An attitude-adjustable landing buffer device for an unmanned aerial vehicle includes a pressure lever assembly connected to the unmanned aerial vehicle so that the unmanned aerial vehicle is subjected to an impact load from the unmanned aerial vehicle when landing, and when the pressure lever assembly is subjected to the impact load, the pressure lever assembly moves away from an original position; the energy absorption mechanism is connected to the pressing rod assembly and is configured to absorb the impact load transmitted to the pressing rod assembly; and the posture adjusting assembly can be operated to move and selectively connected with or separated from the pressing rod assembly, and after the energy absorption mechanism completes absorption of the impact load, the posture adjusting assembly is operated to be connected with the pressing rod assembly and drives the pressing rod assembly to move back to the original position.

    一种用于无人飞行器的可调姿着陆缓冲装置,包括压杆组件,该压杆组件连接于无人飞行器,使得在无人飞行器着陆时经受来自无人飞行器的冲击载荷,其中,当压杆组件经受冲击载荷时,压杆组件运动远离原始位置;吸能机构,该吸能机构连接于压杆组件,并构造成吸收传递至压杆组件的冲击载荷;以及调姿组件,该调姿组件能够被操作以进行运动,以及选择性地与压杆组件接合或分离,其中,当吸能机构完成对冲击载荷的吸收之后,调姿组件被操作以接合压杆组件,并带动压杆组件运动回到原始位置。


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    Title :

    Attitude-adjustable landing buffer device for unmanned aerial vehicle


    Additional title:

    一种用于无人飞行器的可调姿着陆缓冲装置


    Contributors:
    YU LIANG (author) / MEI RONG (author) / SUN JIANYU (author) / MA WENBO (author)

    Publication date :

    2024-11-22


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64U / B64C AEROPLANES , Flugzeuge



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