The embodiment of the invention discloses a deformation monitoring device for an aircraft wing. The deformation monitoring device comprises a flexible capacitor assembly, a direct-current power supplyand a current monitoring module, the flexible capacitor assembly is attached to the inner side of a wing skin, one electrode of the flexible capacitor assembly is connected to one end of the direct-current power source, and the other electrode of the flexible capacitor assembly is connected to the other end of the direct-current power source through the current monitoring module. And the currentmonitoring module is configured to monitor current generated in a loop formed by the flexible capacitor assembly, the direct-current power supply and the current monitoring module. According to the embodiment of the invention, a driver can know the deformation condition of the wing at any time, so that the problem of harmful wing deformation or damage caused by overlarge overload is avoided.

    本发明实施例公开了一种飞机机翼的形变监测装置,包括:柔性电容组件,直流电源和电流监控模块;柔性电容组件贴合于机翼蒙皮的内侧,柔性电容组件的一个电极连接到直流电源的一端,另一个电极通过电流监控模块连接到直流电源的另一端;电流监控模块,被配置为监测柔性电容组件,直流电源和电流监控模块形成的回路中产生的电流。本发明实施例实现了驾驶员随时了解机翼的变形情况,从而避免因过载过大产生有害的机翼变形或破坏的问题。


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    Title :

    Deformation monitoring device for aircraft wing


    Additional title:

    一种飞机机翼的形变监测装置


    Contributors:
    LI CHI (author)

    Publication date :

    2020-05-19


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen / G01B MEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS , Messen der Länge, der Dicke oder ähnlicher linearer Abmessungen



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