A method for repairing a gas turbine component

A method for repairing a gas turbine component (10) comprises the steps of: €¢ identifying on said gas turbine component (10) a worn out location, where said gas turbine component (10) is damaged; €¢ removing said damaged location, thereby creating a missing zone (18); €¢ manufacturing an insert, wh...

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Bibliographische Detailangaben
Hauptverfasser:	AMBROSY, GUENTER, HOEVEL, SIMON, HOEBEL, MATTHIAS
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	BLASTING COMBINED OPERATIONS 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 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 OTHER WORKING OF METAL PERFORMING OPERATIONS STEAM ENGINES 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 TRANSPORTING UNIVERSAL MACHINE TOOLS WEAPONS
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Beschreibung
Zusammenfassung:	A method for repairing a gas turbine component (10) comprises the steps of: €¢ identifying on said gas turbine component (10) a worn out location, where said gas turbine component (10) is damaged; €¢ removing said damaged location, thereby creating a missing zone (18); €¢ manufacturing an insert, which fits into said missing zone (18); €¢ putting said insert into said missing zone (18); €¢ adjusting said insert in said gas turbine component (10); and €¢ joining said adjusted insert to said gas turbine component (10).