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 |
US2006277921(A1) |
申请公布日期 |
2006.12.14 |
申请号 |
US20050149264 |
申请日期 |
2005.06.10 |
申请人 |
PRATT & WHITNEY CANADA CORP. |
发明人 |
PATEL BHAWAN;PARKER RUSSELL |
分类号 |
F02C3/14 |
主分类号 |
F02C3/14 |
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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