More details later in this Application). Please go to Tube 60 entering Rotor 61, (10 cms from top of centre of Drawing Page 1/9, Fig. 1) near junction of Tubes 59, 60 and 80.

The pure water flows through Tube 60 down the core of the integral (Motor 61 for starting, then Dynamo when up to operating speed), and then into Turbine Rotor 62.

The beauty of this high pressure, high temperature water is that it is cool enough to stop the Motor/Dynamo 61 and Rotor 62 melting, yet hot enough and at more than high enough pressure to be injected just down stream of the combustion flames in the Rotor, (shown later in this Application), to absorb the heat of the flames to convert the heat to thrust and then pass the remaining heat back into my machine by condensing on the refrigerated ducting 35, 34, 37 and 36 thus maximum conserving energy. The actual concentrated salt combusting in compressed air in the Rotor 62, (shown later in this Application), provides the prime mover (overall surplus power).

Returning our attention to Evaporator (52, 53,) the salt water concentrates as it evaporates off pure water as it travels along the bottom of 52 from 51 to 73, the fluid level emanating from 73 activates Float 74, this moves the arm the Float 74 is connected to, to pivot about 75, this controls Rehostat (variable resistance) 76. If level 73 rises, Float 74 rises, so variable resistance 76 diminishes, this will speed up Rotor 77 moving in direction 78, (just below 75). The above indicates Rotor 77 is thus electric¬ ally driven. This description will show Rotor 77 is the sole electrically driven pump shown on Page 1 of Drawings.

If level 73 falls this will increase resistance 76 so that Rotor 77 moving in direction 78 will slow down thus returning level 73 to datum position. So we have hot concentrated salt water flowing from 73 through Inlet Port 79 around Rotor 77 in direction 78 that pressurises the concentrated salt solution through 92 (please follow 92), this prevents further evaporation until the combustion chamber in Rotor 62 is reached. Pressurising the hot concentrated salt water through Tube 92 also prevents any elements precepitating out of solution and transports the salt solution (please follow Tube 92). The hotter the near saturated salt solution is the more salt it will carry in solution. An electrical current is passed through Tube 92 (onwards to Rotor 62) to keep the salt in the water by heating. Tube 92 must be an electrical conductor. Following 92 in the direction of the arrows one gets to Flap Valve 71 that allows the concentrated salt water through to co-axil Tubing 72 into Rotor 62.

To the left of co-axil Tubing 72 there is a Tank 64 for any non-water base fuel, (oil base fuel and other base fuels). The fuel is poured in if a liquid, placed in if a meltable solid, (i.e. fat and/or vegetable oil), and passed in via gas tight tubing if an inflammable gas, (all through 63, top of Tank 64).

Flap Valve 71 prevents fuels flowing other than directly to Rotor 62. So the widest range of fuels can be burnt simultaneously or singly quite without pollution. The applications of this are endless and can be literalTy~life saving. ^" For example, in a siege situation, and in military situations, mobility means decisive victory to save all to the best; and economically, not tied to one source of power, combined with my machines high efficiency, means prosperity.

Heaters 66 under the Tank 64 melt solids, for example fats, and vegetable oil, and make sluggish liquids more suitable,

for example heavy oil. Just above the outlet of the Tank there is an i peler driven by Motor 65 to keep the fuel circulating in the tank to make it most suitable by heating. The heating of the tank is controlled by the pressure in the tank (more details later in this Application). The hot fuel then flows into Inlet Port 67 around Rotor 68 in direction 69 that pressurises the hot fuel through Exhaust Port 70, this pressure will push Flap Valve 71 to allow the hot high pressure fuel up to 72 and thence up co-axil Tubes to Rotor 62 (more details later in this Application).

This means my machine will run on a mixture of fuels simultaneously. Power generation in a siege would thus be provided, a priceless life saver.

