The invention belongs to the technical field of aviation aircrafts, and particularly relates to a hovering flapping wing aircraft and a hovering flapping wing flight method.The hovering flapping wing aircraft comprises a rack, main supports are movably connected to the left side and the right side of the upper portion of the rack, main flapping wings are installed above the main supports on the two sides, and when flapping, the main flapping wings only vibrate in a first quadrant or a second quadrant; the main flapping wings are responsible for providing upward lifting force during flapping, auxiliary supports are movably connected to the left side and the right side of the lower portion of the rack, auxiliary flapping wings are installed at the upper ends of the auxiliary supports, when the auxiliary flapping wings flap, the main flapping wings in the first quadrant and the second quadrant vibrate firstly, and when the flapping-wing aircraft flies to the enough height, the flapping wings are driven to rotate. The auxiliary flapping wings start to vibrate, so that the auxiliary flapping wings vibrating in the third quadrant and the fourth quadrant are prevented from flapping to the ground, and the service life of the flapping-wing aircraft can be prolonged by protecting the auxiliary flapping wings.

    本发明公开的属于航空飞行器技术领域,具体为一种悬停扑翼飞行器以及悬停扑翼飞行方法,包括机架,所述机架的上方左右侧活动连接有主支架,两侧所述主支架的上方安装有主扑翼,所述主扑翼在煽动时,只在第一象限或第二象限振动,所述主扑翼在煽动时负责提供向上的升力,所述机架的下方左右侧活动连接有辅支架,所述辅支架的上端安装有辅扑翼,所述辅扑翼在煽动时,在第一象限和第二象限的主扑翼先进行振动,当扑翼飞行器飞行到足够的高度后,辅扑翼在开始振动,从而避免了在第三象限及第四象限振动的辅扑翼拍打到地面,通过对辅扑翼进行保护,进而可以延长扑翼飞行器的使用寿命。


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    Title :

    Hovering flapping wing aircraft and hovering flapping wing flight method


    Additional title:

    一种悬停扑翼飞行器以及悬停扑翼飞行方法


    Contributors:
    WANG JUN (author) / LI FUQIANG (author) / WU BAOLEI (author)

    Publication date :

    2023-06-09


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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