The invention relates to the technical field of aircrafts, and discloses a tilting rotor aircraft. The aircraft comprises a fuselage; an empennage which is arranged at the tail part of the fuselage; at least one pair of side wings, wherein each pair of side wings is symmetrically arranged at two sides of the fuselage; at least two tilting support, wherein each side wing is provided with at least one tilting support arm, and the tilting support arms are rotatably connected with the side wings, so the tilting support arms rotate on a plane parallel to the axial direction of the fuselage; at least four rotating wings, wherein the two ends of each tilting supporting arm are each provided with one rotating wing, and the rotating wings rotate along with the tilting supporting arms. The aircraftcan vertically take off and land, has the advantages of high flight speed and high loading capacity, has a simple rotor structure, and can be stably switched between a multi-rotor mode and a fixed-wing mode.

    本发明涉及飞行器技术领域,公开了一种倾转旋翼飞行器,包括:机身;尾翼,所述尾翼设置在所述机身的尾部;至少一对侧翼,每对所述侧翼对称设置在所述机身的两侧;至少两个倾转支臂,每个所述侧翼上至少设有一个所述倾转支臂,所述倾转支臂与所述侧翼转动连接,使所述倾转支臂沿与机身轴向方向平行的一平面上转动;至少四个旋转翼,每个所述倾转支臂的两端分别设有一个所述旋转翼,所述旋转翼随所述倾转支臂转动。倾转旋翼飞行器可以垂直起降,同时具有飞行速度快而且载重能力强的能力,并且旋翼结构简单,可以在多旋翼模式与固定翼模式之间进行平稳切换。


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    Titel :

    Tilting rotor aircraft


    Weitere Titelangaben:

    一种倾转旋翼飞行器


    Beteiligte:
    WU ZHIGUANG (Autor:in)

    Erscheinungsdatum :

    2020-11-03


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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