Component repair using brazed surface textured superalloy foil
US-2015375346-A1 · Dec 31, 2015 · US
US12428713B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-12428713-B2 |
| Application number | US-202318454365-A |
| Country | US |
| Kind code | B2 |
| Filing date | Aug 23, 2023 |
| Priority date | Dec 23, 2016 |
| Publication date | Sep 30, 2025 |
| Grant date | Sep 30, 2025 |
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A nickel-based braze alloy composition is described, including nickel, about 1 weight % to about 5 weight % boron (B); and about 1 weight % to about 20 weight % germanium (Ge). The composition is free of any silicon. Superalloy articles that contains a crack or other type of void or gap filled with the nickel-based braze alloy composition are also described, along with methods for filling such a gap. Related articles of manufacture and brazing processes to join metal components are also disclosed.
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What is claimed: 1. A method for joining a first metal component to a second metal component by brazing, the method comprising: introducing a braze alloy composition between the first metal component and the second metal component, wherein the braze alloy composition consists of: at least 40 weight % nickel; 1 weight % to 5 weight % boron; 7 weight % to 15 weight % chromium; 1 weight % to 20 weight % germanium; wherein said braze alloy composition is free of silicon, hafnium, and zirconium; and optionally, at least one element selected from 0.5 weight % to 40 weight % cobalt, 0.05 weight % to about 10 weight % gold, 0.01 weight % to 0.2 weight % carbon, 0.01 weight % to 0.2 weight % yttrium, 5 weight % to 28 weight % manganese, 0.5 weight % to 8 weight % iron, 0.5 weight % to 8 weight % niobium, 0.5 weight % to 8 weight % tantalum, 0.5 weight % to 8 weight % molybdenum, 0.5 weight % to 8 weight % tungsten, or combinations thereof; and heating the first metal component, the second metal component, and the braze alloy composition to form a braze joint between the first metal component and the second metal component. 2. The method of claim 1 , wherein 14 weight % to 15 weight % of chromium is present in the braze alloy composition. 3. The method of claim 1 , wherein 0.5 weight % to 30 weight % of cobalt is present in the braze alloy composition. 4. The method of claim 1 , wherein 1 weight % to about 7 weight % of gold is present in the braze alloy composition. 5. The method of claim 1 , wherein at least one element selected from 0.01 weight % to 0.2 weight % carbon or 0.01 weight % to 0.2 weight % yttrium is present in the braze alloy composition. 6. The method of claim 1 , wherein 1 weight % to 3.4 weight % of boron is present in the braze alloy composition. 7. The method of claim 1 , wherein 2 weight % to 18 weight % of germanium is present in the braze alloy composition. 8. The method of claim 1 , wherein an atomic ratio of manganese to germanium is greater than 1.1:1.0. 9. The method of claim 1 , wherein the braze alloy composition has an amorphous microstructure. 10. The method of claim 1 , wherein the braze alloy composition is free of aluminum. 11. The method of claim 1 , wherein the braze alloy composition is free of palladium. 12. The method of claim 1 , wherein the braze alloy composition has a melting point of 870° C. to 1260° C.
Articles made by soldering, welding or cutting · CPC title
Superalloys · CPC title
Repairing methods or devices · CPC title
Repairing, retrofitting or upgrading methods · CPC title
Non-ferrous metals or alloys · CPC title
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