发明名称 ENGINE PROXIMATE NITROGEN GENERATION SYSTEM FOR AN AIRCRAFT
摘要 A nitrogen generation system 10 includes a bleed air source. The system also includes an air separation module 20 having an inlet for receiving bleed air, a hollow fiber membrane 62 for substantially removing oxygen from the bleed air to produce a stream of oxygen enriched air and a stream of nitrogen enriched air, a first outlet 54 for exhausting the nitrogen enriched air, a second outlet 58 for exhausting the oxygen enriched air from the air separation module 20. The system also includes a nitrogen enriched air line configured to receive the nitrogen enriched air and a fuel tank 28 disposed downstream from the air separation module. The air separation module 20 is positioned within a one of the group consisting of a gas turbine engine, a nacelle, a pylon, an aircraft wing, and combinations thereof.
申请公布号 EP3070000(A3) 申请公布日期 2016.12.07
申请号 EP20160161097 申请日期 2016.03.18
申请人 Hamilton Sundstrand Corporation 发明人 DANIELLO, Robert
分类号 B64D37/32 主分类号 B64D37/32
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