The invention relates to a foldable multi-rotor unmanned aerial vehicle platform, belongs to the technical field of unmanned aerial vehicles, and solves the problems that a multi-rotor unmanned aerial vehicle is low in folding automation degree and insufficient in storage space. The deployable and retractable multi-rotor unmanned aerial vehicle platform comprises a fuselage component, an arm component, a propeller component, an undercarriage component, an arm folding component and a propeller retracting and releasing component, one end of each arm component is hinged to the peripheral side of the fuselage component through an arm folding component; the multiple vehicle arm components are evenly distributed on the peripheral side of the vehicle body component in the horizontal plane. The propeller component is movably connected to the other end of the arm component through the propeller folding and unfolding component, and the propeller component is folded or unfolded relative to the fuselage component in a vertical plane; the undercarriage component is connected to the lower end of the fuselage component. According to the unmanned aerial vehicle, horizontal folding of the vehicle arms controlled by the steering engines and vertical folding and unfolding of the unpowered propellers are achieved, the storage space of the unmanned aerial vehicle is reduced to the maximum extent, energy is saved in the unfolding and folding process, and the automation degree is high.

    本发明涉及一种可展收多旋翼无人机平台,属于无人机技术领域,解决了多旋翼无人机折叠自动化程度低、节约收纳空间不够的问题。本发明的可展收多旋翼无人机平台包括机身部件、机臂部件、螺旋桨部件、起落架部件、机臂折叠部件和螺旋桨收放部件;机臂部件一端通过机臂折叠部件铰接在所述机身部件周侧;多个机臂部件在水平面内均布在机身部件周侧;螺旋桨部件通过螺旋桨收放部件活动连接在机臂部件另一端,螺旋桨部件在竖直平面内相对于机身部件收拢或展开;起落架部件连接在机身部件下端。本发明实现了舵机控制的机臂水平折叠、无动力的螺旋桨竖直收放,最大程度的减小了无人机收纳空间,且展收过程节约能源、自动化程度高。


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Multi-rotor unmanned aerial vehicle platform capable of being unfolded and folded


    Weitere Titelangaben:

    一种可展收多旋翼无人机平台


    Beteiligte:
    ZHOU HONGZHI (Autor:in) / ZENG QINGGUO (Autor:in) / DUAN XIAOYU (Autor:in) / KIM SUNG-NAM (Autor:in) / LI KEWEI (Autor:in) / WANG ANPING (Autor:in) / ZHANG GUOWEI (Autor:in) / YU YAN (Autor:in) / SHI WEIXING (Autor:in) / XU MENGJIA (Autor:in)

    Erscheinungsdatum :

    2023-04-07


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64U



    Miniature unmanned aerial vehicle capable of being automatically folded and unfolded

    YAN ZHIPING / HUA YUANYUAN / QU NIANMENG et al. | Europäisches Patentamt | 2022

    Freier Zugriff

    Multi-rotor unmanned aerial vehicle capable of being quickly folded

    GONG BANGMIN / AI JIANLIANG | Europäisches Patentamt | 2022

    Freier Zugriff

    Rotary unmanned aerial vehicle undercarriage capable of being folded and unfolded in real time

    CHU RUIZHONG / LIU PENGFEI / LIANG DEXIANG et al. | Europäisches Patentamt | 2023

    Freier Zugriff

    Miniature propeller unmanned aerial vehicle capable of being unfolded automatically

    SUN YU / ZHA ZIYAN / NI JUN et al. | Europäisches Patentamt | 2024

    Freier Zugriff

    Six-rotor unmanned aerial vehicle with wings capable of being folded and stored

    ZHOU ZHUXUE / LIU WEI / HAO YULIANG et al. | Europäisches Patentamt | 2022

    Freier Zugriff