发明授权
US6076767A Flight control surface actuation system 失效
飞行控制面驱动系统

Flight control surface actuation system
摘要:
A flight control surface actuation system is provided in which a plurality of actuators (6-13) are connected to one another in order to synchronize their operation. Each actuator has its own gearbox such that the torque transmitted in the synchronizing element is kept low.
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