This means when my machine is powering a tank, aircraft or other essential machine in an area that is surrounded by an enemy, it will run on any fuel locally available. This is also of great economic and convenience value to all applic¬ ations. Self-sufficiency is most important, the only way of reducing the cost of living and raising profitability.

If the machine is running on solely water base fuel, Flap Valve 71 will prevent water getting into the non-water base fuel pump.

If the machine is running on solely non-water base fuel, Flap Valve 71 stops non water base fuel going into the water base fuel system.

The remaining system on Page 1 of Drawings that I have not described yet I will now describe: (bottom of Page 1 of Drawings, Fig. 1.), is a system for preparing water base fuel from any available combustible materials, for example newspapers, old telephone books, magazines, any paper material, sawdust, coal dust, soot, dry plant material, tree thinnings, any dry combustible material made of small enough particles to be admitted to the system. The shorter a time the combustible materials are in the system the better, they will burn in the combustion chambers in Rotor 62.

From Fuel Pipe 92 to the combustion chambers in Rotor 62 must be heated by passing an electrical current (maximum) through it, (92), (it must be an electrical conducting material, aluminium or stainless steel 316 is ideal), to the highest achievable temperature thus the combustible particles will vaporize in dry steam thus aiding combustion in combustion chambers in Rotor 62, (more details later in this Application). Any combustible particles small enough

are put in through tank entrance 4 (about 6.5 cms up from bottom of Page 1 of Drawings and 8 cms in from the left-hand side of said page). These combustible particles meet extremely sharp blades 5, rotating at the highest achievable speed driven by Motor 9 underneath tank. Impeller 6 on the same shaft as 5 driven by Motor 9 keeps circulating the water plus combustible particles around Tank 13 thus permit- ing Blades 5 to make endless passes, through any particles in Tank 13. Water plus combustible particles gravitate to 14 near the base of the tank where it gravitates to Inlet 10 where parallel rotating discs driven by Motor 9 (they will not clog) drive the fuel up Pipe 11 to 12 and then to 7 that is a clear glass tube, one must look through the glass at the fuel, if it is too thick add any clean water through 3 (on the left hand side). If the fuel is too thin (not enough particles per unit volume of water) add more combustible particles through 4. If the tank is already full and/or if no more suitable combustible particles are available activate Heating Coil 8, this will evaporate surplus water as water vapour rising above 4, remaining fuel will pour into rotating blades 5 to further reduce combustible particle size. To the right of Tank 13 at the base, prepared fuel gravitates into Inlet Port 15 and flows around Rotor 16 in direction 17 propelled by Vane 18 through Exhaust Port 19, if this fuel from Tank 13 is being used it flows past blow off Valve 20 to Valve 21 which will seal off Inlet 1 from outside the system. Thus fuel from Tank 13 will rise above 1 and will pass into Inlet Port 2 and continue as already described in this Application.

If the fuel from 19 is not needed Valve 21 near 1, (one) will be shut forcing the fuel through blow off Valve 20 up to 22 and 23 and then back to where the fuel pours onto Blades 5, thus reducing particle size and distributing into the tank via Impeler 6.

With reference to Page 4 of Drawings, Fig. 13:- Starting my machine is effected by charging in advance in the factory Gas Sphere 108 with hydrogen under pressure and Sphere 107 with oxygen. Butterfly Valve 105 is shut and non return Valve 112 is shut by sphere pressure. Butterfly Valve 106 is shut and non return Valve 113 is shut by Gas Sphere (107) pressure.

Already in Fig. 14 (centre of Page 4 of Drawings):- Prior to first start up, and before every end of running mode, Butterfly Valve 110 is shut between the sea and [1, (one), from bottom right hand side of Page 1 of Drawings], and Butterfly Valve 109 is open, thus air is sucked around the

system aiding the hydrogen and oxygen to combust in the Rotor 62 when 105 and 106 are opened and 61 is energized as a starter and heaters and ignition are energized in the combustion chambers.

