The invention discloses a vertical take-off and landing flying-wing aircraft, belongs to the field of aircraft design, and solves the problem that an existing vertical take-off and landing flying-wing aircraft is poor in stability. A vertical take-off and landing flying wing aircraft comprises a fuselage, wings, a rotor wing module and a tail thrust module, the wings are arranged on the fuselage, the rotor wing module is arranged on the wings, and the tail thrust module is arranged at the tail end of the fuselage; when the aircraft is in take-off, landing and hovering stages, lift force is provided for the aircraft through the rotor wing module, and when the aircraft is in a cruising stage, thrust is provided for the aircraft under the action of the tail thrust module and the wings, so that the effect of improving the stability of the aircraft is achieved. The aircraft has two flight modes, namely a vertical take-off and landing mode and a horizontal cruise mode, so that a farther voyage and a higher speed of the aircraft are realized.

    本发明公开了一种垂直起降飞翼飞行器,属于飞行器设计领域,解决了现有的垂直起降飞翼飞行器的稳定性不好的问题。一种垂直起降飞翼飞行器,包括机身、机翼、旋翼模块和尾推模块,所述机翼设于所述机身上,所述旋翼模块设于所述机翼上,所述尾推模块设于所述机身末端;当该飞行器处于起降和悬停阶段时,通过所述旋翼模块为该飞行器提供升力,该飞行器处于巡航阶段时,在所述尾推模块和所述机翼的作用下为该飞行器提供推力,进而达到提升该飞行器的稳定性的作用。本发明的飞行器具备两种飞行模式:垂直起降模式和水平巡航模式,以实现飞行器更远的航程和更高的速度。


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    Title :

    Vertical take-off and landing flying wing aircraft


    Additional title:

    一种垂直起降飞翼飞行器


    Contributors:
    GU HONGYUAN (author)

    Publication date :

    2025-01-03


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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