CA3003158A1 - Improved wrought 7xxx aluminum alloys, and methods for making the same - Google Patents
Improved wrought 7xxx aluminum alloys, and methods for making the same Download PDFInfo
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- CA3003158A1 CA3003158A1 CA3003158A CA3003158A CA3003158A1 CA 3003158 A1 CA3003158 A1 CA 3003158A1 CA 3003158 A CA3003158 A CA 3003158A CA 3003158 A CA3003158 A CA 3003158A CA 3003158 A1 CA3003158 A1 CA 3003158A1
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- 7xxx aluminum
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C21/00—Alloys based on aluminium
- C22C21/10—Alloys based on aluminium with zinc as the next major constituent
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
- C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
- C22F1/04—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon
- C22F1/053—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon of alloys with zinc as the next major constituent
Abstract
New wrought 7xxx aluminum alloys are disclosed. The new wrought 7xxx aluminum alloys generally include from 3.75 to 8.0 wt. % Zn, from 1.25 to 3.0 wt. % Mg, where the wt. % Zn exceeds the wt. % Mg, from 0.35 to 1.35 wt. % Cu, from 0.04 to 0.20 wt. % V, from 0.06 to 0.20 wt. % Zr, where V+Zr <= 0.23 wt. %, from 0.01 to 0.25 wt. % Ti, up to 0.50 wt. % Mn, up to 0.40 wt. % Cr, up to 0.35 wt. % Fe, and up to 0.25 wt. % Si, the balance being aluminum and impurities, wherein the wrought 7xxx aluminum alloy include not greater than 0.10 wt. % each of any one impurity, and wherein the wrought 7xxx aluminum alloy includes not greater than 0.35 wt. % in total of the impurities.
Description
IMPROVED WROUGHT 7XXX ALUMINUM ALLOYS, AND METHODS FOR
MAKING THE SAME
CROSS-REFERENCE TO RELATED APPLICATIONS
[001] This patent application claims priority to Prov. U.S. Pat. App. Ser.
No. 62/248,165, filed Oct. 29, 2015 and entitled "WROUGHT 7XXX ALUMINUM ALLOYS, AND METHODS
FOR MAKING THE SAME," the entire disclosure of which is hereby incorporated herein by reference.
MAKING THE SAME
CROSS-REFERENCE TO RELATED APPLICATIONS
[001] This patent application claims priority to Prov. U.S. Pat. App. Ser.
No. 62/248,165, filed Oct. 29, 2015 and entitled "WROUGHT 7XXX ALUMINUM ALLOYS, AND METHODS
FOR MAKING THE SAME," the entire disclosure of which is hereby incorporated herein by reference.
[002] This patent application is related to commonly-owned U.S. Patent Application No.
14/694,109, filed April 23, 2015, entitled "IMPROVED 7XX ALUMINUM CASTING
ALLOYS, AND METHODS FOR MAKING THE SAME".
BACKGROUND
14/694,109, filed April 23, 2015, entitled "IMPROVED 7XX ALUMINUM CASTING
ALLOYS, AND METHODS FOR MAKING THE SAME".
BACKGROUND
[003] Aluminum alloys are useful in a variety of applications. However, improving one property of an aluminum alloy without degrading another property is elusive.
For example, it is difficult to increase the strength or corrosion resistance of a wrought 7xxx aluminum alloy without affecting other properties.
SUMMARY OF THE DISCLOSURE
For example, it is difficult to increase the strength or corrosion resistance of a wrought 7xxx aluminum alloy without affecting other properties.
SUMMARY OF THE DISCLOSURE
[004] Broadly, the present patent application relates to improved wrought 7xxx aluminum alloys, and methods for producing the same. The new wrought 7xxx aluminum alloys may realize, for instance, an improved combination of at least two of strength, corrosion resistance, fatigue failure resistance, and quench insensitivity, among other properties.
[005] The new wrought 7xxx aluminum alloys generally comprise (and in some instance consist essentially of, or consist of), zinc (Zn), magnesium (Mg), copper (Cu), vanadium (V), zirconium (Zr), and titanium (Ti), as primary alloying elements, optionally with manganese (Mn) and/or chromium (Cr), the balance being aluminum (Al), iron (Fe), silicon (Si), and unavoidable impurities, as defined below. Some embodiments of new wrought 7xxx aluminum alloy compositions are shown in FIG. 1.