As soon as Rotor 62 is up to speed 61 switches from starter to dynamo to energize electrolysis (that helps keep the sodium chloride fully combusting in Rotor 62) and drive Pump 77. Surplus goes to heaters and then external use. In submarine use the equipment shown on Page 1 of Drawings would be used when the submarine was surfaced to either charge up batteries servicing propulsion when submerged and/or to drive compressors to run on compressed air drive when submerged and/or silent running and/or generate electrolysis of pure water to make compressed hydrogen in one tank and compressed oxygen in the other tank to combust to drive a steam turbine when submerged/silent running that would exhaust to a condenser that would then evacuate itself of pure water that could be pumped out under water. Thus providing great submerged/silent running range and speed/ manoeuyrability. All other pumps are driven by mechanical link to 61 for efficiency, as shown on Page 5 of Drawings.

77 (shown on Page 1 of Drawings - Fig. 1 -) has to drive via fluid level control 74, 75, 76 controlling its drive motor voltage.

Shown on Page 4 of Drawings the speed of Rotor 62 is controlled by Butterfly Valves 105 and 106, one cannot put a Butterfly Valve in 72 without a blow off Valve because salt water is virtually incompressible, the Butterfly Valve would sheer away, so when 62 is at maximum completely safe velocity Vent 72 to external use and/or back to correct fuel tank when the Rotor 62 speed rises above maximum safe speed. If, despite this, Rotor 62s speed continues to rise above maximum safe speed, progressively shut 105 and 106; 108 and

107 (Page 4 of Drawings) refill during normal running. Vent

108 and 107 to external use when near maximum safe pressure. On Page 4 of Drawings, as soon as Heat Exchanger 34, 35, 36 and 37 is hot enough, a bi-metal strip, by direct mechanical link to 109 (Fig. 14) via 110 (Fig. 14) via 111, opens 110 and shuts 109 thus sending salt water around the system. If external salt water and/or any other external water base fuel is not available, bring fuel through from water-base fuel Tank 13. If Tank 13 is empty pump fuel through from non water base fuel Tank 64, in which case stop Rotor 77 rotating. In this case, except for the refrigeration circuit, the remaining pumps will pump air that will aid combustion in Rotor 62.

There will be enough cooling for safety.

Prior to shut down override is used to open 109 and shut 110 thus clearing the fuel system with air, when fuel system is cleared shut 105 and 106 in 88 and 91, (non return Valves 113 and 112 shut automatically with back pressure). Thus the machine is ready for the next start up.

Please go to Page 5 of Drawings.

Page 5 of Drawings - Fig. 15 - simply shows a system of shafts and gears to most effectively drive the pumps. 31 and 49 actually put a bit of energy back into the system by helping to drive the other pumps.

We will now show a bit more than half of a section through Rotor 62 to show how the combustion chambers (arranged radially) are arranged, one is shown, (Page 6 of Drawings - Fig. 16). Any practical number of combustion chambers arranged peripherally to Rotor 62 can be deployed. Oxygen plus air under great pressure flow along 88. 88 is insulated from other tubes it is co-axil with, so a high tension voltage is passed along 88, so a perpetual arc crosses where 91 tapers towards it at the very end, near 134, to Tube 91, thus igniting the high pressure hydrogen emerging from the end of Tube 91 with high pressure excess air + oxygen coming from the end of Tube 88. Extra high pressure air is already in the oxygen and hydrogen encounter. This air, greatly heated by the oxygen combining with the hydrogen, meets high pressure atomized and vaporized sodium chloride and dry steam coming from 72 which is electrically heated peripherally, (the little circles above 72 on Page 6 of Drawings is a heating coil in ceramic sectioned away). All the above encounter is well above the flash point of sodium chloride in air, the air is greatly compressed by centripetal (centrifugal) force so all the elements above spontaneously combust at an extremely high pressure ratio. Since excess air is present, complete, most efficient combustion takes place.

