The invention discloses a flapping-wing air vehicle with wings capable of adjusting attack angles. The flapping-wing air vehicle comprises a vehicle body, wing devices, a run-up device, a motor and abattery. 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, the wing devices adopt a flapping wing mode, imitate flying of birds and are combinedwith rotor wings on the basis, rotor wing blades are driven to rotate while the driving mechanism flaps, and the running-up device is driven to run; the rotation directions of the wings are the same during downward flapping and rising, continuous and stable lifting force is provided, stable flight of the aircraft is guaranteed, and the flight efficiency is improved.

    本发明公开了一种翼片能够调节迎角的扑翼飞行器,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,所述机翼装置和所述助跑装置均由电机驱动,多个电机通过电池供电,其中机翼装置采用扑翼形式,模仿鸟类飞行,并在此基础上与旋翼相结合,在驱动机构进行扑动的同时带动旋翼翼片旋转,且下扑与回升时翼片旋转方向相同,提供持续稳定的升力,保证飞行器的稳定飞行,提高飞行效率。


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    Titel :

    Flapping-wing air vehicle with adjustable attack angles of wings


    Weitere Titelangaben:

    一种翼片能够调节迎角的扑翼飞行器


    Beteiligte:
    WANG ZHICHENG (Autor:in)

    Erscheinungsdatum :

    2021-02-05


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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