According to the unmanned aerial vehicle load elastic launching device, a hollow motor is arranged on a connecting shaft in a sleeving mode, a launching triggering device is arranged, one face of the launching triggering device is fixedly connected with the hollow motor, an elastic triggering mechanism is arranged on the other face of the launching triggering device, and the elastic triggering mechanism is fixedly connected with a fixing sleeve; the elastic launching mechanism is lifted to the optimal elastic launching position through the external lifting mechanism, the hollow motor triggers the elastic triggering mechanism in the process of driving the launching triggering device to rotate, elastic launching of the load is achieved, the load projection precision can be higher, energy consumption is reduced, and environmental pollution is avoided.

    本发明公开了一种无人机载荷弹性发射装置,通过在连接轴上套装空心电机,设置发射触发装置,其一面与空心电机固定连接,另一面设置弹性触发机构,所述弹性触发机构与固定套筒固定连接;通过外部升降机构将弹性发射机构升降至弹性发射最佳位置,空心电机在带动发射触发装置旋转的过程中触发弹性触发机构,实现载荷的弹性发射,可使载荷投射精度更高,消耗能源降低,无环境污染。


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    Title :

    Unmanned aerial vehicle load elastic launching device


    Additional title:

    一种无人机载荷弹性发射装置


    Contributors:
    WU HUSHENG (author) / LING XIAODONG (author) / ZHENG SHIJUN (author) / ZHAO YU (author) / CHEN XINHANG (author) / LANG CHENGCHANG (author) / TANG YIQI (author) / ZHAO SHENJIE (author) / ZHANG CHAOCHAO (author) / WEI CHAOQIANG (author)

    Publication date :

    2024-09-06


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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