ASSEMBLY COMPRISING A TURBINE COMPONENT AND PROCESS OF TREATING A TURBINE COMPONENT

In some embodiments, a process treats a turbine component (200). The turbine component (200) includes an article (108) and a wear component (202) brazed to the article (108). The process includes applying a braze tape (302) on at least a portion of the wear component (202) and thermal processing the...

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Bibliographische Detailangaben
Hauptverfasser:	CUI, Yan, KOTTILINGAM, Srikanth Chandrudu, TOLLISON, Brian Lee
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	ALLOYS BLASTING CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS ANDNON-FERROUS ALLOYS CHEMISTRY CLADDING OR PLATING BY SOLDERING OR WELDING COMBINED OPERATIONS CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING ENGINE PLANTS IN GENERAL FERROUS OR NON-FERROUS ALLOYS GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUSMETALS OR ALLOYS HEATING LIGHTING MACHINE TOOLS MACHINES OR ENGINES IN GENERAL MAKING METAL MALLEABLE BY DECARBURISATION, TEMPERING OR OTHERTREATMENTS MECHANICAL ENGINEERING METAL-WORKING NOT OTHERWISE PROVIDED FOR METALLURGY METALLURGY OF IRON MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES OTHER WORKING OF METAL PERFORMING OPERATIONS SOLDERING OR UNSOLDERING STEAM ENGINES TRANSPORTING TREATMENT OF ALLOYS OR NON-FERROUS METALS UNIVERSAL MACHINE TOOLS WEAPONS WELDING WORKING BY LASER BEAM
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Beschreibung
Zusammenfassung:	In some embodiments, a process treats a turbine component (200). The turbine component (200) includes an article (108) and a wear component (202) brazed to the article (108). The process includes applying a braze tape (302) on at least a portion of the wear component (202) and thermal processing the turbine component (200) while the braze tape (302) is on the at least a portion of the wear component (202) to treat the turbine component (200). In some embodiments, an assembly (300) includes a turbine component (200). The turbine component (200) includes an article (108) and a pre-sintered preform brazed to a surface of the article (108). The assembly (300) also includes a braze tape (302) on at least a portion of the pre-sintered preform. In some embodiments, a treated turbine component (400) includes a treated article (402) and a pre-sintered preform brazed to a surface of the treated article (402). The treated turbine component (400) has been thermally processed with the pre-sintered preform being substantially free of re-flow.