发明名称 METHOD OF STARTING COMPRESSOR OR THE LIKE BY SINGLE SHAFT GAS TURBINE
摘要 PURPOSE:To make the start of a compressor etc. by means of a single shaft gas turbine smooth by throttling a variable diffuser vane etc. to reduce the specific gravity and flow rate of a fluid sucked into said compressor and preventing the starting curves of said single shaft gas turbine and said compressor, etc. from intersecting with each other. CONSTITUTION:When starting a compressor 2 with a single shaft gas turbine 1, valves A, B, D are fully opened, reducing the specific gravity of air in piping by means of a vacuum pump 5. In this case, a valve F is fully opened. Then, a variable diffuser vane 3 is throttled to reduce flow rate in order to prevent a point of intersection of the starting torque curve of the single shaft gas turbine 1 and the starting torque curve of the compressor (load side). Then, the single shaft gas turbine 1 is started and, after the start is completed, the suction valve A is gradually opened, to apply load to the turbine 1. Further, the blow-off valve B and the valve D are opened, and the valve F is totally closed and, when a rated load is obtained, the variable diffuser vane 3 is opened. Thereby, the compressor, etc. can be smoothly started by means of the single shaft turbine 1.
申请公布号 JPS61226582(A) 申请公布日期 1986.10.08
申请号 JP19850066629 申请日期 1985.04.01
申请人 MITSUBISHI HEAVY IND LTD 发明人 TAKAMORI AKINORI;SHIMADA TAMOTSU
分类号 F04B49/02;F04D27/00 主分类号 F04B49/02
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