The invention discloses a variable-amplitude bionic butterfly aircraft, and relates to the technical field of aircrafts, the variable-amplitude bionic butterfly aircraft comprises a differential system, a variable-amplitude system, a direction control system, a flexible wing system and a power supply control system, two output ends of the variable-amplitude system are respectively connected with two wings of the flexible wing system, and the amplitudes of the two wings are respectively adjusted; the differential system is in transmission connection with the amplitude variation system and can drive wings to vibrate, the direction control system is connected with an outer frame of the differential system and can drive the flexible wing system to achieve steering, and the differential system and the direction control system are both electrically connected with the power supply control system. Lift force adjustment and steering are more flexible.

    本发明公开了一种变振幅仿生蝴蝶飞行器,涉及飞行器技术领域,包括差速器系统、变幅系统、方向控制系统、柔性翅翼系统和电源控制系统,变幅系统的两个输出端分别连接柔性翅翼系统的两个翅膀并分别调整两个翅膀的振幅,差速器系统传动连接变幅系统,并能够带动翅膀振动,方向控制系统连接差速器系统的外框架,并能够带动柔性翅翼系统实现转向,差速器系统和方向控制系统均电连接电源控制系统。本发明升力调节和转向更灵活。


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    Title :

    Variable-amplitude bionic butterfly aircraft


    Additional title:

    一种变振幅仿生蝴蝶飞行器


    Contributors:
    LIU YIZHEN (author)

    Publication date :

    2025-01-24


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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