发明名称 Guide vane system for a turbomachine having segmented guide vane carriers
摘要 A turbine guide vane system, in particular for a gas turbine is provided. The turbine guide vane system includes a number of guide vane rows and a guide vane carrier, to enable particularly simple replacement of guide vanes, while maintaining a particularly high degree of efficiency, and thus designed for particularly short repair durations. For this purpose, the guide vane carrier has a number of segments, wherein a segment extends over the entire radial extension of the guide vane carrier and the connection of the remaining segments may be detached, and wherein the turbine guide vane carrier includes at least two sections along the axial extension thereof that are connected to one another and have a different number of segments.
申请公布号 US2012039716(A1) 申请公布日期 2012.02.16
申请号 US201013145353 申请日期 2010.01.05
申请人 AHMAD FATHI;GAIO GIUSEPPE;GROTE HOLGER;LERNER CHRISTIAN;MILAZAR MIRKO;STUTT MATTHIAS;TENRAHM THOMAS-DIETER;VONNEMANN BERND 发明人 AHMAD FATHI;GAIO GIUSEPPE;GROTE HOLGER;LERNER CHRISTIAN;MILAZAR MIRKO;STUTT MATTHIAS;TENRAHM THOMAS-DIETER;VONNEMANN BERND
分类号 F01D5/02 主分类号 F01D5/02
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