| 发明名称 |
SYSTEM AND METHOD FOR OPTIMIZING PERFORMANCE OF AN AIRCRAFT |
| 摘要 |
A system for optimizing performance of an aircraft may include a flight control computer for computing an optimum flap setting based on aircraft data. The system may further include a flap control system having a flap control device. The system may additionally include a flap actuation system coupled to the flap control system for positioning the trailing edge device at the optimum flap setting. |
| 申请公布号 |
US2015083850(A1) |
申请公布日期 |
2015.03.26 |
| 申请号 |
US201314034920 |
申请日期 |
2013.09.24 |
| 申请人 |
The Boeing Company |
发明人 |
Moser Matthew A.;Finn Michael R.;Gardner Mark J.;Murphy Robert M.;Thoreen Adam |
| 分类号 |
B64C13/16 |
主分类号 |
B64C13/16 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A system for optimizing performance of an aircraft, comprising:
a flight control computer configured to compute an optimum flap setting based on aircraft data; a flap control system having a flap control device; and a flap actuation system coupled to the flap control system and being configured to position a trailing edge device at the optimum flap setting. |
| 地址 |
Chicago IL US |
