The ornithopter comprises a rack, two sets of steering engines, two flapping wings, the fixed wing, a gyroscope, an accelerometer and a control module, the fixed wing is fixedly connected to the front end of the rack, the two flapping wings are located behind the fixed wing and symmetrically located on the two sides of the rack respectively, the flapping wings are bionic flapping wings, and the control module is connected with the two sets of steering engines. A framework of the bionic flapping wing is provided with a wing spanwise bending deformation structure and a wing chordwise twisting deformation structure, two sets of steering engines are symmetrically and fixedly connected to the two sides of a rack respectively, a gyroscope, an accelerometer and a control module are fixedly connected to the rack, and a left steering engine and a right steering engine drive side flapping wings of the left steering engine and the right steering engine to flap so as to generate lift force. And the control module realizes different flapping modes by controlling the movement of the steering engine. The flexibility and stability of the ornithopter are improved, vibration of the ornithopter in the flying process can be effectively reduced, and noise is reduced.

    本发明公开一种固翼前置的扑翼飞行器,包括机架、两组舵机、两只扑翼、固翼、陀螺仪、加速度计和控制模块,固翼固定连接于机架的前端,两只扑翼位于固翼的后方并且分别对称位于机架的两侧,扑翼为仿生扑动翼,仿生扑动翼的骨架具有翼展向弯曲变形结构和翼弦向扭曲变形结构,两组舵机分别对称固定连接于机架的两侧,机架上固定连接有陀螺仪、加速度计和控制模块,左舵机和右舵机分别驱动其自身侧扑翼扑动从而产生升力,控制模块通过控制舵机的运动实现不同的扑动模式。本发明提高了扑翼飞行器的灵活性和稳定性,能够有效降低了飞行器飞行过程中的震动,减小了噪音的产生。


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    Title :

    Ornithopter with front fixed wings


    Additional title:

    一种固翼前置的扑翼飞行器


    Contributors:
    JIANG ZENG (author) / XU JIANGTAO (author) / ZHOU GUOCHENG (author) / ZHANG YUAN (author)

    Publication date :

    2024-08-06


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge




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