The invention discloses a pigeon-like flapping wing aircraft comprising an aircraft body shell, an aircraft body framework, flapping wings, a driving assembly and a V-shaped empennage; the aircraft body framework is arranged in the aircraft body shell; the number of the flapping wings is two, the two flapping wings are symmetrically distributed on the left side and the right side of the aircraft body shell, and each flapping wing is of a single-section wing composite type airfoil layout. The driving assembly is mounted on the aircraft body framework and drives the flapping wings to perform vertical flapping motion and passive torsional motion of wing sections so as to simulate flapping wing motion of pigeons in nature, so that the lift force and thrust of the pigeon-like flapping wing aircraft are improved; the V-shaped empennage is fixed to the tail of the aircraft body framework, located outside the aircraft body shell and used for conducting attitude control, attitude balance and direction control and providing part of lift force in the flying process of the pigeon-like flapping-wing aircraft. The pigeon-like flapping wing aircraft can fly at a high speed, can carry more effective loads and is small in flapping wing size.

    本发明公开了一种仿鸽类扑翼飞行器,包括机身壳体、机身骨架、扑翼、驱动组件和V型尾翼;机身骨架设置在机身壳体内;扑翼有两个,两个扑翼对称地分布在机身壳体的左右两侧,每一扑翼采用单段翼复合型翼面布局;驱动组件安装在机身骨架上,驱动组件驱动扑翼进行上下扑动运动和翼剖面的被动扭转运动,以模仿大自然中鸽类的扑翼运动,来提升仿鸽类扑翼飞行器的升力和推力;V型尾翼与机身骨架的尾部固定且位于机身壳体外,用于在仿鸽类扑翼飞行器飞行过程中进行姿态控制、姿态平衡、方向控制和提供部分升力。本发明仿鸽类扑翼飞行器能够高速飞行,能够携带较多的有效载荷,扑翼尺寸较小。


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    Title :

    Pigeon-like flapping wing aircraft


    Additional title:

    仿鸽类扑翼飞行器


    Contributors:
    ZHAO XIAOWEI (author) / ZENG DONGHONG (author) / WANG XIANYU (author) / YIN MINGWEI (author) / LI JINGYANG (author) / BAOYIN HEXI (author)

    Publication date :

    2021-04-23


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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