A fuel tank inerting system is provided including an air flow comprising air from a first source having a first temperature and air from a second source having a second temperature. The second temperature is cooler than the first temperature. At least one separating module is configured to separate an inert gas from the air flow.


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    Titel :

    TEMPERATURE CONTROL SYSTEM FOR FUEL TANK INERTING SYSTEM


    Beteiligte:
    D'ORLANDO PAUL M (Autor:in) / SURAWSKI ERIC (Autor:in)

    Erscheinungsdatum :

    18.01.2018


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B01D SEPARATION , Trennen



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