发明名称 |
Aircraft Fuel Tank And Inerting System Therefor |
摘要 |
An inerting system for an aircraft fuel tank ( 10 ) uses an air separation device ( 12 ) to produce a supply of nitrogen-enriched air to replenish the fuel tank on consumption of fuel and to maintain the pressure difference across the walls of the tank ( 10 ) below design limits. The air separation device ( 12 ) provides substantially the whole of the mass of the gas required and so there is substantially no inward venting. This provides a substantially homogenous nitrogen content in the air in the tank ( 10 ).
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申请公布号 |
US2008017248(A1) |
申请公布日期 |
2008.01.24 |
申请号 |
US20050590716 |
申请日期 |
2005.02.28 |
申请人 |
MASSEY ALAN;WOOD JOHN;ASHTON DOMINIC |
发明人 |
MASSEY ALAN;WOOD JOHN;ASHTON DOMINIC |
分类号 |
B64D37/04;A62B7/14;A62C3/06;A62C3/08;B64D37/32 |
主分类号 |
B64D37/04 |
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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