An aircraft tail and an aircraft comprising such an aircraft tail, the aircraft tail comprising: a tail body extending substantially in a longitudinal direction; the pair of horizontal empennages respectively extend out from the two sides of the tail main body and approximately extend along a horizontal plane; the power fan is arranged at the tail end of the tail body, and the power fan is located on the rear side of the horizontal tail; the aircraft tail further comprises paired vertical tails, and the vertical tails are symmetrically arranged at the paired horizontal tails relative to the rotation axis of the power fan and extend approximately perpendicular to the horizontal tails. According to the aircraft tail, the boundary layer suction effect is improved.

    一种飞行器尾部和包括这种飞行器尾部的飞行器,飞行器尾部包括:机尾主体,该机尾主体大致沿纵向方向延伸;成对的水平尾翼,该对水平尾翼分别从机尾主体两侧延伸而出,大致沿水平平面延伸;动力风扇,该动力风扇布置成在机尾主体的尾端处,动力风扇位于水平尾翼的后侧;其中,飞行器尾部还包括成对的垂直尾翼,该垂直尾翼相对于动力风扇的回转轴线对称地设置在成对的水平尾翼处,并大致垂直于水平尾翼延伸。本发明的飞行器尾部提升了附面层吸入效果。


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    Titel :

    Aircraft tail and aircraft comprising such aircraft tail


    Weitere Titelangaben:

    飞行器尾部及包括这种飞行器尾部的飞行器


    Beteiligte:
    LI JINYE (Autor:in) / WANG QIMIN (Autor:in) / WANG LI (Autor:in) / WU DAWEI (Autor:in) / YAN FANFEI (Autor:in) / TAN ZHAOGUANG (Autor:in)

    Erscheinungsdatum :

    01.11.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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