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
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