The invention discloses a variable-amplitude steering adjusting mechanism, which relates to the technical field of aircrafts, and comprises a rack, two flapping wing rods, a swing driving assembly, a swing driving assembly and a swing amplitude adjusting assembly, the two flapping wing rods are movably arranged relative to the rack, and the two flapping wing rods are used for being connected with the two bionic flapping wings respectively; the swing driving assembly is arranged on the rack and connected with the two flapping wing rods, and the swing driving assembly is used for driving the two flapping wing rods to swing; the steering adjusting assembly is arranged on the rack and can adjust the flapping wing angles of the two flapping wing rods; the swing amplitude adjusting assembly is arranged on the rack and connected with the two flapping wing rods, and the swing amplitude adjusting assembly can adjust the swing amplitudes of the two flapping wing rods respectively. The variable-amplitude steering adjusting mechanism provided by the invention can improve the flexibility of the aircraft. The invention further provides a bionic flapping wing aircraft comprising the amplitude-variable steering adjusting mechanism.

    本发明公开了一种可变幅转向调节机构,涉及飞行器技术领域,包括机架、两个扑翼杆、摆动驱动组件、摆动驱动组件及摆幅调节组件;两个扑翼杆相对于机架活动设置,两个扑翼杆用于分别连接两个仿生扑翼;摆动驱动组件设置于机架上,并与两个扑翼杆连接,摆动驱动组件用于驱动两个扑翼杆摆动;转向调节组件设置于机架上,转向调节组件能够调节两个扑翼杆的扑翼角度;摆幅调节组件设置于机架上,并与两个扑翼杆连接,摆幅调节组件能够分别调节两个扑翼杆的摆动幅度。本发明提供的可变幅转向调节机构,能够提升飞行器的灵活性。本发明还提供一种包括可变幅转向调节机构的仿生扑翼飞行器。


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    Title :

    Amplitude-variable steering adjusting mechanism and bionic flapping wing aircraft


    Additional title:

    可变幅转向调节机构及仿生扑翼飞行器


    Contributors:
    ZHU ZHUANGZHUANG (author) / FU LONGXI (author) / DENG HAOWEN (author) / JIANG TAOTAO (author) / ZHAO XIANFU (author)

    Publication date :

    2025-01-24


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64U



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