The invention belongs to the field of unmanned aerial vehicles, and particularly relates to a self-disintegration unmanned aerial vehicle with a damping function. The waterproof shock-absorbing unmanned aerial vehicle comprises a vehicle head, a vehicle body, wings, a vertical fin and a horizontal tail, and is characterized in that the vehicle head and the vehicle body, the wings and the vertical fin, and the vertical fin and the horizontal tail of the waterproof shock-absorbing unmanned aerial vehicle are connected through connecting parts, and a shock pad is arranged at the bottom of the vehicle body; wherein the connecting part can be disconnected when the connecting part is subjected to impact force larger than a set threshold value during falling, and self-disassembly unloading of the whole unmanned aerial vehicle is achieved. Due to the adoption of the technical scheme, the nose, the fuselage, the wings, the vertical fin and the horizontal tail are made of light waterproof materials. Meanwhile, all the parts are connected through the connecting parts which can be fractured under certain impact force, self-disintegration, buffering, damage resistance and water resistance of the unmanned aerial vehicle are achieved, and the unmanned aerial vehicle flies in rain and snow and lands and is recycled in a water region; the application range of the unmanned aerial vehicle is expanded, and the cost of the unmanned aerial vehicle is greatly reduced.

    本发明属于无人机领域,具体涉及一种具有减震功能的可自解体无人机。所述防水减震无人机包括机头、机身、机翼、垂尾和平尾,其特征在于,所述防水减震无人的机头和机身、机翼和垂尾,以及垂尾和平尾之间均通过接连件连接,且位于机身的底部设有减震垫;其中,所述接连件能够在跌落时受到大于设置阈值以上的冲击力时连接件断开,实现无人机整体自解体卸载。由于采用上述技术方案,本发明的机头、机身、机翼、垂尾和平尾采用轻质防水材料制成,同时各个部件之间采用收到一定冲击力下可断裂的连接件连接,同时实现了无人机自解体缓冲抗损和防水,实现了无人机雨雪飞行和水域降落回收,扩大了无人机的使用范围,大幅度降低了无人机的成本。


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    Titel :

    Self-disintegration unmanned aerial vehicle with damping function


    Weitere Titelangaben:

    一种具有减震功能的可自解体无人机


    Beteiligte:
    WANG ZILONG (Autor:in) / MENG XUHANG (Autor:in) / HAO MINGLEI (Autor:in) / XU XIANG (Autor:in) / CHEN LINGFEI (Autor:in) / HUANG SIJIE (Autor:in) / FAN XIAOJUN (Autor:in)

    Erscheinungsdatum :

    2021-08-20


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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