Aluminum alloy comprising lithium with improved fatigue properties
US-2020165707-A1 · May 28, 2020 · US
US2021404038A1 · US · A1
| Field | Value |
|---|---|
| Publication number | US-2021404038-A1 |
| Application number | US-202117307453-A |
| Country | US |
| Kind code | A1 |
| Filing date | May 4, 2021 |
| Priority date | Nov 7, 2018 |
| Publication date | Dec 30, 2021 |
| Grant date | — |
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New 2xxx aluminum alloys having are disclosed. The new 2xxx aluminum alloys generally include 2.5-3.9 wt. % Cu, 0.82-1.20 wt. % Li, 0.5-2.0 wt. % Zn, 0.10-0.60 wt. % Mn, 0.05-0.35 wt. % Mg, from 0.05 to 0.50 wt. % of at least one grain structure control element, wherein the at least one grain structure control element is selected from the group consisting of Zr, Sc, Cr, V, Hf, other rare earth elements, and combinations thereof, up to 0.22 wt. % Ag, up to 0.15 wt. % Fe, up to 0.12 wt. % Si, and up to 0.15 wt. % Ti, the balance being aluminum, incidental elements and impurities. The new 2xxx aluminum alloys may realize an improved combination of two or more of strength, fracture toughness, elongation, and corrosion resistance.
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What is claimed is: 1 . A 2xxx aluminum alloy comprising: 3.1-3.8 wt. % Cu; 0.82-1.20 wt. % Li; 0.5-1.4 wt. % Zn; 0.10-0.60 wt. % Mn; 0.05-0.35 wt. % Mg; from 0.05 to 0.50 wt. % of at least one grain structure control element, wherein the at least one grain structure control element is selected from the group consisting of Zr, Sc, Cr, V, Hf, other rare earth elements, and combinations thereof, up to 0.05 wt. % Ag; up to 0.15 wt. % Fe; up to 0.12 wt. % Si; and up to 0.15 wt. % Ti; the balance being aluminum, incidental elements and impurities. 2 . The 2xxx aluminum alloy of claim 1 , wherein the 2xxx aluminum alloy includes not greater than 0.01 wt. % Ag. 3 . The 2xxx aluminum alloy of claim 1 , wherein the 2xxx aluminum alloy includes at least 0.7 wt. % Zn. 4 . The 2xxx aluminum alloy of claim 1 , wherein the 2xxx aluminum alloy includes at least 0.10 wt. % Mg. 5 . The 2xxx aluminum alloy of claim 1 , wherein (wt. % Cu)/(wt. % Zn) is not greater than 4.10. 6 . The 2xxx aluminum alloy of claim 1 , wherein the 2xxx aluminum alloy is in the form of a wrought product having a thickness of at least 101.6 mm; and wherein the wrought product realizes at least one of: (i) a tensile yield strength (ST) of at least 440 MPa in the T8 temper; (ii) a plane-strain (K IC ) fracture toughness (S-L) of at least 20 MPa-sqrt-m in the T8 temper; (iii) an elongation (ST) of at least 1.5% in the T8 temper; or (iv) wherein the wrought product is stress corrosion cracking resistant in the T8 temper. 7 . A 2xxx aluminum alloy comprising: 2.5-3.4 wt. % Cu; 0.82-1.20 wt. % Li; 1.1-2.0 wt. % Zn; 0.10-0.60 wt. % Mn; 0.05-0.35 wt. % Mg; from 0.05 to 0.50 wt. % of at least one grain structure control element, wherein the at least one grain structure control element is selected from the group consisting of Zr, Sc, Cr, V, Hf, other rare earth elements, and combinations thereof, up to 0.05 wt. % Ag; up to 0.15 wt. % Fe; up to 0.12 wt. % Si; and up to 0.15 wt. % Ti; the balance being aluminum, incidental elements and impurities. 8 . The 2xxx aluminum alloy of claim 7 , wherein the 2xxx aluminum alloy includes not greater than 0.01 wt. % Ag. 9 . The 2xxx aluminum alloy of claim 7 , wherein the 2xxx aluminum alloy includes at least 1.3 wt. % Zn. 10 . The 2xxx aluminum alloy of claim 7 , wherein the 2xxx aluminum alloy includes not greater than 3.2 wt. % Cu. 11 . The 2xxx aluminum alloy of claim 7 , wherein the 2xxx aluminum alloy includes at least 0.10 wt. % Mg. 12 . The 2xxx aluminum alloy of claim 7 , wherein (wt. % Cu)/(wt. % Zn) is not greater than 3.5. 13 . The 2xxx aluminum alloy of claim 7 , wherein the 2xxx aluminum alloy is in the form of a wrought product having a thickness of at least 101.6 mm; and wherein the wrought product realizes at least one of: (i) a tensile yield strength (ST) of at least 440 MPa in the T8 temper; (ii) a plane-strain (K IC ) fracture toughness (S-L) of at least 20 MPa-sqrt-m in the T8 temper; (iii) an elongation (ST) of at least 1.5% in the T8 temper; or (iv) wherein the wrought product is stress corrosion cracking resistant in the T8 temper.
with low melting point, e.g. Al 659 degrees C, Mg 650 degrees C · CPC title
Powder bed fusion, e.g. selective laser melting [SLM] or electron beam melting [EBM] · CPC title
with zinc · CPC title
with magnesium · CPC title
with silicon · CPC title
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