The invention provides a push-control integrated flapping wing mechanism. The push-control integrated flapping wing mechanism comprises a machine body, a crank, a first sliding block, an arc-shaped sliding groove rod, a long connecting rod, a second sliding block and a linear sliding groove rod. The middle of the arc-shaped sliding groove rod is hinged to the machine body, and one end of the arc-shaped sliding groove rod is hinged to the linear sliding groove rod. The first sliding block is arranged at the other end of the arc-shaped sliding groove rod in a sliding mode along an arc-shaped track. The second sliding block is arranged on the linear sliding groove rod in the extending direction of the linear sliding groove rod in a sliding mode. The two ends of the long connecting rod are hinged to the first sliding block and the second sliding block respectively. One end of the crank is hinged to the first sliding block, and the other end of the crank is connected with a driving part for driving the crank to rotate; and the linear sliding groove rod is provided with a connecting rod used for installing an outer section wing.

    本公开提供了推控一体扑翼机构,包括:机体、曲柄、滑块一、弧形滑槽杆、长连杆、滑块二、和直线滑槽杆;所述弧形滑槽杆的中部与所述机体铰接,所述弧形滑槽杆的一端铰接至所述直线滑槽杆;所述滑块一沿弧形轨迹滑动设于所述弧形滑槽杆的另一端;所述滑块二沿所述直线滑槽杆的延伸方向滑动设于所述直线滑槽杆;所述长连杆的两端分别铰接至所述滑块一和所述滑块二;所述曲柄的一端铰接至所述滑块一,另一端连接有驱动其转动的驱动部件;所述直线滑槽杆具有用于安装外段机翼的连接杆。


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    Titel :

    Push-control integrated flapping wing mechanism



    Erscheinungsdatum :

    2024-07-02


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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