| 发明名称 |
TAIL ROTOR FAILURE RECOVERY CONTROLLER |
| 摘要 |
A tail rotor recovery control system has a detection module configured to detect a loss of tail rotor drive from a tail rotor sensor of an aircraft; and a regulation module configured to augment or deactivate manual flight control signals and transmit automated signals to control modules of a primary flight control system. The automated signals facilitate the aircraft to attain or maintain a preset tip path plane level, attain or maintain a preset aircraft state, or to execute an automated recovery to forward flight. |
| 申请公布号 |
US2016325830(A1) |
申请公布日期 |
2016.11.10 |
| 申请号 |
US201615145264 |
申请日期 |
2016.05.03 |
| 申请人 |
Sikorsky Aircraft Corporation |
发明人 |
Waltner Peter James;Knaust Glen |
| 分类号 |
B64C27/82;B64D25/00;B64C27/57;B64C27/605;G05D1/08;B64C13/16 |
主分类号 |
B64C27/82 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A tail rotor recovery control system comprising:
a detection module configured to detect a loss of tail rotor drive from a tail rotor sensor of an aircraft; and a regulation module configured to augment or deactivate manual flight control signals and transmit automated signals to control modules of a primary flight control system, the automated signals facilitate the aircraft to maintain or attain a tip path plane level or aircraft state. |
| 地址 |
Stratford CT US |
