The invention discloses a flapping-wing air vehicle with an auxiliary lifting force device. The flapping-wing air vehicle comprises a vehicle body, wing devices, a run-up device, a motor and a battery, an empennage is mounted at the tail of the fuselage; the run-up device is mounted on the lower side of the machine body; the two sets of wing devices are installed on the two sides of the fuselage,the wing devices and the run-up device are driven by motors, the multiple motors are powered by batteries, and an auxiliary lift device is arranged above the top of the fuselage. A fixed wing, A hydrogen balloon, A multi-axis aircraft and other devices capable of improving the lifting force of the aircraft are additionally arranged on the basis of the flapping-wing aircraft, stable lifting force is provided for the aircraft, and flying is better facilitated.

    本发明公开了一种具备辅助提升升力装置的扑翼飞行器,包括:机身、机翼装置、助跑装置、电机和电池;所述机身尾部安装尾翼;所述助跑装置安装在所述机身下侧;两组所述机翼装置安装在所述机身两侧,所述机翼装置、所述助跑装置均由电机驱动,多个电机通过电池供电,所述机身顶部上方设置有辅助升力装置;本发明在扑翼飞行器的基础上增设了具有提升飞行器升力的固定翼、氢气球、多轴飞行器等装置,为飞行器提供稳定的升力,更有利于飞行。


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    Titel :

    Flapping-wing air vehicle with auxiliary lifting force device


    Weitere Titelangaben:

    一种具备辅助提升升力装置的扑翼飞行器


    Beteiligte:
    WANG ZHICHENG (Autor:in)

    Erscheinungsdatum :

    2021-01-29


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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