A pressurizing device and method, for pressurizing a first tank, the device including at least a second tank configured to contain a cryogenic fluid, a first pressurizing circuit for putting the second tank into communication with the first tank, the first pressurizing circuit including at least a f
A pressurizing device and method, for pressurizing a first tank, the device including at least a second tank configured to contain a cryogenic fluid, a first pressurizing circuit for putting the second tank into communication with the first tank, the first pressurizing circuit including at least a first heat exchanger for heating a flow of the cryogenic fluid extracted from the second tank through the first pressurizing circuit, and a second pressurizing circuit with a compressor, branched off from the first pressurizing circuit and leading to the second tank. A feed system for feeding a reaction engine with at least a first liquid propellant includes at least a first tank configured to contain the first liquid propellant, and a device for pressurizing the first tank.
대표청구항▼
1. A pressurizing device for pressurizing a first tank, the device comprising: a second tank configured to contain a cryogenic fluid;a first pressurizing circuit to put the second tank into communication with the first tank, the first pressurizing circuit including at least a first heat exchanger to
1. A pressurizing device for pressurizing a first tank, the device comprising: a second tank configured to contain a cryogenic fluid;a first pressurizing circuit to put the second tank into communication with the first tank, the first pressurizing circuit including at least a first heat exchanger to heat a flow of the cryogenic fluid extracted from the second tank through the first pressurizing circuit; anda second pressurizing circuit including a compressor, branched off from the first pressurizing circuit and leading to the second tank. 2. A pressurizing device according to claim 1, wherein the second pressurizing circuit is branched off from the first pressurizing circuit upstream from the first heat exchanger. 3. A pressurizing device according to claim 1, wherein the second pressurizing circuit is branched off from the first pressurizing circuit downstream from the first heat exchanger. 4. A pressurizing device according to claim 1, further comprising a turbine to drive the compressor. 5. A pressurizing device according to claim 1, further comprising an electric motor to drive the compressor. 6. A feed system for feeding a reaction engine with at least a first liquid propellant, the system comprising: a first tank configured to contain the first liquid propellant; anda pressurizing device to pressurize the first tank, the device comprising: a second tank configured to contain a cryogenic fluid;a first pressurizing circuit to put the second tank into communication with the first tank, the first pressurizing circuit including at least a first heat exchanger to heat a flow of the cryogenic fluid extracted from the second tank through the first pressurizing circuit; anda second pressurizing circuit including a compressor, branched off from the first pressurizing circuit and leading to the second tank. 7. A feed system according to claim 6, wherein the cryogenic fluid of the second tank is inert. 8. A feed system according to claim 7, wherein the cryogenic fluid of the second tank is helium. 9. A feed system according to claim 7, wherein the cryogenic fluid of the second tank is nitrogen. 10. A feed system according to claim 6, wherein the first liquid propellant is an oxidizer. 11. A feed system according to claim 6, wherein the first liquid propellant is a cryogenic liquid with a condensation point higher than that of the cryogenic fluid of the second tank. 12. A feed system according to claim 6, further comprising at least one turbopump to pump at least the first liquid propellant, and a hot gas generator to drive the at least one turbopump, the first heat exchanger configured to heat the flow of cryogenic fluid extracted from the second tank using heat generated by the hot gas generator. 13. A method of pressurizing a first tank, wherein a flow of cryogenic fluid is extracted from a second tank through a first pressurizing circuit, and is heated in at least a first heat exchanger, the heated flow then being introduced into the first tank to pressurize the heated flow, the method comprising: compressing, by a compressor of a second pressurizing circuit, a second portion of the flow extracted from the second tank that is taken from the first pressurizing circuit via the second pressurizing circuit, and introducing the second portion of the flow into the second tank to pressurize the second tank.
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이 특허에 인용된 특허 (5)
Henderson, John B.; Goodzeit, Neil E., Enhanced high-efficiency spacecraft propulsion system.
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