The invention discloses a fixed-wing helicopter with multiple layers of propellers. A cross beam is arranged at the top of a helicopter body and above the gravity center, longitudinal beams are arranged on the left side and the right side of the cross beam, a row of front-end motors are downwards arranged at the front ends of the longitudinal beams, and a row of front-end thrust propellers with horizontally-arranged rotating faces are installed on the row of front-end motors. A row of longitudinal beam rear-end motor mounting seats are upwards arranged at the rear ends of the longitudinal beams, a row of longitudinal beam rear-end motors are mounted on the row of motor mounting seats, a row of longitudinal beam rear-end tension propellers with horizontally arranged rotating surfaces are mounted on the row of motors, and a first row of high-aspect-ratio fixed wings in front of one or more rows of cross beams are arranged in front of the cross beams and on the longitudinal beams; one or more rows of high-aspect-ratio fixed wings in the first row behind the cross beams are arranged behind the cross beams and on the longitudinal beams, a horizontal empennage is mounted on the tail extension beam, a backward thrust propeller and a forward tension propeller of which the rotating surfaces are perpendicular to the horizontal plane are arranged in the middle of the horizontal empennage, and an undercarriage is arranged below the fuselage near the gravity center. The fixed-wing helicopter is applied to transportation, agricultural operation, forest fire extinguishing, exploration and the like.

    一种多层螺旋桨固定翼直升飞机,机身顶部、重心的上面设置横梁,在横梁左右两边设置纵梁,在纵梁的前端向下设置一行前端电机,在一行前端电机上安装一行旋转面水平设置的前端推力螺旋桨,在纵梁的后端向上设置一行纵梁后端电机安装座,在该行电机安装座上安装一行纵梁后端电机,在该行电机上安装一行旋转面水平设置的纵梁后端拉力螺旋桨,在横梁前、纵梁上设置一行或多行横梁前第一行大展弦比固定翼,在横梁后、纵梁上设置一行或多行横梁后第一行大展弦比固定翼,在尾部延长梁上安装水平尾翼,在水平尾翼的中间设置旋转面垂直于水平面的向后推力螺旋桨和向前拉力螺旋桨,重心附近机身下设置起落架,应用于运输,农业作业、森林灭火,勘探等领域。


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    Title :

    Fixed-wing helicopter with multiple layers of propellers


    Additional title:

    多层螺旋桨固定翼直升飞机


    Contributors:
    JIANG FUYU (author)

    Publication date :

    2022-02-15


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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