| 发明名称 |
Combuster and operating method for gas-or liquid-fuelled turbine arrangement |
| 摘要 |
In a combustor for a gas turbine, combustor 1 utilizes at least 50% of the air supplied thereto by a compressor to mix with the fuel to form a lean mixture, the remainder of the air is utilized for impingement cooling and the spent impingement cooling air is injected as radial jets into a post-primary combustion zone 17 through perforations 6.
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| 申请公布号 |
US5784876(A) |
申请公布日期 |
1998.07.28 |
| 申请号 |
US19960604675 |
申请日期 |
1996.02.21 |
| 申请人 |
EUROPEAN GAS TURBINES LIMITED |
发明人 |
ALKABIE, HISHAM SALMAN |
| 分类号 |
F02C7/18;F23M5/08;F23R3/00;F23R3/06;F23R3/34;(IPC1-7):F02C7/18;F23R3/04 |
主分类号 |
F02C7/18 |
| 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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