Continuing with Page 6 of Drawings, (top of Drawing, top of Rotor 62), high pressure water is incident via 60, (follow arrows), then via 133, this flows as shown to enter just after the flame to convert the flame from heat to thrust, thus exiting, (when viewed from above), (Page 6a of Drawings, tangentially from the periphery of Rotor 62, thus spinning it round, so energizing Dynamo 61 and providing thrust. The high water content transfers any remaining heat effectively to ^* the ducting, (refrigerated),

34, 35, 36, 37, (shown on Page 1 of Drawings).

Page 6a of Drawings shows an overhead view of Rotor 62 showing Tangential Vanes, (water cooled), (high temp alloy is ideal for this), i.e. nimonic alloy, but when much clean water is permanently available, aluminium, ceramics, steel, cast iron, even carbon fibre can be used.

Immediately following Page 7/12 of Drawings - Fig. 17 shows all of the following - a combustion chamber to convert, (to run on all the fuels the part of the machine shown on Page 1 of Drawings can run on), a conventional jet engine, this new application is novel, new, not obvious and valid, from Page 1/12 of Drawings - Heat Exchanger 34, 35, 36, 37 is moved to a coil of refrigeration tubing around the Exhaust 139, (Page 7/12 of Drawings - Fig. 17), coldest input of refrigerant nearest tail, hotest output of refrigerant most upstream. 135 shows a section of final stage of axial compressor. Oxygen plus air 88 comes in the centre of the co-axial tubing feeding the flame into the combustion chamber, igniting by sparks from its tapered end, electrically, high pressure hydrogen from 91, tapered to end, so sparks at very end of 91, co-axial with 88 and 72, ignite oxygen and hydrogen, thus heating concentrated sodium chloride + dry steam from 72 to ignition that perpetuates itself by maximum contact with hot high pressure air from high pressure blades 135 by facing it, still referring to Page 7/12 of Drawings - the shape of the combustion chamber guarantees maximum rearward propulsion and there is less drag than conventional cans because there are no holes to generate drag, the flame from the just described combustion of hydrogen, oxygen, and sodium chloride also maximizes contact with 72, (72 is wrapped all around the can), thus heating the dry steam plus sodium chloride in 72 to maximum above its flash point, (Line all the combustion area plus down stream with catalyst so NO.2 goes to separate N + 02), excess air is used in all my combustion processes so the complete combustion guaranteed by all just decribed pushes the Turbine 138 round (and all the following Turbines, (out of picture),). 139 is the equivalent of 34, 35, 36 and 37, (Page 1 of Drawings), that is, pipes carrying refrigerant to Tailpipe and stators, thus gaining heat from exhaust, reducing noise, by tapering accelerating the flow, and making exhaust cooler than background, thus deflecting heat seeking missiles away to warmer background, also thermal stress will be reduced.

With reference to Page 8 of Drawings, Fig. 18, - this is the non water base fuel Tank 64, from Drawing 1, Fig. 1, (a bit more than half way down Page ^" 1 of Drawings, left hand side),

- because said tank with entrance 63 is heated, it must be sealed and fitted with a diaphragm that will cut out Heater 66 when pressure is too high.

On Page 8/12 of Drawings, Fig. 18, (lower drawing) is Fig. 18 enlarged at diaphragm 140 for clarity, showing when pressure in Tank 64 is too high, electrical contact to Heaters 66 is broken. To avoid dangerous, serious, explosions, all air and all oxygen must be kept out of Tank 64 and supplying tubes, by feeding in carbon dioxide when not running on inflammable gas. Shut off 67 when not using fuel via Tank 64.

Thank you for all your patience.

