Invention Grant
US08757544B2 Aircraft control surface drive mechanism 有权
飞机控制面驱动机构

Aircraft control surface drive mechanism
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.
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