The invention relates to the related technical field of unmanned aerial vehicles, in particular to a small unmanned aerial vehicle structure and a servo steering engine control system.The small unmanned aerial vehicle structure comprises an unmanned aerial vehicle shell, an unmanned aerial vehicle rack is fixedly connected to the inner side surface of the unmanned aerial vehicle shell, and a damping mechanism is arranged on the surface of one side of the unmanned aerial vehicle rack; a transmission mechanism is arranged on the surface of one side of the unmanned aerial vehicle rack, and propellers are installed on the surface of the upper portion of the transmission mechanism. According to the small unmanned aerial vehicle structure and the servo steering engine control system, when an unmanned aerial vehicle lands, an unmanned aerial vehicle rack is subjected to descending force and moves downwards to extrude a whole spring to enable the whole spring to be shrunk, a fixing plate is in a limiting groove and stretches out and draws back under the action of elastic force, and therefore the damping effect on the whole unmanned aerial vehicle rack is achieved; the anti-collision rod can prevent the whole unmanned aerial vehicle from inclining at a large angle, so that the propeller of the unmanned aerial vehicle touches the ground and is damaged, and meanwhile, the propeller is prevented from being collided to affect the transmission effect of the output control motor.

    本发明涉及无人机相关技术领域,尤其涉及一种小型无人机结构及伺服舵机控制系统,包括无人机外壳,所述无人机外壳的内侧表面固定连接有无人机机架,所述无人机机架的一侧表面设置有减震机构,所述无人机机架的一侧表面设置有传动机构,所述传动机构的上方表面安装有螺旋桨。该一种小型无人机结构及伺服舵机控制系统,当无人机降落时,无人机机架受到下降的力,向下运动挤压弹簧整体,使弹簧整体收缩,其中固定板在限位槽中,受弹力作用伸缩,从而实现对无人机机架整体的减震作用,无人机重心不稳定时,防撞杆可以放置无人机整体大角度倾斜,导致无人机螺旋桨触碰地面,导致螺旋桨损坏,同时防止螺旋桨磕碰影响输出控制电机传动效果。


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    Titel :

    Small unmanned aerial vehicle structure and servo steering engine control system


    Weitere Titelangaben:

    一种小型无人机结构及伺服舵机控制系统


    Beteiligte:
    RONG ZHEN (Autor:in) / CHEN WEIFANG (Autor:in) / XIANG HUAAN (Autor:in) / ZHANG ZHANLIANG (Autor:in)

    Erscheinungsdatum :

    01.03.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64U / B64C AEROPLANES , Flugzeuge



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