Immediately following Page 8/12 of Drawings, Page 9/12 of Drawings refers to all the following - (until the next Page of Drawings is mentioned), this shows how a rotating drum, (three dimensional view - Fig. 19), (overhead view - Fig. 20

- same Page), is carrying cams in the correct place and driven by being geared into the engine it is relating to, activates plungers in the correct sequence to send the contents of the pipes from Drawing 1 - Fig. 1 down a heated tube, (preferably really tough glass as insulator), into a spark plug /injector replacement to convert a piston engine to running on all the things the part of machine shown on Page 1 can run on.

A separate extra battery must be carried to provide, via an extra (extremely) high voltage (tension) converter, and a really huge capacitor, a high voltage, down the spark plug/ injector replacement, from an electrical connection at the top, (top left of Page 9/12 of Drawings) E.H.T. , (extremely high tension), (voltage), Condenser 158 stores the electrical charge and passes it on to the tube terminating at 162. Tube terminating at 162 (surrounded by ceramic) containing L.T. (low tension), (low voltage), Heater 156, surrounded by more ceramic, then a steel metal case, is the spark plug /injector replacement that screws into the existing place for a spark plug /injector on a conventional engine. The tube that terminates at 162 must have an extremely high melting point and so must be composed of a high melting point conducter, e.g. nimonic alloy, not very much is needed so it will not be expensive. The Tube 154, near top of Page 9/12 of Drawings, connecting the Plug 162 to the cam activated plungers must be an insulator such as extremely thick tough glass to build up thermal capacity and to insulate the cam and plunger assembly electrically from the plug. This glass tube must be heated by a low voltage

SUBSTITUTESHEET(RULE26}

high current, separate from the high voltage to the plug.

The low voltage high current heating 154 will also be used to heat the low voltage heater in the ceramic body of the plug (156). Referring to Fig. 19 and Fig. 20 on Page 9 of Drawings:- (Extremely high pressure gas behaves almost as immediately as a liquid yet combusts extremely rapidly, when inflammable, in contact with oxygen/air). On right of Fig. 20 (Page 9/12- of Drawings), is all extremely compressed supply coming from Page 1/12 of Drawings, 83 is air, 91 is hydrogen, 72 is any fuel being sent at the time, 88 is oxygen, 59 ±S water. Because of Drum 155 presenting cams to the plungers, extremely high pressure air thus passes down 153, (Fig. 20 - Page 9 of Drawings -), and then 154, (Fig. 19 - Page 9 of Drawings -), to clear it of any electrical conductors and clear the tube through to tip of Plug 162. Similarly hydrogen flows via 91, 152, 154 to tip of Plug 162. At exactly the same time oxygen flows via 88, 160, 154 to tip of Plug 162, these will burn intensely to make 154 and the plug as hot as possible. Then fuel (i.e. concentrated salt water) is sent via 72, 151, 154 to 162 by which time i+ will be well above its flash point and constitute a vapour. The extremely high voltage is on all the time, no spark arcs from 162 to 159 until the compressed air + oxygen is now sent to push the vaporized hot fuel plus dry steam from plug tip 162 towards the Piston 159 as it nears top dead centre. (Two thirds of the way down left- hand side of Page 9 of Drawings - Fig. 19).

The charged up Capacitor 158, (top left hand side of Page 9 of Drawings), now discharges through the vaporized fuel vapour to the piston, this raises the molecules to above 2,500 degrees centigrade, more than enough to completely burn any fuel including sodium chloride. Pure water from 59, 150 then goes directly into the combustion chamber to convert temperature to thrust. Exhaust is just above 100 degrees centigrade so there is (no corrosion) and maximum thrust. A bi- etal strip at the end of 150 will stop water from entering the combustion chamber when this would take it to as low as 100 degrees centigrade. As soon as the engine is warmed up the bi-metal strip will bend and admit the high pressure water to convert temperature to thrust to maximum just above 100 degrees centigrade so there will be no corrosion, tnsulate the engine to maximize performance, it is best with no cooling system except the water injection to convert temperature to performance. Holding the temperature just above 100 degrees centigrade maximizes efficiency and prevents lubricating oil being burnt. So even extremely worn engines will run beautifully when converted to my

inventxon.

