Gas turbine engine driven by supercritical power generation system
First Claim
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1. A gas turbine engine, comprising:
- a shaft having a first air compressor coupled thereto;
a combustor positioned to receive compressed air from the first compressor;
a power source coupled to the shaft, the power source powered by a working fluid other than the compressed air, the power source including;
a second compressor coupled to the shaft;
a turbine coupled to the shaft; and
a first closed circuit that directs a working fluid from a heat exchanger, through the second compressor, through the combustor, to the turbine, and to the heat exchanger, providing power from the turbine to the shaft; and
a second closed circuit that draws the working fluid from the heat exchanger, passes the working fluid through at least one expansion device and to at least one evaporator to receive thermal load, and to at least one third compressor that is coupled to at least one related shaft.
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Abstract
A gas turbine engine includes a shaft having a first air compressor coupled thereto, a combustor positioned to receive compressed air from the first compressor, and a power source coupled to the shaft, the power source powered by a working fluid other than the compressed air.
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Citations
14 Claims
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1. A gas turbine engine, comprising:
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a shaft having a first air compressor coupled thereto; a combustor positioned to receive compressed air from the first compressor; a power source coupled to the shaft, the power source powered by a working fluid other than the compressed air, the power source including; a second compressor coupled to the shaft; a turbine coupled to the shaft; and a first closed circuit that directs a working fluid from a heat exchanger, through the second compressor, through the combustor, to the turbine, and to the heat exchanger, providing power from the turbine to the shaft; and a second closed circuit that draws the working fluid from the heat exchanger, passes the working fluid through at least one expansion device and to at least one evaporator to receive thermal load, and to at least one third compressor that is coupled to at least one related shaft. - View Dependent Claims (2, 3, 4, 5)
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6. A method of providing power, comprising:
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passing compressed air from a first compressor to a combustor, wherein the first compressor is coupled to a shaft; providing power to the shaft using a working fluid other than the compressed air; passing the working fluid in a closed circuit from a heat exchanger to a second compressor; passing the working fluid from the second compressor to the combustor; passing the working fluid from the combustor to a turbine that is coupled to the shaft; passing the working fluid from the turbine to the heat exchanger; drawing the working fluid from the heat exchanger; passing the drawn working fluid through at least one expansion device and to at least one evaporator; receiving a thermal load in the working fluid, heating the working fluid that is in said at least one evaporator; and compressing the heated working fluid from at least one said evaporator in at least one third compressor that is coupled to at least one related shaft. - View Dependent Claims (7, 8, 9, 10)
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11. A device, comprising:
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a shaft having a thrust-producing device coupled thereto; a combustor positioned to receive compressed air from the thrust-producing device; a power circuit coupled to the shaft, the power circuit powered by carbon dioxide, the power circuit including; a carbon dioxide compressor coupled to the shaft; a carbon dioxide turbine coupled to the shaft; and flow lines that direct the carbon dioxide through the carbon dioxide compressor, to the combustor, to the carbon dioxide turbine, and to a heat exchanger, providing power from the carbon dioxide turbine to the shaft; and a cooling circuit that draws the carbon dioxide from the heat exchanger, passes the carbon dioxide through at least one expansion device and to at least one evaporator to receive thermal load, and to at least one second carbon dioxide compressor that is coupled to at least one related shaft. - View Dependent Claims (12, 13, 14)
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Specification