A fuel tank inerting system (20) is provided including an air flow comprising air from a first source (24) having a first temperature and air from a second source (32) having a second temperature. The second temperature is cooler than the first temperature. At least one air separating module (30) is configured to separate an inert gas from the air flow.


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    Title :

    TEMPERATURE CONTROL SYSTEM FOR FUEL TANK INERTING SYSTEM


    Additional title:

    TEMPERATURSTEUERUNGSSYSTEM FÜR KRAFTSTOFFTANKINERTISIERUNGSSYSTEM
    SYSTÈME DE RÉGULATION DE TEMPÉRATURE POUR SYSTÈME D'INERTAGE DE RÉSERVOIR DE CARBURANT


    Contributors:

    Publication date :

    2022-01-05


    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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