An aircraft fuel tank inerting system for a fixed wing aircraft having at least one main fuel tank in the wing and an associated surge tank includes a source of inerting fluid and a flow passage for supplying said inerting fluid to the main fuel tank and discharging it into the main filet tank through at least one discharge outlet. The flow passage includes a pressure relief arrangement adapted to discharge into the surge tank if a pressure in the main fuel tank exceeds a predetermined threshold.


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    Titel :

    AIRCRAFT FUEL TANK INERTING SYSTEMS


    Beteiligte:

    Erscheinungsdatum :

    11.02.2016


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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