- 专利标题: METHOD TO MEASURE AIRCRAFT HIGH-LIFT SYSTEM BRAKE RESPONSE TIME
-
申请号: US15587546申请日: 2017-05-05
-
公开(公告)号: US20180319483A1公开(公告)日: 2018-11-08
- 发明人: Timothy Michael Mayer , Artemio Pérez , Victor Barger
- 申请人: HAMILTON SUNDSTRAND CORPORATION
- 主分类号: B64C13/50
- IPC分类号: B64C13/50 ; B60T8/17 ; B60T17/22 ; B64C9/24 ; B64C9/18 ; B64D45/00 ; H02P29/04 ; H02P29/024 ; H02K7/102 ; H02K11/21 ; H02K11/24 ; H02K7/14
摘要:
A braking test for a high lift system. The system including a plurality of high lift surfaces movably arranged at a wing, a plurality of drive stations coupled with the high lift surfaces via a transmission shaft, a power drive unit coupled with the transmission shaft including an electric motor operably coupled with a brake, and a control unit operably coupled to the power drive unit. The control unit executing a method for testing the brake, including actuating an electric motor, acquiring a sensor output of a sensor coupled during the actuating of the motor and determining a motion of the motor, activating a selected brake under test, measuring an elapsed time until the brake has arrested the motion, and determining if the elapsed time is less than a threshold. Generating a brake failure signal for the selected brake if the elapsed time exceeds the threshold.
公开/授权文献
信息查询