Supersonic caret inlet system leading edge slat for improved inlet performance at off-design flight conditions

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United States of America Patent

PATENT NO 9964038
SERIAL NO

14659148

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Abstract

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An engine inlet for efficient operation at both design Mach number and off-design Mach numbers with an inlet having a caret configuration with rotatably extending effective leading edges on the inlet from a retracted position aligned with a nominal Mach number shock wave to an extended position aligned with an off-design Mach number shock wave.

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Patent Owner(s)

Patent OwnerAddress
THE BOEING COMPANYCHICAGO IL

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Inventor(s)

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

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