(All the "extra detail" is in fact in the original Patent 9317157.7, the following explains it better) Thank you.

As soon as any of my machines are up to maximum power running on salt water some concentrated sodium chloride solution can be vented off and fractionally distilled out of air with the water content keeping it from burning so all the elements in the sea can be recovered economically. This includes the entire electrochemical scale including sodium chloride, gold, silver, platinum, aluminium^iron, copper, zinc, tin, lead, mercury, all the rare trace metals and other chemicals that are really valuable for many modern processes, for instance iridium and much more.

Surplus electricity from my machine can be used for electrolysis of sea water. This will produce vast amounts of chlorine, as well as hydrogen. Chlorine as you know is one of the most important feedstocks for the chemical industry to produce PVC and many other things. The world uses over 4,000,000,000 tons of chlorine a year.

Normally vast amounts of fossil fuels are most expensively used to get chlorine, sodium chloride and to drive every industry.

One of the many qualities of my machine is once it has been made, which is very easy, using low technology it can make vast amounts of chlorine and sodium chloride and oxygen and hydrogen and electricity and purest water, all for free, out of the sea.

My machine makes the most absolutely effective self- sufficiency, the most valuable of all.

One off designs are normally extremely expensive, (for instance power stations) and are extremely expensive to maintain. The beauty of my machine is that one can mass produce it, and float it in ships around the coast and send the power my invention generates straight into the electricity system by reversing the flow from the national grid to the coast one will not need any extra wiring. And electrolysis of the pure water by-product will produce vast amounts of hydrogen to pump straight into the gas systems. The oxygen can go straight to industry, steel-making for instance, and hospitals, thus saving any Government and any Nation perpetually vast amounts of money.

And because the whole of this design is fundamentally good, it stimulates endless sustained genuine growth that will get us away from the old boom and then bust that was mainly caused by increasing energy costs. Rapidly rising fuel costs really caused the last World recession and slump.

THIS COULD NOT BE MORE IMPORTANT. MY DESIGN, FUNDAMENTALLY CORRECT, WILL CAUSE COMPLETE SELF-SUFFICIENCY AND SO DO ALL THE MOST GOOD. THUS, WITH MY DESIGN NOBODY LOSES, ALL WIN.

Low cost energy from my machine Increases the value of ALL OTHER RESOURCES because low cost energy from my machines can process ALL OTHER RESOURCES, ENHANCING ALL THEIR VALUE AS PERMANENT, RE-USABLE, MOST USEFUL ARTIFACTS, rather than being burnt and lost for ever. Thus all benefit the most from my design.

Referring to Page ll/l of Drawings. This is a plug to replace any conventional spark plugs or injectors in a conventional piston engine. The most convenient place to take the impulse consistent with top dead centre of the piston is near the top of the travel of the cam lobe controlling the Inlet Valve 163 on Page 11/lA.of Drawings. This is the least expensive method of applying my design to a conventional engine. The Accelerator 168, when at idling, causes the extemely high water pressure from 60, pulsed through Slide Valve 166 by Cam 163 to vent at 169 back to water reservoir, so the water pressure is near minimum as it goes on to pass Bi-metal Strip 178 that allows the maximum flow of high pressure water past consistent with the water turning to steam at Plug Nose 179 not going cooler than about 110 degrees centigrade so that there is no rust and to maximize thrust. 172 (centre of Page 11/12 of Drawings), is a matrix of ceramics and catalyst holding complete combustion of hydrogen from 91 and other fuels from 72 (all from Page 1 of Drawings) in excess air/oxygen from 88, from . high pressure air/oxygen, (Page 1 of Drawings)* On Page J.C/V2. of Drawings, when the water pulse from 166 gets to Fingers 180 it makes them open as shown in Fig. 21 - Page 10/12 of Drawings, thus converting the products of full continuous combustion in 172 from heat to extremely high pressure most efficiently. Ignition comes from electrical current flowing from 173 to 172 then to 179 (Page 11/12 of Drawings).

