The invention relates to an empennage linkage control variable ornithopter, and belongs to the technical field of ornithopters. The front end of the hollow cup motor is fixedly connected with a motor support in the flapping wing support, an output shaft of the hollow cup motor extends to the other side of the motor support to be connected with a horizontal cam of the flapping wing mechanism, and the rear end of the hollow cup motor is fixedly connected with the empennage support. The front end of the empennage support is further fixedly connected with the two flapping wing supporting rods, the middle of the empennage support is connected with the vertical empennage mechanism, the rear end of the empennage support is connected with the horizontal empennage mechanism, and a vertical empennage of the vertical empennage mechanism is fixedly bonded with a horizontal empennage of the horizontal empennage mechanism. The flapping-wing aircraft has the advantages that the structure is novel, the effect of maintaining high lift force is achieved, the aerodynamic performance of the wings is improved, sweeping motion is increased, the flexibility of the wings and the bionic degree of the flapping-wing aircraft are improved, the empennage is divided into the horizontal empennage and the vertical empennage and is driven by the linear steering engine, linkage control over the horizontal empennage and the vertical empennage can be achieved, and the overall flexibility is improved.

    本发明涉及一种尾翼联动控制的可变体扑翼飞行器,属于扑翼飞行器技术领域。空心杯电机前端与扑翼支架中的电机支架固定连接,空心杯电机的输出轴伸出到电机支架的另一侧与扑翼机构的水平凸轮连接,空心杯电机的后端与尾翼支架固定连接,尾翼支架前端还与两个扑翼支撑杆固定连接、中部与竖直尾翼机构连接、后端与水平尾翼机构连接,竖直尾翼机构的竖直尾翼与水平尾翼机构的水平尾翼固定粘接。优点是结构新颖,达到维持高升力的效果,改善机翼的气动性能,增加了扫掠运动,提高了机翼的灵活性和扑翼飞行器仿生程度,尾翼分为水平尾翼和竖直尾翼,由直线舵机驱动,可以实现水平尾翼和竖直尾翼的联动控制,增加了整体的灵活性。


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    Title :

    Variable ornithopter with empennage in linkage control


    Additional title:

    一种尾翼联动控制的可变体扑翼飞行器


    Contributors:
    LIU QIANG (author) / ZHANG TINGQI (author) / XU PENGZI (author) / ZHU JINGRONG (author) / XUE JIAHENG (author) / ZHANG LIDONG (author) / ZHOU XIAOQIN (author) / ZHANG XU (author)

    Publication date :

    2023-08-01


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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