The invention provides an aircraft fuselage section and an aircraft. The aircraft fuselage section includes a first fuel storage tank and a second fuel storage tank arranged in a tail tandem configuration. More specifically, the invention relates to an arrangement of said first and second tanks in which respective housings containing conduits are arranged in the same section of the fuselage and spaced apart between the first and second tanks, the conduits being configured for dispensing fuel to and from the interior of the tanks.

    本发明提供了一种飞行器机身部段以及飞行器。该飞行器机身部段包括以尾部串联构型布置的第一燃料储存罐和第二燃料储存罐。更具体地,本发明涉及所述第一罐和第二罐的布置结构,在该布置结构中,容纳有导管的相应壳体布置在机身的相同部段中并且在第一罐与第二罐之间间隔开,该导管构造成用于将燃料分配到罐的内部和从罐的内部分配燃料。


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    Titel :

    Aircraft fuselage section and aircraft


    Weitere Titelangaben:

    飞行器机身部段以及飞行器



    Erscheinungsdatum :

    17.12.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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