Is a
Patent attributes
Patent Jurisdiction
Patent Number
Date of Patent
March 14, 2023
0Patent Application Number
176696800
Date Filed
February 11, 2022
0Patent Citations Received
0
0
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Patent Primary Examiner
Aircraft engines include a burner section and a turbine section arranged along a shaft, wherein an exhaust from the burner section is directed through the turbine section to drive rotation of the turbine section and a core flow path passes through the burner section and then the turbine section. A condenser assembly is arranged downstream of the turbine section along the core flow path. A cryogenic fuel source is configured to supply fuel to the burner section along a fuel line passing through the condenser assembly and the fuel within the fuel line is configured to pick up heat from the exhaust from the burner section and condense water therefrom.
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