[006] Regarding zinc, the new wrought 7xxx aluminum alloys generally include from 3.75 to 8.0 wt. % Zn. In one embodiment, a new wrought 7xxx aluminum alloy includes not greater than 7.5 wt. % Zn. In another embodiment, a new wrought 7xxx aluminum alloy includes not greater than 7.0 wt. % Zn. In yet another embodiment, a new wrought 7xxx aluminum alloy
7 PCT/US2016/059120 includes not greater than 6.5 wt. % Zn. In another embodiment, a new wrought 7xxx aluminum alloy includes not greater than 6.0 wt. % Zn. In yet another embodiment, a new wrought 7xxx aluminum alloy includes not greater than 5.5 wt. % Zn. In another embodiment, a new wrought 7xxx aluminum alloy includes not greater than 5.0 wt. % Zn. In another embodiment, a new wrought 7xxx aluminum alloy includes not greater than 4.75 wt. % Zn. In one embodiment, a new wrought 7xxx aluminum alloy includes at least 4.0 wt. % Zn. In another embodiment, a new wrought 7xxx aluminum alloy includes at least 4.25 wt. % Zn. In yet another embodiment, a new wrought 7xxx aluminum alloy includes at least 4.35 wt. % Zn.
[007] The new wrought 7xxx aluminum alloys generally include magnesium in the range of from 1.25 to 3.0 wt. % Mg. In one embodiment, a new wrought 7xxx aluminum alloy includes not greater than 2.75 wt. % Mg. In another embodiment, a new wrought 7xxx aluminum alloy includes not greater than 2.5 wt. % Mg. In yet another embodiment, a new wrought 7xxx aluminum alloy includes not greater than 2.25 wt. % Mg. In another embodiment, a new wrought 7xxx aluminum alloy includes not greater than 2.0 wt. % Mg. In yet another embodiment, a new wrought 7xxx aluminum alloy includes not greater than 1.8 wt. % Mg. In one embodiment, a new wrought 7xxx aluminum alloy includes at least 1.35 wt. % Mg. In another embodiment, a new wrought 7xxx aluminum alloy includes at least 1.40 wt. % Mg. In yet another embodiment, a new wrought 7xxx aluminum alloy includes at least 1.45 wt. % Mg. In another embodiment, a new wrought 7xxx aluminum alloy includes at least 1.50 wt. % Mg.
[007] The new wrought 7xxx aluminum alloys generally include magnesium in the range of from 1.25 to 3.0 wt. % Mg. In one embodiment, a new wrought 7xxx aluminum alloy includes not greater than 2.75 wt. % Mg. In another embodiment, a new wrought 7xxx aluminum alloy includes not greater than 2.5 wt. % Mg. In yet another embodiment, a new wrought 7xxx aluminum alloy includes not greater than 2.25 wt. % Mg. In another embodiment, a new wrought 7xxx aluminum alloy includes not greater than 2.0 wt. % Mg. In yet another embodiment, a new wrought 7xxx aluminum alloy includes not greater than 1.8 wt. % Mg. In one embodiment, a new wrought 7xxx aluminum alloy includes at least 1.35 wt. % Mg. In another embodiment, a new wrought 7xxx aluminum alloy includes at least 1.40 wt. % Mg. In yet another embodiment, a new wrought 7xxx aluminum alloy includes at least 1.45 wt. % Mg. In another embodiment, a new wrought 7xxx aluminum alloy includes at least 1.50 wt. % Mg.
[008] In some embodiments, the amount of zinc and magnesium may be limited (e.g., to improve corrosion resistance). Thus, in one embodiment, the combined amount of zinc and magnesium in a new wrought 7xxx aluminum alloy may be not greater than 7.0 wt.
% (i.e., wt.
% Zn + wt. % Mg < 7.0 wt. %). In another embodiment, the combined amount of zinc and magnesium in a new wrought 7xxx aluminum alloy is not greater than 6.75 wt. %
(i.e., wt. % Zn + wt. % Mg < 6.75 wt. %). In yet another embodiment, the combined amount of zinc and magnesium in a new wrought 7xxx aluminum alloy is not greater than 6.50 wt. %
(i.e., wt. % Zn + wt. % Mg < 6.50 wt. %). In another embodiment, the combined amount of zinc and magnesium in a new wrought 7xxx aluminum alloy is not greater than 6.25 wt. %
(i.e., wt. % Zn + wt. % Mg < 6.25 wt. %). In yet another embodiment, the combined amount of zinc and magnesium in a new wrought 7xxx aluminum alloy is not greater than 6.00 wt. %
(i.e., wt. % Zn + wt. % Mg < 6.00 wt. %).
% (i.e., wt.
