Invention Grant
- Patent Title: Aircraft control surface drive mechanism
- Patent Title (中): 飞机控制面驱动机构
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Application No.: US13476844Application Date: 2012-05-21
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Publication No.: US08757544B2Publication Date: 2014-06-24
- Inventor: Koji Ito
- Applicant: Koji Ito
- Applicant Address: JP Tokyo
- Assignee: Nabtesco Corporation
- Current Assignee: Nabtesco Corporation
- Current Assignee Address: JP Tokyo
- Agency: Studebaker & Brackett PC
- Priority: JP2011-123906 20110602
- Main IPC: B64C13/24
- IPC: B64C13/24 ; B64C13/28

Abstract:
An actuator includes a plurality of cylinder units each including a cylinder and a rod, and is pivotably attached, at a first end thereof, to a control surface. A reaction link is pivotably attached, at a first end thereof, to a fulcrum shaft rotatably supporting the control surface. The reaction link is pivotably attached, at a second end thereof, to a second end of the actuator between the plurality of cylinder units.
Public/Granted literature
- US20120305701A1 AIRCRAFT CONTROL SURFACE DRIVE MECHANISM Public/Granted day:2012-12-06
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