The invention relates to a double-synchronous-swing parallelogram-driven roller shutter type flapping-wing unmanned aerial vehicle. The unmanned aerial vehicle comprises flapping wings, swing shafts, connecting pieces, first speed reducers, driving motors, a transmission mechanism, second speed reducers, stepping motors, a fuselage frame, third speed reducers and a motor; the two swing shafts in the horizontal direction are symmetrically and fixedly mounted on the two sides of the fuselage frame, and the two connecting pieces are connected to the two swing shafts correspondingly and rotate relatively; the two flapping wings are connected to the two connecting pieces respectively and can rotate relatively, each flapping wing comprises a flapping wing frame and a roller blind mounted on the flapping wing frame, and a parallelogram mechanism and a driving motor are further arranged in each flapping wing frame and used for switching between the working state and the reset state of the flapping wings; the transmission mechanism is connected to the two connecting pieces; and the motor drives the transmission mechanism to move after being decelerated by the third speed reducer, so that the two connecting pieces synchronously swing up and down, and the two stepping motors respectively drive the two flapping wings to rotate after being decelerated by the two second speed reducers.

    本发明涉及双同步摆动平行四边形传动卷帘式扑翼无人机。包括扑翼、摆动轴、连接件、第一减速器、驱动电机、传动机构、第二减速器、步进电机、机身框架、第三减速器以及电动机,机身框架两侧对称的安装固定有两个水平方向的摆动轴,两个连接件分别连接在两个摆动轴上且相对转动,两个扑翼分别连接在两个连接件上且可相对转动,扑翼包括扑翼框架,以及安装在扑翼框架上的卷帘,扑翼框架内还设置有平行四边形机构以及驱动电机,用于扑翼工作状态与复位状态的切换,传动机构连接在两个连接件上,电动机通过第三减速器减速后带动传动机构运动使两个连接件同步上下摆动,两个步进电机通过两个第二减速器减速后分别带动两个扑翼转动。


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    Titel :

    Double-synchronous-swing parallelogram-driven roller shutter type flapping-wing unmanned aerial vehicle


    Weitere Titelangaben:

    双同步摆动平行四边形传动卷帘式扑翼无人机


    Beteiligte:
    QIU MING (Autor:in) / CHEN YONGPING (Autor:in) / ZHAO XUE (Autor:in) / WANG JIE (Autor:in) / XIA QINGYUAN (Autor:in) / WANG TAO (Autor:in) / HU CHENG (Autor:in) / LIAO ZHENQIANG (Autor:in)

    Erscheinungsdatum :

    11.01.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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