The invention discloses a separated piston device for putting of a folding wing unmanned aerial vehicle, and belongs to the technical field of unmanned aerial vehicle equipment. The separated piston device comprises a piston and a parachute; the upper end face of the piston is used for making contact with the unmanned aerial vehicle. The lower end face of the piston is connected with the parachute. When the piston ascends, the parachute can be automatically unfolded, and the sizes of the piston and the unmanned aerial vehicle are limited. The unmanned aerial vehicle can be separated from the unmanned aerial vehicle in time, and the unmanned aerial vehicle can be repeatedly launched for multiple times. The technical problem that a current unmanned aerial vehicle launcher piston is not disengaged in time, the risk that a propeller of an unmanned aerial vehicle is clamped exists, and therefore take-off of the unmanned aerial vehicle is affected is solved.

    本发明公开的一种用于折叠翼无人机投放的分离式活塞装置,属于无人机装备技术领域,所述分离式活塞装置包括:活塞和降落伞;所述活塞的上端面用于与无人机接触;所述活塞的下端面与降落伞连接;当所述活塞作上升运动时,降落伞能够自动展开,且对活塞和无人机的尺寸进行了限定。本发明既能实现与无人机的及时分离,又能实现多次重复发射无人机。解决了当前无人机发射器活塞脱离不及时,存在卡住无人机螺旋桨的风险,从而影响无人机起飞的技术问题。


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    Titel :

    Separated piston device for putting folding wing unmanned aerial vehicle


    Weitere Titelangaben:

    一种用于折叠翼无人机投放的分离式活塞装置


    Beteiligte:
    WANG BO (Autor:in) / CHEN XIAOQING (Autor:in) / WANG SHEN (Autor:in) / FENG RONG (Autor:in) / MENG ZHIPENG (Autor:in)

    Erscheinungsdatum :

    30.05.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64U / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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