Component repair using brazed surface textured superalloy foil
US-2015375346-A1 · Dec 31, 2015 · US
US12589450B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-12589450-B2 |
| Application number | US-202218579882-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jun 24, 2022 |
| Priority date | Aug 3, 2021 |
| Publication date | Mar 31, 2026 |
| Grant date | Mar 31, 2026 |
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Brazing sheets, articles formed from or including all or a portion of brazing sheets, and methods of forming articles are provided. A brazing sheet comprises a core layer, a brazing layer, and an interliner layer intermediate the core layer and the brazing layer. The core layer comprises a first aluminum alloy and the core layer is at least partially recrystallized. The brazing layer comprises a 4XXX series aluminum alloy. The interliner layer comprises a second aluminum alloy, and the interliner layer is unrecrystallized.
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What is claimed is: 1 . A brazing sheet comprising: a core layer comprising a first aluminum alloy, wherein the core layer is at least partially recrystallized; a brazing layer comprising a 4XXX series aluminum alloy; and an interliner layer intermediate the core layer and the brazing layer and comprising a second aluminum alloy comprising, in weight percentages based on the total weight of the second aluminum alloy: 0.02 to 0.2 silicon; 0.3 to 0.6 copper; 1.75 to 1.9 manganese; 0.1 to 0.2 chromium; 0 to 0.15 zirconium; 0.05 to 0.4 iron; 0 to 1.0 zinc; 0.01 to 0.1 magnesium; 0 to 0.3 titanium; 0 to 0.1 vanadium; 0 to 0.5 bismuth; and aluminum; wherein the interliner layer is unrecrystallized. 2 . The brazing sheet of claim 1 , wherein the first aluminum alloy has a first recrystallization temperature, the second aluminum alloy has a second recrystallization temperature, and the second recrystallization temperature is greater than the first recrystallization temperature. 3 . The brazing sheet of claim 1 , wherein the core layer is homogenized. 4 . The brazing sheet of claim 1 , wherein the interliner layer has a dislocation density of at least 100,000,000 per cm 2 . 5 . The brazing sheet of claim 1 , wherein the interliner layer does not comprise recrystallized grains that have a dislocation density no greater than 10,000,000 per cm 2 . 6 . The brazing sheet of claim 1 , wherein the core layer has a dislocation density no greater than 10,000,000 per cm 2 . 7 . The brazing sheet of claim 1 , wherein grains of the core layer have a first aspect ratio and grains of the interliner layer have a second aspect ratio, wherein the second aspect ratio is greater than the first aspect ratio, and wherein each aspect ratio refers to a ratio between the mean grain length and the grain height in the length to short transverse plane. 8 . The brazing sheet of claim 1 , wherein the interliner layer is unhomogenized. 9 . The brazing sheet of claim 1 , wherein the interliner layer is configured to inhibit liquid film migration. 10 . The brazing sheet of claim 1 , wherein the second aluminum alloy comprises at least 0.01 weight percent zirconium, based on the total weight of the second aluminum alloy. 11 . The brazing sheet of claim 1 , wherein the core layer, the interliner layer, and the brazing layer are bonded together. 12 . The brazing sheet of claim 1 , wherein the first aluminum alloy is a 3XXX series aluminum alloy or a 6XXX series aluminum alloy. 13 . The brazing sheet of claim 1 , wherein the first aluminum alloy comprises, in weight percentages based on total weight of the first aluminum alloy: 0 to 1.2 silicon; 0 to 1.0 copper; 0 to 0.25 zirconium; 0 to 0.8 iron; 0 to 2.0 manganese; 0 to 3.0 zinc; 0 to 1.5 magnesium; 0 to 0.25 titanium; 0 to 0.3 chromium; 0 to 0.5 bismuth; aluminum; and impurities. 14 . The brazing sheet of claim 1 , wherein: the brazing layer is a first brazing layer disposed on a first side of the core layer; and a second brazing layer is disposed on a second side of the core layer opposite the first side of the core layer, wherein the second brazing layer comprises 1XXX series aluminum alloy, a 3XXX series aluminum alloy, a 3XXX series aluminum alloy, a 4XXX series aluminum alloy or a 7XXX series aluminum alloy. 15 . The brazing sheet of claim 1 , wherein: the brazing layer is a first brazing layer disposed on a first side of the core layer; the interliner layer is a first interliner layer; a second brazing layer is disposed on a second side of the core layer opposite the first side of the core layer, wherein the second brazing layer comprises a 1XXX series aluminum alloy, a 3XXX series aluminum alloy, a 4XXX series aluminum alloy or a 7XXX series aluminum alloy; and a second interliner layer is disposed intermediate the core layer and the second brazing layer. 16 . The brazing sheet of claim 1 , wherein the brazing sheet is suitable for at least one of controlled atmospheric brazing and vacuum brazing. 17 . The brazing sheet of claim 1 , wherein the 4XXX series aluminum alloy of each brazing layer comprises, in weight percentages based on total weight of the 4XXX series aluminum alloy: 5 to 15 silicon; 0 to 2.0 magnesium; 0 to 1.0 iron; 0 to 3.0 zinc; 0 to 2.0 copper; 0 to 1.0 manganese; 0 to 0.2 titanium; 0 to 0.3 bismuth; aluminum; and impurities. 18 . The brazing sheet of claim 1 , wherein: the core layer comprises a first thickness in a range of 60% to 90% of a total thickness of the brazing sheet; the interliner layer comprises a second thickness in a range of 3% to 20% of the total thickness of the brazing sheet; and the brazing layer comprises a third thickness in a range of 3% to 20% of the total thickness of the brazing sheet. 19 . A heat exchanger comprising a structural element comprising all or a portion of the brazing sheet of any of claim 1 . 20 . A method for forming an article, the method comprising: contacting a first part comprising a first material with a second part comprising all or a portion of the brazing sheet of claim 1 ; and brazing the first part to the second part by a process comprising at least one of controlled atmospheric brazing and vacuum brazing. 21 . The method of claim 20 , wherein the first material comprises aluminum or an aluminum alloy. 22 . The method of claim 20 , wherein the article is a heat exchanger.
with zinc as the next major constituent · CPC title
with silicon as the next major constituent · CPC title
with Sn or Zn · CPC title
Brazing of heat exchangers · CPC title
Heat exchangers · CPC title
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