Heat shield and stator vane for a gas turbine

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...

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Bibliographische Detailangaben
Hauptverfasser:	ANDREAS BOETTCHER DR, TERTILT, MARC, UWE GRUSCHKA, SEILER, BEATE, JENS KLEINFELD, CHRISTIAN LERNER
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	BLASTING COMBUSTION APPARATUS COMBUSTION PROCESSES ENGINE PLANTS IN GENERAL GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS HEATING LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS
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Beschreibung
Zusammenfassung:	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.