Aluminum alloy sheet for structural material
US-2015376742-A1 · Dec 31, 2015 · US
US10208371B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10208371-B2 |
| Application number | US-201715406153-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jan 13, 2017 |
| Priority date | Jul 13, 2016 |
| Publication date | Feb 19, 2019 |
| Grant date | Feb 19, 2019 |
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The disclosure provides aluminum alloys having varying ranges of alloying elements and properties. In some variations, the alloy can include 3.4 to 4.9 wt % Zn, 1.3 to 2.1 wt % Mg, no greater than 0.06 wt % Cu, no greater than 0.06 wt % Zr, 0.06 to 0.08 wt % Fe, no greater than 0.05 wt % Si, and the balance is aluminum and incidental impurities.
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The invention claimed is: 1. An aluminum alloy comprising: 3.4 to 4.9 wt % Zn; 1.3 to 2.1 wt % Mg, no greater than 0.06 wt % Cu, no greater than 0.06 wt % Zr, 0.06 to 0.08 wt % Fe, no greater than 0.05 wt % Si, and the balance is aluminum and incidental impurities; and wherein the alloy has a wt % ratio of Zn to Mg from 2.5 to 3.5. 2. The aluminum alloy according to claim 1 , comprising 4.7-4.9 wt % Zn and 1.75-1.85 wt % Mg. 3. The aluminum alloy according to claim 1 , comprising 4.3-4.5 wt % Zn and 1.45-1.55 wt % Mg. 4. The aluminum alloy according to claim 1 , comprising 3.9-4.1 wt % Zn and 1.55-1.65 wt % Mg. 5. The aluminum alloy according to claim 1 , comprising 4.3-4.5 wt % Zn and 1.35-1.45 wt % Mg. 6. The aluminum alloy according to claim 1 , comprising 3.5-3.7 wt % Zn and 1.95-2.05 wt % Mg. 7. The aluminum alloy according to claim 1 , comprising 4.2-4.4 wt % Zn and 1.85-1.95 wt % Mg. 8. The aluminum alloy according to claim 1 , comprising 0.03-0.06 wt % Zr. 9. The aluminum alloy according to claim 1 , comprising 0.04-0.05 wt % Zr. 10. The aluminum alloy according to claim 1 , comprising less than 0.01 wt % Zr. 11. The aluminum alloy according to claim 1 , comprising 0.025-0.06 wt % Cu. 12. The aluminum alloy according to claim 1 , comprising 0.04-0.05 wt % Cu. 13. The alloy according to claim 1 , comprising: no greater than 0.02 wt % Mn, no greater than 0.02 wt % Cr, no greater than 0.02 wt % Ti, no greater than 0.02 wt % Ga, no greater than 0.02 wt % Sn, no greater than 0.03 wt % total of Mn and Cr, no greater than 0.02 wt % of any one additional element, and no greater than 0.10 wt % total of additional elements. 14. The alloy according to claim 1 , wherein the stress corrosion cracking of the alloy is greater than 12 days to failure measured according to G30/G44 ASTM standards. 15. The alloy according to claim 1 , wherein the alloy comprises equiaxed grains, wherein the alloy has an average grain aspect ratio less than or equal to 1:1.2. 16. The alloy according to claim 1 , wherein the Charpy impact energy in the L-T orientation is greater than or equal to 11 J/cm 2 . 17. The alloy according to claim 1 , wherein the alloy has a yield strength of about at least 300 MPa. 18. A method for producing an aluminum alloy, the method comprising: forming a melt that comprises an alloy comprising: 3.4 to 4.9 wt % Zn; 1.3 to 2.1 wt % Mg, no greater than 0.06 wt % Cu, no greater than 0.06 wt % Zr, 0.06 to 0.08 wt % Fe, no greater than 0.05 wt % Si, and the balance is aluminum and incidental impurities; cooling the melt to room temperature; homogenizing the cooled alloy by heating to a first elevated temperature; hot-working the homogenized alloy; solution treating the hot-worked alloy at a second elevated temperature; and aging the solution treated alloy at a third elevated temperature for a period of time. 19. An article comprising the alloy comprising: 3.4 to 4.9 wt % Zn; 1.3 to 2.1 wt % Mg, no greater than 0.06 wt % Cu, no greater than 0.06 wt % Zr, 0.06 to 0.08 wt % Fe, no greater than 0.05 wt % Si, and the balance is aluminum and incidental impurities.
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