The invention relates to an unmanned aerial vehicle load structure comprises a first quick assembly part, a second quick assembly part, a damping assembly and a load. The first quick assembly part isprovided with a first power connection port, the second quick assembly part is provided with a second power connection port electrically connected with the load, and the first power connection port isconnected with the second power connection port in an inserted mode; the damping assembly comprises a first shock absorption part, a second shock absorption part and a shock reduction part; the firstquick assembly part is detachably connected with the second quick assembly part, the second quick assembly part is connected with the first shock absorption part, the load is connected with the second shock absorption part, the shock reduction part has elasticity, and the first shock absorption part and the second shock absorption part are respectively connected with the shock reduction part, sothat at least three non-linear connections are realized. Damping between the first damping part and the second damping part can be achieved, meanwhile, it is guaranteed that planes of the first damping part and the second damping part are kept stable, and load stability is guaranteed; and it can be ensured that the position of the shock reduction part relative to the first damping piece or the second damping piece in the vertical direction is stable, and meanwhile the anti-swing effect in the horizontal plane can be improved.

    本发明涉及无人机载荷结构,其包括第一快装件、第二快装件、减震组件及载荷;第一快装件设置有第一接电口,第二快装件设置有与载荷电性连接的第二接电口,第一接电口与第二接电口插接;减震组件包括第一减震件、第二减震件及减少震动件;第一快装件与第二快装件可拆卸地连接,第二快装件与第一减震件连接,载荷与第二减震件连接,减少震动件具备弹性,第一减震件、第二减震件分别与减少震动件连接,而实现至少三处的非直线的连接。本发明能够使第一减震件、第二减震件之间减震的同时确保两者的平面之间保持稳定,保证载荷的稳定;能够确保减少震动件相对第一减震件或第二减震件在竖直方向上的位置稳定,同时能够提高在水平面内的防摆效果。


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    Title :

    Unmanned aerial vehicle load structure


    Additional title:

    无人机载荷结构


    Contributors:
    ZHANG YAN (author) / GU WENREN (author)

    Publication date :

    2021-03-26


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge / F16F SPRINGS , Federn



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