초록 ▼

This invention describes a miniaturized hybrid diesel-electric engine formed by a closed-loop system powered by plasma-aided combustion of JP-8 fuel (or other hydrocarbon fuels) working in tandem with a vapor cycle utilizing miniaturized expanders and condensers. The output of this engine is electri

This invention describes a miniaturized hybrid diesel-electric engine formed by a closed-loop system powered by plasma-aided combustion of JP-8 fuel (or other hydrocarbon fuels) working in tandem with a vapor cycle utilizing miniaturized expanders and condensers. The output of this engine is electric power and mechanical work. Water, or organic fluids, heated by the combustion product developed inside a special burner, undergoes an explosive, quasi-supersonic conversion to steam. This steam drives a high-speed turbine connected together with a gas turbine outputting shaft work. This work output is utilized to power internal subsystems, cool down the miniaturized condensers, and to produce torque and electric power. The dimensions of this miniaturized hybrid-engine are so compact that it can fit inside the battery compartment of most applications requiring high-density miniaturized power sources.

대표청구항 ▼

What is claimed is: 1. A small-scale hybrid engine comprising: a combustion chamber configured to generate heat energy from combustion of a combustible fuel; a turbine coupled to a shaft and configured to convert the heat energy into a mechanical energy to rotate the shaft; a fluid channel having a

