| 发明名称 |
MONITORING OF HIGH-LIFT SYSTEMS FOR AIRCRAFT |
| 摘要 |
Monitoring of high-lift systems for aircraft. In one configuration, a method for monitoring a high-lift system includes monitoring a first current draw of a first drive station of the high-lift system, and monitoring a second current draw of a second drive station of the high-lift system. The method further includes comparing the first current draw and the second current draw to determine if a differential between the first current draw and the second current draw exceeds a threshold, and generating a failure signal if the differential between the first current draw and the second current draw exceeds the threshold. |
| 申请公布号 |
US2014297102(A1) |
申请公布日期 |
2014.10.02 |
| 申请号 |
US201313852828 |
申请日期 |
2013.03.28 |
| 申请人 |
THE BOEING COMPANY |
发明人 |
Moy George;Padilla Peter A. |
| 分类号 |
B64D45/00 |
主分类号 |
B64D45/00 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A method of monitoring a high-lift system on an aircraft, the method comprising:
monitoring a first current draw of a first drive station of the high-lift system; monitoring a second current draw of a second drive station of the high-lift system; comparing the first current draw and the second current draw to determine if a differential between the first current draw and the second current draw exceeds a first threshold; and generating a failure signal if the differential between the first current draw and the second current draw exceeds the first threshold. |
| 地址 |
US |
