The invention discloses a coaxial reverse propeller unmanned aerial vehicle vector control mechanism which is compact in structure and resistant to impact. The coaxial reverse propeller unmanned aerial vehicle vector control mechanism comprises a motor base unit, a driving arm mechanism and a power assembly which are sequentially connected from top to bottom. According to the coaxial reverse propeller unmanned aerial vehicle vector control mechanism which is compact in structure and resistant to impact, power of the vector control mechanism is provided by the two steering engines installed on the two sides of the same fixed base, the two steering engines control swing of the driving arms respectively and jointly control the pose of the motor base, and therefore pitching and transverse rolling movement of an unmanned aerial vehicle is achieved. The invention has the characteristics of compact structure, small volume, impact resistance and high reliability, and is suitable for small unmanned aerial vehicle systems.

    本发明公开了结构紧凑、抗冲击的共轴反浆无人机矢量控制机构,包括从上至下依次连接的电机座单元、驱动臂机构及动力组件。本发明提供的结构紧凑、抗冲击的共轴反浆无人机矢量控制机构,该矢量控制机构的动力由装在同一固定基座两侧的两个舵机提供,两个舵机分别控制驱动臂的摆动,共同控制电机座的位姿,从而实现无人机的俯仰与横滚运动。本发明具有结构紧凑、体积小、抗冲击、可靠性高的特点,适用于小型无人机系统。


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    Titel :

    Compact-structure impact-resistant coaxial reverse propeller unmanned aerial vehicle vector control mechanism


    Weitere Titelangaben:

    结构紧凑、抗冲击的共轴反浆无人机矢量控制机构


    Beteiligte:
    LIU YANWEI (Autor:in) / HUANG WENQING (Autor:in) / CHEN ZHEYANG (Autor:in) / LI JIANGCHAO (Autor:in) / LI PENGYANG (Autor:in) / LI SHUJUAN (Autor:in)

    Erscheinungsdatum :

    15.10.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64U



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