发明名称 |
METHOD FOR A PART LOAD CO REDUCTION OPERATION FOR A SEQUENTIAL GAS TURBINE |
摘要 |
<p>The invention concerns a method for a part load CO reduction operation and a low-CO emissions operation of a gas turbine with sequential combustion. The gas turbine essentially includes at least one compressor, a first combustor which is connected downstream to the compressor. The hot gases of the first combustor are admitted at least to an intermediate turbine or directly or indirectly to a second combustor. The hot gases of the second combustor are admitted to a further turbine or directly or indirectly to an energy recovery. At least one combustor runs under a caloric combustion path having a can-architecture, and wherein the air ratio (λ) of the combustion at least of the second combustor is kept below a maximum air ratio (λmax).</p> |
申请公布号 |
KR20150023516(A) |
申请公布日期 |
2015.03.05 |
申请号 |
KR20147036703 |
申请日期 |
2013.06.24 |
申请人 |
ALSTOM TECHNOLOGY LTD. |
发明人 |
DUESING MICHAEL;EROGLU ADNAN |
分类号 |
F02C3/14;F02C6/00;F02C7/228;F02C9/34;F23C6/04 |
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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