发明名称 Heat shield and stator vane for a gas turbine
摘要 <p>The thermal flow housing has a guide vane and a thermal shield element. A thermal shield element (113) has a hot gas surface (114) which is opposite the support structure and which forms a wall section of the flow path. The guide vane and the thermal shield element are placed relative to each other so that the surface of the thermal shield on the hot gas side (114) is located further inside relative to the flow path than the platform surface (108, 110) or so that the thermal shield surface on the hot gas side is aligned with the platform surface. An independent claim is included for a gas turbine arrangement, a vane, heat shielding element.</p>
申请公布号 EP1741877(A1) 申请公布日期 2007.01.10
申请号 EP20050014475 申请日期 2005.07.04
申请人 SIEMENS AKTIENGESELLSCHAFT 发明人 SEILER, BEATE;TERTILT, MARC;ANDREAS BOETTCHER DR.;UWE GRUSCHKA;JENS KLEINFELD;CHRISTIAN LERNER
分类号 F01D9/02;F01D5/14;F01D11/00;F23R3/00 主分类号 F01D9/02
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