A fuel tank inerting system including: a catalytic reactor (222) comprising an inlet, an outlet, a reactive flow path between the inlet and the outlet, a catalyst on the reactive flow path, and a temperature sensor located between the inlet and outlet, wherein the catalytic reactor is arranged to receive fuel from a fuel source and air from an air source that are mixed to form a combined flow, and to react the combined flow along the reactive flow path to generate an inert gas.


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    Titel :

    CATALYST DEACTIVATION MONITORING OF CATALYTIC INERTING SYSTEM


    Weitere Titelangaben:

    KATALYSATORDEAKTIVIERUNGSÜBERWACHUNG EINES KATALYTISCHEN INERTISIERUNGSSYSTEMS
    SURVEILLANCE DE DÉSACTIVATION DE CATALYSEUR DE SYSTÈME D'INERTAGE CATALYTIQUE


    Beteiligte:
    COCKS PETER AT (Autor:in) / SMITH LANCE L (Autor:in)

    Erscheinungsdatum :

    17.11.2021


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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