Engine producing thrust using an induction heating assembly to energize the fuel
An example engine for producing thrust includes: a fuel supply to supply a fuel; a chamber fluidly coupled to the fuel supply to receive the fuel; an induction heating assembly operatively coupled to the chamber to inductively energize the fuel in the chamber; and an exhaust nozzle coupled to the chamber to receive energized fuel from the chamber to produce thrust.
1. An engine comprising:
a fuel supply to supply a fuel, wherein the fuel is an electrically conducting fuel, including a reactive metal compound, wherein the fuel includes a micro/nano-thermite;
a chamber fluidly coupled to the fuel supply to receive the fuel;
an induction heating assembly operatively coupled to the chamber to inductively energize the fuel in the chamber;
wherein the induction heating assembly includes a coil and a power supplying circuit configured to pass a current through the coil, wherein the power supplying circuit is an electronic oscillator or other suitable circuitry for passing a high frequency alternating current through the coil to induce a magnetic field; and
wherein the power supplying circuit is further configured to vary the current passing through the coil, thereby varying the magnetic field, wherein the varying magnetic field induces eddy currents in nearby conductors, and in particular, in the fuel, wherein the eddy currents, in turn, flow through the resistance of the fuel to energize the fuel; and
an exhaust nozzle coupled to the chamber to receive energized fuel from the chamber to produce thrust.
2. The engine of claim 1 , wherein the fuel supply comprises a primary tank to contain the fuel and a pump to pump the fuel from the primary tank to the chamber.
3. The engine of claim 2 , wherein the fuel supply further comprises a mixing system including one or more secondary tanks to contain secondary fluids, each secondary tank having a corresponding control valve to control a flow of a respective secondary fluid.
4. The engine of claim 3 , wherein the secondary fluids are secondary fuels or catalysts.
5. The engine of claim 2 , wherein the fuel supply further comprises a compressor to compress the fuel.
6. The engine of claim 5 , wherein the compressor comprises one or more of: a convection compressor and a scroll compressor.
7. The engine of claim 1 , wherein the fuel supply comprises an intake and a compressor.
8. The engine of claim 7 , wherein the compressor comprises one or more of: a convection compressor and a scroll compressor.
9. The engine of claim 1 , further comprising a thermal battery associated to store thermal energy and release the stored thermal energy to energize the fuel.
10. The engine of claim 1 , further comprising:
a plasma tube associated with the chamber to circulate plasma adjacent to the chamber to facilitate energization of the fuel; and
a coolant tube associated with the chamber and surrounding the plasma tube, the coolant tube configured to circulate a coolant to manage dissipation of thermal energy from the plasma tube.
11. The engine of claim 1 , further comprising an arrangement of permanent magnets to augment a magnetic field produced by the induction heating assembly.
12. The engine of claim 1 , further comprising a secondary induction heating assembly configured to inductively heat the exhaust nozzle.
13. The engine in claim 1 , further comprising regenerative heat exchangers to heat and energize the fuel.
14. The engine in claim 1 , wherein the induction heating assembly is configured to energize the fuel by applying one or more of: a high frequency alternating current and a direct current.
15. The engine in claim 1 , further comprising a further power generation system.
16. The engine of claim 15 , wherein the further power generation system employs one or more of: cogeneration, trigeneration and multigeneration of cooling, heating, power, propulsion, and industrial products.
17. The engine in claim 1 , wherein the induction heating assembly is further configured to energize the fuel via sintering.
18. A method in an induction engine, the method comprising:
receiving, in a chamber, a fuel, wherein the fuel is an electrically conducting fuel, including a reactive metal compound, wherein the fuel includes a micro/nano-thermite;
inductively energizing the fuel using an induction heating assembly, wherein the induction heating assembly includes a coil and a power supplying circuit configured to pass a current through the coil, wherein the power supplying circuit is an electronic oscillator or other suitable circuitry for passing a high frequency alternating current through the coil to induce a magnetic field; and
wherein the power supplying circuit is further configured to vary the current passing through the coil, thereby varying the magnetic field, wherein the varying magnetic field induces eddy currents in nearby conductors, and in particular, in the fuel, wherein the eddy currents, in turn, flow through the resistance of the fuel to energize the fuel; and
at an exhaust nozzle of the engine, producing thrust from the energized fuel.
19. The method of claim 18 , further comprising, prior to energizing the fuel, pre-heating the fuel using a thermal battery.
20. The method of claim 18 , further comprising, prior to energizing the fuel, compressing the fuel.
21. The method of claim 20 , wherein the fuel is compressed using one or more of a cyclonic convection compressor and a scroll compressor.
22. The method of claim 18 , further comprising, prior to energizing the fuel, mixing the fuel with a secondary fuel.
23. The method of claim 18 , further comprising, prior to energizing the fuel, mixing the fuel with a catalyst.