The invention relates to an aircraft fuselage intended to receive two storage tanks designed to contain liquid hydrogen. The fuselage (1) comprises a first section for the cockpit (6), a second section for the passenger cabin (7), and a third section (T3) different from the first (T1) and second (T2) sections. The third section (T3) comprises two housings (3) each for accommodating a tank (2). The two housings (3) are arranged symmetrically with respect to a vertical plane of symmetry (P1). This arrangement of the tanks (2) in sections different from the other sections allows these tanks to be positioned as close as possible to the motor (5) to which they must be supplied.

    本发明涉及一种旨在接收被设计成盛装液氢的两个储罐的飞行器机身。机身(1)包括用于驾驶舱(6)的第一区段、用于客舱(7)的第二区段以及与第一区段(T1)和第二区段(T2)不同的第三区段(T3)。第三区段(T3)包括各自用以容纳储罐(2)的两个壳体(3)。两个壳体(3)相对于竖直对称平面(P1)对称地布置。储罐(2)在与其他区段不同的区段中的这种布置允许这些储罐定位得尽可能靠近它们必须供给的马达(5)。


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    Titel :

    Aircraft fuselage intended to receive two storage tanks designed to contain liquid hydrogen


    Weitere Titelangaben:

    旨在接收被设计成盛装液氢的两个储罐的飞行器机身


    Beteiligte:

    Erscheinungsdatum :

    2023-10-20


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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