The invention relates to the technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle with a cantilever synchronous folding function, which comprises an unmanned aerial vehicle main body, multiple groups of first cantilevers are connected to both sides of the unmanned aerial vehicle main body, cavities are formed in the inner walls of the multiple groups of first cantilevers, and two groups of fixing seats are fixedly mounted in the cavities; and round through grooves are formed in the outer surfaces of the two sets of fixing bases, lead screws are movably installed in the round through grooves, and movable blocks are movably installed on the outer surfaces of the lead screws. According to the folding device, motors in the first cantilevers are driven at the same time, synchronous folding of the cantilevers is achieved, coordinated movement among different parts in the folding process is ensured, and the folding efficiency is improved. According to the unmanned aerial vehicle, the stability of the whole system is improved, the problem of asynchronization or jamming is prevented, the size of the whole unmanned aerial vehicle is greatly reduced when the unmanned aerial vehicle is folded through mutual folding of the first cantilever and the second cantilever, the unmanned aerial vehicle is crucial to optimization of portability and storage space, and a user can carry and store the unmanned aerial vehicle more conveniently.

    本发明涉及无人机技术领域,具体为一种具有悬臂同步折叠功能的无人机,包括无人机主体,所述无人机主体的两侧皆连接有多组第一悬臂,且多组第一悬臂的内壁开设有空腔,所述空腔中固定安装有两组固定座,且两组固定座的外表面皆开设有圆形通槽,所述圆形通槽中皆活动安装有丝杆,且丝杆的外表面活动安装有活动块,该发明通过同时驱动第一悬臂中的电机,实现了悬臂的同步折叠,确保了折叠过程中不同部件之间的协调运动,提高了整个系统的稳定性,防止不同步或卡顿的问题,且通过第一悬臂与第二悬臂的互相折叠,使得整个无人机的体积在折叠时大幅度减小,对于便携性和储存空间的优化至关重要,使得用户能够更方便地携带和存储无人机。


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    Title :

    Unmanned aerial vehicle with cantilever synchronous folding function


    Additional title:

    一种具有悬臂同步折叠功能的无人机


    Contributors:
    LU ZHIHUI (author) / CHEN JINYING (author) / ZHOU QINGLIN (author) / XIAO CHUYU (author) / ZENG JIANWEI (author) / XIAO HONGMIN (author) / LIU XUAN (author) / FENG TONG (author)

    Publication date :

    2024-03-12


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64U / B64C AEROPLANES , Flugzeuge



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