The invention provides a flapping-amplitude-variable hovering flapping wing experimental device which comprises an integral support, a motor is mounted at the top of the integral support, and an output shaft of the motor is in driving connection with a reduction gear set; the reduction gear set is in driving connection with an output gear set; the output gear set is in driving connection with flapping wings; according to the invention, the large-amplitude reciprocating flapping of the flapping wings can be realized, the flapping amplitude can be adjusted within the range of 120-180 degrees, the structure is simple, the transmission efficiency is high, the reliability is good, and the universality is high.

    本发明提供的一种可变扑动幅度的悬停扑翼实验装置,包括整体支架,所述整体支架的顶部安装有电机,所述电机的输出轴驱动连接有减速齿轮组;所述减速齿轮组驱动连接有输出齿轮组;所述输出齿轮组驱动连接有扑动翼;本发明可实现扑动翼的大幅度往复扑动,并且扑动幅度在120°‑180°范围内可调,结构简单,传动效率高,可靠性好,通用性高。


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    Title :

    Hovering flapping wing experimental device with variable flapping amplitude


    Additional title:

    一种可变扑动幅度的悬停扑翼实验装置


    Contributors:
    YANG XIAOJUN (author) / LANG XINYU (author) / SONG BIFENG (author) / XUAN JIANLIN (author)

    Publication date :

    2023-03-28


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen / B64C AEROPLANES , Flugzeuge



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