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 |