Age-hardenable and highly formable aluminum alloys and methods of making the same
US-11932924-B2 · Mar 19, 2024 · US
US2024175109A1 · US · A1
| Field | Value |
|---|---|
| Publication number | US-2024175109-A1 |
| Application number | US-202418433819-A |
| Country | US |
| Kind code | A1 |
| Filing date | Feb 6, 2024 |
| Priority date | Mar 13, 2019 |
| Publication date | May 30, 2024 |
| Grant date | — |
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Provided herein are new aluminum alloy products and methods of making these alloys. The aluminum alloy products are age-hardenable, display high strength and formability, and allow for the use of recycled scrap. The aluminum alloys can serve as the core in a clad aluminum alloy product. The alloy products can be used in a variety of applications, including automotive, transportation, and electronics applications.
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What is claimed is: 1 . An aluminum alloy, comprising: from 0.5 wt. % to 1.6 wt. % Mg; from 0.2 wt. % to 0.5 wt. % Si; up to 1.0 wt. % Fe; up to 0.5 wt. % Cu; up to 0.5 wt. % Mn; up to 0.3 wt. % Cr; up to 0.3 wt. % Ti; up to 0.5 wt. % Zn; up to 0.25 wt. % impurities; and Al. 2 . The aluminum alloy of claim 1 , wherein: the amount of Mg is from 0.6 wt. % to 1.5 wt. %; the amount of Si is from 0.3 wt. % to 0.45 wt. %; the amount of Fe is up to 0.5 wt. %; the amount of Cu is up to 0.4 wt. %; the amount of Mn is up to 0.4 wt. %; the amount of Cr is up to 0.25 wt. %; the amount of Ti is up to 0.15 wt. %; the amount of Zn is up to 0.4 wt. %; and the amount of impurities is up to 0.20 wt. %. 3 . The aluminum alloy of claim 1 , wherein the Mg and Si are present in a ratio of from 5:1 to 2:1 of Mg to Si by weight. 4 . The aluminum alloy of claim 1 , wherein the Mg and Si are present in a ratio of from 4:1 to 2:1 of Mg to Si by weight. 5 . The aluminum alloy of claim 1 , wherein: the amount of Mg is from 0.7 wt. % to 1.5 wt. %; the amount of Si is from 0.25 wt. % to 0.45 wt. %; the amount of Fe is from 0.01 wt. % to 1.0 wt. %; the amount of Cu is from 0.01 wt. % to 0.5 wt. %; the amount of Mn is from 0.01 wt. % to 0.5 wt. %; the amount of Cr is from 0.005 wt. % to 0.3 wt. %; the amount of Ti is from 0.01 wt. % to 0.25 wt. %; the amount of Zn is up to 0.4 wt. %; and the amount of impurities is up to 0.20 wt. %. 6 . The aluminum alloy of claim 1 , wherein the aluminum alloy, when in a T8x temper, has a yield strength (Rp0.2) of from 160 MPa to 230 MPa when tested according to ISO 6892-1 (2016). 7 . The aluminum alloy of claim 1 , wherein the aluminum alloy has a bake hardening value from 70 MPa to 140 MPa. 8 . The aluminum alloy of claim 1 , comprising at least 40 wt. % recycled content. 9 . The aluminum alloy of claim 1 , comprising at least 40 wt. % UBC. 10 . The aluminum alloy of claim 1 , wherein the combined concentration of Fe, Mn and Cu in the aluminum alloy is at least 0.7 wt. %. 11 . The aluminum alloy of claim 1 , wherein the combined concentration of Fe, Mn, and Cu in the aluminum alloy is between 0.7 wt. % and 3.0 wt. %. 12 . The aluminum alloy of claim 1 , wherein the aluminum alloy is a core layer in a clad product. 13 . A monolithic sheet, comprising the aluminum alloy of claim 1 . 14 . A clad aluminum alloy product, comprising: a core layer having a first side and a second side; and a first clad layer in contact with the first side of the core layer; wherein the core layer comprises from 0.5 wt. % to 1.6 wt. % Mg and from 0.2 wt. % to 0.5 wt. % Si. 15 . The clad aluminum alloy product of claim 14 , wherein the first clad layer has a thickness of from 0.05 mm to 0.80 mm. 16 . The clad aluminum alloy product of claim 14 , wherein the core layer has a thickness of from 0.7 to 2.3 mm. 17 . The clad aluminum alloy product of claim 14 , further comprising a second clad layer in contact with the second side of the core layer. 18 . The clad aluminum alloy product of claim 14 , wherein the first clad layer comprises an 1xxx series aluminum alloy, 2xxx series aluminum alloy, a 3xxx series aluminum alloy, a 4xxx series alloy, a 5xxx series aluminum alloy, a 6xxx series aluminum alloy, a 7xxx series aluminum alloy, or an 8xxx series aluminum alloy. 19 . The clad aluminum alloy product of claim 14 , wherein the clad aluminum alloy product when in a T8x temper has a yield strength of at least 150 MPa and when in a T4 temper has a total elongation above 20% in all directions. 20 . The clad aluminum alloy product of claim 14 , wherein the clad aluminum alloy product is a sheet, a plate, an electronic device housing, an automotive structural part, an aerospace structural part, an aerospace non-structural part, a marine structural part, or a marine non-structural part.
with silicon · CPC title
all layers being formed of aluminium or aluminium alloys · CPC title
of alloys with magnesium as the next major constituent · CPC title
Next to Al-base component · CPC title
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