A tank (10) having a casing (20) with a bottom (21) together with a side wall (23) and a top wall 22. The tank (10) has at least one sloping wall (30) for providing at least one slope (30) for directing fuel towards a predetermined zone (100) of the tank (10) by gravity, the sloping wall (30) subdividing the inside volume of the tank into a main volume (V1) and an under-slope volume (V2) both of which are to receive fuel. The tank (10) is provided with a fuel transfer system (40) for transferring fuel from the under-slope volume (V2) to the main volume (V1), and from the main volume (V1) to the under-slope volume (V2).


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    Titel :

    Fuel storage tank, an aircraft, and a method


    Beteiligte:
    MEILLAT ROLAND (Autor:in) / MOUGIN STEPHANE (Autor:in) / BRESCON QUITTERIE (Autor:in)

    Erscheinungsdatum :

    27.10.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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




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