SCALABLE AIR FILTER CONFIGURATION FOR FUEL TANK INERTING SYSTEM
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United States of America Patent
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Sep 22, 2016
app pub date -
Mar 20, 2015
filing date -
Mar 20, 2015
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Abstract
An aircraft fuel tank inerting system includes a filter apparatus and an air separation module configured to separate oxygen from a fluid stream. The filter apparatus includes a housing unit with a fluid inlet port configured to receive a first fluid stream, a fluid outlet port configured to deliver a second fluid stream, and a plurality of filter cartridges. Each of the plurality of filter cartridges is substantially the same and positioned within the housing unit. The air separation module is in fluid communication with the filter apparatus.
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