The invention discloses a novel tandem wing device and a tandem wing aircraft. The tandem wing device comprises an annular movement device and a plurality of wings arranged on the annular movement device. The annular movement device can circularly move in an annular manner; and the plurality of wings can circularly move along with the annular moving device, so that the tandem wing device obtains lift force or simultaneously obtains lift force and thrust force. The motion trail of the geometric center of each wing is on a horizontal plane or a plane forming an included angle of less than 45 degrees with the horizontal plane; according to the arrangement mode of the wings, the wings are not divided into an upper layer and a lower layer, lift force can be generated during vertical take-off and landing, hovering and low-speed flight at the speed lower than the rotating speed, and the lift force is large; when the wing runs to the arc section, the attack angle of the wing is not changed or is slightly changed, and large rotating resistance and forward flying resistance cannot be generated; when the wing runs to the arc section, the centrifugal force direction is consistent with the extension direction of the wing, the requirement for the strength of the wing is not increased, and the wing is light.

    本发明公开了一种新型的串列翼装置及串列翼飞行器。串列翼装置,包括:环形运动装置、以及设置在所述环形运动装置上的若干翼;所述环形运动装置能够环形循环运动;若干翼能够随所述环形运动装置循环运动,以使该串列翼装置获得升力或同时获得升力和推力。本发明的各个翼几何中心的运动轨迹在水平面上或与水平面成小于45度夹角的平面上;翼的这种布置方式使得翼不分上下层,在垂直起降、悬停、低于转动速度较多的低速飞行时都能产生升力,升力大;翼运行到圆弧段时翼的迎角不变或变化小,不会产生较大的转动阻力和前飞阻力;翼运行到圆弧段时离心力方向和翼的展长方向一致,对翼的强度要求没有增加,翼重量轻。


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    Titel :

    Novel tandem wing device and tandem wing aircraft


    Weitere Titelangaben:

    一种新型串列翼装置及串列翼飞行器


    Beteiligte:
    FU HAIYU (Autor:in) / FU HAIJIAO (Autor:in) / XUE HAIFENG (Autor:in)

    Erscheinungsdatum :

    2022-02-22


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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