The invention discloses an airplane wheel brake torque testing device which comprises a left clamping plate and a right clamping plate which are arranged on the left and right, the left clamping plateand the right clamping plate are connected through a moving assembly, and the moving assembly is used for driving the left clamping plate and the right clamping plate to get close to each other or get away from each other. One side of the moving assembly is provided with a ruler which moves in the reverse direction of the moving assembly and is used for detecting the distance between the left clamping plate and the right clamping plate, the ruler is slidably provided with a testing assembly, and the testing assembly is provided with a testing opening used for testing torque. The device has the beneficial effect of conveniently and accurately measuring the brake torque of the wheel mounted on the undercarriage.

    本发明公开了一种机轮刹车力矩测试装置,包括左右设置的左夹板与右夹板,所述左夹板与右夹板之间通过移动组件连接,所述移动组件用于带动左夹板与右夹板相互靠近或相互远离;所述移动组件的一侧设置有与移动组件逆向移动且用于检测左夹板与右夹板之间间距的标尺,所述标尺上滑动设置有测试组件,所述测试组件上设置有用于测试力矩的测试口;本发明具有针对安装在起落架上机轮进行便捷准确测量其刹车力矩的有益效果。


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    Title :

    Airplane wheel brake torque testing device


    Additional title:

    一种机轮刹车力矩测试装置


    Contributors:
    CHENG LINGPIN (author) / CHEN HU (author) / WANG BO (author)

    Publication date :

    2020-10-30


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    G01L Messen von Kraft, mechanischer Spannung, Drehmoment, Arbeit, mechanischer Leistung, mechanischem Wirkungsgrad oder des Drucks von Fluiden , MEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE / 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



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