According to the flapping wing aircraft, the transmission mechanism and the rotation control mechanism are installed on the first support, the flapping wing mechanism is installed on the second support, the second support is driven to rotate through the rotation control mechanism, and then the flapping wing mechanism on the second support is driven to rotate around the first axis; according to the ornithopter, the first flapping wing and the second flapping wing rotate in position, the direction of thrust generated by flapping of the flapping wings is changed due to the change of the positions of the flapping wings, so that the flight path and attitude of the ornithopter can be adjusted, a control wing for controlling flight does not need to be additionally arranged, and the overall weight of the ornithopter is reduced.

    本发明提供的扑翼飞行器,在第一支架上安装传动机构和旋转控制机构,在第二支架上安装扑翼机构,通过所述旋转控制机构带所述第二支架旋转,进而带动所述第二支架上的所述扑翼机构绕第一轴线旋转,以实现第一扑翼和第二扑翼的位置发生转动,由于扑翼的位置变化,其扑动产生的推力方向也发生变化,因此能够调节所述扑翼飞行器的飞行轨迹和姿态,无需额外设置控制飞行的控制翼,有利于减小扑翼飞行器的整体重量。


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    Titel :

    Flapping wing air vehicle


    Weitere Titelangaben:

    扑翼飞行器


    Beteiligte:
    LI SHUFAN (Autor:in) / MA PENGPENG (Autor:in) / HOU DAN (Autor:in) / SHI CHENYANG (Autor:in) / ZHANG DONGYANG (Autor:in)

    Erscheinungsdatum :

    2023-12-29


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64U



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