Thermal barrier coating system, components coated therewith and method for applying a thermal barrier coating system to components

A thermal barrier coating system (5) on a base material (1) is proposed comprising a bond coat layer (2) on its lower face in direct contact with said base material (1) and on its upper face in direct contact with a first ceramic layer (3). The thermal barrier coating system comprises further a seco...

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Bibliographische Detailangaben
Hauptverfasser:	ESQUERRE MATTHIEU, SCHAUDINN MARKUS, BOSSMANN HANS-PETER, WITZ GREGOIRE
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	BLASTING CHEMICAL SURFACE TREATMENT CHEMISTRY COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATIONOR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY IONIMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL COATING MATERIAL WITH METALLIC MATERIAL COATING METALLIC MATERIAL DIFFUSION TREATMENT OF METALLIC MATERIAL ENGINE PLANTS IN GENERAL GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS HEATING INDEXING SCHEME FOR ASPECTS RELATING TONON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES ORJET-PROPULSION PLANTS INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUSSUBCLASSES OF CLASSES F01-F04 INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION INGENERAL LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING METALLURGY NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THESURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION TECHNICAL SUBJECTS COVERED BY FORMER USPC TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS WEAPONS
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Beschreibung
Zusammenfassung:	A thermal barrier coating system (5) on a base material (1) is proposed comprising a bond coat layer (2) on its lower face in direct contact with said base material (1) and on its upper face in direct contact with a first ceramic layer (3). The thermal barrier coating system comprises further a second ceramic layer (4) on the outermost, hot gas exposed surface of the coating system. The first ceramic layer (3) consists of yttria- stabilised zirconia (ZrO2) with a yttria content in the range of 6-8 wt-% (6w/o to 8w/o Y2O2), of YTaO4 doped zirconia and/or titania doped zirconia. The material of the second ceramic layer (4, 4a, 4b) is selected from the group of: YTaO4 doped zirconia, titania doped zirconia, scandia stabilised zirconia, ceria containing perovskite material, yttrium aluminium garnet material, Monazite material, spinel material, and combinations, mixtures, alloys, blends or multilayer structures thereof, with the proviso that if the first ceramic layer (3) consists of YTaO4 doped zirconia and/or ti