% Zn + wt. % Mg < 7.0 wt. %). In another embodiment, the combined amount of zinc and magnesium in a new wrought 7xxx aluminum alloy is not greater than 6.75 wt. %
(i.e., wt. % Zn + wt. % Mg < 6.75 wt. %). In yet another embodiment, the combined amount of zinc and magnesium in a new wrought 7xxx aluminum alloy is not greater than 6.50 wt. %
(i.e., wt. % Zn + wt. % Mg < 6.50 wt. %). In another embodiment, the combined amount of zinc and magnesium in a new wrought 7xxx aluminum alloy is not greater than 6.25 wt. %
(i.e., wt. % Zn + wt. % Mg < 6.25 wt. %). In yet another embodiment, the combined amount of zinc and magnesium in a new wrought 7xxx aluminum alloy is not greater than 6.00 wt. %
(i.e., wt. % Zn + wt. % Mg < 6.00 wt. %).
[009] The new wrought 7xxx aluminum alloys generally include copper and in the range of from 0.35 to 1.35 wt. % Cu, and where the amount of magnesium exceeds the amount of copper.
As shown below, copper may facilitate, for example, improved corrosion resistance (e.g., improved SCC resistance) and/or strength. In one embodiment, a new wrought 7xxx aluminum alloy includes not greater than 1.15 wt. % Cu. In another embodiment, a new wrought 7xxx aluminum alloy includes not greater than 1.00 wt. % Cu. In yet another embodiment, a new wrought 7xxx aluminum alloy includes not greater than 0.95 wt. % Cu. In another embodiment, a new wrought 7xxx aluminum alloy includes not greater than 0.90 wt. % Cu. In yet another embodiment, a new wrought 7xxx aluminum alloy includes not greater than 0.85 wt. % Cu. In another embodiment, a new wrought 7xxx aluminum alloy includes not greater than 0.80 wt. %
Cu. In one embodiment, a new wrought 7xxx aluminum alloy includes at least 0.40 wt. % Cu.
In another embodiment, a new wrought 7xxx aluminum alloy includes at least 0.45 wt. % Cu.
In yet another embodiment, a new wrought 7xxx aluminum alloy includes at least 0.50 wt. %
Cu. In another embodiment, a new wrought 7xxx aluminum alloy includes at least 0.55 wt. %
Cu. In yet another embodiment, a new wrought 7xxx aluminum alloy includes at least 0.60 wt.
% Cu.
As shown below, copper may facilitate, for example, improved corrosion resistance (e.g., improved SCC resistance) and/or strength. In one embodiment, a new wrought 7xxx aluminum alloy includes not greater than 1.15 wt. % Cu. In another embodiment, a new wrought 7xxx aluminum alloy includes not greater than 1.00 wt. % Cu. In yet another embodiment, a new wrought 7xxx aluminum alloy includes not greater than 0.95 wt. % Cu. In another embodiment, a new wrought 7xxx aluminum alloy includes not greater than 0.90 wt. % Cu. In yet another embodiment, a new wrought 7xxx aluminum alloy includes not greater than 0.85 wt. % Cu. In another embodiment, a new wrought 7xxx aluminum alloy includes not greater than 0.80 wt. %
Cu. In one embodiment, a new wrought 7xxx aluminum alloy includes at least 0.40 wt. % Cu.
In another embodiment, a new wrought 7xxx aluminum alloy includes at least 0.45 wt. % Cu.
In yet another embodiment, a new wrought 7xxx aluminum alloy includes at least 0.50 wt. %
Cu. In another embodiment, a new wrought 7xxx aluminum alloy includes at least 0.55 wt. %
Cu. In yet another embodiment, a new wrought 7xxx aluminum alloy includes at least 0.60 wt.
% Cu.
[0010] The new wrought 7xxx aluminum alloys generally include from 0.04 to 0.20 wt. % V.
As shown below, vanadium may facilitate, for example, improved corrosion resistance and/or quench insensitivity. In one embodiment, a new wrought 7xxx aluminum alloy includes not greater than 0.18 wt. % V. In another embodiment, a new wrought 7xxx aluminum alloy includes not greater than 0.16 wt. % V. In yet another embodiment, a new wrought 7xxx aluminum alloy includes not greater than 0.15 wt. % V. In another embodiment, a new wrought 7xxx aluminum alloy includes not greater than 0.14 wt. % V. In yet another embodiment, a new wrought 7xxx aluminum alloy includes not greater than 0.13 wt. % V. In another embodiment, a new wrought 7xxx aluminum alloy includes not greater than 0.12 wt. % V. In yet another embodiment, a new wrought 7xxx aluminum alloy includes not greater than 0.11 wt. % V. In one embodiment, a new wrought 7xxx aluminum alloy includes at least 0.05 wt. %
V. In another embodiment, a new wrought 7xxx aluminum alloy includes at least 0.06 wt. % V.
In yet another embodiment, a new wrought 7xxx aluminum alloy includes at least 0.07 wt. % V.
