초록 ▼

A hydrogen fueled powerplant including an internal combustion engine that drives a motor-generator, and has a two-stage turbocharger, for an aircraft. A control system controls the operation of the motor-generator to maintain the engine at a speed selected based on controlling the engine equivalence

A hydrogen fueled powerplant including an internal combustion engine that drives a motor-generator, and has a two-stage turbocharger, for an aircraft. A control system controls the operation of the motor-generator to maintain the engine at a speed selected based on controlling the engine equivalence ratio. The control system controls an afterburner, an intercooler and an aftercooler to maximize powerplant efficiency. The afterburner also adds power to the turbochargers during high-altitude restarts. The turbochargers also include motor-generators that extract excess power from the exhaust.

대표청구항 ▼

1. A powerplant, comprising: a combustion engine configured to produce motive force, and having an inlet and an outlet, and being characterized at any given time by an engine equivalence ratio;a generator configured to generate power from the motive force of the engine, and configured to apply a var

1. A powerplant, comprising: a combustion engine configured to produce motive force, and having an inlet and an outlet, and being characterized at any given time by an engine equivalence ratio;a generator configured to generate power from the motive force of the engine, and configured to apply a variable-level motive force to the engine; anda control system configured to control the motive force applied to the engine by the generator, wherein the control system is configured to control the generator such that the generator maintains the engine speed based upon a calculation of the engine equivalence ratio. 2. The powerplant of claim 1, wherein the engine is configured with a passageway connecting an engine inlet to a source of gaseous reactant, and wherein the passageway is configured to pass a stream of gaseous reactant from the source of gaseous reactant without limitation from a controllable obstruction that would cause a reduction in pressure of the stream of gaseous reactant. 3. The powerplant of claim 2, and further comprising a compressor configured to compress the stream of gaseous reactant from the source of gaseous reactant, wherein the passageway is configured to always provide the stream of gaseous reactant to the engine inlet at substantially the pressure level established by the compressor. 4. The powerplant of claim 2, wherein the engine is a hydrogen-fueled engine configured to run with an equivalence ratio of less than one, and the stream of gaseous reactant is an oxidizer. 5. The powerplant of claim 1, wherein the generator generates power at a power generation level related to a rate at which fuel is provided to the engine, and wherein the control system is configured to change the power generation level by varying the rate at which fuel is provided to the engine. 6. The powerplant of claim 5, and further comprising a turbocharger including a turbine driven by an exhaust stream of the engine and a compressor configured to compress stream of gaseous reactant for the engine, wherein the control system is configured to control the operation of the turbocharger based on a calculation of an efficiency level of the powerplant. 7. The powerplant of claim 6, and further comprising an afterburner in the exhaust stream intermediate the engine and the turbine, the afterburner being configured to react additional reactants in the exhaust stream, wherein the control system is configured to control the operation of the turbocharger by controlling the amount of additional reactants reacted in the exhaust stream. 8. The powerplant of claim 7, and further comprising a second turbocharger including a turbine driven by an exhaust stream of the engine and a compressor configured to compress stream of gaseous reactant for the engine, wherein the second turbocharger turbine is upstream of the afterburner. 9. The powerplant of claim 6, wherein the control system is configured to control the operation of the turbocharger such that the calculation of the efficiency level of the powerplant is maximized at all required power levels and ambient operating conditions. 10. The powerplant of claim 5, and further comprising a compressor configured to compress the stream of gaseous reactant for the engine, and an aftercooler configured to cool the stream of gaseous reactant compressed by the compressor, wherein the control system is configured to control the operation of the aftercooler based on a calculation of an efficiency level of the powerplant. 11. The powerplant of claim 10, wherein the control system is configured to control the operation of the aftercooler such that the calculation of the efficiency level of the powerplant is maximized at all required power levels and ambient operating conditions. 12. The powerplant of claim 5, and further comprising two serial compressors configured to compress gaseous reactant for the engine, and an intercooler configured to cool the gaseous reactant intermediate the two compressors, wherein the control system is configured to control the operation of the intercooler based on a calculation of an efficiency level of the powerplant. 13. The powerplant of claim 12, wherein the control system is configured to control the operation of the intercooler such that the calculation of the efficiency level of the powerplant is maximized at all required power levels and ambient operating conditions. 14. A method of generating power using powerplant including a combustion engine configured to produce motive force, the engine having an inlet and an outlet, and the engine being characterized at any given time by an engine equivalence ratio, and further including a generator configured to generate power from the motive force of the engine, the generator being configured to apply motive force to the engine when electrical power is applied to the generator, comprising: controlling the motive force applied to the engine by the generator such that the generator maintains the engine speed based upon a calculation of the engine equivalence ratio. 15. The method of claim 14, wherein the generator generates power at a power generation level related to a rate at which fuel is provided to the engine, and further comprising changing the power generation in response to varied power needs by varying the rate at which fuel is provided to the engine. 16. The method of claim 15, wherein the powerplant includes a turbocharger including a turbine driven by an exhaust stream of the engine and a compressor configured to compress a stream of gaseous reactant for the engine, and further includes an afterburner in the exhaust stream intermediate the engine and the turbine, the afterburner being configured to react additional reactants in the exhaust stream, and further comprising controlling the amount of additional reactants reacted in the exhaust stream based on a calculation of an efficiency level of the powerplant. 17. A powerplant, comprising: a combustion engine configured to produce motive force, and having an inlet and an outlet;a generator configured to generate power from the motive force of the engine, and configured to apply motive force to the engine when electrical power is applied to the generator; anda means for controlling the motive force applied to the engine by the generator such that the generator maintains the engine speed based upon a calculation of the engine equivalence ratio. 18. The powerplant of claim 17, wherein the generator is configured to generate power at a power generation level related to a rate at which fuel is provided to the engine, and further comprising a means for changing the power generation in response to varied power needs by varying the rate at which fuel is provided to the engine. 19. The powerplant of claim 18, wherein the engine includes a turbine driven by an exhaust stream of the engine, and a compressor configured to compress a stream of gaseous reactant for the engine, and an afterburner in the exhaust stream intermediate the engine and the turbine, the afterburner being configured to react additional reactants in the exhaust stream, and further comprising a means for controlling the amount of additional reactants reacted in the exhaust stream based on a calculation of an efficiency level of the powerplant.