초록 ▼

This invention presents improved combustion methods, systems, engines and apparatus utilizing H2, O2 and H2O as fuel, thereby providing environmentally friendly combustion products, as well as improved fuel and energy management methods, systems, engines and apparatus. The Water Combustion Technolog

This invention presents improved combustion methods, systems, engines and apparatus utilizing H2, O2 and H2O as fuel, thereby providing environmentally friendly combustion products, as well as improved fuel and energy management methods, systems, engines and apparatus. The Water Combustion Technology; WCT, is based upon water (H2O) chemistry, more specifically H2O combustion chemistry and thermodynamics. WCT does not use any hydrocarbon fuel source, rather the WCT uses H2 preferably with O2 and secondarily with air. The WCT significantly improves the thermodynamics of combustion, thereby significantly improving the efficacy of combustion, utilizing the first and second laws of thermodynamics. The WCT preferably controls combustion temperature with H2O and secondarily with air in the combustion chamber. The WCT preferably recycles exhaust gases as fuel converted from water. The WCT minimizes external cooling loops and minimizes exhaust and/or exhaust energy, thereby maximizing available work and internal energy while minimizing enthalpy and entropy losses.

대표청구항 ▼

1. An engine comprising a combustion chamber, wherein a mixture of oxygen, as O2, and hydrogen, as H2, is combusted, creating steam, whereinat least a portion of the oxygen is obtained by the separation of air, whereinthe separation of air is selected from the group consisting of:(a) cryogenic separ

1. An engine comprising a combustion chamber, wherein a mixture of oxygen, as O2, and hydrogen, as H2, is combusted, creating steam, whereinat least a portion of the oxygen is obtained by the separation of air, whereinthe separation of air is selected from the group consisting of:(a) cryogenic separation,(b) membrane separation,(c) pressure swing adsorption, andany combination thereof, whereinthe air separation is at least partially powered by torque or mechanical rotating energy, wherein the torque or mechanical rotating energy is at least partially obtained from at least one of:the steam turning a steam turbine,the steam in the combustion chamber driving a piston,the steam in the combustion chamber driving a steam turbine, andany combination therein, and whereinthe temperature of combustion is at least partially controlled with the addition of water or steam to the combustion chamber in a way that maintains the temperature of combustion or of combustion exhaust. 2. The engine of claim 1, wherein said torque or said mechanical rotating energy turns a generator to create electrical energy. 3. The engine of claim 1, wherein the steam produced by combustion turns a steam turbine, and wherein said steam turbine turns a generator to create electrical energy. 4. The engine of claim 1, wherein heat is created. 5. The engine of claim 2 or 3, wherein at least a portion of said electrical energy is used in the electrolysis of water to hydrogen and oxygen, and wherein at least a portion of at least one of said hydrogen and oxygen is used in said mixture. 6. The engine of claim 1, further comprising nitrogen or argon in said mixture. 7. The engine of claim 1, wherein said oxygen further comprises air. 8. The engine of claim 1, wherein at least a portion of the steam produced by combustion is converted to hydrogen by the corrosion of at least one metal. 9. The engine of claim 8, wherein the conversion of said steam into said hydrogen is increased by an electrical current in said metal(s). 10. The engine of claim 8 or 9, wherein said hydrogen is at least partially used in said mixture. 11. The engine of claim 1, wherein a generator turns due to the movement of air or water, and wherein said generator creates electrical energy, and whereinsaid electrical energy is at least partially utilized in the electrolysis of water to hydrogen and oxygen, and whereinat least a portion of at least one of said hydrogen and oxygen is used in said mixture. 12. The engine of claim 1, wherein a photovoltaic cell creates electrical energy, wherein said electrical energy is at least partially used in the electrolysis of water to hydrogen and oxygen, and whereinat least a portion of at least one of said hydrogen and oxygen is used in said mixture. 13. The engine of claim 1, wherein at least a portion of the nitrogen separated from air in said cryogenic air separation unit is used to cool any portion of at least one selected from a list consisting of: said cryogenic air separation unit, the storage of oxygen, the storage of hydrogen, electrolysis, coolant for said engine, said engine and any combination thereof. 14. The engine of claim 13, wherein said nitrogen separated from air in said cryogenic air separation unit is at least partially used to cool air or water. 15. The engine of claim 1, wherein said oxygen separated from air is at least one of enriched oxygen, pure oxygen and very pure oxygen. 16. The engine of claim 1, wherein at least one selected from a list consisting of a: corrosion inhibitor, chelant, dispersant and any combination therein is added to at least a portion of the water in said engine. 17. The engine of claim 1, wherein said engine performs at least one of: internal, turbine and heating combustion. 18. The engine of claim 1, wherein at least one of oxygen and hydrogen is stored in at least one of a cooled gas state and a liquid state by liquefaction. 19. The engine of claim 18, wherein compressor(s) for at least one of cooling and liquefaction is powered by at least one of said engine and a fuel cell. 20. The engine of claim 19, wherein said fuel cell is powered by hydrogen and at least one of oxygen and air. 21. The engine of claim 1, wherein at least one of said hydrogen and oxygen is stored in a mixture with frozen water crystals to form a gel. 22. The engine of claim 1, wherein at least one selected from a list consisting of: hydrogen, oxygen and water is preheated prior to combustion with the energy from at least one selected from a list consisting of: ambient temperature, said engine, said engine exhaust, an electrical radiant heat source and any combination therein. 23. The engine of claim 1, wherein said mechanical rotating energy enters a transmission, wherein said transmission engage in a manner that is inversely proportional to at least one of the torque and work output of said engine, and whereinsaid transmission output mechanical rotating energy turns a generator to create electrical energy. 24. The engine of claim 23, wherein said transmission engage a flywheel capable of storing said mechanical rotational energy. 25. The engine of claim 23, wherein at least a portion of said electrical energy is used in the electrolysis of water to hydrogen and oxygen. 26. The engine of claim 25, wherein at least a portion of at least one of said hydrogen and oxygen is used in said mixture. 27. The engine of claim 1 or 3, wherein a pressure control device is in said engine exhaust. 28. The engine of claim 1, wherein at least one of said engine combustion heat energy and said engine exhaust energy is used to heat at least one of a gas and a liquid. 29. The engine of claim 28, wherein at least one of the gas is air and the liquid is water. 30. The engine of claim 29, wherein said exhaust discharge directly into said air or water. 31. The engine of claim 1, wherein at least a portion of said engine is insulated. 32. The engine of claim 1, wherein hydrogen is separated from at least one selected from a list consisting of: water, air, nitrogen, oxygen and any combination thereof within said air separation unit. 33. The engine of claim 1, wherein the temperature of said engine exhaust is at least partially cooled with the addition of water to said engine exhaust. 34. The engine of claim 33, comprising jet propulsion. 35. The engine of claim 1 or 33, comprising rocket propulsion. 36. The engine of claim 1, wherein said engine comprises a turbine. 37. The engine of claim 1, comprising jet propulsion wherein air is stoichiometrically increased in the jet intake for hydrogen thermodynamics and/or to operate with excess air for cooling.