A brazing method is disclosed. The brazing method includes providing a substrate, providing at least one groove in the substrate, providing a support member, positioning the support member over the at least one groove in the substrate, providing a braze material, applying the braze material over the
A brazing method is disclosed. The brazing method includes providing a substrate, providing at least one groove in the substrate, providing a support member, positioning the support member over the at least one groove in the substrate, providing a braze material, applying the braze material over the support member to form an assembly, and heating the assembly to braze the braze material to the substrate. Another brazing method includes providing a preform, providing a wire mesh, pressing the wire mesh into the preform, heating the preform to form a braze material including the wire mesh, providing a substrate, providing at least one groove in the substrate, applying the braze material over the at least one groove in the substrate, then brazing the braze material to the substrate.
대표청구항▼
1. A brazing method, comprising: providing a preform;providing a mesh;pressing the mesh into the preform;heating the preform to form a braze assembly;providing a substrate;providing at least one groove in the substrate;applying the braze assembly over the at least one groove in the substrate; thenbr
1. A brazing method, comprising: providing a preform;providing a mesh;pressing the mesh into the preform;heating the preform to form a braze assembly;providing a substrate;providing at least one groove in the substrate;applying the braze assembly over the at least one groove in the substrate; thenbrazing the braze assembly to the substrate. 2. The brazing method of claim 1, comprising maintaining the preform above the at least one groove without the preform entering the groove and forming a convex border. 3. The brazing method of claim 1, wherein each of the at least one grooves forms a cooling microchannel with unimpeded flow between the substrate and the braze assembly. 4. The brazing method of claim 1, wherein the preform comprises a high-melting alloy, a low-melting alloy, and a binder. 5. The brazing method of claim 4, wherein heating the preform to form the braze assembly comprises sintering the preform, volatilizing or burning the binder, and securing together the high-melting alloy, the low-melting alloy, and the mesh. 6. The brazing method of claim 4, wherein heating the preform to form the braze assembly comprises providing incipient melting of the low-melting alloy to provide binding of the high-melting alloy and the mesh. 7. The brazing method of claim 1, comprising shaping the braze assembly prior to brazing to conform with a shape of the substrate. 8. The brazing method of claim 1, wherein the brazing comprises vacuum brazing. 9. The brazing method of claim 1, wherein the brazing comprises atmospheric brazing. 10. The brazing method of claim 1, wherein the substrate comprises a nickel-based alloy. 11. The brazing method of claim 1, wherein the substrate comprises a cobalt-based alloy. 12. The brazing method of claim 1, wherein the mesh increases a rigidity of the braze assembly. 13. The brazing method of claim 12, wherein the mesh reduces at least one of slumping, sagging, and drooping of the braze assembly into the at least one groove during the brazing of the braze assembly to the substrate. 14. The brazing method of claim 1, wherein the mesh remains within the braze assembly, forming a portion of a brazed article formed by the brazing method. 15. The brazing method of claim 1, further comprising assimilating the mesh into the braze assembly during a process selected from the group consisting of the brazing of the braze assembly to the substrate and operation of a turbine including the braze assembly. 16. A brazing method, comprising: providing a preform comprising a high-melting alloy, a low-melting alloy, and a binder;providing a mesh;pressing the mesh into the preform;heating the preform to form a braze assembly of the high-melting alloy, the low-melting alloy, and the mesh secured together;providing a substrate;providing at least one groove in the substrate;applying the braze assembly over the at least one groove in the substrate; thenbrazing the braze assembly to the substrate. 17. The brazing method of claim 16, wherein the mesh increases a rigidity of the braze assembly. 18. The brazing method of claim 16, wherein the mesh reduces at least one of slumping, sagging, and drooping of the braze assembly into the at least one groove during the brazing of the braze assembly to the substrate. 19. A brazing method, comprising: providing a preform comprising a high-melting alloy, a low-melting alloy, and a binder;providing a mesh;pressing the mesh into the preform;heating the preform to form a braze assembly of the high-melting alloy, the low-melting alloy, and the mesh secured together;providing a substrate;providing at least one groove in the substrate;applying the braze assembly over the at least one groove in the substrate; thenbrazing the braze assembly to the substrate;wherein the mesh increases a rigidity of the braze assembly, reducing at least one of slumping, sagging, and drooping of the braze assembly into the at least one groove during the brazing of the braze assembly to the substrate. 20. The brazing method of claim 19, further comprising assimilating the mesh into the braze assembly during a process selected from the group consisting of the brazing of the braze assembly to the substrate and operation of a turbine including the braze assembly.
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