Component repair using brazed surface textured superalloy foil
US-2015375346-A1 · Dec 31, 2015 · US
US10265792B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10265792-B2 |
| Application number | US-201715806565-A |
| Country | US |
| Kind code | B2 |
| Filing date | Nov 8, 2017 |
| Priority date | Dec 11, 2015 |
| Publication date | Apr 23, 2019 |
| Grant date | Apr 23, 2019 |
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A hybrid article is disclosed including a coating disposed on and circumscribing the lateral surface of a core having a core material. The coating includes about 35% to about 95% of a first metallic material having a first melting point, and about 5% to about 65% of a second metallic material having a second melting point lower than the first melting point. The coating is sinter-bonded to the core. A method for forming the hybrid article is disclosed including disposing the core in a die, introducing a slurry having the metallic materials into a gap between the lateral surface and the die, and sintering the slurry, forming the coating. A method for closing an aperture of an article is disclosed including inserting the hybrid article into the aperture, and brazing the hybrid article to the article, welding the aperture with the hybrid article serving as weld filler, or both.
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What is claimed is: 1. A hybrid article, comprising: a core including a lateral surface and a core material; and a coating disposed on and circumscribing the lateral surface, the coating including about 35% to about 95% of a first metallic material having a first melting point, and about 5% to about 65% of a second metallic material having a second melting point, the first melting point being higher than the second melting point, wherein the coating is sinter-bonded to the core. 2. The hybrid article of claim 1 , wherein the hybrid article is free of gaps between the lateral surface and the coating. 3. The hybrid article of claim 1 , wherein the hybrid article includes a length along the core of at least about 50 mm. 4. The hybrid article of claim 1 , wherein the core is a hollow core including a channel disposed within the lateral surface. 5. The hybrid article of claim 1 , wherein the core material and the first material are independently selected from the group consisting of at least one a superalloy, a nickel-based superalloy, a cobalt-based superalloy, an iron-based superalloy, a hard-to-weld (HTW) alloy, a refractory alloy, GTD 111, GTD 444, HAYNES 188, INCONEL 738, MAR-M-247, René 108, René 142, René 195, and René N2. 6. The hybrid article of claim 1 , wherein the coating further includes an average coating thickness of from about 0.5 mm to about 5 mm, and the core further includes an average diameter of from about 0.5 mm to about 30 mm. 7. The hybrid article of claim 1 , further including an article cross-sectional conformation and a core cross-sectional conformation independently selected from the group consisting of a circle, an ellipse, an oval, a triangle, a rounded triangle, a square, a rounded square, a rectangle, a rounded rectangle, a pentagon, a rounded pentagon, a hexagon, a rounded hexagon, and combinations thereof. 8. A method for forming a hybrid article, comprising: disposing a core in a die, the core including a lateral surface; forming a gap between the lateral surface and the die, the gap circumscribing the lateral surface; introducing a slurry into the gap, the slurry including a first metallic material having a first melting point, and a second metallic material having a second melting point, the first melting point being higher than the second melting point; coating the lateral surface with the slurry; and sintering the slurry to form a coating circumscribing the lateral surface, forming the hybrid article, the coating including about 35% to about 95% of the first metallic material and about 5% to about 65% of the second metallic material, wherein the coating is sinter-bonded to the core. 9. The method of claim 8 , wherein the hybrid article is free of gaps between the lateral surface and the coating. 10. The method of claim 8 , wherein the hybrid article includes a length along the core of at least about 50 mm. 11. The method of claim 8 , wherein the core is a hollow core including a channel disposed within the lateral surface. 12. The method of claim 8 , wherein disposing the core in the die includes passing the core through the die in a continuous process. 13. The method of claim 8 , further including sizing the hybrid article to a predetermined length. 14. A method for closing an aperture of an article, comprising: inserting a hybrid article into the aperture, the hybrid article including: a core including a lateral surface and a core material, and a coating disposed on and circumscribing the lateral surface, the coating including about 35% to about 95% of a first metallic material having a first melting point, and about 5% to about 65% of a second metallic material having a second melting point, the first melting point being higher than the second melting point, wherein the coating is sinter-bonded to the core; and closing the aperture, closing the aperture including a technique selected from the group consisting of brazing the hybrid article to the article, welding the aperture with the hybrid article serving as a weld filler, and combinations thereof. 15. The method of claim 14 , wherein the hybrid article is free of gaps between the lateral surface and the coating. 16. The method of claim 14 , wherein the hybrid article includes a length along the core of at least about 50 mm. 17. The method of claim 14 , wherein the core is a hollow core including a channel disposed within the lateral surface. 18. The method of claim 14 , wherein closing the aperture includes welding the aperture with the hybrid article serving as the weld filler to a hard-to-weld (HTW) alloy of the article. 19. The method of claim 14 , wherein closing the aperture includes brazing the hybrid article to the article. 20. The method of claim 14 , wherein inserting the hybrid article into the aperture includes inserting the hybrid article into a turbine component.
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