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 US9193479(B2) 申请公布日期 2015.11.24
申请号 US201514668911 申请日期 2015.03.25
申请人 The Boeing Company 发明人 Moy George;Padilla Peter A.
分类号 B64D45/00;B64C13/50;G01R19/165 主分类号 B64D45/00
代理机构 Duft Bornsen & Fettig LLP 代理人 Duft Bornsen & Fettig LLP
主权项 1. A method of monitoring a high-lift system on an aircraft having a first drive station installed on a first side of a flap and a second drive station installed on a second side of the flap, the method comprising: monitoring, at a controller of the high-lift system, a first current draw of a first electric motor in the first drive station for actuating the flap; identifying, at the controller, an expected current draw of the first drive station; comparing, at the controller, the first current draw of the first drive station to the expected current draw of the first drive station to determine if a differential between the first current draw and the expected current draw of the first drive station exceeds a first threshold; and generating a failure signal in the controller if the differential between the first current draw and the expected current draw of the first drive station exceeds the first threshold to indicate a failure in the high-lift system.
地址 Chicago IL US