Aircraft Fuel Tank Inerting System Adapted To Compute The Quantity Of Oxygen Present In An Inerting Gas Injected Into Said Tank
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United States of America Patent
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Jun 8, 2017
app pub date -
Dec 2, 2016
filing date -
Dec 3, 2015
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Abstract
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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