An aircraft fuel tank inerting system is disclosed. An aircraft fuel tank inerting system may include a paramagnetic pump arranged to apply a magnetic field to a source of gas to provide a motivational force for removing oxygen from said gas. A paramagnetic pump may include a series of magnetic field generating elements configured to provide a sequence of discrete spaced apart magnetic fields. The series of magnetic field generating elements may include a series of spaced apart pairs of magnetic field generating elements. Each spaced apart pair of magnetic field generating elements may be arranged to generate a respective spaced apart magnetic field, of the sequence of discrete spaced apart magnetic fields, across an airspace therebetween.


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    Title :

    Fuel tank inerting


    Contributors:

    Publication date :

    2021-02-23


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / A62C FIRE-FIGHTING , Feuerbekämpfung / H02K Dynamoelektrische Maschinen , DYNAMO-ELECTRIC MACHINES



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