Methods of continuously casting new 6xxx aluminum alloys, and products made from the same
US-10550455-B2 · Feb 4, 2020 · US
US11530473B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-11530473-B2 |
| Application number | US-201715838651-A |
| Country | US |
| Kind code | B2 |
| Filing date | Dec 12, 2017 |
| Priority date | Dec 16, 2016 |
| Publication date | Dec 20, 2022 |
| Grant date | Dec 20, 2022 |
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Disclosed are high-strength, highly deformable aluminum alloys and methods of making and processing such alloys. More particularly, disclosed is a heat treatable aluminum alloy exhibiting improved mechanical strength and formability. The processing method includes casting, homogenizing, hot rolling, solutionizing, pre-aging and in some cases pre-straining. In some cases, the processing steps can further include cold rolling and/or heat treating.
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What is claimed is: 1. A method of producing an aluminum alloy metal product, the method comprising; casting an aluminum alloy to form a cast aluminum alloy product, wherein the aluminum alloy comprises 0.6-1.1 wt. % Cu, 0.6-1.1 wt. % Si, 0.7-1.2 wt. % Mg, up to 0.25 wt. % Cr, up to 0.35 wt. % Mn, 0.15-0.3 wt. % Fe, up to 0.25 wt. % Zr, up to 1.0 wt. % Zn, up to 0.1 wt. % Ti, up to 0.04 wt. % Ni, and up to about 0.15 wt. % of impurities, and Al; homogenizing the cast aluminum alloy product; hot rolling the cast aluminum alloy product to produce a sheet, plate, or shate; solutionizing the sheet, plate, or shate at a temperature between about 520° C. and about 580° C.; pre-aging the sheet, plate, or shate; coiling the sheet, plate, or shate, and aging the sheet, plate, or shate at a temperature of from 180° C. to 225° C., wherein an annealing step is not performed while processing the sheet, plate, or shate. 2. The method of claim 1 , wherein the aluminum alloy comprises 0.6-1.1 wt. % Cu, 0.6-1.1 wt. % Si, 0.7-1.2 wt. % Mg, up to 0.25 wt. % Cr, up to 0.35 wt. % Mn, 0.15-0.3 wt. % Fe, up to 0.25 wt. % Zr, up to 0.3 wt. % Zn, up to 0.10 wt. % Ti, up to 0.04 wt. % Ni, and up to 0.15 wt. % of impurities, and Al. 3. The method of claim 1 , wherein the aluminum alloy comprises 0.75-0.9 wt. % Cu, 0.65-0.9 wt. % Si, 0.85-1.0 wt. % Mg, 0.05-0.18 wt. % Cr, 0.05-0.18 wt. % Mn, 0.15-0.3 wt. % Fe, up to 0.15 wt. % Zr, up to 0.1 wt. % Zn, 0.01-0.04 wt. % Ti, up to 0.034 wt. % Ni, and up to 0.15 wt. % of impurities, and Al. 4. The method of claim 1 , wherein the pre-aging comprises heating the sheet, plate, or shate to a temperature of about 115° C. to about 135° C. after solutionizing. 5. The method of claim 1 , wherein the pre-aging comprises heating the sheet, plate, or shate to a temperature of about 120° C. to about 130° C. after solutionizing. 6. The method of claim 1 , wherein the aluminum alloy metal product comprises a strain hardening exponent of at least 0.23. 7. The method of claim 1 wherein the aluminum alloy metal product comprises a strength of at least 300 MPa after a 2% pre-strain hardening and thermal treatment of about 185° C. for a time period of about 20 minutes. 8. The method of claim 1 , wherein the aluminum alloy metal product comprises a strength of at least 300 MPa. 9. The method of claim 1 , further comprising strain hardening and thermal treating. 10. The method of claim 9 , wherein the strain hardening comprises about 2% and the thermal treating comprises maintaining the aluminum alloy metal product at a temperature of about 185° C. for a time period of about 20 minutes. 11. The method of claim 1 , further comprising a thermal treatment of maintaining the aluminum alloy metal product at a temperature of about 185° C. for a time period of about 20 minutes. 12. The method of claim 1 , further comprising quenching the aluminum alloy metal product after the solutionizing step. 13. The method of claim 1 , further comprising cold rolling the aluminum alloy metal product. 14. The method of claim 1 , further comprising pre-straining the aluminum alloy metal product, wherein the pre-straining comprises applying a tensile strain to the aluminum alloy metal product after solutionizing. 15. The method of claim 1 , wherein the aluminum alloy metal product is resistant to natural age hardening.
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