发明名称 Flight control surface actuation system
摘要 A flight control surface actuation system has a plurality of actuators attached to one or more summing levers. Each summing lever has an actuator output point that is attached to the flight control surface. The summing lever position corresponds with a sum of the positions of the actuators attached to it. If one of the actuators jams and becomes immovable, other actuators attached to the same summing lever as the malfunctioning actuator compensates for the malfunctioning actuator to bring the flight control surface to a neutral position. The summing lever makes it possible for flight control surface actuation systems to use actuators other than actuators having a bypass mode or any other features that prevent the actuators from jamming.
申请公布号 US6776376(B2) 申请公布日期 2004.08.17
申请号 US20020274024 申请日期 2002.10.18
申请人 HAMILTON SUNSTRAND 发明人 COLLINS ANDREW J.
分类号 B64C13/30;B64C13/42;B64C13/50;(IPC1-7):B64C9/02 主分类号 B64C13/30
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