| 发明名称 |
Wingtip Control System |
| 摘要 |
A method and apparatus for a wingtip control system. The wingtip control system comprises a switch system for a flight deck of an aircraft and a controller. The switch system is configured to be placed into an armed state and generate an armed signal. The controller is in communication with the switch system. The controller is configured to receive the armed signal from the switch system, visually indicate a desired position for a wingtip of the aircraft in the switch system in response to an event occurring during operation of the aircraft, and generate a movement command to move the wingtip. |
| 申请公布号 |
US2015108283(A1) |
申请公布日期 |
2015.04.23 |
| 申请号 |
US201314056475 |
申请日期 |
2013.10.17 |
| 申请人 |
The Boeing Company |
发明人 |
Thoreen Adam Marshall;Baer Joshua Jay;Sikora Joseph Adam;Lassen Matthew August;Foster Michael Edwin;Gallagher Timothy P. |
| 分类号 |
B64C13/04;B64C23/06 |
主分类号 |
B64C13/04 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A wingtip control system comprising:
a switch system for a flight deck of an aircraft, wherein the switch system is configured to be placed into an armed state and generate an armed signal; and a controller in communication with the switch system, wherein the controller is configured to receive the armed signal from the switch system; visually indicate a desired position for a wingtip of the aircraft in the switch system in response to an event occurring during operation of the aircraft; and generate a movement command to move the wingtip. |
| 地址 |
Chicago IL US |
