The invention relates to the field of aircrafts, and discloses a fixed-wing vertical take-off and landing aircraft which comprises a fuselage, a fixed-wing assembly and a rotor assembly are arranged on the fuselage, the fixed-wing assembly comprises two fixed wings arranged on the two sides of the fuselage and an empennage arranged at the tail of the fuselage, and first engines are arranged at the bottoms of the fixed wings; the fixed wings are internally provided with vertically-through first containing cavities, the rotor wing assembly comprises two main rotor wings, and the two main rotor wings are rotationally arranged in the first containing cavities of the two fixed wings with the height direction of the fuselage as the axis. The aircraft has the advantages that by adopting the fixed wing assembly and the rotor wing assembly, when the aircraft takes off, the two main rotor wings rotate, and the aircraft is vertically lifted; when the aircraft flies, the first engine provides power for the aircraft, so that the aircraft flies at a high speed; when the aircraft lands, the main rotor rotates again, so that the aircraft can land vertically, and the aircraft can fly at a high speed and take off and land vertically.

    本申请涉及飞行器领域,公开了一种固定翼垂直起降飞行器,包括机身,机身上设置有固定翼组件和旋翼组件,固定翼组件包括设置于机身两侧的两个固定翼以及设置于机身尾部的尾翼,固定翼底部设置有第一发动机,固定翼内开设有上下贯通的第一容置腔,旋翼组件包括两个主旋翼,两个主旋翼均以机身高度方向为轴线转动设置在两个固定翼的第一容置腔内。本申请具有能够通过采用固定翼组件和旋翼组件,飞行器起飞时,连个主旋翼转动并将飞行器垂直抬升;飞行器飞行时,第一发动机为飞行器提供动力,使得飞行器高速飞行;飞行器降落时,主旋翼再次转动,使得飞行器能够垂直降落,如此使得飞行器能够兼顾高速飞行和垂直起降。


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    Title :

    Fixed-wing vertical take-off and landing aircraft


    Additional title:

    一种固定翼垂直起降飞行器


    Contributors:

    Publication date :

    2024-08-06


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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