发明名称 |
Combustor apparatus in a gas turbine engine |
摘要 |
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.
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申请公布号 |
US8549859(B2) |
申请公布日期 |
2013.10.08 |
申请号 |
US20080233903 |
申请日期 |
2008.09.19 |
申请人 |
FOX TIMOTHY A.;WIEBE DAVID J.;RITLAND DAVID M.;GLESSNER JOHN CARL;SIEMENS ENERGY, INC. |
发明人 |
FOX TIMOTHY A.;WIEBE DAVID J.;RITLAND DAVID M.;GLESSNER JOHN CARL |
分类号 |
F02C7/22 |
主分类号 |
F02C7/22 |
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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