发明名称 Method for operating a gas turbine
摘要 The gas turbine (1) has a compressor (2) with variable inlet guide vanes (6). The gas turbine output power is controlled at least by controlling the variable inlet guide vanes opening. The variable inlet guide vanes opening is controlled between a maximum opening and a minimum opening. A function (F) indicative of the mechanical stress undergone by compressor blades downstream of the variable inlet guide vanes (6) has an increasing line trend (T) from the maximum opening to the minimum opening of the variable inlet guide vanes (6). The function (F) has operating windows (OW1, OW2, OW3) in which the function (F) is smaller than a stress limit (L) and at least one intermediate window (IW1, IW2) between two operating windows (OW1, OW2, OW3), in the intermediate window (IW1, IW2) the function (F) being greater than the stress limit (L). Regulation of the variable inlet guide vanes (6) in the operating windows (OW1, OW2, OW3) is done by opening or closing the variable inlet guide vanes (6) with a given velocity when moving from one operating window (OW1, OW2, OW3) to another operating window (OW1, OW2, OW3) passing through an intermediate window (IW1, IW2).
申请公布号 EP3067530(A1) 申请公布日期 2016.09.14
申请号 EP20150158141 申请日期 2015.03.09
申请人 GENERAL ELECTRIC TECHNOLOGY GMBH 发明人 SORATO, SEBATIANO;MICHELI, MARCO;KAPPIS, WOLFGANG;MAGNI, FULVIO
分类号 F02C7/042;F01D17/04;F02C9/20 主分类号 F02C7/042
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