| 发明名称 |
Gas turbine engine combustor with improved cooling |
| 摘要 |
A gas turbine engine combustor liner having a plurality of holes defined therein for directing air into the combustion chamber. The plurality of holes provide improved cooling efficiency in regions of the combustor dome corresponding to predetermined hotspots.
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| 申请公布号 |
US7451600(B2) |
申请公布日期 |
2008.11.18 |
| 申请号 |
US20050175046 |
申请日期 |
2005.07.06 |
| 申请人 |
PRATT & WHITNEY CANADA CORP. |
发明人 |
PATEL BHAWAN;SAMPATH PARTHASARATHY;PARKER RUSSELL |
| 分类号 |
F23R3/10;F23R3/54 |
主分类号 |
F23R3/10 |
| 代理机构 |
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代理人 |
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| 地址 |
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