A system and method for repairing a gas turbine engine component

A method of repairing a defect (18) in a component (10) includes forming a slot (30; 78) in the component (10), thereby removing at least a substantial part of the defect (18) from the component (10), where the slot (30; 78) has a predetermined geometry.

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Bibliographische Detailangaben
Hauptverfasser:	SORVILLO, WILLIAM G. SR, SIMARD, DALE A, DUNNE, PHILIP J, ARRIGONI, JOHN P, LEIBFRIED, PETER E
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 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 repairing a defect (18) in a component (10) includes forming a slot (30; 78) in the component (10), thereby removing at least a substantial part of the defect (18) from the component (10), where the slot (30; 78) has a predetermined geometry.