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公开(公告)号:US6076767A
公开(公告)日:2000-06-20
申请号:US931670
申请日:1997-09-17
CPC分类号: F15B11/22 , B64C13/38 , B64D45/0005 , B64D2045/001
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.
摘要翻译: 提供了一种飞行控制表面致动系统,其中多个致动器(6-13)彼此连接以便使其操作同步。 每个致动器具有其自己的变速箱,使得在同步元件中传递的扭矩保持为低。