Optimised nozzle geometry

Number of patents in Portfolio can not be more than 2000

United States of America

PATENT NO 12187420
APP PUB NO 20220306309A1
SERIAL NO

17635122

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Abstract

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A compressed gas ejection assembly for a rotating wing aircraft blade comprising a compressed gas passage adapted to allow a substantially constant mass flow through the compressed gas ejection assembly across at least a portion of the width of the compressed gas ejection assembly.

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Patent Owner(s)

Patent OwnerAddress
GENESIS AEROTECH LIMITED67B CARNLEA ROAD FINTONA COUNTY TYRONE BT78 2JD

International Classification(s)

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Leslie, Martin Fintona, GB 3 0
Mallon, Patrick Fintona, GB 5 71
Rice, Michael Fintona, GB 100 5907

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