发明名称 |
COMBUSTION LINER HAVING TURBULATORS |
摘要 |
A combustor for a turbine is provided. The combustor includes a plurality of fuel nozzles and a combustion zone is aligned with a combustion process associated with each of the fuel nozzles. A combustion liner includes a plurality of turbulator groups, and each of the turbulator groups has or more individual turbulators. Each of the turbulator groups is aligned with a hot streak caused by the combustion zone associated with the fuel nozzle. Each of the turbulator groups are circumferentially spaced from a neighboring turbulator group. |
申请公布号 |
US2012304654(A1) |
申请公布日期 |
2012.12.06 |
申请号 |
US201113153778 |
申请日期 |
2011.06.06 |
申请人 |
MELTON PATRICK BENEDICT;CIHLAR DAVID WILLIAM;TORONTO DAVID KAYLOR |
发明人 |
MELTON PATRICK BENEDICT;CIHLAR DAVID WILLIAM;TORONTO DAVID KAYLOR |
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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