Aircraft control surface operating device

Number of patents in Portfolio can not be more than 2000

United States of America Patent

PATENT NO 8596582
APP PUB NO 20120091283A1
SERIAL NO

13275676

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ATTORNEY / AGENT: (SPONSORED)

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Abstract

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An aircraft control surface operating device is provided for operating a control surface on an aircraft body portion to move between a retracted position and an extended position. The aircraft control surface operating device includes a control surface mounting assembly which movably secures the control surface to the aircraft body portion, a drive arm rotatable about a drive axis relative to the aircraft body portion, an actuator for rotating the drive, and a drive link connecting the drive arm to the control surface mounting assembly. The drive link has a control end connected to the control surface mounting assembly and a driven end connected to the drive arm via a drive bearing joint. The drive link connects the drive arm and the control surface mounting assembly such that rotation of the drive arm is causes extending or retracting movement of the control surface.

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Patent Owner(s)

Patent OwnerAddress
AMERICAN HONDA MOTOR CO INC1919 TORRANCE BOULEVARD TORRANCE CA 90501

International Classification(s)

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Uchida, Minoru Tokyo, JP 61 507
Yamanouchi, Hiroshi Oak Ridge, US 19 316

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Patent Citation Ranking

  • 16 Citation Count
  • B64C Class
  • 67.86 % this patent is cited more than
  • 12 Age
Citation count rangeNumber of patents cited in rangeNumber of patents cited in various citation count ranges15156551492101 - 1011 - 2021 - 3031 - 4041 - 5071 - 800102030405060708090100110120130140150160170

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