The sequence of operation is identical throughout my one original design, I am simply projecting the same design into the manifestations needed to do the most good in each aspect of my machine.

lubricating oil even in a worn engine.

I do wish to help everybody.

When not using water base fuel, pass some water with the alternative fuel through 72 (Page 11/12 of Drawings - Fig. 22).

The overall effect because of the Bi-metal strips 181 and 178 is the water is used to keep all fuel above its flashpoint by using dry steam to present all the fuel to surplus excess oxygen/air and hence to continuous complete combustion that never gets to NO.2 and N0.X formation because of the thermal capacity of the water.

Hence no pollution even without the catalyst.

(All the following are on Page ^" 11/12. of Drawings - Fig. 22 -

unless otherwise stated):- The gates (fingers) 180 then are forced out by water pressure from 60 controlled by accelerator setting 168 (maximum power is no venting of water through Blow Off Valve 169 at all) hen e temperature is converted to pressure on Piston 175 to maximum efficiency (Fig. 21 bottom of Page 10/12 of Drawings immediately after Page 10/12 of Drawings). Fingers 180 never wear out because they are a perfect fit (self machining).

Thank you.

Please go to Page 23.

Page 12/12 of Drawings shows a more sophisticated version of the principle I have already described, the main difference is the water pressure that opens the fingers as were 180 in Page 11/13. of Drawings - Fig 22 is now controlled by 201 at bottom of page 12/12 of Drawings - Fig. 23 which is the end of the engine crankshaft, that drives through Spline 200 to control Cam 198. The Accelerator 202 slides Cam 198 so accelerator forward means 197 is kept open a long time. Accelerator back produces minimum Valve 197 opening. Thus, controlled by Accelerator 202, the high pressure water pulses to Fingers 203, similar to Fingers 180 previously.

Bi-metal Strip 206 controls water flow to fuel flow at 190, so temperature at combustion is above flashpoint of fuel for full combustion in surplus high pressure air plus oxygen undergoing continuous combustion for perfect efficiency, and the thermal capacity of the water holds combustion temperature to below NO.2 and N0.X formation temperatures hence no pollution.

Near the top of Page 12/12 of Drawings shows 187, a high frequency, high voltage coil of many windings that induces eddy currents in metal solid Cap 189 to heat fuel above flashpoint. Once we have ignition heat flows through the walls of Cap 189 to maintain full combustion. Fuel flows into 190 and by the design is kept against Cap 189 to guarantee full combustion. Heat is then converted to efficient thrust as in the previous versions.

Thank you for your endless patience.

From Page 1/12 of Drawings we, (to convert to use of spark

eddy currents from high frequency, high voltage Coil 187, together with excess air + oxygen from 184, 185, 186, 188 produces complete combustion. This heats Bi-metal Strip 195 that switches 192 to gradually transfer from 193 to 194 (from hydrogen or petrol or equally volatile fuels) TO (water base fuel, i.e. concentrated sodium chloride solution) .

When pressure in 180 and 179 is up to maximum, surplus fuel blows off through 207 to the appropriate fuel tank via a switch controlled by the specific gravity of the blown off fuel, so that the fuel that does make it to 190 (a ring main around the inside of solid Cap 189) immediately goes to above its flashpoint to complete combustion in excess air plus oxygen plus the correct amount of water via Bi-metal Strip Control 206 to hold its temperature below the formation of NO.2 and NO.X then goes down 180 and through platinum ceramic Matrix 179 and then through Fingers 203 solely when water via Valve 197 opens them and at the same time converts temperature (heat) to pressure via 204 and hence to thrust on the piston in the engine via the cushion of compressed air in the engine.

The whole point of all my design is no pollution and maximum efficiency in order to do the most good.

Thank you.

Please go to Page 25.