The embodiment of the invention discloses a micro bionic flapping wing mechanism, relates to the bionic flapping wing design technology, and can give consideration to both light weight and lift forceoutput. The mechanism comprises a transmission gear, a motor, a connecting rod, a rocker and a fixing frame for fixing the motor and a transmission mechanism, wherein a hollow cup motor is installed on the fixing frame, a small gear installed on a motor shaft is meshed with a large gear of the transmission mechanism, each large gear is hinged to a connecting rod, and the other end of each connecting rod is connected with a rocker. The mechanism is advantaged in that the flapping wing achieved through the crank and rocker mechanism not only can meet the high frequency requirement of the flapping wing aircraft, but also can generate enough lifting force in the vertical direction. The invention is suitable for the lightweight ornithopter.

    本发明实施例公开了一种微小型仿生扑翼机构,涉及仿生扑翼设计技术,能够兼顾轻量化和输出升力。本发明包括:包括传动齿轮、电机、连杆、摇杆,以及固定电机和传动机构的固定架;空心杯电机安装在固定架上,电机轴上安装的小齿轮与传动机构的大齿轮啮合,每个大齿轮上铰接一根连杆,每根连杆的另一端连接一根摇杆;这样通过曲柄摇杆机构实现的扑翼不但能满足扑翼飞行器较高的频率要求,而且能产生足够的竖直方向的升力。本发明适用于轻量化扑翼飞行器。


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    Titel :

    Micro bionic flapping wing mechanism


    Weitere Titelangaben:

    一种微小型仿生扑翼机构


    Beteiligte:
    GUO CE (Autor:in) / LI XIN (Autor:in) / HUANG QIUYE (Autor:in) / YU ZHIWEI (Autor:in) / LI LONGHAI (Autor:in)

    Erscheinungsdatum :

    08.09.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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