The embodiment of the invention provides a fuel tank for a fixed-wing aircraft. The fuel tank comprises a first-section shell, a second-section shell connected with the first-section shell in an inserted mode, and a third-section shell connected with the second-section shell in an inserted manner; the first-section shell is sealed in a radial direction and connected with the second-section shell in an inserted mode through a first butt joint frame; and the second-section shell is sealed in a radial direction and connected with the third-section shell in an inserted mode through a second butt joint frame. The fuel tank for the fixed-wing aircraft is high in overall rigidity and light in weight.

    本发明的实施例提供一种用于固定翼飞行器的燃料箱,包括:第一段壳体;与所述第一段壳体插接的第二段壳体;以及与所述第二段壳体插接的第三段壳体;其中,所述第一段壳体径向密封,并通过第一对接框与所述第二段壳体插接,所述第二段壳体径向密封,并通过第二对接框与所述第三段壳体插接。本发明的用于固定翼飞行器的燃料箱的整体刚度高、重量轻。


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    Titel :

    Fuel tank for fixed-wing aircraft


    Weitere Titelangaben:

    一种用于固定翼飞行器的燃料箱


    Beteiligte:
    JI BAOFENG (Autor:in) / WANG ZHIYONG (Autor:in) / WANG FEI (Autor:in) / LIU FAJIE (Autor:in) / LIU HANYANG (Autor:in)

    Erscheinungsdatum :

    15.09.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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