发明名称 Commercial Aircraft On-Board Inerting System
摘要 An inerting system ( 10 ) for an aircraft ( 12 ) includes one or more fuel tank circuits ( 15 ) associated with fuel tanks ( 16 ). An air source ( 17 ) supplies pressurized air. A heat exchanger ( 56 ) cools the pressurized air. An air separation module ( 46 ) is in fluid communication with the heat exchanger ( 56 ) and separates inerting gas from the pressurized air. A controller ( 40 ) controls flow of the inerting gas from the air separation module ( 46 ) to the fuel tanks ( 16 ).
申请公布号 US2005173017(A1) 申请公布日期 2005.08.11
申请号 US20040708110 申请日期 2004.02.10
申请人 THE BOEING COMPANY 发明人 MORAVEC BRADFORD L.;BOGGS ROYAL E.;GRAHAM RODNEY N.;GRIM ALAN;ADKINS DAVID A.;SNOW DONALD JR;HAACK GREG A.
分类号 B64D37/32;B65B31/04;(IPC1-7):B65B31/04 主分类号 B64D37/32
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