US Patent 11286881 Gas turbine engine with reversible heat exchanger
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Patent Number
112868810
Date of Patent
March 29, 2022
0Patent Application Number
166547060
Date Filed
October 16, 2019
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Patent Number
112868810
Date of Patent
March 29, 2022
0Patent Application Number
166547060
Date Filed
October 16, 2019
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US Patent 11286881 Gas turbine engine with reversible heat exchanger
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A gas turbine engine system includes a gas turbine engine having a fan bypass duct, a heat exchanger system, and a flow transfer unit configured to selectively allow or preclude flow between the fan bypass duct and the heat exchanger system. A controller is coupled to and configured to vary the state of one or more of a fan exit nozzle, a heat exchanger exit nozzle, and a flow control valve controlling flow between the fan bypass duct and the heat exchanger system.
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Patent jurisdiction
Patent number
11286881
Date of patent
March 29, 2022
Patent application number
16654706
Date Filed
October 16, 2019
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