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US Patent 11542866 Adaptable flow control for engine nacelles
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Patent
Date Filed
May 13, 2020
Date of Patent
January 3, 2023
Patent Application Number
15931328
Patent Citations
US Patent 10605113 Methods and apparatus for reducing flow distortion at engine fans of nacelles
US Patent 10131443 Aircraft engine nacelle
US Patent 10161773 Methods and apparatus to determine airflow conditions at an inlet of an engine
Patent Jurisdiction
United States Patent and Trademark Office
Patent Number
11542866
Patent Primary Examiner
Alain Chau
CPC Code
F02C 6/08
F02C 7/04
F02C 7/042
F02C 7/057
B64D 33/02
B64D 2033/0226
B64C 21/04
B64C 21/06
F02C 6/06
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