发明名称 |
Shrouded fluid-conducting apparatus |
摘要 |
A shrouded fluid-conducting apparatus is provided that includes at least one outer conduit and at least one inner conduit disposed within the outer conduit. Preferably, the shrouded fluid-conducting apparatus further includes at least one shrouded end fitting disposed at an end of the shrouded fluid-conducting apparatus and at least one support member engaged with the inner and outer conduits. The shrouded end fitting allows the shrouded fluid-conducting apparatus to be engaged with an additional shrouded fluid-conducting apparatus. The support member allows for the transfer of loads from the inner and/or outer conduits to one or more components external to the shrouded fluid-conducting apparatus. Accordingly, the shrouded fluid-conducting apparatus may be used to transport fuel through an aircraft "ignition zone" in an FAA-compliant manner. |
申请公布号 |
US2005120534(A1) |
申请公布日期 |
2005.06.09 |
申请号 |
US20040988309 |
申请日期 |
2004.11.13 |
申请人 |
CARNS JAMES A.;CUTLER THERON L.;SHELLY MARK A. |
发明人 |
CARNS JAMES A.;CUTLER THERON L.;SHELLY MARK A. |
分类号 |
F16L39/00;(IPC1-7):F16L39/00;B23P11/00 |
主分类号 |
F16L39/00 |
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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