The invention discloses a flapping wing aircraft, and relates to the technical field of aircrafts. The flapping wing aircraft comprises a gear transmission mechanism mounted on the lower side of a fixed plate, and a wing mechanism mounted on the gear transmission mechanism; the gear transmission mechanism is driven by a motor; a supporting rod is transversely installed on the upper side of the fixed plate, and an empennage mechanism is installed at the other end of the supporting rod. The mechanism is of a bionic flapping wing structure, the mechanical structure is small, the aircraft flies by utilizing buoyancy of air, energy loss is greatly reduced, and the weight of the aircraft is fully reduced; a flapping wing flying mode is more flexible than a rotor wing or a fixed wing, and can enter and exit some places where other mechanisms cannot enter; in the nature, the mechanism can also be used as an observation machine and can be well fused into a flying organism group; from the aspect of flight efficiency, the flight efficiency of the flapping wings is higher than that of other flight modes under the same condition, and the flight distance can be increased.

    本发明公开了一种扑翼飞行器,涉及飞行器技术领域,包括固定板下侧安装有齿轮传动机构,齿轮传动机构上安装有翅膀机构;齿轮传动机构通过电机驱动;固定板上侧横向安装有支撑杆,支撑杆另一端安装有尾翼机构。本发明机构为仿生扑翼结构,该机械结构小,利用空气的浮力飞行,极大的减少了能量损耗,以及充分减少自身的重量;利用扑翼的飞行方式,会比旋翼或者固定机翼更加灵活,可以出入一些其他机构无法进入地方;在自然界中,该机构也可以做为观察机使用,能很好的融入到飞行生物的群体中;从飞行的效率的角度,扑翼的飞行效率在同等的条件下会比其他的飞行方式要高一些,能够加强飞行的距离。


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    Titel :

    Flapping wing aircraft


    Weitere Titelangaben:

    一种扑翼飞行器


    Beteiligte:
    XU JINGGE (Autor:in) / YUAN SHUO (Autor:in) / HU JIAXUN (Autor:in) / TIAN MO (Autor:in) / ZHANG YUNXIANG (Autor:in)

    Erscheinungsdatum :

    18.06.2021


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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