The invention discloses a hybrid energy-saving four-wing flapping-wing aircraft with an auxiliary lifting device. The hybrid energy-saving four-wing flapping-wing aircraft comprises an aircraft body,wing devices, a run-up device, a motor and a battery, the run-up device is mounted on the lower side of the machine body; the four 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 auxiliary lift devices are arranged at the nose and the tail of the top of the fuselage.A solar cell panel is mounted on the surface of the machine body; the solar cell panel is connected with the battery; the wing device adopts a flapping wing form, simulates bird flight, can effectively improve the flight stability and reduce the fall of a flapping wing flight path through four groups of wings in diagonal linkage, is provided with independent and symmetrical auxiliary lifting devices, can steer, adopts a battery to supply power, and is provided with a solar cell panel to supplement electric power, so that the cruising ability of the aircraft is improved; stable flight of the aircraft is ensured, and the flight distance is increased.

    本发明公开了一种具备辅助提升装置的混动节能四翼扑翼飞行器,包括:机身、机翼装置、助跑装置、电机和电池;所述助跑装置安装在所述机身下侧;四组所述机翼装置安装在所述机身两侧,所述机翼装置和所述助跑装置均由电机驱动,多个电机通过电池供电,所述机身顶部机头和机尾处设置有辅助升力装置;所述机身表面安装有太阳能电池板;所述太阳能电池板连接所述电池;机翼装置采用扑翼形式,模仿鸟类飞行,对角联动的四组机翼可有效提升飞行稳定性,减少扑翼飞行轨迹的落差,具备独立且对称设置的辅助提升装置,可进行转向,采用电池供电,并设置了太阳能电池板进行电力补充,提高飞行器的续航能力,保证飞行器的稳定飞行,提高飞行路程。


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    Title :

    Hybrid energy-saving four-wing flapping wing aircraft with auxiliary lifting device


    Additional title:

    一种具备辅助提升装置的混动节能四翼扑翼飞行器


    Contributors:

    Publication date :

    2021-01-29


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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