A tank (10) including a container (15) and a flow line (20) for discharging excess fuel. Said flow line (20) is provided with a pipe (21) and an over-pressure valve (24) arranged inside the container (15). In addition, the tank (10) includes a leaktight bell (30) arranged inside said container, said bell (30) being over the over-pressure valve (24) and surrounding the over-pressure valve (24) at least in part so as to hold air captive in order to isolate the over-pressure valve (24) from the fuel content when said pressure is below said threshold.


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    Titel :

    RESERVOIR MUNI D'UN CLAPET DE SURPRESSION


    Beteiligte:
    BASSET GREGORY (Autor:in)

    Erscheinungsdatum :

    25.12.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Französisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F16K VALVES , Ventile



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