The invention provides a tail cone with a speed reduction assembly and an aircraft with the tail cone. The tail cone includes a first deceleration plate disposed on the tail cone and having a first closed position in which the first deceleration plate is conformal to the tail cone and covers a portion of the tail cone and a first open position in which the first deceleration plate is conformal to the tail cone and covers a portion of the tail cone. The first deceleration plate pivots about a first end of the first deceleration plate and a second end of the first deceleration plate is remote from the tail cone.

    本发明提供了具有减速组件的尾锥及装有尾锥的飞机。尾锥包括第一减速板,第一减速板设置在尾锥上并且具有第一闭合位置和第一打开位置,在第一闭合位置中,第一减速板适形于尾锥并且覆盖尾锥的一部分,在第一打开位置中,第一减速板围绕第一减速板的第一端枢转并且第一减速板的第二端远离尾锥。


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    Titel :

    Tail cone with speed reduction assembly and aircraft with tail cone


    Weitere Titelangaben:

    具有减速组件的尾锥及装有尾锥的飞机


    Beteiligte:
    ZHANG PENGFEI (Autor:in) / SHAO XINGXIANG (Autor:in) / REN YUKANG (Autor:in) / ZHANG KAIWEN (Autor:in) / CHEN QI (Autor:in) / LI XUHUI (Autor:in)

    Erscheinungsdatum :

    2022-06-03


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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