Cryogenic bottoming cycle with variable fluid mixture
AssigneeRtx Corporation
InventorsBrandon M. Evans, Neil J. Terwilliger
Life of this patent
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AssigneeRtx Corporation
InventorsBrandon M. Evans, Neil J. Terwilliger
Estimating the term…
An aircraft propulsion system includes a core engine that includes a main compressor where an inlet airflow is compressed and communicated to a combustor to generate an exhaust gas flow that is expanded through a main turbine section to generate power used to drive the main compressor and a propulsive fan, a bottoming cycle where a working fluid mixture within a closed circuit is heated and expanded through a bottom turbine to generate shaft power, the working fluid mixture includes at least two fluids that have different properties that change a capability of the working fluid mixture at different bottoming cycle operating points, a first heat exchanger where heat is input into the working fluid mixture, and a second heat exchanger where the working fluid mixture is cooled.
An aircraft propulsion system comprising:
A gas turbine engine comprising:
A method of operating an aircraft propulsion system comprising:
Dependencies are inferred from the claim text.