Helicopter blade aerofoil

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United States of America Patent

PATENT NO 5961290
SERIAL NO

09023699

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Abstract

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The coordinates defining the upper surface, lower surface, leading edge configuration and center of circle for a helicopter blade airfoil are given to increase maximum lift coefficient and lift-to-drag ratio, and to reduce noise level.

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Patent Owner(s)

Patent OwnerAddress
ADVANCED TECHNOLOGY INSTITUTE OF COMMUTER-HELICOPTER LTD2 KAWASAKI-CHO KAKAMIGAHARA-SHI GIFU

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Aoki, Makoto Kakamigahara, JP 185 3294
Nishimura, Hiroki Kakamigahara, JP 12 218
Yamakawa, Eiichi Kakamigahara, JP 18 488

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