Method to produce a coated gas turbine component having opening holes

The method involves visually predetermining surface configuration of a component (1) to detect position and the form of opening before coating in a three-dimensional manner. A tool is positioned opposite to the component based on the configuration such that the tool sets the corresponding opening op...

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
Hauptverfasser:	Irmisch, Stefan A., Dr, Bolms, Hans-Thomas, Dr, Münzer, Jan
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	BLASTING CLADDING OR PLATING BY SOLDERING OR WELDING CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING ENGINE PLANTS IN GENERAL HEATING LIGHTING MACHINE TOOLS MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING METAL-WORKING NOT OTHERWISE PROVIDED FOR NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES PERFORMING OPERATIONS SOLDERING OR UNSOLDERING STEAM ENGINES TRANSPORTING WEAPONS WELDING WORKING BY LASER BEAM
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!

Beschreibung
Zusammenfassung:	The method involves visually predetermining surface configuration of a component (1) to detect position and the form of opening before coating in a three-dimensional manner. A tool is positioned opposite to the component based on the configuration such that the tool sets the corresponding opening open through local removal of the coating material. The actual surface configuration of the component is detected three dimensionally. Independent claims are also included for the following: (1) a device for removal of coating material from the opening in a gas turbine component (2) a coated turbine blade.