System For Sampling And Analyzing Contrails Generated By An Aircraft
US-2021285851-A1 · Sep 16, 2021 · US
US11828200B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-11828200-B2 |
| Application number | US-202217670043-A |
| Country | US |
| Kind code | B2 |
| Filing date | Feb 11, 2022 |
| Priority date | Feb 11, 2022 |
| Publication date | Nov 28, 2023 |
| Grant date | Nov 28, 2023 |
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A powerplant is provided that includes an engine and a water recovery system. The engine includes an engine combustor, an engine turbine, a flowpath and a fluid delivery system. The flowpath extends out of the engine combustor and through the engine turbine. The fluid delivery system includes a hydrogen reservoir and an oxygen reservoir. The hydrogen reservoir is configured to store fluid hydrogen as liquid hydrogen. The oxygen reservoir is configured to store fluid oxygen as liquid oxygen. The fluid delivery system is configured to provide the fluid hydrogen and the fluid oxygen for combustion within the engine combustor to produce combustion products within the flowpath. The water recovery system is configured to extract water from the combustion products. The water recovery system is configured to provide the water to a component of the powerplant.
Opening claim text (preview).
What is claimed is: 1. A powerplant, comprising: an engine comprising an engine combustor, an engine turbine, a flowpath and a fluid delivery system, the flowpath extending out of the engine combustor and through the engine turbine, the fluid delivery system including a hydrogen reservoir and an oxygen reservoir, the hydrogen reservoir configured to store fluid hydrogen as liquid hydrogen, the oxygen reservoir configured to store fluid oxygen as liquid oxygen, and the fluid delivery system configured to provide the fluid hydrogen and the fluid oxygen for combustion within the engine combustor to produce combustion products within the flowpath; a water recovery system configured to extract water from the combustion products, the water recovery system configured to provide the water to a component of the powerplant, and the water recovery system including a condenser and an evaporator; the condenser arranged with the flowpath, the water recovery system configured to extract the water from the combustion products using the condenser, and the water extracted from the combustion products comprising liquid water; the evaporator arranged with the flowpath, and the evaporator configured to vaporize at least some of the liquid water directed by the water recovery system towards the component into steam; a steam turbine fluidly coupled between the evaporator and the component, the steam turbine including a steam turbine rotor configured to be rotatably driven by the steam; a heat exchanger system configured to transfer heat energy from the combustion products to at least one of the fluid hydrogen or the fluid oxygen, wherein the heat exchanger system is fluidly coupled along the flowpath between the engine turbine and the evaporator. 2. The powerplant of claim 1 , wherein the engine combustor comprises the component. 3. The powerplant of claim 1 , wherein the engine turbine comprises the component. 4. The powerplant of claim 1 , wherein the water recovery system is configured to provide at least some of the water to the component as the steam. 5. The powerplant of claim 1 , wherein the condenser comprises a condensing turbine. 6. The powerplant of claim 1 , wherein the water recovery system further comprises a water pump fluidly coupled between the condenser and the evaporator. 7. The powerplant of claim 1 , wherein the water recovery system comprises a water reservoir for storing at least some of the water. 8. The powerplant of claim 1 , wherein the heat exchanger system comprises a heat exchanger; and the heat exchanger is configured to transfer the heat energy from the combustion products to the fluid hydrogen as the fluid delivery system directs the fluid hydrogen to the engine combustor. 9. The powerplant of claim 8 , wherein the fluid delivery system further includes a turboexpander downstream of the heat exchanger; the heat exchanger is configured to vaporize the fluid hydrogen to provide gaseous hydrogen; and the turboexpander is configured to expand the gaseous hydrogen and generate mechanical power. 10. The powerplant of claim 1 , wherein the heat exchanger system comprises a heat exchanger; and the heat exchanger is configured to transfer the heat energy from the combustion products to the fluid oxygen as the fluid delivery system directs the fluid oxygen to the engine combustor. 11. The powerplant of claim 10 , wherein the fluid delivery system further includes a turboexpander downstream of the heat exchanger; the heat exchanger is configured to vaporize the fluid oxygen to provide gaseous oxygen; and the turboexpander is configured to expand the gaseous oxygen and generate mechanical power. 12. The powerplant of claim 1 , further comprising: a pre-burner arranged upstream of the engine combustor along the flowpath; the fluid delivery system further configured to provide the fluid hydrogen and the fluid oxygen for combustion within the pre-burner. 13. The powerplant of claim 12 , further comprising a second turbine arranged along the flowpath between the pre-burner and the engine combustor. 14. The powerplant of claim 1 , further comprising a propulsor rotor coupled to and rotatably driven by the engine turbine. 15. The powerplant of claim 1 , further comprising an electric generator comprising a generator rotor coupled to and rotatably driven by the engine turbine. 16. A powerplant, comprising: an engine comprising an engine combustor, an engine turbine, a flowpath, a fluid delivery system and a water recovery system; the flowpath extending out of the engine combustor and through the engine turbine; the fluid delivery system including a hydrogen reservoir, an oxygen reservoir and a heat exchanger system, and the fluid delivery system configured to deliver fluid hydrogen and fluid oxygen for combustion within the engine combustor to produce combustion products within the flowpath; the hydrogen reservoir configured to store the fluid hydrogen as liquid hydrogen; the oxygen reservoir configured to store the fluid oxygen as liquid oxygen; the heat exchanger system configured to transfer heat energy from the combustion products to at least one of the fluid hydrogen as the fluid delivery system directs the fluid hydrogen towards the engine combustor; or the fluid oxygen as the fluid delivery system directs the fluid oxygen towards the engine combustor; and the water recovery system including a condenser and an evaporator, the water recovery system configured to extract water from the combustion products using the condenser, and the water recovery system configured to provide the water to a component of the powerplant as steam using an evaporator, wherein the heat exchanger system is fluidly coupled along the flowpath between the engine turbine and the evaporator. 17. A method, comprising: providing a powerplant for an aircraft, the powerplant including a mechanical load, an engine combustor, an engine turbine, a hydrogen reservoir, an oxygen reservoir, a water recovery system, an evaporator, a heat exchanger system and a flowpath, the flowpath extending out from the engine combustor and through the engine turbine and the evaporator, and the heat exchanger system fluidly coupled along the flowpath between the engine turbine and the evaporator; directing fluid hydrogen from the hydrogen reservoir to the engine combustor, the fluid hydrogen stored within the hydrogen reservoir as liquid hydrogen; directing fluid oxygen from the oxygen reservoir to the engine combustor, the fluid oxygen stored within the oxygen reservoir as liquid oxygen; combusting the fluid hydrogen with the fluid oxygen within the engine combustor to provide combustion products; directing the combustion products through the engine turbine to rotatably drive the mechanical load; extracting water from the combustion products using the water recovery system; evaporating the water to provide steam using the evaporator; transferring heat energy from the combustion products to at least one of the fluid hydrogen or the fluid oxygen using the heat exchanger system; driving a steam turbine rotor by directing the steam through a steam turbine that includes the steam turbine rotor; and cooling a component of the powerplant using the steam output from the steam turbine.
the working fluid being steam, created by combustion of hydrogen with oxygen · CPC title
of condensing type · CPC title
the engines being only of turbine type (the engines using steam of critical or overcritical pressure F01K7/32; the engines being of extraction or non-condensing type F01K7/34) · CPC title
for driving vehicles, e.g. locomotives · CPC title
Plants modified to use their waste heat, other than that of exhaust, e.g. engine-friction heat · CPC title
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