发明名称 Method and flow system for the control of turbine temperatures during bypass operation
摘要 Method and apparatus to limit and control rotational loss heating such as occurs in a large steam turbine in the bypass mode of operation under no-load and low-load operating conditions. According to the invention, a portion of the high pressure bypass steam is admitted to the lower pressure sections of the turbine to provide motive fluid for driving the turbine while, simultaneously, a second portion of the high-pressure bypass steam is admitted to the high-pressure section of the turbine in a reverse-flow direction to pass backwards therethrough and limit the rotational loss heating. The two flows may be proportioned to control rotational loss heating in both the high-pressure and lower pressure sections of the turbine. A reverse-flow valve and a ventilator valve are provided for routing the reverse-flow of steam.
申请公布号 US4309873(A) 申请公布日期 1982.01.12
申请号 US19790105019 申请日期 1979.12.19
申请人 GENERAL ELECTRIC COMPANY 发明人 KORAN, KENNETH W.;PARRY, WILLIAM T.
分类号 F01K7/24;F01D25/08;F01D25/12;F01K7/22;F01K9/04;F01K13/00;F01K13/02;(IPC1-7):F01K13/00 主分类号 F01K7/24
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