The invention provides an integrated unmanned aerial vehicle wing rotating mechanism and an integrated unmanned aerial vehicle, and relates to the technical field of unmanned aerial vehicles, the rotating mechanism comprises a shell, the shell is used for being arranged in a fuselage of the unmanned aerial vehicle, a mounting opening is formed in the top end of the shell, and an annular concave surface is arranged at the top end of the interior of the shell and located on the peripheral side of the mounting opening; an annular convex surface is arranged on the peripheral side of the top end of the rotating center piece, the rotating center piece is rotationally connected into the shell, and the annular convex surface is rotationally connected into the annular concave surface; the bottom end of the rotary connecting piece penetrates through the mounting opening and is connected with the top end of the rotary center piece, the top end of the rotary connecting piece is used for penetrating through the top of the fuselage and is connected with a wing of the unmanned aerial vehicle, and the wing can rotate relative to the fuselage; the rotating mechanism is simple in form and compact in assembly mode, and can simultaneously realize rotation of the wings and transfer of the wing load to the fuselage.

    本发明提供一种一体式无人机机翼旋转机构及一体式无人机,涉及无人机技术领域,该旋转机构包括:壳体,壳体用于设置在无人机的机身内部,壳体的顶端设有安装口,壳体的内部顶端并位于安装口的周侧设有环形的凹面;旋转中心件,旋转中心件的顶端周侧设有环形的凸面,旋转中心件转动连接在壳体内,环形的凸面转动连接在环形的凹面内;旋转连接件,旋转连接件的底端贯穿安装口,并与旋转中心件的顶端连接,旋转连接件的顶端用于贯穿机身的顶部,并与无人机的机翼连接,机翼能够相对于机身旋转;该旋转机构形式简洁,装配方式紧凑,能够同时实现机翼的旋转和机翼载荷向机身的传递。


    Access

    Download


    Export, share and cite



    Title :

    Integrated unmanned aerial vehicle wing rotating mechanism and integrated unmanned aerial vehicle


    Additional title:

    一种一体式无人机机翼旋转机构及一体式无人机


    Contributors:
    WANG YANWEI (author) / YANG LIGONG (author) / WEN XI (author) / JANG EUN HWA (author)

    Publication date :

    2024-02-20


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64U



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

    ZHANG KE / ZHANG XIAOPAN / ZHANG YING et al. | European Patent Office | 2023

    Free access

    Unmanned aerial vehicle wing folding mechanism and unmanned aerial vehicle

    WANG YANWEI / SHI XUDONG / MA CUNWANG | European Patent Office | 2021

    Free access

    Unmanned aerial vehicle wing folding mechanism and unmanned aerial vehicle

    GUO YITING / WANG JUN / KANG CHUANMING et al. | European Patent Office | 2022

    Free access

    Unmanned aerial vehicle wing and unmanned aerial vehicle

    XU JIAO / YAN SHI / LI QIRUN et al. | European Patent Office | 2023

    Free access

    WING OF UNMANNED AERIAL VEHICLE AND UNMANNED AERIAL VEHICLE

    BAI MO / DUO XIAO BO / SONG BING YIN | European Patent Office | 2019

    Free access