The invention relates to a flapping wing structure and an aircraft. The flapping wing structure comprises a rack, wing assemblies are rotationally installed on the two sides of the rack respectively,and the wing assemblies can swing in a reciprocating mode in the horizontal direction; each wing assembly comprises a swing arm and a wing plate component, the swing arm is rotationally connected withthe rack, and the swing arm can swing in the horizontal plane, the swing arm is rotationally connected with the wing plate component, the rotating axis of the wing plate component is horizontal, andthe wing plate component can swing within a set angle range relative to the swing arm; when the whole wing assembly swings in the set horizontal direction, the wing plate component can rotate to the limit position in the direction opposite to the set horizontal direction with the rotating axis of the wing plate component as the rotating center, so that the extending direction of the wing plate component is opposite to the advancing direction of the wing assembly.

    本发明涉及一种扑翼结构及飞行器,包括机架,机架的两侧分别转动安装有机翼组件,机翼组件能够在水平方向内往复摆动;所述机翼组件包括摆臂与翼板构件,摆臂与机架转动连接,摆臂能够在水平面内摆动;摆臂与翼板构件转动连接,翼板构件的转动轴线水平,翼板构件能够相对于摆臂在设定角度范围内摆动;在机翼组件整体朝着设定水平方向摆动时:翼板构件能够以自身转动轴线为旋转中心,朝着与设定水平方向相反的方向转动至极限位置,以使得翼板构件的延伸方向与机翼组件的前进方向相反。


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    Titel :

    Flapping wing structure and aircraft


    Weitere Titelangaben:

    一种扑翼结构及飞行器


    Beteiligte:
    JI BING (Autor:in) / ZHAO JINGTAI (Autor:in) / YANG FAN (Autor:in)

    Erscheinungsdatum :

    30.06.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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