| 发明名称 |
Aircraft Flight Control Surface Actuation Monitoring System and Method |
| 摘要 |
A system for monitoring actuation of a flight control surface, the flight control surface being connected to a track that moves the flight control surface between at least a retracted position and an extended position, the system including a rack connected to the track, a pinion engaged with the rack and a rotation detector operatively connected to the pinion. |
| 申请公布号 |
US2017073082(A1) |
申请公布日期 |
2017.03.16 |
| 申请号 |
US201514850084 |
申请日期 |
2015.09.10 |
| 申请人 |
The Boeing Company |
发明人 |
Ungar Lior;Soderquist Timothy J. |
| 分类号 |
B64D45/00;B64C9/22 |
主分类号 |
B64D45/00 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A system for monitoring actuation of a flight control surface, said flight control surface being connected to a track that moves said flight control surface between at least a retracted position and an extended position, said system comprising:
a rack connected to said track; a pinion engaged with said rack; and a rotation detector operatively connected to said pinion. |
| 地址 |
Chicago IL US |
