发明名称 STEAM COOLING SYSTEM FOR GAS TURBINE
摘要 PROBLEM TO BE SOLVED: To provide a gas turbine steam cooling system for cooling the blades of a gas turbine and a high temperature cooled portion such as a tail pipe of a combustor with steam exhausted by a high pressure turbine in a combined cycle plant, without reducing the entrance pressure of a medium pressure turbine and thus decreasing combined efficiency while preventing the increase of the pressure loss of cooled steam. SOLUTION: A cooled steam temperature reducer is provided at the downstream side of a medium pressure evaporator for supply of part of high pressure exhaust through the cooled steam temperature reducer to a high temperature cooled portion, so that the high pressure exhaust can be controlled at a temperature somewhat higher than the temperature of medium pressure saturated water and desirable for cooling. Thus, a less amount of steam is required for cooling, the increase of the pressure loss of cooled steam is prevented, the entrance pressure of a medium pressure turbine is kept higher, not lower, and the expansion ratio and output in the medium pressure turbine is increased for more combined efficiency.
申请公布号 JP2001090552(A) 申请公布日期 2001.04.03
申请号 JP19990272970 申请日期 1999.09.27
申请人 MITSUBISHI HEAVY IND LTD 发明人 SUGISHITA HIDEAKI;MORI HIDETAKA;UEMATSU KAZUO
分类号 F02C7/18;F02C6/18;(IPC1-7):F02C7/18 主分类号 F02C7/18
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