The invention relates to the field of unmanned aerial vehicles, in particular to a tandem dual-rotor unmanned aerial vehicle structure which comprises an unmanned aerial vehicle body, a mounting plate slidably connected to the unmanned aerial vehicle body, spiral wings rotatably connected to the two ends of the unmanned aerial vehicle body and a driving device used for driving each spiral wing to rotate. The two spiral wings are located at the front end and the rear end of the unmanned aerial vehicle body correspondingly, the mounting plate slides in the width direction of the unmanned aerial vehicle body, and a plurality of mounting holes used for mounting an operation platform are formed in the mounting plate. The application has the advantages that the application range of the unmanned aerial vehicle can be widened, and the flight stability of the unmanned aerial vehicle can be guaranteed when different operation platforms are installed on the unmanned aerial vehicle.

    本申请涉及无人机的领域,尤其是涉及一种纵列双旋翼无人机结构,包括无人机本体、滑动连接在所述无人机本体上的安装板、转动连接在所述无人机本体两端的螺旋翼以及用于驱动每个所述螺旋翼旋转的驱动装置,两个所述螺旋翼分别位于所述无人机本体的前后两端,所述安装板沿所述无人机本体的宽度方向滑动,所述安装板上开设有多个用于安装作业平台的安装孔。本申请具有可以提高无人机的适用范围,使得不同的作业平台安装在无人机上时都能够保证无人机飞行稳定性的效果。


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    Titel :

    Tandem dual-rotor unmanned aerial vehicle structure


    Weitere Titelangaben:

    一种纵列双旋翼无人机结构


    Beteiligte:
    JIANG HUA (Autor:in) / CHEN LANXIN (Autor:in) / WANG YUNJIAN (Autor:in)

    Erscheinungsdatum :

    18.02.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64U / B64C AEROPLANES , Flugzeuge



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