JOINING INDIVIDUAL TURBINE VANES WITH FIELD ASSISTED SINTERING TECHNOLOGY (FAST)
Abstract:
A method of joining first and second turbine vanes is provided. The method includes casting and machining each of the first and second turbine vanes, coating each of the first and second turbine vanes with thermal barrier coating (TBC) and executing field assisted sintering technology (FAST) processing to join the first and second turbine vanes.
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