Component repair using brazed surface textured superalloy foil
US-2015375346-A1 · Dec 31, 2015 · US
US11851735B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-11851735-B2 |
| Application number | US-202218004662-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jun 7, 2022 |
| Priority date | Sep 30, 2021 |
| Publication date | Dec 26, 2023 |
| Grant date | Dec 26, 2023 |
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A type of high-strength and ductile multicomponent precision resistance alloys and fabrication methods thereof are provided. The alloys are composed of the following components by atomic percentage: Ni 45-60%, Cr 15-30%, Fe 5-20%, Al 5-15%, Mn 3-5%, Cu 0.2-3%, Si 1-5%. Particularly, the sum of the atomic percentages of Mn, Cu and Si is ≤13% and ≥4.2%, the sum of the atomic percentages of Ni, Cr, Fe and Al is ≥70% and ≤95.8%, and the sum of the atomic percentages of all the components is 100%. The multicomponent alloys prepared by the methods exhibit face-cantered cubic matrix and possess high strength and good ductility; further, they have high resistivity and excellent resistivity stability in wide temperature ranges below 773 K.
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The invention claimed is: 1. A high-strength and ductile multicomponent precision resistance alloy, consisting essentially of the following components by atomic percentage: 45-60% of Ni, 15-30% of Cr, 5-20% of Fe, 5-15% of Al, 3-5% of Mn, 0.2-3% of Cu, and 1-5% of Si; wherein the sum of the atomic percentage of Ni, Cr, Fe and Al is ≥70% and ≤95.8%, the sum of the atomic percentage of Mn, Cu and Si is ≥4.2% and ≤13%, and the sum of the atomic percentage of all components is 100%; wherein the alloy has a yield strength from 300 MPa to 900 MPa, an ultimate tensile strength from 700 MPa to 1200 MPa, and a total elongation from 30% to 70%, and the alloy has a resistivity between 120 μΩ·m to 160 μΩ·cm and a temperature coefficient of resistivity between +300 ppm/K to −300 ppm/K in a temperature range below 773 K, and the alloy has a face-centered cubic (FCC) phase structure. 2. A method of fabricating the alloy of claim 1 , comprising: batching each alloy component according to atomic percentage; melting all the components together in a vacuum or noble gas protection to prepare an as-cast alloy ingot; and hot-rolling the as-cast alloy, followed by homogenization, cold-rolling, annealing and aging to obtain an alloy. 3. The method of claim 2 , wherein the melting is conducted at a temperature between 1623-2473 K. 4. The method of claim 2 , wherein the melting is carried out at a furnace having a vacuum degree of 1-0.0001 Pa or a noble gas condition with noble gas pressure between 0.000001-5 MPa. 5. The method of claim 2 , wherein the hot-rolling is a multi-pass hot-rolling procedure with a hot-rolling temperature between 1173-1473 K, a thickness reduction ratio per pass ≤25% and a total thickness reduction ratio of 30-80%. 6. The method of claim 2 , wherein the homogenization is performed at a temperature between 1223-1573 K for around 30-600 minutes. 7. The method of claim 2 , wherein the cold-rolling is a multi-pass cold-rolling procedure with a thickness reduction ratio per pass ≤25% and a total thickness reduction ratio between 40-90%. 8. The method of claim 2 , wherein the annealing is conducted at the temperature range from 773-1473 K for 2-600 minutes, and the annealing is performed under a vacuum condition with a vacuum degree between 1-0.0001 Pa or noble gas condition with a noble gas pressure between 0.000001-5 MPa. 9. The method of claim 2 , wherein the aging treatment is carried out at an aging temperature between 573-973K for 2-1000 hours; further, the aging treatment is performed under a vacuum condition with a vacuum degree of 1-0.0001 Pa or noble gas condition with a noble gas pressure of 0.000001-5 MPa.
without Mo and W · CPC title
Alloys based on nickel · CPC title
of nickel or cobalt or alloys based thereon · CPC title
containing copper · CPC title
in inert or controlled atmosphere or vacuum (adjusting the composition of the atmosphere C21D1/76) · CPC title
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