Rotor blade for rotary wing aircraft

Number of patents in Portfolio can not be more than 2000

United States of America Patent

PATENT NO 6231308
SERIAL NO

08925526

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ATTORNEY / AGENT: (SPONSORED)

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Abstract

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The root end is attached to the rotor head for rotationally driving. The central portion has aerodynamic characteristics depending on the leading and trailing edges and which extend linearly from the root end in parallel to each other, and the chord dimension therebetween. A planform shape of the blade tip portion is defined by the first leading edge which extends forwardly as the distance from the outboard end of the leading edge of the central portion outwardly increases, the second leading edge and the side edge which are rearwardly swept as the distance from the outboard end of the first leading edge toward outboard side outwardly increases, the first trailing edge which is curved forwardly as the distance from an outboard end of the trailing edge of the central portion outwardly increases, and the second trailing edge which is swept rearwardly as the distance from the outboard end point of the first trailing edge outwardly increases. This configuration makes it possible to eliminate the delocalization in the supersonic region and greatly reduce high-speed impulsive noises.

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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
Kondo, Natsuki Kakamigahara, JP 5 123
Tsujiuchi, Tomoka Kakamigahara, JP 5 47
Yamakawa, Eiichi Kakamigahara, JP 18 488

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