BOTTOMING CYCLE WITH ISOLATED TURBO-GENERATORS
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United States of America Patent
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Issued Date -
Nov 2, 2023
app pub date -
Apr 27, 2022
filing date -
Apr 27, 2022
priority date (Note) -
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Abstract
A propulsion system for an aircraft includes a core engine that includes a core flow path that is in communication with a compressor section, combustor section and a turbine section, the core engine is configured to generate a high energy gas flow, a first cycle turbine that is configured to drive a first cycle compressor at a cycle speed in response to expansion of a heated working fluid flow between a first inlet and a first outlet of the first cycle turbine, and a first power turbine that is configured to drive a first output shaft at a power speed that is different than the cycle speed in response to expansion of a working fluid flow received from the first outlet of the first cycle turbine.
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