发明名称 |
COMBUSTOR APPARATUS IN A GAS TURBINE ENGINE |
摘要 |
<p>A combustion apparatus in a gas turbine engine comprises a combustor shell for receiving air, a fuel injection system associated with the combustor shell, a first fuel supply structure, and a shield structure. The fuel supply structure is in fluid communication with a source of fuel for delivering fuel from the source of fuel to the fuel injection system and comprises a first fuel supply elements including a first section extending along a first path having a component in an axial direction and a second section extending from the first section along a second path having a component in a circumferential direction. The shield structure is associated with at least a portion of the second section of the first fuel supply element.</p> |
申请公布号 |
EP2318765(B1) |
申请公布日期 |
2013.07.17 |
申请号 |
EP20090788707 |
申请日期 |
2009.02.17 |
申请人 |
SIEMENS ENERGY, INC. |
发明人 |
FOX, TIMOTHY A.;WIEBE, DAVID J.;RITLAND, DAVID M.;GLESSNER, JOHN CARL |
分类号 |
F23R3/16;F23R3/28;F23R3/34 |
主分类号 |
F23R3/16 |
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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