发明名称 |
NESTED CHANNEL DUCTS FOR NOZZLE CONSTRUCTION AND THE LIKE |
摘要 |
A multiple conduit system for a gas turbine engine, the multiple conduit system extending between a plurality of conduit inlet and outlets. A channel, adapted for conveying fuel flow, is formed in a surface of a gas turbine engine component. The channel includes at least a first discrete conduit and a second discrete conduit. The first and second discrete conduits are each adapted to direct an independent fluid flow from respective inlets to respective outlets.
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申请公布号 |
US2009320479(A1) |
申请公布日期 |
2009.12.31 |
申请号 |
US20080124593 |
申请日期 |
2008.05.21 |
申请人 |
PROCIW LEV ALEXANDER;SHAFIQUE HARRIS;SOKALSKI JOHN;PELLETIER CLAUDE RAYMOND |
发明人 |
PROCIW LEV ALEXANDER;SHAFIQUE HARRIS;SOKALSKI JOHN;PELLETIER CLAUDE RAYMOND |
分类号 |
F02C7/232;F02C7/24;F02C7/22;F23K5/06;F23R3/28 |
主分类号 |
F02C7/232 |
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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