| 发明名称 |
MAST DAMPENER AND COLLECTIVE PITCH FOR A ROTORCRAFT |
| 摘要 |
An embodiment includes a system for controlling blade pitch in a rotorcraft having an engine; a drive shaft with a first end and a second end and connected at the first end to the engine; a rotor with two or more blades connected to the second end of the drive shaft; and one or more actuators positioned adjacent to the rotor blades operable to change a blade pitch of the rotor blades. |
| 申请公布号 |
US2016257399(A1) |
申请公布日期 |
2016.09.08 |
| 申请号 |
US201514645348 |
申请日期 |
2015.03.11 |
| 申请人 |
Carter Aviation Technologies, LLC |
发明人 |
Carter, JR. Jay W.;Lewis Jeffrey R.;Robinson M. Keith |
| 分类号 |
B64C27/72;B64C27/59;B64C27/57;B64C27/02 |
主分类号 |
B64C27/72 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A system for controlling blade pitch in a rotorcraft, comprising:
a drive mechanism; a rotor having two or more blades connected to the drive mechanism; and one or more actuators positioned adjacent to the rotor blades operable to change a blade pitch of the rotor blades. |
| 地址 |
Wichita Falls TX US |
