A device for controlling pitching and heading through combination of three thrust propellers is characterized in that three water tower type motor mounting seats of a Y-shaped motor mounting seat are rotationally arranged around the central axis of a circular arm mounting seat, the included angle between every two adjacent water tower type motor mounting seats is 120 degrees, a lower motor and a lower thrust propeller are sequentially connected to the lower portion of the lower water tower type motor mounting seat, and the lower water tower type motor mounting seats are connected to the lower portion of the lower thrust propeller; the left inclined motor and the left inclined thrust propeller are sequentially connected to the left inclined water tower type motor mounting seat, and the right inclined motor and the right inclined thrust propeller are sequentially connected to the right inclined water tower type motor mounting seat, so that the three-thrust-propeller combined pitching and heading control device is formed. The vertical downward component force of the lift force of the left oblique thrust propeller and the right oblique thrust propeller and the vertical upward lift force of the lower thrust propeller differentially control the pitching of the aircraft, the horizontal component force of the lift force of the left oblique thrust propeller and the right oblique thrust propeller differentially control the course of the aircraft, and the course of the aircraft is controlled through torque. And the course control capability is high.

    一种三个推力螺旋桨组合操纵俯仰和航向装置,Y型电机安装座的三个水塔型电机安装座绕圆形的机臂安装座中心轴线旋转排列,相邻两个水塔型电机安装座的夹角是120°,下电机、下推力螺旋桨顺序连接在下水塔型电机安装座下面,左斜电机、左斜推力螺旋桨顺序连接在左斜水塔型电机安装座上面,右斜电机、右斜推力螺旋桨顺序连接在右斜水塔型电机安装座上面,构成三个推力螺旋桨组合操纵俯仰和航向装置,应用于多螺旋桨飞行器,左斜推力螺旋桨、右斜推力螺旋桨的升力的垂直向下分力与下推力螺旋桨的垂直向上的升力差动操纵飞行器的俯仰,左斜推力螺旋桨、右斜推力螺旋桨的升力的水平分力差动操纵飞行器的航向,采用力矩操纵飞行器的航向,航向的操纵能力强。


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    Title :

    Device for controlling pitching and heading through combination of three thrust propellers


    Additional title:

    三个推力螺旋桨组合操纵俯仰和航向装置


    Contributors:
    JIANG FUYU (author)

    Publication date :

    2025-05-27


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge




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