Patent ID: 8413877
Filing Date: 2013-04-09
Classification: B23K,F01D,Y10T

Abstract:
1. A method for manufacturing a turbine engine component, the method comprising: providing a layered structure having a major surface and a brazing layer secured to the major surface, wherein the major surface is a first major surface and the brazing layer is a first brazing layer, wherein the layered structure also has a second major surface opposite the first major surface, and wherein the layered structure further comprises a second brazing layer secured to the second major surface; positioning the layered structure onto a turbine engine component surface such that at least a portion of the brazing layer contacts the turbine engine component surface; heating the turbine engine component containing the layered structure; and cooling the turbine engine component, thereby fusing the layered structure to the turbine engine component with the brazing layer.