Method of repairing a turbine blade and corresponding combination of a turbine blade and a repair component

A method of repair of a turbine blade (30) involves inspecting a turbine blade (30) having an internal cavity (54) and a cap (42). The cap (42) is removed and replaced with a replacement cap (46). The replacement cap (46) has an opening (58). The opening (58) provides access to the internal cavity (...

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Bibliographische Detailangaben
1. Verfasser:	HISKES, DAVID J
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 of repair of a turbine blade (30) involves inspecting a turbine blade (30) having an internal cavity (54) and a cap (42). The cap (42) is removed and replaced with a replacement cap (46). The replacement cap (46) has an opening (58). The opening (58) provides access to the internal cavity (54) of the blade (30) so that the replacement cap (46) may be attached to the turbine blade (30) through the opening (58).