The invention provides a hovering multi-wing bionic aircraft which comprises an integral support, four direct-drive transmission mechanisms are arranged on the integral support, and a flapping wing is mounted on each direct-drive transmission mechanism; each direct-drive transmission mechanism is connected to a flight control driving system; on the basis of ensuring the transmission power and the torque requirement, the transmission system structure is greatly simplified, and the overall transmission efficiency and the mechanical reliability of the aircraft are improved; through reasonable spatial distribution layout, aerodynamic interference between the front wing and the rear wing is effectively reduced, and the overall aerodynamic performance of the aircraft is improved.

    本发明提供的一种可悬停的多翼仿生飞行器,包括整体支架,所述整体支架上设置有四个直驱传动机构,每个直驱传动机构上安装有一个扑动翼;每个直驱传动机构均连接至飞控驱动系统;本发明能够在保证传动功率和扭矩要求的基础上,极大的简化了传动系统结构,提高了飞行器整体的传动效率以及机械可靠性;通过合理的空间分布布局,有效的减小了前后翼之间的气动干扰,提升了飞行器整体的气动性能。


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    Title :

    Hovering multi-wing bionic aircraft


    Additional title:

    一种可悬停的多翼仿生飞行器


    Contributors:
    YANG XIAOJUN (author) / ZHANG MINGHAO (author) / SONG BIFENG (author) / LANG XINYU (author) / LIU HENG (author) / YANG CHI (author)

    Publication date :

    2022-01-21


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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