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发明申请
US20070018040A1 Flight control surface actuation system with redundantly configured and lockable actuator assemblies 有权
飞行控制表面致动系统，具有冗余配置和可锁定的执行器组件

Flight control surface actuation system with redundantly configured and lockable actuator assemblies
摘要：
A flight control surface actuator assembly includes a pair of flight control surface actuators and a pivot arm. One of the flight control surface actuators is coupled to a flight control surface and a static airframe structure, the other flight control surface actuator is coupled to the flight control surface and the pivot arm. The pivot arm coupled to the static airframe structure and is configured to pivot relative to the second flight control surface actuator and the static airframe structure.
摘要（中）：

飞行控制表面致动器组件包括一对飞行控制表面致动器和枢转臂。 飞行控制表面致动器中的一个联接到飞行控制表面和静态机身结构，另一个飞行控制表面致动器联接到飞行控制表面和枢转臂。 枢转臂联接到静态机身结构并且构造成相对于第二飞行控制表面致动器和静止机身结构枢转。

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