发明名称 Tail Rotor Actuation System
摘要 In some embodiments, an actuation system includes a an actuator assembly, a yoke, and a control rod. The actuator assembly comprises a first actuator. The first actuator is configured to extend in a first direction and retract in a second direction opposite of the first direction. The yoke is coupled to the first actuator at a first actuator end proximate to the first direction. The control rod is coupled to the yoke at a first control rod end and extends in the second direction past the actuator assembly to a second end in mechanical communication with an output device.
申请公布号 US2016200430(A1) 申请公布日期 2016.07.14
申请号 US201414286197 申请日期 2014.05.23
申请人 Bell Helicopter Textron Inc. 发明人 Dickman Corey;Fenny Carlos A.;Schultz David
分类号 B64C27/12;B64C13/50;B64C27/82 主分类号 B64C27/12
代理机构 代理人
主权项 1. A rotorcraft, comprising: a body; a power train coupled to the body and comprising an engine and a drive shaft coupled to the engine; a rotor system coupled to the power train, the rotor system comprising at least one rotor blade; and an actuation system in mechanical communication with the rotor system, the actuation system comprising: an actuator assembly comprising a first actuator, the first actuator configured to extend in a first direction and retract in a second direction opposite of the first direction; a yoke coupled to the first actuator at a first actuator end proximate to the first direction; a control rod coupled to the yoke at a first control rod end and extending in the second direction past the actuator assembly to a second end in mechanical communication with the rotor system.
地址 Fort Worth TX US