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.
СИСТЕМА НЕЙТРАЛЬНОГО ГАЗА ДЛЯ ТОПЛИВНОГО БАКА ВОЗДУШНОГО СУДНА, ПРИСПОСОБЛЕННАЯ ДЛЯ ВЫЧИСЛЕНИЯ КОЛИЧЕСТВА КИСЛОРОДА, ПРИСУТСТВУЮЩЕГО В НЕЙТРАЛЬНОМ ГАЗЕ, НАГНЕТАЕМОМ В УКАЗАННЫЙ БАК
2018-06-01
Patent
Electronic Resource
Russian
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 |
European Patent Office | 2018
СИСТЕМА ПРЕДОСТАВЛЕНИЯ УСЛУГ ПАССАЖИРУ ДЛЯ ВОЗДУШНОГО СУДНА
European Patent Office | 2015