US Patent 11958623 Thermal management system for gas turbine engine
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US Patent 11958623 Thermal management system for gas turbine engine
Article
Patent abstract
A thermal management system for a gas turbine engine includes an additively manufactured nacelle component, at least a portion of the additively manufactured nacelle component forming an additively manufactured heat exchanger that extends into a fan bypass flow.
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Patent Number
Patent Inventor Names
Gary D. Roberge0
Date of Patent
April 16, 2024
0Patent Application Number
179793930
Date Filed
November 2, 2022
0Patent Citations
Patent Primary Examiner
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