The invention belongs to the technical field of aircraft V-tail design, and particularly relates to an aircraft V-tail structure which comprises two V-tails, and each V-tail is correspondingly arranged on one side of an aircraft body; and one end of each rotating shaft correspondingly extends into one V tail, the other end of each rotating shaft is bent and extends into the machine body, and the ends are horizontal with the machine body and can drive the corresponding V tails to rotate around the axes of the bent ends.

    本申请属于飞机V尾设计技术领域,具体涉及一种飞机V尾结构,包括:两个V尾,每个V尾对应在机体的一侧设置;两个转轴,每个转轴的一端对应伸入到一个V尾内设置,其另一端弯折伸入到机体内设置,该端与机体水平,能够驱动对应的V尾绕弯折端的轴线转动。


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    Titel :

    Airplane V tail structure


    Weitere Titelangaben:

    一种飞机V尾结构


    Beteiligte:
    SON JI-HYO (Autor:in) / HE GUANGHONG (Autor:in) / ZHANG JIAN (Autor:in) / XU LU (Autor:in) / ZHANG PEILIANG (Autor:in)

    Erscheinungsdatum :

    2022-07-29


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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