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 ).
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
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