An aircraft section comprising a first fuel storage tank and a second fuel storage tank arranged in a caudal tandem configuration. The corresponding casings, housing conduits configured for distribution of fuel to and from inside the tanks, are arranged in a common section of the fuselage and spaced between them. Also an aircraft with such a section.


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    Titel :

    AIRCRAFT FUSELAGE SECTION



    Erscheinungsdatum :

    19.12.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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