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US Patent 11958623 Thermal management system for gas turbine engine

Overview Structured Data Issues Contributors Activity

Is a

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Patent attributes

Patent Jurisdiction

United States Patent and Trademark Office

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Patent Number

Patent Inventor Names

Gary D. Roberge0

Date of Patent

April 16, 2024

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Patent Application Number

179793930

Date Filed

November 2, 2022

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Patent Citations

US Patent 10914185 Additive manufactured case with internal passages for active clearance control

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US Patent 11519295 Thermal management system for gas turbine engine

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US Patent 6931834 Cooling systems

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US Patent 7856824 Cooling systems for use on aircraft

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US Patent 9051943 Gas turbine engine heat exchanger fins with periodic gaps

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US Patent 9233757 Nacelle

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US Patent 9599410 Plate-like air-cooled engine surface cooler with fluid channel and varying fin geometry

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US Patent 9844807 Tube with fins having wings

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Patent Primary Examiner

Christopher R Legendre

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CPC Code

0

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F05D 2260/22141

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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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