According to the attack angle single-parameter control bionic butterfly aircraft, a direct-acting driving motor is adopted to drive a flapping part to swing in a reciprocating mode through a transmission part, so that wing parts are driven to swing up and down, the direct-acting flight function of the aircraft is achieved, the traditional mode that gears are directly driven by a motor is abandoned, high-precision gear matching is not needed, and the transmission efficiency is greatly improved; the two turning driving motors are adopted to change the attack angles of the wings through the swing arms, the parameters of the attack angles are only determined by the output pace of the turning driving motors, it is guaranteed that the attack angles of the wings are not changed in the flapping process, and good operability and stability are achieved in the flying process. Therefore, the two motion modes of direct motion and turning do not interfere with each other, the conversion of motion states is realized, and the maneuverability is excellent.

    一种攻角单参数控制仿生蝴蝶飞行器,采用直动驱动电机通过传动部驱动扑动部往复摆动,从而驱动翅部上下摆动,实现飞行器直动飞行功能,摒弃传统电机直驱齿轮的方式,无需高精度的齿轮配合,极大地提高了传递效率;采用两个转弯驱动电机通过摆臂改变翅部的攻角,攻角的参数只由转弯驱动电机的输出步调决定,确保了翅膀在拍打过程中攻角不会变化,实现了飞行过程中具有良好的可操作性和稳定性。因此,能够实现直动和转弯两种运动方式互不干扰,实现运动状态的转换,具有优越的可操纵性。


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    Titel :

    Attack angle single parameter control bionic butterfly aircraft


    Weitere Titelangaben:

    一种攻角单参数控制仿生蝴蝶飞行器


    Beteiligte:
    ZHU LAIFA (Autor:in) / ZHOU YAOYANG (Autor:in) / CHEN LUYING (Autor:in) / YAO CHUANG (Autor:in) / TAN ZHONGCHENG (Autor:in) / XUE HUIPENG (Autor:in) / JIN HUAXUE (Autor:in)

    Erscheinungsdatum :

    16.08.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64U / B64C AEROPLANES , Flugzeuge



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