The invention relates to a design of a controllable folding rotor unmanned aerial vehicle, which comprises a vehicle body top plate, a vehicle body bottom plate, a rocker arm steering engine, a rotaryarm steering engine, a steering engine connecting shell, a steering engine connecting shell, a steering engine connecting piece, a steering engine connecting piece, a brushless motor seat, a brushless motor and a propeller, the rocker arm steering engine and the steering engine connecting shell are fixed together through a bolt; then the steering engine connecting shell is fixed to the machine body bottom plate through bolts, the steering engine connecting piece is fixed to the steering engine through bolts and hinged to the steering engine connecting shell through a bearing, the steering engine connecting piece is fixedly connected with the steering engine connecting piece through bolts, and the steering engine connecting piece is fixedly connected with the steering engine connecting shell through bolts, the steering engine is fixedly connected with the steering engine connecting shell through bolts, the brushless motor base is fixedly connected with the steering engine, the brushless motor is fixedly connected with the brushless motor base, and the propeller is fixedly connected with the brushless motor. The design has the advantages of being simple in structure, convenient to operate and capable of being widely applied to operation tasks and investigation in narrow spaces, has good stability and high loading capacity of a rotor unmanned aerial vehicle with a large axle distance, can penetrate through a narrow space like a small unmanned aerial vehicle to carry out operation tasks and investigation, and has practical and promotional values.

    本发明涉及了一种可控折叠旋翼无人机设计,机体顶板,机体底板,摇臂舵机,旋臂舵机,舵机连接壳,舵机连接壳,舵机连接件,舵机连接件,无刷电机座,无刷电机,螺旋桨,所述的摇臂舵机与舵机连接壳通过螺栓固定在一起,然后舵机连接壳再与机体底板通过螺栓固定,舵机连接件与舵机通过螺栓固定并与舵机连接壳通过轴承铰接,舵机连接件与舵机连接件通过螺栓固定连接,舵机连接件与舵机连接壳通过螺栓固定连接,舵机与舵机连接壳通过螺栓固定连接,无刷电机座与舵机连接固定,无刷电机与无刷电机座连接固定,螺旋桨与无刷电机连接固定,有益效果:结构简单,操作方便,广泛应用于狭窄空间的作业任务与勘察,既有轴距大的旋翼无人机的较好的稳定性和较高的载重能力,同时也能像小型无人机那样穿过狭窄的空间进行作业任务和勘察,具有实用和推广价值。


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    Titel :

    Design of controllable folding rotor unmanned aerial vehicle


    Weitere Titelangaben:

    一种可控折叠旋翼无人机设计


    Beteiligte:
    ZHANG FENNA (Autor:in) / XUE LIKUN (Autor:in) / ZHANG YINGYING (Autor:in) / HAN SHUAI (Autor:in) / SONG YUNFEI (Autor:in)

    Erscheinungsdatum :

    05.02.2021


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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