The invention discloses a buffering landing gear for an unmanned aerial vehicle. The buffering landing gear comprises supporting modules, a hydraulic module, a driving module, a ventilation cover, a connecting plate and a supporting cover; the driving module is arranged in the middle of the interior of the supporting cover; the hydraulic module is arranged on the outer side of the driving module;the supporting modules are arranged at the four corners of the supporting cover; and the connecting plate is fixedly connected to the upper portion of the supporting cover through the ventilation cover. The supporting modules are arranged, when the unmanned aerial vehicle takes off, supporting legs can be folded, so that the resistance between the supporting legs and the air during flight of the unmanned aerial vehicle is reduced, the cruising ability of the unmanned aerial vehicle is improved; the driving module is adopted, when the unmanned aerial vehicle lands, upward thrust can be providedfor the unmanned aerial vehicle, so that the impact force between the supporting legs and a bottom surface during the landing of the unmanned aerial vehicle is reduced.

    本发明公开了一种无人机缓冲起落装置,包括支撑模块、液压模块、驱动模块、透气罩、连接板和支撑罩,所述支撑罩内部的中部设置有驱动模块,驱动模块的外侧设置有液压模块,所述支撑罩的四角处均设置有支撑模块,所述支撑罩的上方通过透气罩固定连接有连接板。本发明通过设置支撑模块,当无人机起飞时,而可以将支撑腿收起,从而减少无人机在飞行时支撑腿与空气之间的阻力,进而提高了无人机的续航能力,通过设置驱动模块,当无人机降落时,可以为无人机提供一个向上的推力,从而降低无人机降落时支撑腿与底面的冲击力。


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    Titel :

    Buffering landing gear of unmanned aerial vehicle


    Weitere Titelangaben:

    一种无人机缓冲起落装置


    Beteiligte:
    CAO JIANBAO (Autor:in)

    Erscheinungsdatum :

    2020-09-15


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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