发明名称 |
Aircraft fuel tank arrangement |
摘要 |
<p>An aircraft fuel tank arrangement 101 for the relief of a pressure differential between the interior of the aircraft fuel tank and the ambient atmosphere is provided. The aircraft fuel tank arrangement comprises a removable cartridge 106 received within a cartridge-receiving body 102 located at least partially in the fuel tank, said cartridge comprising a first burstable member 104 operable to rupture in the presence of a pressure differential between the interior of the aircraft fuel tank and the ambient atmosphere which is greater than a predetermined pressure differential.</p> |
申请公布号 |
EP2772437(A2) |
申请公布日期 |
2014.09.03 |
申请号 |
EP20140156904 |
申请日期 |
2014.02.27 |
申请人 |
AIRBUS OPERATIONS LIMITED |
发明人 |
HASKINS, RICHARD;JONES, JOHN |
分类号 |
B64D37/32 |
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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