US2023374632A1PendingUtilityA1
New 6xxx aluminum alloys
Est. expiryJan 29, 2041(~14.5 yrs left)· nominal 20-yr term from priority
C22C 21/02C22F 1/002C22F 1/05
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Claims
Abstract
New 6xxx aluminum alloys are disclosed. In one embodiment, a new 6xxx aluminum alloy sheet product includes from 0.75 to 1.05 wt. % Si, from 0.65 to 0.95 wt. % Mg, wherein (wt. % Mg)/(wt. % Si) is not greater than 0.99:1, from 0.50 to 0.75 wt. % Cu, from 0.02 to 0.40 wt. % Mn, from 0.06 to 0.26 wt. % Cr, wherein (wt. % Mn)+(wt. % Cr) is at least 0.22 wt. %, from 0.01 to 0.30 wt. % Fe, up to 0.25 wt. % Zn, up to 0.20 wt. % Zr, up to 0.20 wt. % V, and up to 0.15 wt. % Ti, the balance being aluminum, optional incidental elements and impurities.
Claims
exact text as granted — not AI-modifiedWhat is claimed is:
1 . A aluminum alloy sheet product comprising:
from 0.75 to 1.05 wt. % Si; from 0.65 to 0.95 wt. % Mg;
wherein (wt. % Mg)/(wt. % Si) is not greater than 0.99:1;
from 0.50 to 0.75 wt. % Cu; from 0.02 to 0.40 wt. % Mn; from 0.06 to 0.26 wt. % Cr;
wherein (wt. % Mn)+(wt. % Cr) is at least 0.22 wt. %;
from 0.01 to 0.30 wt. % Fe; up to 0.25 wt. % Zn; up to 0.20 wt. % Zr; up to 0.20 wt. % V; up to 0.15 wt. % Ti; the balance being aluminum, optional incidental elements and impurities;
wherein the aluminum alloy sheet product has a thickness of from 1.0 to 4.0 mm;
wherein the aluminum sheet product realizes a tensile yield strength (LT) of at least 315 MPa in a T6 temper, wherein the artificial aging of the T6 temper is 30 minutes at 225° C. (437° F.).
2 . The aluminum alloy sheet product of claim 1 , wherein the aluminum alloy includes at least 0.80 wt. % Si.
3 . The aluminum alloy sheet product of claim 2 , wherein the aluminum alloy includes not greater than 1.0 wt. % Si.
4 . The aluminum alloy sheet product of claim 1 , wherein the aluminum alloy includes at least 0.70 wt. % Mg.
5 . The aluminum alloy sheet product of claim 4 , wherein the aluminum alloy includes not greater than 0.90 wt. % Mg.
6 . The aluminum alloy sheet product of claim 1 , wherein (wt. % Mg)/(wt. % Si) is not greater than 0.95:1.
7 . The aluminum alloy sheet product of claim 6 , wherein (wt. % Mg)/(wt. % Si) is at least 0.7:1.
8 . The aluminum alloy sheet product of claim 1 , wherein the aluminum alloy includes at least 0.55 wt. % Cu.
9 . The aluminum alloy sheet product of claim 8 , wherein the aluminum alloy includes not greater than 0.73 wt. % Cu.
10 . The aluminum alloy sheet product of claim 1 , wherein the aluminum alloy includes at least 0.04 wt. % Mn.
11 . The aluminum alloy sheet product of claim 10 , wherein the aluminum alloy includes not greater than 0.35 wt. % Mn.
12 . The aluminum alloy sheet product of claim 1 , wherein the aluminum alloy includes at least 0.08 wt. % Cr.
13 . The aluminum alloy sheet product of claim 12 , wherein the aluminum alloy includes not greater than 0.24 wt. % Cr.
14 . The aluminum alloy sheet product of claim 1 , wherein (wt. % Mn)+(wt. % Cr) is at least 0.24 wt. %.
15 . The aluminum alloy sheet product of claim 1 , wherein the aluminum alloy sheet product realizes at least one of:
a three-point bend extension of at least 10.0 mm in the T6 temper; a three-point bend extension of at least 16.0 mm in the T4 temper; a maximum depth of attack of not greater than 200 micrometers when tested in accordance with ASTM G110-92(2015) for 6 hours; and an f/r of at least 0.05.
16 . The aluminum alloy sheet product of claim 1 , wherein the aluminum alloy sheet product is fully recrystallized.
17 . The aluminum alloy sheet product of claim 1 , wherein the aluminum alloy sheet product realizes at least one of:
an area weighted average grain size of not greater than 50 micrometers; at least 10 vol. % cube texture; and a dispersoid area fraction of at least 0.5%.
18 . The aluminum alloy sheet product of claim 1 , wherein, in the T4 or T43 temper, the aluminum alloy sheet product realizes an increase of not greater than 15 MPa in tensile yield strength (LT) over the period of 2 weeks of natural aging to 6 months of natural aging.
19 . The aluminum alloy sheet product of claim 1 , wherein the aluminum alloy sheet product realizes not greater than 21 MPa strength loss in tensile yield strength (LT) over the period of 2 weeks of natural aging to 6 months of natural aging relative to the T6 temper.
20 . An automotive sheet product made from the aluminum alloy sheet product of claim 1 .Cited by (0)
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