METHOD OF BRAZING A TREATMENT AREA OF A LOAD-BEARING GAS TURBINE COMPONENT

A method of brazing a treatment area (22) of a load-bearing component (12) includes applying a repair material (24) over the treatment area (22) of the component (12) and positioning an induction brazing coil (26) having a geometry corresponding to the treatment area (22) over the repair material (2...

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Bibliographische Detailangaben
Hauptverfasser:	SHUBERT, Gary Charles, CUI, Yan, DORRIETY, Daniel James, COOK, Paul Albert, HENDERSON, Brian Leslie
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	BLASTING CLADDING OR PLATING BY SOLDERING OR WELDING COMBINED OPERATIONS 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 OTHER WORKING OF METAL PERFORMING OPERATIONS SOLDERING OR UNSOLDERING STEAM ENGINES TRANSPORTING UNIVERSAL MACHINE TOOLS WEAPONS WELDING WORKING BY LASER BEAM
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Beschreibung
Zusammenfassung:	A method of brazing a treatment area (22) of a load-bearing component (12) includes applying a repair material (24) over the treatment area (22) of the component (12) and positioning an induction brazing coil (26) having a geometry corresponding to the treatment area (22) over the repair material (24) and the treatment area (22). The method further includes heating the repair material (24) utilizing the induction brazing coil (26) to a temperature sufficient to cause at least partial melting of the repair material (24), thereby effecting a brazed joint between the treatment area (22) and the repair material (24).