发明名称 GAS TURBINE STARTING METHOD
摘要 <p>Gas turbine starting method is improved to start operation with bleed valves being first throttled, then fully opened on the way and then fully closed at 90% speed, thereby fluid unstableness phenomenon is suppressed and starter motor power is reduced. While inlet guide vane (11) and variable stator vanes (C1 to C5) are set to predetermined opening from starting to rated speed, bleed valves (1, 2, 3) are set to predetermined opening until 52% speed for the bleed valve (1) and until 51% speed each for the bleed valves (2, 3), then the bleed valves (1, 2, 3) are fully opened until the speed exceeds 90%, when they are fully closed for rated operation. In the prior art, starting operation is done with bleed valves being first fully opened until the speed is elevated to 90% and then fully closed, but in the present invention, air discharged into ambient air in vain can be reduced and thereby starter motor power can be also reduced.</p>
申请公布号 CA2300606(A1) 申请公布日期 2000.10.02
申请号 CA20002300606 申请日期 2000.03.14
申请人 MITSUBISHI HEAVY INDUSTRIES, LTD. 发明人 ARIMURA, HISATO;SEKI, NAOYUKI
分类号 F02C9/18;F02C7/26;F04D27/02;(IPC1-7):F01D19/00 主分类号 F02C9/18
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