The invention discloses an unmanned aerial vehicle rotor testing device, and relates to the technical field of unmanned aerial vehicles, the unmanned aerial vehicle rotor testing device comprises an L-shaped seat, a top plate is arranged at the upper part of one side of the L-shaped seat, a tension sensor is fixedly arranged at the lower side of the L-shaped seat, a pay-off cover is fixedly arranged at the upper part of the tension sensor, and a traction rope is arranged in the pay-off cover; one end of the traction rope slidably extends out of the interior of the pay-off cover and is connected with a limiting shaft, and the end, away from the traction rope, of the limiting shaft slidably penetrates through the bottom of the top plate and is connected with a positioner. The unmanned aerial vehicle rotor testing device can automatically test the performance condition of the unmanned aerial vehicle rotor, after the unmanned aerial vehicle rises, the lift force condition of the rotor can be detected through the tension sensor so as to judge the quality condition of the unmanned aerial vehicle rotor, and after the test is completed and the unmanned aerial vehicle returns to the initial position, the unmanned aerial vehicle rotor can be automatically tested through the elasticity of the clockwork spring. And the traction rope can be automatically retracted, so that the traction rope can be conveniently stored.

    本发明公开了无人机旋翼测试装置,本发明涉及无人机技术领域,包括L型座,所述L型座的一侧靠上方处设置有顶板,且L型座的下侧固定设置有拉力传感器,拉力传感器的上部固定设置有放线罩,放线罩的内部设置有牵引绳,牵引绳的一端滑动延伸出放线罩的内部并连接有限位轴,限位轴远离牵引绳的一端滑动穿过顶板的底部并连接有定位器。该无人机旋翼测试装置,能够自动的测试无人机旋翼的性能情况,当无人机升起后,通过拉力传感器能够检测旋翼的升力情况,从而判断无人机旋翼的质量情况,当测试完毕后,无人机回到初始位置后,利用发条弹簧的弹性,能够使牵引绳自动的被收回,便于对牵引绳进行收纳。


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    Title :

    Unmanned aerial vehicle rotor wing testing device


    Additional title:

    无人机旋翼测试装置


    Contributors:
    LIU XIAOLONG (author) / LU ZHENHUI (author) / WU JINGYUAN (author) / FU BIQIONG (author) / GUAN YUWEI (author) / LIU CHANGRU (author) / LIN ZHILONG (author) / SHEN TIANHANG (author) / ZHOU RUNSONG (author) / DONG ZIXIA (author)

    Publication date :

    2024-08-09


    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



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