An inerting system for inerting a fuel tank of an aircraft. The system includes: a sensor including a phosphorescent material, arranged in a distribution mechanism for distributing an inerting gas and in contact with the inerting gas; a light source illuminating the phosphorescent material; a measurement mechanism for measuring the phosphorescence of the phosphorescent material; and a computation mechanism for computing the quantity of oxygen present in the inerting gas as a function of the attenuation of the phosphorescence as measured that is directly related to the quantity of oxygen in the inerting gas.


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    Titel :

    SYSTEME D'INERTAGE D'UN RESERVOIR DE CARBURANT D'UN AERONEF, ADAPTE POUR CALCULER LA QUANTITE D'OXYGENE PRESENTE DANS UN GAZ D'INERTAGE INJECTE DANS LEDIT RESERVOIR


    Beteiligte:
    REYNARD BRUNO (Autor:in) / DENAT FREDERIC (Autor:in)

    Erscheinungsdatum :

    01.12.2017


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Französisch


    Klassifikation :

    IPC:    G01N Untersuchen oder Analysieren von Stoffen durch Bestimmen ihrer chemischen oder physikalischen Eigenschaften , INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT