发明名称 GAS TURBINE INTAKE COOLING SYSTEM AND COOLING METHOD
摘要 <p>A gas turbine intake cooling system having a first gas turbine (T1) and a second gas turbine (T2) used therein, comprising a gas compressing part (B) operated by receiving an excess electric power, a compressed gas storing part (A) formed by the filling of heavy slurry (101a) and allowing the compressed gas to be stored, a steam boiler (C) converting an exhaust heat to steam, and an ice producing means (D) producing ice with ammonia medium with the steam converted by the steam boiler (C) used as a heat source, wherein the first gas turbine (T1) is driven by the compressed gas in daytime zone and the second gas turbine (T2) forms a gas turbine intake cooling system allowing intake to be cooled by the cooling air of the ice, drives the first gas turbine (T1) by injecting the compressed gas stored in night zone to the daytime zone, and produces ice using much exhaust heat produced during the gas compressive process of a gas compressor so as to cool the intake of the second gas turbine (T2) for doubly leveling a load.</p>
申请公布号 WO2001059278(P1) 申请公布日期 2001.08.16
申请号 JP2001000944 申请日期 2001.02.09
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