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Title:
航空機燃料タンク内に注入される不活性化ガス中に存在する酸素量を計算するように適合された航空機燃料タンク不活性化システム
Document Type and Number:
Japanese Patent JP6550367
Kind Code:
B2
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.

Inventors:
Bruno Reynard
Frederick Denato
Application Number:
JP2016234647A
Publication Date:
July 24, 2019
Filing Date:
December 02, 2016
Export Citation:
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Assignee:
Zodiac Aerotechnics
International Classes:
B64D37/02; B64D37/32; G01N21/64
Domestic Patent References:
JP2010506173A
JP59170748A
JP4233456A
Foreign References:
US20080060523
US20090141280
WO2015066416A1
Attorney, Agent or Firm:
Asamura patent office