An aircraft fuel tank inerting arrangement 1 is provided for providing oxygen-depleted gas to one or more aircraft fuel tanks. The arrangement comprises a gas inlet 2 supplying oxygen-containing gas to an oxygen remover 10 that is configured to remove oxygen to produce an oxygen-depleted gas. A first flow control valve 12 controls the flow of oxygen depleted gas to at least one gas outlet for supply of oxygen-depleted gas to an aircraft fuel tank.


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    Title :

    Aircraft fuel tank inerting arrangement


    Contributors:

    Publication date :

    2015-06-03


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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