发明名称 Gas turbine inlet air cooling method for combined cycle power plants
摘要 In a combined cycle power system having a gas turbine and one or more bottoming cycle expansion turbines for driving one or more generators, compressor inlet air to the gas turbine is cooled. An extraction (74) is taken from the distillation condensation sub-system (70) of the Kalina cycle and throttled (82) to a lower pressure, with a corresponding temperature drop for supply to a low pressure evaporator (78) in heat exchange relation with ambient air (76) flowing to the compressor inlet to cool the ambient air. The partially evaporated multi-component mixture (84) exiting the low pressure evaporator is returned to the spent vapor stream (44) from the low pressure expansion turbine for combination therewith and condensation (72). Consequently, compressor inlet air inlet to the gas turbine is cooled, thereby increasing mass flow and turbine output. <IMAGE>
申请公布号 KR100624990(B1) 申请公布日期 2006.09.20
申请号 KR19990013951 申请日期 1999.04.20
申请人 发明人
分类号 F02C7/141;F01K23/10;F01K25/06;F01K25/10;F02C6/18;F02C7/143 主分类号 F02C7/141
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