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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    Title :

    СИСТЕМА НЕЙТРАЛЬНОГО ГАЗА ДЛЯ ТОПЛИВНОГО БАКА ВОЗДУШНОГО СУДНА, ПРИСПОСОБЛЕННАЯ ДЛЯ ВЫЧИСЛЕНИЯ КОЛИЧЕСТВА КИСЛОРОДА, ПРИСУТСТВУЮЩЕГО В НЕЙТРАЛЬНОМ ГАЗЕ, НАГНЕТАЕМОМ В УКАЗАННЫЙ БАК


    Publication date :

    2018-06-01


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Russian


    Classification :

    IPC:    B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen