发明名称 |
Combustion chamber for gas turbine |
摘要 |
<p>The combustion chamber arrangement has a combustion chamber wall (1) encompassing the combustion chamber, which encloses a flow channel in the area of the combustion chamber outlet for hot gases formed inside the combustion chamber. A combustion chamber wall edge (4) is constructed in profiled manner, such that by this a profile (17), with an overflow of the combustion chamber wall edge by a cooling air in the annular space region (13) is guided axially through the flow channels (12), where an inhibitory diffuser effect arises.</p> |
申请公布号 |
EP2189723(A1) |
申请公布日期 |
2010.05.26 |
申请号 |
EP20090176855 |
申请日期 |
2009.11.24 |
申请人 |
ALSTOM TECHNOLOGY LTD |
发明人 |
POYYAPAKKAM, MADHAVAN NARASIMHAN;MAGNI, FULVIO;INCE, NADIR |
分类号 |
F23R3/08;F01D9/02;F01D11/00;F23R3/00 |
主分类号 |
F23R3/08 |
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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