发明名称 GAS TURBINE FUEL HEATING SYSTEM
摘要 PROBLEM TO BE SOLVED: To improve controllability by restraining temperature of heated fuel from being suddenly fluctuated in relation to a heat exchanger having high exchanging calorific value and having a little fluid to be heat-exchanged. SOLUTION: In this system, a system 103 for bypassing a heat exchanger 100 for fuel is arranged, and the fuel flow rate 121 of a fuel system 101 to be heated and the fuel temperature 23 obtained after fuel which has bypassed the heat exchanger 100 and fuel heated by the heat exchanger 100 are joined are detected. Normally, a signal of the heat-exchanged fuel temperature and a signal of the fuel flow rate are calculated in a fuel temperature controller 130 to control the valve opening of a feed water flow rate control valve 111. When a gas turbine is shut off, the feed water flow rate control valve 111 is closed to the minimum openingα% for T2 seconds, and a bypass flow rate control valve 113 is opened to the specified openingβ% for T1 seconds. After that, the bypass flow rate control valve 113 is controlled until the T2 seconds pass, finally, the feed water flow rate control valve 111 is controlled, and the fuel temperature 123 is controlled to a set value.
申请公布号 JP2000213374(A) 申请公布日期 2000.08.02
申请号 JP19990014269 申请日期 1999.01.22
申请人 HITACHI LTD;HITACHI ENG CO LTD 发明人 IWAMOTO YUICHI;HATTORI YOICHI;HOIZUMI SHINICHI
分类号 F01K23/10;F02C6/18;F02C7/224;(IPC1-7):F02C7/224 主分类号 F01K23/10
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