METHOD FOR MANUFACTURING A TURBOMACHINE COMPONENT WITH A PARTING JOINT, AND A STEAM TURBINE COMPRISING SAID TURBOMACHINE COMPONENT

The turbomachine component comprises two sub-components (4, 5) that are separated by a parting joint (3) and each comprise a sealing surface at the parting joint, where one of the two sealing surfaces: is convex to form a linear contact of the two sealing surfaces; and has a coating, applied on the...

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
1. Verfasser:	SCHÜRHOFF, JÖRG
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 ENGINEERING ELEMENTS AND UNITS GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS HEATING INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION INGENERAL JOINTS OR FITTINGS FOR PIPES LIGHTING MACHINES OR ENGINES IN GENERAL MEANS FOR THERMAL INSULATION IN GENERAL MECHANICAL ENGINEERING METALLURGY NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES NON-POSITIVE DISPLACEMENT PUMPS PIPES POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC FLUIDS STEAM ENGINES SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THESURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION THERMAL INSULATION IN GENERAL WEAPONS
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!

Beschreibung
Zusammenfassung:	The turbomachine component comprises two sub-components (4, 5) that are separated by a parting joint (3) and each comprise a sealing surface at the parting joint, where one of the two sealing surfaces: is convex to form a linear contact of the two sealing surfaces; and has a coating, applied on the sealing surfaces, which comprises a hard material having a thickness of maximum 30 mu m and is applied using a vapor deposition method, or a coating, which comprises a chrome-containing alloy having a thickness of maximum 30 mu m and is applied by a vapor deposition method. The turbomachine component comprises two sub-components (4, 5) that are separated by a parting joint (3) and each comprise a sealing surface at the parting joint, where one of the two sealing surfaces: is convex to form a linear contact of the two sealing surfaces; and has a coating, applied on the sealing surfaces, which comprises a hard material having a thickness of maximum 30 mu m and is applied using a vapor deposition method, or a coating, which comprises a chrome-containing alloy having a thickness of maximum 30 mu m and is applied by a vapor deposition method or having a thickness of maximum 300 mu m and applied using a thermal spraying method. The coating applied by the thermal spraying method comprises particles of an additional hard material (70-80 mass%). The particle is a ceramic particle. The thermal spraying method includes high-velocity flame spraying method, and cold spraying or detonation spraying method. The vapor deposition method includes physical vapor deposition method or chemical vapor deposition method. An independent claim is included for a steam turbine.