The invention relates to the technical field of aircrafts, in particular to a double-wing flight structure. The double-wing flight structure comprises translation wings, a driving device and a carrier, the carrier is provided with a support and a center shaft, the lower end of the support is fixedly connected with the carrier, the center shaft is rotatably connected with the upper end of the support, and the support is provided with an angle adjusting device for changing the inclination angle of the center shaft; two translation wings which are spaced up and down are arranged on the central shaft, and the translation wings are connected with the central shaft in a matched manner; the driving device is in transmission connection with the two translational wings respectively, so that the twotranslational wings can reciprocate up and down along the central shaft respectively; the double-wing flight structure is reasonable in structure, the center shaft and the translation wing structureson the center shaft can integrally rotate on the support to adjust the lift force output angle, the driving device drives the two translation wings to reciprocate up and down through the crank connecting rod to achieve synchronous opening and closing movement, and the translation wings are promoted to rotate in one direction through the pressure difference of the translation wings in the ascending process; when the translational wing descends, a vertically upward acting force is generated between the flapping wing surface and air, so that the carrier obtains a lifting force to achieve the flying purpose.

    本发明涉及飞行器技术领域,具体指一种双翼飞行结构;包括平动翼、驱动装置和载体,所述载体上设有支架和中心轴,支架下端与载体固定连接,中心轴与支架上端转动连接,且支架上设有改变中心轴倾斜角的调角装置;所述中心轴上设有两个上下间隔的平动翼,平动翼与中心轴配合连接;驱动装置分别传动连接两个平动翼,从而使两个平动翼可分别沿中心轴上下往复运动;本发明结构合理,中心轴以及其上平动翼结构可一体在支架上转动以调节升力输出角度,驱动装置通过曲柄连杆带动两个平动翼上下往复实现同步张合运动,平动翼在上升时的压力差促使平动翼单向旋转,平动翼在下降时扇动翼面与空气之间产生竖直向上的作用力,进而使载体获得升力实现飞行目的。


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    Titel :

    Double-wing flight structure


    Weitere Titelangaben:

    一种双翼飞行结构


    Beteiligte:
    WANG ZHICHENG (Autor:in)

    Erscheinungsdatum :

    2021-03-02


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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