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Summary:The invention discloses a combined cycle system of an intercooling combustion gas turbine and relates to the technical field of combustion gas turbines. The combined cycle system of the intercooling combustion gas turbine comprises a waste heat boiler, a low-pressure compressor, a high-pressure turbine, a high-pressure compressor, a turbine assembly, an afterburning combustion chamber and an intercooler, wherein the afterburning combustion chamber is arranged between the high-pressure turbine and the turbine assembly; fuel gas exhausted out of the high-pressure turbine is heated again through the afterburning combustion chamber and enters the turbine assembly, and the temperature of exhausted gas of the turbine assembly is increased; the gas exhaust end of the turbine assembly is connected with the air inlet end of the waste heat boiler; the intercooler is located between the low-pressure compressor and the high-pressure compressor. The combined cycle system of the intercooling combustion gas turbine has the advantages that the afterburning combustion chamber is added in the combined cycle system of the intercooling combustion gas turbine, so that the temperature of gas exhausted out of the low-pressure turbine and the power turbine assembly is high, and the efficiency of the waste heat boiler is improved.
Bibliography:Application Number: CN20151600405