An inerting system for aircraft including a gas circuit with successively at least one air inlet, a compressor and an air separation module. The air separation module includes an outlet for oxygen-enriched gas and an outlet for inerting gas. The air separation module includes gas permeation membranes resistant to a temperature greater than or equal to 100° C. and preferably 140° C., and the inerting gas outlet is connected to a turbine for releasing pressure and cooling the inerting gas.


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    Title :

    SYSTEME D'INERTAGE ET PROCEDE DE GENERATION D'UN GAZ D'INERTAGE DANS UN AERONEF, FONCTIONNANT SANS PRELEVEMENT D'AIR EXTERIEUR


    Additional title:

    INERTING SYSTEM AND METHOD FOR GENERATING AN INERTING GAS IN AN AIRCRAFT, OPERATING WITHOUT EXTERNAL AIR COLLECTION
    INERTISIERUNGSSYSTEM UND ERZEUGUNGSVERFAHREN VON INERTISIERUNGSGAS IN EINEM LUFTFAHRZEUG, DAS OHNE AUSSENLUFTENTNAHME FUNKTIONIERT


    Contributors:

    Publication date :

    2021-04-28


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

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