The invention discloses a flapping-wing aircraft with the gravity center below two wings. The flapping-wing aircraft comprises wing devices, a cockpit and a run-up device. The wing device is installedat the top of the cockpit and comprises a driving cabin body, a driving assembly, a connecting assembly and wings. The driving assembly is installed in the driving cabin body, and the connecting assembly and the wings are installed on the outer side of the driving cabin body; a seat, armrests and a pedal device are mounted in the cockpit; an empennage is arranged at the tail part of the cabin body and is connected with the handrail through a pull rod; the run-up device is mounted at the bottom of the cockpit; the ornithopter has the advantages that the ornithopter is in a flapping wing form and is combined with the rotor wings on the basis of the flapping wing form, accordingly, the flight efficiency can be improved, the gravity center can be arranged below the wing devices, and the ornithopter is high in stability; the unmanned aerial vehicle can be driven by electric power and manpower, the situation that safe landing cannot be achieved due to power exhaustion in the flight state isprevented, and the flight safety guarantee is improved.

    本发明公开了一种重心在两翼之下的扑翼飞行器,包括机翼装置、驾驶舱和助跑装置;所述机翼装置安装在所述驾驶舱的顶部,包括驱动舱体、驱动组件、连接组件和机翼;所述驱动组件安装在所述驱动舱体内,所述连接组件和机翼安装在所述驱动舱体外侧;所述驾驶舱内部安装有座椅、扶手和踏板装置;并在舱体尾部设置有尾翼,所述尾翼通过拉杆与所述扶手连接;所述助跑装置安装在所述驾驶舱底部;所述助跑装置和所述机翼装置均通过电机驱动,本发明采用扑翼形式,并在此基础上与旋翼相结合,提高飞行效率,将重心设置在机翼装置下方,稳定性更高;可通过电力和人力两种方式驱动,防止在飞行状态时,电量耗尽无法安全降落,提高了飞行的安全保证。


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    Titel :

    Flapping-wing air vehicle with gravity center below two wings


    Weitere Titelangaben:

    一种重心在两翼之下的扑翼飞行器


    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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