发明名称 COMBINED CYCLE GAS TURBINE SYSTEM
摘要 Combined cycle gas turbine system is improved to enhance a gas turbine efficiency and a combined efficiency by effecting steam-cooling of a combustor transition piece and a turbine blade. In a combined cycle system comprising; a gas turbine (8) having a generator (1), a compressor (2), a combustor (3), a blade cooling air cooler (4) and a turbine (6); a steam turbine (29) having a high pressure turbine (21), an intermediate pressure turbine (22) and a low pressure turbine (23); and a waste heat recovery boiler (9), saturated water of a high pressure pump (27) is partially led into a demineralizer (118) and a water sprayer (116) for cooling steam to be supplied into a moving blade (52) and the steam, after used for the cooling, is recovered into a reheater (20). Outlet steam of the high pressure turbine (21) is led into a stationary blade (53) for cooling thereof and the steam is then recovered into an inlet of the intermediate pressure turbine (22). Also, steam of an intermediate pressure superheater (16) is led into a combustor transition piece (54) for cooling thereof and the steam is recovered into the inlet of the intermediate pressure turbine (22). Thus, moving blade cooling steam is reduced and the combined efficiency is enhanced.
申请公布号 CA2357595(C) 申请公布日期 2005.12.20
申请号 CA20012357595 申请日期 2001.09.20
申请人 MITSUBISHI HEAVY INDUSTRIES, LTD. 发明人 HYAKUTAKE, YOSHINORI;UEMATSU, KAZUO;SUGISHITA, HIDEAKI
分类号 F01D25/12;F01K23/10;F02C7/16;F02C7/18;(IPC1-7):F01K23/10;F02C6/04 主分类号 F01D25/12
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