A manned aircraft and a control device thereof comprise a lift force module, a control platform, a power module, a propulsion module and a flight control module, and are characterized in that the lift force module is composed of 2-16 propellers, the propellers are driven by an electric motor or an internal combustion engine to rotate so as to generate lift force, and the control platform is composed of a core control unit. The electric motor can be adjusted through the electronic speed regulator, the flight attitude and speed of the aircraft can be controlled, the power module is composed of a battery or an internal combustion engine, the flight control module is composed of 3-8 propellers, lift force on the left side, the right side, the front side and the rear side of the aircraft can be adjusted, and the effects of adjusting the flight attitude and controlling balance are achieved.

    一种载人飞行器及其控制装置,包括升力模块,操控平台,动力模块,推进模块和飞行控制模块,其特征在于升力模块由2‑16个螺旋桨组成,螺旋桨由电动马达或内燃机驱动旋转以产生升力,操控平台由核心控制单元组成,可以通过电子调速器调整电动马达,控制飞行器的飞行姿态和速度,动力模块由电池或内燃机组成的,飞行控制模块由3‑8个螺旋桨组成,可以调节飞行器左右和前后两侧的升力,起到调整飞行姿势和控制平衡的作用。


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    Title :

    Manned aircraft and control device thereof


    Additional title:

    一种载人飞行器及其控制装置


    Contributors:

    Publication date :

    2022-11-04


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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