The invention discloses a fixed-wing unmanned aerial vehicle undercarriage, and relates to the technical field of unmanned aerial vehicles. Comprising a substrate; the gyroscope is arranged below the substrate and is connected with the middle part of the substrate; the multiple first lifting systems operate independently, and the tops of the first lifting systems are connected with the base plate. The multiple second lifting systems are arranged corresponding to the first lifting systems, and each second lifting system is connected with the end, away from the base plate, of the corresponding first lifting system. The remote sensing device is connected with one end, away from the substrate, of the gyroscope; the control chip is electrically connected with the gyroscope, the first lifting system, the second lifting system and the remote sensing device. By arranging the gyroscope, it can be guaranteed that the upper portion of the undercarriage is always kept in the horizontal state when the unmanned aerial vehicle lands, and by arranging the first lifting system and the second lifting system, the unmanned aerial vehicle can land on the ground with the large inclination angle or the bumpy ground.

    本发明公开了一种固定翼无人机起落架,涉及无人机技术领域。包括:基板;陀螺仪设置在基板下方,陀螺仪与基板中部连接;第一升降系统设置有多个并独立运行,第一升降系统顶部与基板连接;第二升降系统设置有多个,多个第二升降系统与第一升降系统对应设置,且每个第二升降系统分别与对应的第一升降系统远离基板的一端连接;遥感装置与陀螺仪远离基板的一端连接;控制芯片分别与陀螺仪、第一升降系统、第二升降系统和遥感装置电性连接。本发明通过设置陀螺仪,可保证无人机在降落时起落架的上方始终保持水平状态,通过设置第一升降系统和第二升降系统,可以实现无人机在倾斜角度较大或者崎岖不平的地面上进行降落。


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Fixed-wing unmanned aerial vehicle undercarriage


    Weitere Titelangaben:

    一种固定翼无人机起落架


    Beteiligte:
    CHENG TIANCAI (Autor:in) / LIU QIANG (Autor:in) / ZHAO QI (Autor:in) / JIANG GUANGJUN (Autor:in) / BAO-YIN HEXI (Autor:in) / LI QI (Autor:in) / CHEN HUIDONG (Autor:in) / LIU ZIHAO (Autor:in) / KANG XIYUE (Autor:in)

    Erscheinungsdatum :

    28.07.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64U / B64C AEROPLANES , Flugzeuge



    Fixed-wing unmanned aerial vehicle undercarriage

    XU CHENYANG | Europäisches Patentamt | 2023

    Freier Zugriff

    Unmanned aerial vehicle undercarriage

    BIAN CHUNJIANG / ZHAO HONG / GAO DONG | Europäisches Patentamt | 2021

    Freier Zugriff

    Unmanned aerial vehicle undercarriage

    OUYANG BIN / JIN HAILEI / XIONG XIAOMIN et al. | Europäisches Patentamt | 2024

    Freier Zugriff

    Unmanned aerial vehicle undercarriage

    WU QINGTAO / ZHANG SEN / QI BINGHUI et al. | Europäisches Patentamt | 2024

    Freier Zugriff

    unmanned aerial vehicle undercarriage

    ZHANG JIANMIN | Europäisches Patentamt | 2021

    Freier Zugriff