Inerting fuel systems and methods for inerting fuel tanks are disclosed. An inerting fuel system may include an air inlet passage to receive inlet air, air separation modules to separate oxygen from the inlet air when received, and air separation module valves coupled between the air inlet passage and the air separation modules. The air separation module valves are associated with the air separation modules such that opening of one of the air separation module valves passes a portion of inlet air from the air inlet passage to the air separation module associated with that air separation module valve. A controller selectively opens the air separation module valves such that each of the air separation modules receives a substantially equal level of wear.


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    Titel :

    INERTING FUEL SYSTEMS, METHODS, AND APPARATUSES


    Beteiligte:

    Erscheinungsdatum :

    2016-07-28


    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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