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 ...
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 ...
CONSTITUTION: The method comprises a step (S101) of calculating an amount of dissolved oxygen contained in feed water supplied per a unit time; a step (S102) of calculating quantity of required chemical; a step (S103) of calculating quantity of diluted water; and a step (S104) of ...
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 ...
The present invention relates to an inerting system (1) of a fuel tank of an aircraft. Said system comprises: - a sensor (6) comprising a phosphorescent material (7), arranged in distribution means (4) for an inerting gas and in contact with said inerting gas; a light source (10) ...
for calculating the amount of oxygen present in the neutral gas as a function of the attenuation of the measured phosphorescence directly related to the amount of oxygen in the neutral gas.;EFFECT: precise calculation of the amount of oxygen in a neutral gas is provided for a long time.;6 ...