Helicopter rotor blade

Number of patents in Portfolio can not be more than 2000

United States of America Patent

PATENT NO 4427344
SERIAL NO

06243498

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ATTORNEY / AGENT: (SPONSORED)

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Abstract

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A helicopter rotor blade is disclosed having a root end for attachment to a rotor head, a tip end defining the end of the blade fartherest from the root end with a central portion of aerofoil section extending between and attached to the root end and the tip end to define a rotor radius wherein an outboard region of the central portion has a negative basic pitching moment coefficient of absolute value not less than 0.02 and an inboard region having a basic pitching moment coefficient more positive than that of the outboard region.

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Patent Owner(s)

Patent OwnerAddress
WESTLAND AIRCRAFT LIMITEDYEOVIL SOMERSET

International Classification(s)

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  • 1981 Application Filing Year
  • B64C Class
  • 129 Applications Filed
  • 2 Patents Issued To-Date
  • 1.56 % Issued To-Date
Click to zoom InYear of Issuance% of Matters IssuedCumulative IssuancesYearly Issuances1981198219831984198519861987198819891990199119921993199419951996199719981999200020012002200320042005200620072008200920100255075100

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Perry, Frederick J Sherborne, GB2 8 113

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  • 12 Citation Count
  • B64C Class
  • 0 % this patent is cited more than
  • 41 Age
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