| 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 a greater cooling air flow in fuel nozzle regions than in other areas of the combustor liner.
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| 申请公布号 |
CA2546881(A1) |
申请公布日期 |
2006.12.10 |
| 申请号 |
CA20062546881 |
申请日期 |
2006.05.15 |
| 申请人 |
PRATT & WHITNEY CANADA, INC. |
发明人 |
PATEL, BHAWAN;PARKER, RUSSEL |
| 分类号 |
F23R3/06;F01D25/12;F02C7/12;F23R3/42;F23R3/54 |
主分类号 |
F23R3/06 |
| 代理机构 |
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代理人 |
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