Ceramic heat insulation coating, in particular for a turbine part, and device and method for determining the temperature of a turbine part

Thermally insulating ceramic layer system comprises an insulating layer (37) and a layer (39) containing a thermographic phosphor. This consists of YAG:Tm, YAG:EU, YSZ:Dy, GZO:Dy, GZO:Tm, YAG:Sm or EZO. Independent claims are included for: (A) turbine components with an insulating layer system as de...

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
Hauptverfasser:	SUBRAMANIAN, RAMESH, WESSLER, BERIT, SCHUMANN, ECKART
Format:	Patent
Sprache:	eng ; fre ; ger
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 HEATING INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION INGENERAL LIGHTING MACHINES OR ENGINES IN GENERAL MEASURING MEASURING QUANTITY OF HEAT MEASURING TEMPERATURE MECHANICAL ENGINEERING METALLURGY NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES PHYSICS STEAM ENGINES SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THESURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION TESTING THERMALLY-SENSITIVE ELEMENTS NOT OTHERWISE PROVIDED FOR WEAPONS
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!

Beschreibung
Zusammenfassung:	Thermally insulating ceramic layer system comprises an insulating layer (37) and a layer (39) containing a thermographic phosphor. This consists of YAG:Tm, YAG:EU, YSZ:Dy, GZO:Dy, GZO:Tm, YAG:Sm or EZO. Independent claims are included for: (A) turbine components with an insulating layer system as described; (B) use of EZO, YAG:Tm, YAG:EU, YSZ:Dy, GZO:Dy, GZO:Tm or YAG:Sm to produce phosphor layers in thermal insulation systems; and (C) apparatus for measuring the temperature of turbine component coated with the layer system comprising a solid state laser whose light is conducted by an optical fiber guide to the components, the light emitted by the phosphor layer being detected by a photomultiplier or camera and the laser beam positioned on the component using a mirror. Es wird eine Keramische Wärmedämmbeschichtung zur Verfügung gestellt, welche mindestens eine Wärmedämmschicht und eine einen thermographischen Leuchtstoff enthaltende Leuchtstoffschicht umfasst. Der thermographische Leuchtstoff ist ausgewählt aus der Gruppe: YAG:Tm, YSZ:Dy, GZO:Dy, GZO:Tm, YAG:Sm, EZO.