A right front propeller and a left front propeller are respectively mounted at the front end of a right front arm and the front end of a left front arm of a fuselage main body, and a right rear propeller and a left rear propeller are respectively mounted at the middle sections of a right rear arm and a left rear arm of the fuselage main body; a right rear offset propeller and a left rear offset propeller are respectively mounted at the rear ends of a right rear arm and a left rear arm of the fuselage main body; the course of the aircraft is differentially controlled by the lift force of the right rear offset propeller and the left rear offset propeller, and the pitching and rolling of the aircraft are differentially controlled by the lift force of the right front propeller, the left front propeller, the right rear propeller and the left rear propeller, so that the available accelerator stroke for controlling the pitching, the rolling and the course is increased, and the crosswind resistance is improved; or a middle large rotor wing is additionally arranged on the middle small tower, or large rotor wings are additionally arranged on the middle front small tower and the middle rear small tower, or large rotor wings are additionally arranged on the left flat knitting arm and the right flat knitting arm to improve the loading capacity of the aircraft, or fixed wings are additionally arranged to improve the horizontal flight efficiency, and a universal flight platform is formed.

    一种双偏置垂直尾螺旋桨多螺旋桨飞行器,机身主体的右前机臂的前端、左前机臂的前端分别安装右前螺旋桨、左前螺旋桨,机身主体的右后机臂、左后机臂的中段分别安装右后螺旋桨、左后螺旋桨,机身主体的右后机臂、左后机臂的后端分别安装右后偏置螺旋桨、左后偏置螺旋桨;右后偏置螺旋桨和左后偏置螺旋桨的升力差动操纵飞行器的航向,右前螺旋桨、左前螺旋桨、右后螺旋桨、左后螺旋桨的升力差动操纵飞行器的俯仰和横滚,提高了操纵俯仰、横滚和航向的可用油门行程,提高了抗侧风能力;或在中部小塔增加中部大旋翼,或中前、中后小塔增加大旋翼,或左右横机臂增加大旋翼提高飞行器的载重能力,或增加固定翼提高水平飞行效率,成为通用的飞行平台。


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    Title :

    Multi-propeller aircraft with double offset vertical tail propellers


    Additional title:

    双偏置垂直尾螺旋桨多螺旋桨飞行器


    Contributors:
    JIANG FUYU (author)

    Publication date :

    2025-03-25


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64U



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