The invention discloses an unmanned aerial vehicle transmission mechanism which comprises a shell. Supporting pipes are symmetrically arranged on the two sides of the shell along the center line, the two sides of each supporting pipe are connected with the shell through mounting blocks, supporting rods are slidably arranged in the supporting pipes, fixing rods are fixedly connected to the tops of the inner walls of the supporting pipes, and the ends, away from the shell, of the fixing rods are elastically connected with the inner walls of the supporting rods. A piston is slidably arranged at the bottom of the first transverse plate, a transmission mechanism correspondingly matched with the supporting pipe is arranged in the shell, the transmission mechanism is in transmission connection with the piston through a hose, and a limiting mechanism moving relative to the supporting rod is arranged on the supporting pipe. During use, when the unmanned aerial vehicle lands, the unmanned aerial vehicle can stably land on the flat or uneven ground through the two sets of supporting rods capable of independently moving and the first transverse plate, and the risk that the unmanned aerial vehicle topples over when the unmanned aerial vehicle lands due to the uneven ground is avoided.

    本发明公开了一种无人机传动机构,包括外壳;外壳的两侧沿中心线对称设置有支撑管,支撑管的两侧通过安装块与外壳连接,支撑管内滑动设置有支撑杆,支撑管的内壁顶部固定连接有固定杆,固定杆远离外壳的一端与支撑杆的内壁弹性连接,支撑杆的底端固定设置有第一横板,第一横板的底部滑动设置有活塞,外壳内设置有与支撑管对应配合的传动机构,传动机构与活塞之间通过软管传动连接,支撑管上设置有相对支撑杆移动的限位机构。使用时,在无人机降落时,通过两组可以独立活动支撑杆、第一横板,让无人机可以在平坦或者凹凸不平的地面进行稳定的降落,避免无人机因为地面凹凸不平在降落时出现倾倒的风险。


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Unmanned aerial vehicle transmission mechanism and unmanned aerial vehicle


    Weitere Titelangaben:

    一种无人机传动机构及无人机


    Beteiligte:
    YUN PEI (Autor:in) / YUAN RONGHAI (Autor:in) / YANG RONGTAO (Autor:in)

    Erscheinungsdatum :

    2023-09-05


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64U



    Unmanned aerial vehicle wing limiting mechanism, unmanned aerial vehicle wing and unmanned aerial vehicle

    ZHANG KE / ZHANG XIAOPAN / ZHANG YING et al. | Europäisches Patentamt | 2023

    Freier Zugriff

    Unmanned aerial vehicle aileron mechanism and unmanned aerial vehicle

    CHEN JIAMING / JU XIAOBIN / GONG RUIJUN et al. | Europäisches Patentamt | 2023

    Freier Zugriff

    Unmanned aerial vehicle arm mechanism and unmanned aerial vehicle

    WU SHAOQIANG / ZHANG LIANG / GUO XIHUA | Europäisches Patentamt | 2024

    Freier Zugriff