A brake device and an aircraft dispatch temperature indicating system, the brake device comprising a piston seat (21), a plurality of pistons (22), a carbon disc (10) and at least one wear indicating device, the wear indicating device comprising a distance measuring sensor (31) and a cable (32), the distance measuring sensor measuring a distance (R1) between the distance measuring sensor and the carbon disc, the distance measuring sensor and the brake control unit are connected through the cable, the distance measuring sensor comprises a sensor shell (311), a signal generator (312) and a signal receiving part (313), and the distance measuring sensor shell is installed on the piston seat in the mode that the signal generator and the signal receiving part face the carbon disc. The measurement accuracy can be improved, the utilization rate of the carbon disc is improved, the carbon disc replacement time of an airplane is prolonged, and the maintenance cost is reduced. In addition, real-time measurement can be realized, and the carbon disc does not need to be additionally processed.
一种刹车装置和飞机派遣温度指示系统,刹车装置包括活塞座(21)、多个活塞(22)、碳盘(10)和至少一个磨损指示装置,所述磨损指示装置包括测距传感器(31)和线缆(32),所述测距传感器对该测距传感器与所述碳盘之间的距离(R1)进行测量,所述线缆将所述测距传感器与刹车控制单元连接,所述测距传感器包括传感器壳体(311)、信号发生器(312)、信号接收部(313),所述测距传感器以所述信号发生器和所述信号接收部面向所述碳盘的方式,将所述测距传感器壳体安装于所述活塞座。能够提高测量的准确性、提高碳盘的使用率、延长飞机更换碳盘的时间、减少维护费用。此外,能够实现实时测量,且不需要对碳盘进行额外的加工。
Brake device and airplane dispatch temperature indicating system
刹车装置和飞机派遣温度指示系统
2024-11-12
Patent
Electronic Resource
Chinese
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