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An engine comprising a detonation chamber in thermal communication with a tank, a fuel system connected to the chamber, and a controller wherein energy from fuel detonations in the chamber is transferred to a fluid in the tank. By rapidly transferring the energy from the chamber, the detonation prod

An engine comprising a detonation chamber in thermal communication with a tank, a fuel system connected to the chamber, and a controller wherein energy from fuel detonations in the chamber is transferred to a fluid in the tank. By rapidly transferring the energy from the chamber, the detonation produces little or no toxic by-products. The fluid in the tank is energized to provide power for a wide range of machines from large equipment to small appliances.

대표청구항 ▼

I claim: 1. An engine comprising: a detonation chamber, said chamber comprising a wall, a chamber sensor and a gauge, said chamber sensor measuring a chamber pressure within the chamber, said gauge measuring a temperature at the wall; a tank, said tank in contact with the wall and comprising a tank

I claim: 1. An engine comprising: a detonation chamber, said chamber comprising a wall, a chamber sensor and a gauge, said chamber sensor measuring a chamber pressure within the chamber, said gauge measuring a temperature at the wall; a tank, said tank in contact with the wall and comprising a tank sensor, a tank inlet, and a tank outlet, said tank sensor measuring a tank pressure within the tank, said tank inlet comprising a tank inlet valve, said tank outlet comprising a tank outlet valve; a fuel system interconnected to the chamber comprising an oxidizer source, at least one fuel injector interconnected to at least one fuel reservoir, and an exhaust, said oxidizer source comprising an oxidizer valve, said fuel injector comprising a fuel valve, said exhaust comprising an exhaust valve; and a controller, said controller: (a) determining a rate and an amount of at least one oxidizer and a rate and an amount of at least one fuel, said rates derived from at least one of the temperature, chamber pressure, a requested amount of an energized fluid, and at least one property of the fuel and the oxidizer; (b) determining a detonation rate derived from at least one of the temperature, chamber pressure, requested amount of energized fluid, the property of the fuel, and the property of the oxidizer; (c) controlling the injection into the chamber from the fuel system of the determined amount of oxidizer at the determined oxidizer rate and the determined amount of fuel at the determined fuel rate; (d) controlling the detonation of a mixture of the oxidizer and fuel in the chamber at the detonation rate, wherein the detonation produces an energy and at least one detonation product; (e) controlling the injection of a fluid into the tank, wherein the energy transfers through the wall to the fluid converting the fluid into energized fluid, said injection determined from the detonation rate; (f) determining the amount of tank pressure in the tank and controlling the release of the energized fluid from the tank; said release determined from the tank pressure and the requested amount of energized fluid; and (g) controlling the release of a portion of the detonation product from the chamber. 2. The engine of claim 1 wherein the oxidizer source is interconnected to at least one oxidizer holding compartment and a compressor and the exhaust is interconnected to the compressor. 3. The engine of claim 2 wherein the portion of the detonation product is directed to the compressor; said detonation product providing a force that operates the compressor, said compressor providing compressed oxidizer to the oxidizer holding compartment. 4. The engine of claim 1 wherein the detonation of the mixture comprises at least one of a detonation device and an increase in chamber pressure. 5. The engine of claim 4 wherein the mixture is detonated by an increase in chamber pressure and a spark. 6. The engine of claim 1 wherein the energy energizes an energized fluid. 7. The engine of claim 1 wherein at least one first fuel is detonated as a primer for at least one second fuel. 8. The engine of claim 1 wherein at least one of the tank inlet and the tank inlet valve comprise a multiple fluid injector. 9. The engine of claim 1 wherein the tank surrounds the chamber and the fluid is injected into the tank onto a side of the wall facing the tank. 10. The engine of claim 9 wherein the fluid is injected into the tank onto the wall through multiple fluid injectors. 11. The engine of claim 1 wherein the wall is a heat sink. 12. The engine of claim 1 wherein the tank comprises at least one of an insulated outer wall and insulated inner wall. 13. The engine of claim 1 wherein the energized fluid, upon an extraction of at least a portion of the energy, is re-injected into the tank. 14. A process using the engine of claim 1 to provide power comprising: (a) selecting the fuel and the oxidizer; (b) sensing the temperature and the pressure in the chamber and the pressure in the tank; (c) determining the detonation rate based on at least one property of the fuel, one property of the oxidizer, the temperature and pressure in the chamber, the pressure in the tank, and the requested amount of energized fluid; (d) injecting an amount of fuel into the chamber; said amount of fuel based on a fuel amount instruction derived from the detonation rate; (e) introducing a quantity of oxidizer into the chamber, said quantity based on an oxidizer amount instruction derived from the detonation rate; (f) selectively detonating the oxidizer-fuel mixture based on a detonation instruction derived from the detonation rate to create the energy; (g) injecting a measure of fluid into the tank, said measure based on a fluid measure instruction derived from the detonation rate; (h) energizing the fluid with the energy to convert the fluid to energized fluid in the tank; (i) exhausting all but a portion of detonation product based on a portion instruction derived from the detonation rate, said portion creating a detonation product pressure; (j) using the exhausted detonation product to drive a compressor, said compressor injecting oxidizer into the oxidizer source; (k) selectively opening the outlet connected to the tank to release the energized fluid based on the requested amount of energized fluid; and (l) repeating steps b-k. 15. The process of claim 14 wherein the step of selecting the fuel and the oxidizer comprises selecting at least one fuel and at least one oxidizer. 16. The process of claim 14 wherein at least one first fuel is detonated as a primer for at least one second fuel. 17. The process of claim 14 wherein the step of energizing energizes an energized fluid. 18. The process of claim 14 wherein the energized fluid is provided to one of at least one machine and at least one storage vessel. 19. The engine of claim 14 wherein the energized fluid provides power to at least one of the compressor and a second compressor. 20. A multi-engine comprising more than one of the engine of claim 1. 21. The multi-engine of claim 20 wherein the energized fluid is provided to one of at least one machine and at least one storage vessel. 22. The engine of claim 20 wherein the energized fluid provides power to a second compressor, said second compressor compressing a second fuel into a fuel storage tank.