发明名称 |
Method and device for inerting an aircraft fuel tank |
摘要 |
<p>Air enriched with an inert gas is produced from a compressed air source (9) inside the aircraft and is admitted into the tank (12). During the aircraft cruise phase a first fraction of air having a first inert gas content is produced and admitted into the tank at a first flow rate. During the descent phase a second fraction of enriched air, having a second inert gas content less than the first, is produced and admitted into the tank at a second higher flow rate. An Independent claim is included for a fuel tank inerting system</p> |
申请公布号 |
EP1253077(A1) |
申请公布日期 |
2002.10.30 |
申请号 |
EP20020290892 |
申请日期 |
2002.04.10 |
申请人 |
L'AIR LIQUIDE, SOCIETE ANONYME A DIRECTOIRE ET CONSEIL DE SURVEILLANCE POUR L'ETUDE ET L'EXPLOITATION DES |
发明人 |
SCHMUTZ, NICOLAS;VANDROUX, OLIVIER |
分类号 |
A62C3/06;A62C3/08;A62C99/00;B64D37/32;(IPC1-7):B64D37/32 |
主分类号 |
A62C3/06 |
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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