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 ).
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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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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