The invention discloses an electric tilt-rotor aircraft and a control system thereof. The fuselage comprises a fuselage body and a rudder and is used for controlling and adjusting the flight direction of the aircraft; the wing body structure adopts a separation mode and comprises an integral wing box section, an aileron, a wing left/right nacelle and a stay bar left/right nacelle, a left stay bar and a right stay bar are integrated on the front side of the integral wing box section, the wing left/right nacelle is connected with the integral wing box section through a tilting shaft, and the wing left/right nacelle rotates around the tilting shaft; the horizontal tail comprises a horizontal tail box section and a horizontal tail left/right nacelle, the horizontal tail left/right nacelle is connected with the horizontal tail box section through a tilting shaft, and the left/right horizontal tail rotates around the tilting shaft; the undercarriage is a three-point undercarriage, a brake system is integrated in the main undercarriage, and the front undercarriage plays a role in balancing and direction control. By adopting the electric tilt-rotor aircraft provided by the invention, urban air traffic can be realized.

    本发明公开一种电动倾转旋翼飞行器及其控制系统。所述飞行器包括:机身包括机身本体和方向舵,控制和调节飞行器飞行方向;机翼翼身结构为分离方式,包括整体式机翼盒段、副翼、机翼左/右短舱和撑杆左/右短舱,整体式机翼盒段前侧集成左右撑杆,机翼左/右短舱与整体式机翼盒段通过倾转轴相连,机翼左/右短舱绕倾转轴旋转;平尾包括平尾盒段和平尾左/右短舱,平尾左/右短舱与平尾盒段通过倾转轴相连,左/右平尾绕倾转轴旋转;起落架采用三点式起落架,主起落架中集成有刹车系统,前起落架起平衡和方向控制的作用。采用本发明提供的电动倾转旋翼飞行器,能够实现城市空中交通。


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    Titel :

    Electric tilt-rotor aircraft and control system thereof


    Weitere Titelangaben:

    一种电动倾转旋翼飞行器及其控制系统


    Beteiligte:
    HWANG IN-GIL (Autor:in) / HUANG YONGWEI (Autor:in) / JIANG JUN (Autor:in)

    Erscheinungsdatum :

    2023-08-29


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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