| 发明名称 |
Backup System |
| 摘要 |
A system and method for a number of backup systems in an aircraft. The apparatus comprises a movement system; a latch system; a lock system; and at least one of a backup valve, a backup actuator, or a backup power source connected to at least one of the movement system, the latch system, or the lock system. The movement system has a first number of actuators and is connected to a hydraulic power source. The latch system has a second number of actuators and is connected to the hydraulic power source. The lock system has a third number of actuators and is connected to the hydraulic power source. |
| 申请公布号 |
US2016251073(A1) |
申请公布日期 |
2016.09.01 |
| 申请号 |
US201414535864 |
申请日期 |
2014.11.07 |
| 申请人 |
The Boeing Company |
发明人 |
Good Mark Steven;Lassen Matthew August;Renzelmann Michael E.;Gardner Mark J.;Lesyna Mark William;Hill Brian Curtis;Tyler Nicholas Seth |
| 分类号 |
B64C3/56;B64C13/50;B64C13/42 |
主分类号 |
B64C3/56 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A method comprising:
determining whether each of a movement system, a latch system, and a lock system is responsive; and in response to determining one of the movement system, the latch system, or the lock system is not responsive, utilizing at least one of a backup valve, a backup actuator, or a backup power source to perform an operation of a folding wing tip with at least one of the movement system, the latch system, or the lock system. |
| 地址 |
Chicago IL US |
