发明名称 |
REDUCED EXHAUST EMISSIONS GAS TURBINE ENGINE COMBUSTOR |
摘要 |
A gas turbine engine combustor includes a plurality of main fuel injector assemblies, and a plurality of pilot fuel injector assemblies, that are arranged and configured to reduce exhaust gas emissions during engine operation. The plurality of main fuel injector assemblies are arranged in a substantially circular pattern of a first radius, and each includes an outlet port having a first divergence angle. The plurality of pilot fuel injector assemblies are arranged in a substantially circular pattern of a second radius. Each pilot fuel injector assembly is disposed between at least two main fuel injector assemblies, and each includes an outlet port having a second divergence angle.
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申请公布号 |
US2010229562(A1) |
申请公布日期 |
2010.09.16 |
申请号 |
US20090361345 |
申请日期 |
2009.01.28 |
申请人 |
HONEYWELL INTERNATIONAL INC. |
发明人 |
ZUPANC FRANK J.;YANKOWICH PAUL R.;BARTON MICHAEL T. |
分类号 |
F02C7/04;F02C3/14;F23R3/28;F23R3/34 |
主分类号 |
F02C7/04 |
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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