Variable geometry flush boundary diverter

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United States of America Patent

PATENT NO 9862482
SERIAL NO

14846356

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Abstract

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An airflow diverter system for an aircraft may include an external aircraft surface upstream from an engine inlet and a passage having an upstream opening adjacent the engine inlet. The passage may be configured to channel boundary airflow from the external aircraft surface away from the engine inlet. The diverter system may include an occlusion device configured to selectively open and close the opening to the passage.

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Patent Owner(s)

Patent OwnerAddress
THE BOEING COMPANY929 LONG BRIDGE DRIVE ARLINGTON VA 22202

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Huynh, Thuy O'Fallon, US 7 37
Werner, Eric Des Peres, US 8 28

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