发明名称 Förfarande för drift av en gasturbingrupp
摘要 A method of operating a gas turbine power plant comprising of a first gas turbine group, consisting of a compressor and a turbine which are connected mechanically with one another, and a second gas turbine group, including a combustion device, which is placed in the gas flow stream between the first group's compressor and turbine, whereby the second gas turbine group consists of a compressor, a fuel injection device, a combustion chamber and a turbine, whereby the second gas turbine group's compressor and turbine are mechanically coupled to one another and at least one of the gas turbine groups having a device for the extraction of work, whereby the fact that a first flow of water and/or steam is heated with heat from the flue gas from the first group's turbine, that further amounts of water and/or steam are heated with heat from a gas stream that is compressed by the first group's compressor, and the produced water and/or steam is injected into the gas stream in such amounts that at least 60% of the oxygen content of the air in the stream is consumed through combustion in the combustion device, and in that the combustion gas that is fed into the turbine of the second gas turbine group has a pressure in the range 50-300 bar.
申请公布号 SE0301585(D0) 申请公布日期 2003.05.30
申请号 SE20030001585 申请日期 2003.05.30
申请人 EUROTURBINE AB 发明人 HANS-ERIK HANSSON;MATS WESTERMARK
分类号 F01K21/04;F02C3/30;F02C6/18;F02C7/08;F02C7/143;F23L7/00 主分类号 F01K21/04
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