发明名称 |
MONITORING DEVICE FOR AN ACTUATION SYSTEM OF AN AIRCRAFT, ACTUATION SYSTEM AND METHOD FOR RECONFIGURING THE ACTUATION SYSTEM |
摘要 |
A monitoring device is disclosed for an actuation system of an aircraft for monitoring a guiding device of a regulating flap with a load sensor. An actuation system with the monitoring device and a method for reconfiguring such an actuation system are disclosed. The monitoring device includes an interface to the load sensor and an interface to a driving device for adjusting the regulating flap. The monitoring device can determine or receive in-flight information actively signaling a predefined flight attitude and/or a predefined operational state of the aircraft. The monitoring device can compare a load value corresponding to a sensor value acquired by the load sensor and a limiting value corresponding to a minimum operational load for the predefined flight attitude and/or the predefined operational state of the aircraft and a monitoring function. The monitoring function can assign a fault mode to the regulating flap.
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申请公布号 |
US2013261852(A1) |
申请公布日期 |
2013.10.03 |
申请号 |
US201313790960 |
申请日期 |
2013.03.08 |
申请人 |
RECKSIEK MARTIN;HEINTJES MARK;WINKELMANN CHRISTOPH;AIRBUS OPERATIONS GMBH |
发明人 |
RECKSIEK MARTIN;HEINTJES MARK;WINKELMANN CHRISTOPH |
分类号 |
B64C13/24 |
主分类号 |
B64C13/24 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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