The invention provides a tilting ducted fixed-wing aircraft which comprises a fuselage, main wings, canards, ducted fan engines and undercarriages, the fuselage comprises a cockpit located on the front portion of the fuselage and a mission load cabin located on the rear portion of the fuselage, the undercarriages are arranged at the bottom of the fuselage, the upper surface of the main wing on each side is provided with a plurality of ducted fan engines, and the ducted fan engines are arranged on the lower surface of the main wing on each side. A plurality of ducted fan engines are arranged on the upper surfaces of the canards on each side, the main wings and the canards can rotate relative to the fuselage along the axes of the wings, and the ducted fan engines on the main wings and the canards rotate to be perpendicular to the ground and parallel to the ground by controlling rotation of the main wings and the canards. Therefore, vertical take-off and landing and horizontal flight during take-off and landing are realized. The tilting ducted fixed-wing aircraft provided by the invention can realize the capabilities of vertical take-off and landing and horizontal high-speed flight at the same time, is compatible with the advantages of a traditional helicopter and a fixed-wing aircraft, is simple in vertical take-off and landing and horizontal flight mode conversion, and is high in safety.

    本申请提供了一种倾转涵道固定翼飞行器,包括:机身、主机翼、鸭翼、涵道风扇发动机及起落架,其中,机身包括位于机身前部的驾驶舱及位于机身后的任务载荷舱,起落架设置在机身的底部,每侧的主机翼上表面设有若干台涵道风扇发动机,以及每侧的鸭翼上表面也设有若干台涵道风扇发动机,主机翼及鸭翼能够沿着机翼轴线相对于机身进行转动,通过控制主机翼及鸭翼的转动,使得主机翼及鸭翼上的涵道风扇发动机旋转至与地面垂直状态和与地面平行状态,从而起飞与着陆时的垂直起降与水平飞行。本申请的倾转涵道固定翼飞行器能够实现同时具备垂直起降、水平高速飞行的能力,兼容传统直升机与固定翼飞机优点,垂直起降与水平飞行模态转换简单,安全性高。


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    Title :

    Tilting ducted fixed-wing aircraft


    Additional title:

    一种倾转涵道固定翼飞行器


    Contributors:
    SUN YAN (author) / QIAN XIANYUN (author) / XING RONG (author)

    Publication date :

    2022-05-13


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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