A two-shaft aircraft capable of taking off and landing vertically and a control device thereof comprise a lift force module, a control platform, a power module and a flight control device and are characterized in that the lift force module is composed of two or four large-size 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 flight attitude and speed of the aircraft can be adjusted by adjusting the electric motor and controlling the rotating speed of the propeller of the lift module through the electronic speed regulator, the power module is composed of a battery or an internal combustion engine, and the control device is controlled by the control platform and can control flowing of air passing through the propeller and adjust lift on the left side and the right side of the propeller. And the effects of adjusting the flight posture and controlling balance are achieved.

    一种两轴可垂直起降飞行器及其控制装置,包括升力模块,操控平台,动力模块和飞行控制装置,其特征在于升力模块由2或4个大尺寸螺旋桨组成,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,控制升力模块螺旋桨的转速调整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,控制装置由操控平台控制,可以控制通过螺旋桨的空气流动,调节螺旋桨左右两侧的升力,起到调整飞行姿势和控制平衡的作用。


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Two-axis vertical take-off and landing aircraft and control device thereof


    Weitere Titelangaben:

    一种两轴可垂直起降飞行器及其控制装置


    Beteiligte:
    FAN CHANGLIANG (Autor:in)

    Erscheinungsdatum :

    2022-12-27


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge