发明名称 |
Aircraft and fuel venting system therefor |
摘要 |
An aircraft comprising a plurality of fuel tanks in each wing is arranged such that each fuel tank is provided with a venting pipe connected to a single venting chamber. The venting chamber is itself located in a central fuel tank located in the wing centre-box and is thus located inwardly of at least two of the fuel tanks. The venting chamber has two venting pipes each being connected via a respective surge tank in each wing to the exterior of the aircraft.
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申请公布号 |
US2005241700(A1) |
申请公布日期 |
2005.11.03 |
申请号 |
US20050112859 |
申请日期 |
2005.04.22 |
申请人 |
COZENS SIMON J;BROWN JEFFREY M;VAN MICHEL T |
发明人 |
COZENS SIMON J.;BROWN JEFFREY M.;VAN MICHEL T. |
分类号 |
B64D37/02;B64D37/14;B64D37/32;(IPC1-7):F16K24/04 |
主分类号 |
B64D37/02 |
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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