US Patent 11408368 Reconfigurable exhaust nozzle for a gas turbine engine
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Patent Number
114083680
Date of Patent
August 9, 2022
0Patent Application Number
168360800
Date Filed
March 31, 2020
0Patent Primary Examiner
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Patent Jurisdiction
Patent Number
114083680
Date of Patent
August 9, 2022
0Patent Application Number
168360800
Date Filed
March 31, 2020
0Patent Primary Examiner
CPC Code
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US Patent 11408368 Reconfigurable exhaust nozzle for a gas turbine engine
Article
A propulsion unit includes a gas turbine engine arranged along an axis and an exhaust system coupled to the gas turbine engine. The gas turbine engine includes an engine core configured to discharge a core flow and a fan configured to be driven by the engine core to discharge a bypass flow. The exhaust system receives the mixed bypass and core flows from the gas turbine engine.
Infobox
Is a
Patent jurisdiction
Patent number
11408368
Date of patent
August 9, 2022
Patent application number
16836080
Date Filed
March 31, 2020
Patent primary examiner
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