A fuel tank for an aircraft, including a fuel pumping system which includes a set of hoses, first ends of which are distributed over a lower part of the tank, a manifold to which second ends of the different hoses of the set of hoses are connected as input, an output of the manifold being connected to a fuel pump, a fuel level sensor associated with each hose of the set of hoses and placed in the vicinity of the first end of said hose, and a valve associated with each hose and controlled by a control system which is configured such that when the fuel level sensor associated with this hose detects a low fuel level, the valve is controlled into a closed position, and otherwise the valve is controlled into an open position.


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    Titel :

    RÉSERVOIR DE CARBURANT POUR AÉRONEF


    Weitere Titelangaben:

    FUEL TANK FOR AIRCRAFT
    KRAFTSTOFFTANK FÜR EIN FLUGZEUG


    Beteiligte:

    Erscheinungsdatum :

    11.06.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Französisch


    Klassifikation :

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



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