The invention relates to a variable-windward-area driving-energy-adjustable double-continuous-winged synchronous swing type unmanned aerial vehicle. The unmanned aerial vehicle comprises belt wings, swing shafts, connecting pieces, first speed reducers, stepping motors, a transmission mechanism, a second speed reducer, a motor, a fuselage frame, a third speed reducer and driving motors; 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 belt wings are connected to the two connecting pieces respectively and can rotate relatively, each belt wing comprises a belt wing frame and a soft belt mounted on the belt wing frame, belt wheels, tensioning wheels and driving motors are further arranged in each belt wing frame and used for switching between the working state and the reset state of the belt wings, and the transmission mechanism is connected to the two connecting pieces; and the motor drives the transmission mechanism to move after being decelerated by the second speed reducer, so that the two connecting pieces synchronously swing up and down, and the two stepping motors respectively drive the two belt wings to rotate after being decelerated by the two first speed reducers.

    本发明涉及变迎风面积驱动能量可调双连续带翼同步摆动式无人机。包括带翼、摆动轴、连接件、第一减速器、步进电机、传动机构、第二减速器、电动机、机身框架、第三减速器以及驱动电机,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,两个带翼分别连接在两个连接件上且可相对转动,带翼包括带翼框架,以及安装在带翼框架上的软质带,带翼框架内还设置有带轮、张紧轮以及驱动电机,用于带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,电动机通过第二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一减速器减速后分别带动两个带翼转动。


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    Titel :

    Variable-windward-area driving-energy-adjustable double-continuous-winged synchronous swing type unmanned aerial vehicle


    Weitere Titelangaben:

    变迎风面积驱动能量可调双连续带翼同步摆动式无人机


    Beteiligte:
    QIU MING (Autor:in) / HAN LIDONG (Autor:in) / SHI YUN (Autor:in) / CAI WEIYI (Autor:in) / FAN LI (Autor:in) / HU YOUQIAN (Autor:in) / LIAO ZHENQIANG (Autor:in)

    Erscheinungsdatum :

    2022-01-11


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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