What is claimed is: 1. A small-scale hybrid engine comprising: a combustion chamber configured to generate heat energy from combustion of a combustible fuel; a turbine coupled to a shaft and configured to convert the heat energy into a mechanical energy to rotate the shaft; a fluid channel having a surface in thermal contact with the combustion chamber, wherein a portion of the heat energy in the combustion chamber is transferred to a fluid flowing through the fluid channel; and a second turbine coupled to the shaft and configured to convert the heat energy transferred to the fluid to rotate the shaft, wherein the surface defines at least a portion of the inner surface of the combustion chamber, and wherein the fluid flowing through the fluid channel does not mix with the combustible fuel or combustion product of the combustible fuel. 2. A small-scale hybrid engine as defined in claim 1, further comprising a generator for generating electricity from rotation of the shaft. 3. A small-scale hybrid engine as defined in claim 1, further comprising a starter for rotating the shaft by an external source of power. 4. A small-scale hybrid engine as defined in claim 3, wherein the external source of power includes a battery. 5. A small-scale hybrid engine as defined in claim 1, wherein the fluid channel is separated from the combustion chamber, so that the fluid does not mix with the combustible fuel. 6. A small-scale hybrid engine as defined in claim 1, further comprising a generator-starter mechanism configured to generate electricity from rotation of the shaft and to rotate the shaft by using an external source of power. 7. A small-scale hybrid engine as defined in claim 6, wherein the generator-starter mechanism includes a rotating disk controlled by a controller. 8. A small-scale hybrid engine as defined in claim 7, wherein the controller includes a computer processor and a sensor adjacent to the rotating disk. 9. A small-scale hybrid engine as defined in claim 7, wherein the rotating disk includes at least one magnets magnetically coupled a stationary coil, the stationary coil controlled by the controller, so that the rotating disk is controlled by the controller. 10. A small-scale hybrid engine as defined in claim 1, wherein the second turbine includes at least one vapor turbine coaxially positioned along the shaft and connected to a first set of gear system. 11. A small-scale hybrid engine as defined in claim 10, further comprising a second set of gear system for indirect coupling of the vapor turbine with the shaft. 12. A small-scale hybrid engine as defined in claim 10, further comprising a second set of gear system for providing an external mechanical coupling. 13. A small-scale hybrid engine as defined in claim 1, further comprising at least one air bleeding system to allow cooling of burned combustible fuel. 14. A small-scale hybrid engine as defined in claim 1, further comprising an igniting system to ignite the combustible fuel. 15. A small-scale hybrid engine as defined in claim 14, wherein the igniting system includes a fuel pump configured to pressurize the combustible fuel. 16. A small-scale hybrid engine as defined in claim 1, wherein at least a portion of the engine is lined with acoustically absorbing materials. 17. A small-scale hybrid engine as defined in claim 1, wherein the second turbine is directly coupled to the shaft. 18. A small-scale hybrid engine as defined in claim 1, wherein the second turbine is indirectly coupled to the shaft through a set of gear system, the gear system, permitting the second turbine to rotate at a speed different from that of the turbine. 19. A small-scale hybrid engine as defined in claim 1, further comprising at least one of an integrated fuel tank, a start-up battery, and a back-up battery. 20. A small-scale hybrid engine as defined in claim 1, further comprising a display unit for displaying status of the engine. 21. A small-scale hybrid engine comprising: a combustion chamber configured to generate heat energy from combustion of a combustible fuel; a turbine coupled to a shaft and configured to convert the heat energy into a mechanical energy to rotate the shaft; a fluid channel having a surface in thermal contact with the combustion chamber, wherein a portion of the heat energy in the combustion chamber is transferred to a fluid flowing through the fluid channel; a second turbine coupled to the shaft and configured to convert the heat energy transferred to the fluid to rotate the shaft; and a cooling channel for condensing the fluid, wherein the surface defines at least a portion of the inner surface of the combustion chamber. 22. A small-scale hybrid engine as defined in claim 21, wherein the cooling channel is separated from the fluid channel by an insulator. 23. A small-scale hybrid engine comprising: a combustion chamber configured to generate heat energy from combustion of a combustible fuel; a turbine coupled to a shaft and configured to convert the heat energy into a mechanical energy to rotate the shaft; a fluid channel having a surface in thermal contact with the combustion chamber, wherein a portion of the heat energy in the combustion chamber is transferred to a fluid flowing through the fluid channel; a second turbine coupled to the shaft and configured to convert the heat energy transferred to the fluid to rotate the shaft; and an air manifold having an inlet and an outlet, the manifold having a surface in thermal contact with the fluid channel, wherein the fluid flowing through the fluid channel does not mix with the combustible fuel or combustion product of the combustible fuel. 24. A small-scale hybrid engine as defined in claim 23, further comprising an air compressor configured to compress the air flowing into the air manifold. 25. A small-scale hybrid engine as defined in claim 24, further comprising a thermal insulator separating the air compressor from the combustion chamber. 26. A small-scale hybrid engine as defined in claim 24, wherein the compressor is a compressor turbine powered by the shaft. 27. A small-scale hybrid engine comprising: a combustion chamber configured to generate heat energy from combustion of a combustible fuel; a turbine coupled to a shaft and configured to convert the heat energy into a mechanical energy to rotate the shaft; a fluid channel having a surface in thermal contact with the combustion chamber, wherein a portion of the heat energy in the combustion chamber is transferred to a fluid flowing through the fluid channel; and a second turbine coupled to the shaft and configured to convert the heat energy transferred to the fluid to rotate the shaft, wherein the fluid channel includes a cavity formed between the combustion chamber and an insulator, wherein the fluid flows through the cavity and expands. 28. A small-scale hybrid engine as defined in claim 27, wherein: the combustion chamber is an elongated cylinder; the insulator is a concentric cylinder surrounding the elongated cylinder; and the cavity is a gap between the elongated cylinder and the concentric cylinder. 29. A small-scale hybrid engine comprising: a combustion chamber configured to generate heat energy from combustion of a combustible fuel; a turbine coupled to a shaft and configured to convert the heat energy into a mechanical energy to rotate the shaft; a fluid channel having a surface in thermal contact with the combustion chamber, wherein a portion of the heat energy in the combustion chamber is transferred to a fluid flowing through the fluid channel; a second turbine coupled to the shaft and configured to convert the heat energy transferred to the fluid to rotate the shaft; and a fluid injector for throttling the fluid into the fluid channel, wherein the fluid flowing through the fluid channel does not mix with the combustible fuel or combustion product of the combustible fuel. 30. A small-scale hybrid engine as defined in claim 29, wherein the fluid injector includes a check valve. 31. A small-scale hybrid engine comprising: a combustion chamber configured to generate heat energy from combustion of a combustible fuel; a turbine coupled to a shaft and configured to convert the heat energy into a mechanical energy to rotate the shaft; a fluid channel having a surface in thermal contact with the combustion chamber, wherein a portion of the heat energy in the combustion chamber is transferred to a fluid flowing through the fluid channel; a second turbine coupled to the shaft and configured to convert the heat energy transferred to the fluid to rotate the shaft; and an igniting system to ignite the combustible fuel, wherein the igniting system includes a set of plasma electrodes, and wherein the fluid flowing through the fluid channel does not mix with the combustible fuel or combustion product of the combustible fuel. 32. A small-scale hybrid engine as defined in claim 31, wherein the set of plasma electrodes comprises at least one hot plasma electrode and at least one cold plasma electrode, wherein the hot plasma electrode and cold plasma electrode are controlled by a plasma controller and generator. 33. A small-scale hybrid engine comprising: a combustion chamber configured to generate heat energy from combustion of a combustible fuel; an igniting system to ignite the combustible fuel, a turbine coupled to a shaft and configured to convert the heat energy into a mechanical energy to rotate the shaft; a fluid channel having a surface in thermal contact with the combustion chamber, wherein a portion of the heat energy in the combustion chamber is transferred to a fluid flowing through the fluid channel; and a second turbine coupled to the shaft and configured to convert the heat energy transferred to the fluid to rotate the shaft, wherein the surface defines at least a portion of the inner surface of the combustion chamber, wherein the igniting system includes a fuel expanding cavity configured to produce a jet of superheated fuel.