| 发明名称 |
SYSTEM AND METHOD FOR OPTIMIZING HORIZONTAL TAIL LOADS |
| 摘要 |
A method of controlling an elevator of an aircraft may include identifying a current stabilizer angle of incidence of a stabilizer of the aircraft. The stabilizer may include an elevator pivotably coupled to the stabilizer. The method may further include comparing the current stabilizer angle of incidence with a threshold stabilizer angle of incidence, and selecting an elevator position limit that is more restrictive if the current stabilizer angle of incidence is greater than or equal to the threshold stabilizer angle of incidence. The method may additionally include moving the elevator to a commanded elevator position that is no greater than the elevator position limit. |
| 申请公布号 |
US2016122000(A1) |
申请公布日期 |
2016.05.05 |
| 申请号 |
US201414278868 |
申请日期 |
2014.05.15 |
| 申请人 |
The Boeing Company |
发明人 |
Mahmulyin Vedad |
| 分类号 |
B64C13/04;B64D43/02;B64C5/02;B64C9/00 |
主分类号 |
B64C13/04 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A method of controlling an elevator of an aircraft, comprising:
identifying a current stabilizer angle of incidence of an aircraft, the aircraft including a stabilizer and an elevator pivotably coupled to the stabilizer; comparing the current stabilizer angle of incidence with a threshold stabilizer angle of incidence; and selecting an elevator position limit that is more restrictive if the current stabilizer angle of incidence is greater than or equal to the threshold stabilizer angle of incidence. |
| 地址 |
Chicago IL US |
