High strength 6XXX aluminum alloys and methods of making the same
US-11920229-B2 · Mar 5, 2024 · US
US2021262065A1 · US · A1
| Field | Value |
|---|---|
| Publication number | US-2021262065-A1 |
| Application number | US-202117314924-A |
| Country | US |
| Kind code | A1 |
| Filing date | May 7, 2021 |
| Priority date | Nov 16, 2018 |
| Publication date | Aug 26, 2021 |
| Grant date | — |
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New 2xxx aluminum alloys are disclosed. The new 2xxx aluminum alloys generally include from 0.08 to 0.20 wt. % Ti. The new 2xxx aluminum alloys may realize an improved combination of two or more of strength, fracture toughness, elongation, and corrosion resistance, for instance.
Opening claim text (preview).
What is claimed is: 1 . A 2xxx aluminum alloy comprising: from 0.08 to 0.20 wt. % Ti from 4.5 to 5.5 wt. % Cu; from 0.20 to 0.6 wt. % Mn; from 0.20 to 0.8 wt. % Mg; from 0.05 to 0.60 wt. % Ag; up to 1.0 wt. % Zn; up to 0.30 wt. % Fe; up to 0.20 wt. % Si; up to 0.25 wt. % Zr; up to 0.25 wt. % Cr; and up to 0.25 wt. % V; the balance being aluminum, incidental elements and impurities. 2 . The 2xxx aluminum alloy of claim 1 , wherein the 2xxx aluminum alloy includes: from 0.08 to 0.13 wt. % Ti; from 4.8 to 5.0 wt. % Cu; from 0.40 to 0.60 wt. % Zn; from 0.30 to 0.40 wt. % Mn; from 0.30 to 0.50 wt. % Mg; from 0.30 to 0.40 wt. % Ag; from 0.08 to 0.12 wt. % Zr; up to 0.15 wt. % Fe; up to 0.10 wt. % Si; up to 0.05 wt. % Cr; and up to 0.05 wt. % V; the balance being aluminum, incidental elements and impurities, wherein the 2xxx aluminum alloy includes not greater than 0.15 wt. %, in total, of the impurities, and wherein the 2xxx aluminum alloy includes not greater than 0.05 wt. % of each of the impurities. 3 . The 2xxx aluminum alloy of claim 1 , wherein the 2xxx aluminum alloy is in the form of a wrought product, and wherein there wrought product has a cross-sectional thickness of from at 12.7 mm to 305 mm. 4 . The 2xxx aluminum alloy of claim 3 , wherein the wrought product is in the T8 temper and wherein the wrought product realizes a tensile yield strength (LT) of at least 390 MPa. 5 . The 2xxx aluminum alloy of claim 4 , wherein the wrought product realizes a plane-strain (K IC ) fracture toughness (T-L) of at least 30 MPa-sqrt-m. 6 . The 2xxx aluminum alloy of claim 5 , wherein the wrought product realizes an elongation (LT) of at least 6.0%. 7 . The 2xxx aluminum alloy of claim 6 , wherein the wrought product is (a) LT stress corrosion cracking resistant, (b) ST stress corrosion cracking resistant or (c) both LT stress corrosion cracking resistant and ST stress corrosion cracking resistant. 8 . A 2x39 aluminum alloy, wherein the 2x39 aluminum alloy comprises from 0.08 to 0.20 wt. % Ti. 9 . The 2x39 aluminum alloy of claim 8 , wherein the 2x39 aluminum alloy includes from 0.05 to 0.20 wt. % Zr. 10 . The 2x39 aluminum alloy of claim 9 , wherein the 2x39 aluminum alloy includes from 0.20 to 0.90 wt. % Zn. 11 . The 2x39 aluminum alloy of claim 8 , wherein the 2x39 aluminum alloy is a 2039 aluminum alloy. 12 . The 2039 aluminum alloy of claim 11 , wherein the 2039 aluminum alloy includes from 0.08 to 0.20 wt. % Ti and from 0 to 0.10 wt. % Zr. 13 . The 2x39 aluminum alloy of claim 8 , wherein the 2x39 aluminum alloy is a 2139 aluminum alloy.
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