| 发明名称 |
GAS TURBINE ENGINE COMBUSTOR WITH TAILORED TEMPERATURE PROFILE |
| 摘要 |
A method of tailoring a combustor flow for a gas turbine engine includes controlling an airflow into a swirler to be generally uniform and controlling an airflow into a quench zone to provide a desired pattern factor. |
| 申请公布号 |
EP2935997(A1) |
申请公布日期 |
2015.10.28 |
| 申请号 |
EP20130864137 |
申请日期 |
2013.12.20 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
SNYDER, TIMOTHY S.;MCKINNEY, RANDAL G.;HOKE, JAMES B. |
| 分类号 |
F23R3/12;F02C9/16;F23R3/00;F23R3/06;F23R3/26 |
主分类号 |
F23R3/12 |
| 代理机构 |
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代理人 |
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| 地址 |
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