The invention relates to the technical field of unmanned aerial vehicle damping, in particular to a geological exploration unmanned aerial vehicle landing damping support which comprises a connecting plate detachably connected with an unmanned aerial vehicle and a plurality of damping rods evenly distributed at the bottom of the connecting plate, and each damping rod comprises an outer cylinder, an inner cylinder, a supporting column and a first spring arranged in the inner cylinder, the upper end of the outer cylinder is connected with the connecting plate, the upper end of the inner cylinder is closed and extends into the outer cylinder to be slidably connected with the inner wall of the outer cylinder, the upper end of the supporting column extends into the inner cylinder to be slidably connected with the inner wall of the outer cylinder in a sealed mode, the upper end of the first spring is fixedly connected with the inner wall of the closed end of the inner cylinder, and the lower end of the first spring is fixedly connected with the upper end of the supporting column. The first limiting mechanism is used for limiting sliding between the supporting column and the inner cylinder; and the second limiting mechanism is used for limiting sliding between the inner cylinder and the outer cylinder. According to the scheme, the exploration unmanned aerial vehicle can land stably, and the inclination and rollover phenomena of the exploration unmanned aerial vehicle are prevented.

    本发明涉及无人机减振技术领域,具体涉及一种地质勘查无人机降落减震支架,包括与无人机可拆卸连接的连接板和均布于连接板底部的多根减震杆,减震杆包括均同轴竖直设置的外筒、内筒、支撑柱和设置于内筒内的弹簧一,外筒的上端与连接板连接,内筒的上端封闭并伸入外筒内与外筒的内壁滑动连接,支撑柱的上端伸入内筒内与外筒的内壁密封滑动连接,弹簧一的上端与内筒的封闭端内壁固定连接,弹簧一的下端与支撑柱的上端固定连接,还包括限制支撑柱与内筒间滑动的第一限位机构和限制内筒与外筒间滑动的第二限位机构。本方案能使得勘查无人机平稳降落,防止出现勘查无人机倾斜侧翻现象。


    Access

    Download


    Export, share and cite



    Title :

    Geologic exploration unmanned aerial vehicle landing damping support


    Additional title:

    一种地质勘查无人机降落减震支架


    Contributors:
    XU BO (author) / TANG WENTAI (author) / LIU CHUANGCHUANG (author) / ZHAO NAN (author) / ZHOU LIWEI (author) / WANG MO (author) / SUI KELIN (author)

    Publication date :

    2024-07-05


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64U / B64C AEROPLANES , Flugzeuge



    Damping type unmanned aerial vehicle safe landing device

    HU SHENGLIANG / FENG CHENGXU / WANG LEI et al. | European Patent Office | 2025

    Free access

    Unmanned aerial vehicle damping support

    ZHI JIANMIN | European Patent Office | 2021

    Free access

    Unmanned aerial vehicle flight takeoff and landing damping device

    CHEN DASHUN | European Patent Office | 2024

    Free access

    Vertical lifting unmanned aerial vehicle with landing damping function

    LI CHENG | European Patent Office | 2021

    Free access

    Unmanned aerial vehicle take-off and landing damping table

    European Patent Office | 2021

    Free access