Supersonic caret inlet system

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United States of America Patent

PATENT NO 9874144
SERIAL NO

14603666

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ATTORNEY / AGENT: (SPONSORED)

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Abstract

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An engine inlet for efficient operation in both subsonic and supersonic flight wherein the inlet has a caret configuration is rotatable about an off-body axis for compression ramp angle and capture area variation and a diffuser is engaged to the inlet in a scrubbing relationship to maintain a seal upon rotation of the inlet.

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Patent Owner(s)

Patent OwnerAddress
THE BOEING COMPANY929 LONG BRIDGE DRIVE ARLINGTON VA 22202

International Classification(s)

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Huynh, Thuy Ofallon, US 7 37

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