发明名称 GAS TURBINE HAVING COOLING INSERT
摘要 <p>The gas turbine has multiple rotor blades arranged at a turbine shaft connected to rotor blade rows, and multiple guide vanes fastened to a turbine case by a blade ring carrier connected to guide vane rows. The blade ring carrier has multiple cooling air holes, and a cooling insert (22) is brought in a cooling air hole.</p>
申请公布号 EP2347100(B1) 申请公布日期 2012.10.17
申请号 EP20090823098 申请日期 2009.09.04
申请人 SIEMENS AKTIENGESELLSCHAFT 发明人 AHMAD, FATHI;LERNER, CHRISTIAN
分类号 F01D25/14;F01D5/18 主分类号 F01D25/14
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