The invention relates to a fixed wing aircraft with a rear rotor and a T-shaped tail wing. An aircraft includes a canard having a trailing edge, a sweep-forward and fixed wing having a horizontal plane and a trailing edge, and a plurality of tilt rotors. At least one of the plurality of tilt rotors is attached to a trailing edge of the canard, and at least one of the plurality of tilt rotors is attached to a trailing edge of the sweepforward and fixed wing. The aircraft further comprises a T-shaped tail wing with a horizontal plane, wherein the horizontal plane of the T-shaped tail wing is at a height higher than the horizontal plane of the sweepforward and fixed wings.

    本申请涉及具有后旋翼和T型尾翼的固定翼飞机。一种飞机包括具有后缘的鸭翼、具有水平面和后缘的前掠和固定翼以及多个倾转旋翼。该多个倾转旋翼中的至少一个被附接到该鸭翼的后缘,并且该多个倾转旋翼中的至少一个被附接到该前掠和固定翼的后缘。该飞机还包括具有水平面的T型尾翼,其中该T型尾翼的水平面处于高于该前掠和固定翼的水平面的高度处。


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    Titel :

    Fixed-wing aircraft with rear rotor and T-shaped empennage


    Weitere Titelangaben:

    具有后旋翼和T型尾翼的固定翼飞机


    Beteiligte:
    SINHA POOJA (Autor:in) / VANDER LIND DAMON (Autor:in)

    Erscheinungsdatum :

    12.11.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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