The vertical take-off and landing jet-propelled high-speed aircraft comprises an aircraft body, a rotor wing device and a jet device, the aircraft body comprises an aircraft body and wings fixed to the left side and the right side of the aircraft body, and ailerons are arranged on the rear sides of the wings; the rotor wing device comprises two rotor wing mechanisms arranged on the wings respectively, each rotor wing mechanism comprises a motor arranged forwards and a paddle arranged on an output shaft of the motor, the paddles are hinged to the output shafts in the length direction, when the motors are started, the paddles are unfolded to rotate, and when the motors are closed, the paddles are unfolded to rotate. The paddles can be folded backwards; and the jet device comprises a jet engine arranged at the tail part of the fuselage. According to the vertical take-off and landing jet-propelled high-speed aircraft, high-speed flight of a vertical take-off and landing fixed-wing aircraft can be achieved.

    本发明公开了一种垂直起降喷气式高速飞行器,包括飞机主体、旋翼装置和喷射装置,所述飞机主体包括机身、固定在所述机身左右两侧的机翼,所述机翼的后侧设有副翼;所述旋翼装置包括2个分别设置在所述机翼的旋翼机构,所述旋翼机构包括朝前设置的电机、设置在所述电机的输出轴的桨叶,所述桨叶与所述输出轴的长度方向铰接,当所述电机启动时,所述桨叶展开旋转,当所述电机关闭时,所述桨叶可向后折叠;所述喷射装置包括设置在所述机身尾部的喷气式发动机。本发明的垂直起降喷气式高速飞行器,能够实现垂直起降固定翼飞行器的高速飞行。


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    Title :

    Vertical take-off and landing jet-propelled high-speed aircraft


    Additional title:

    一种垂直起降喷气式高速飞行器


    Contributors:
    KONG LING (author) / LIANG JIN (author) / ZHI YAFANG (author)

    Publication date :

    2023-01-31


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge