Invention Grant
- Patent Title: Aircraft control surface operating device
- Patent Title (中): 飞机控制面操作装置
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Application No.: US13275676Application Date: 2011-10-18
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Publication No.: US08596582B2Publication Date: 2013-12-03
- Inventor: Minoru Uchida , Hiroshi Yamanouchi
- Applicant: Minoru Uchida , Hiroshi Yamanouchi
- Applicant Address: US CA Torrance
- Assignee: Honda Patents & Technologies North America, LLC
- Current Assignee: Honda Patents & Technologies North America, LLC
- Current Assignee Address: US CA Torrance
- Agency: Rankin Hill & Clark LLP
- Main IPC: B64C9/00
- IPC: B64C9/00

Abstract:
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.
Public/Granted literature
- US20120091283A1 AIRCRAFT CONTROL SURFACE OPERATING DEVICE Public/Granted day:2012-04-19
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