In another embodiment, a new wrought 7xxx aluminum alloy includes at least 0.08 wt. % V.
As shown below, vanadium may facilitate, for example, improved corrosion resistance and/or quench insensitivity. In one embodiment, a new wrought 7xxx aluminum alloy includes not greater than 0.18 wt. % V. In another embodiment, a new wrought 7xxx aluminum alloy includes not greater than 0.16 wt. % V. In yet another embodiment, a new wrought 7xxx aluminum alloy includes not greater than 0.15 wt. % V. In another embodiment, a new wrought 7xxx aluminum alloy includes not greater than 0.14 wt. % V. In yet another embodiment, a new wrought 7xxx aluminum alloy includes not greater than 0.13 wt. % V. In another embodiment, a new wrought 7xxx aluminum alloy includes not greater than 0.12 wt. % V. In yet another embodiment, a new wrought 7xxx aluminum alloy includes not greater than 0.11 wt. % V. In one embodiment, a new wrought 7xxx aluminum alloy includes at least 0.05 wt. %
V. In another embodiment, a new wrought 7xxx aluminum alloy includes at least 0.06 wt. % V.
In yet another embodiment, a new wrought 7xxx aluminum alloy includes at least 0.07 wt. % V.
In another embodiment, a new wrought 7xxx aluminum alloy includes at least 0.08 wt. % V.
[0011] The new wrought 7xxx aluminum alloys generally include from 0.06 to 0.20 wt. %
Zr. As shown by the below data, the combination of vanadium and zirconium may facilitate, for instance, improved fatigue failure resistance properties. In one embodiment, a new wrought 7xxx aluminum alloy includes not greater than 0.18 wt. % Zr. In another embodiment, a new wrought 7xxx aluminum alloy includes not greater than 0.16 wt. % Zr. In yet another embodiment, a new wrought 7xxx aluminum alloy includes not greater than 0.15 wt. % Zr. In another embodiment, a new wrought 7xxx aluminum alloy includes not greater than 0.14 wt. %
Zr. In yet another embodiment, a new wrought 7xxx aluminum alloy includes not greater than 0.13 wt. % Zr. In one embodiment, a new wrought 7xxx aluminum alloy includes at least 0.07 wt. % Zr. In another embodiment, a new wrought 7xxx aluminum alloy includes at least 0.08 wt.
% Zr.
Zr. As shown by the below data, the combination of vanadium and zirconium may facilitate, for instance, improved fatigue failure resistance properties. In one embodiment, a new wrought 7xxx aluminum alloy includes not greater than 0.18 wt. % Zr. In another embodiment, a new wrought 7xxx aluminum alloy includes not greater than 0.16 wt. % Zr. In yet another embodiment, a new wrought 7xxx aluminum alloy includes not greater than 0.15 wt. % Zr. In another embodiment, a new wrought 7xxx aluminum alloy includes not greater than 0.14 wt. %
Zr. In yet another embodiment, a new wrought 7xxx aluminum alloy includes not greater than 0.13 wt. % Zr. In one embodiment, a new wrought 7xxx aluminum alloy includes at least 0.07 wt. % Zr. In another embodiment, a new wrought 7xxx aluminum alloy includes at least 0.08 wt.
% Zr.
[0012] The total amount of vanadium plus zirconium should be controlled to restrict formation of a high volume fraction of constituent particles (e.g., a high volume fraction of A13Zr, A123V4, A17V and/or AlioV constituent particles). In one embodiment, the total amount of vanadium plus zirconium does not exceed 0.23 wt. % V + Zr. In another embodiment, the total amount of vanadium plus zirconium does not exceed 0.22 wt. % V + Zr. In yet another embodiment, the total amount of vanadium plus zirconium does not exceed 0.21 wt. % V + Zr.
In another embodiment, the total amount of vanadium plus zirconium does not exceed 0.20 wt.
% V + Zr. In one embodiment, the total volume fraction of A13Zr, A123V4, A17V
and AlioV
constituent particles does not exceed 0.07%. The total volume fraction of these constituent particles may be determined, for instance, by PandatTM software and the PanAluminum thermodynamic database (CompuTherm LLC, 437 S. Yellowstone Dr. Suite 217, Madison, WI, USA). In one embodiment, the total volume fraction of A13Zr, A123V4, A17V
and AlioV
constituent particles does not exceed 0.06%. In another embodiment, the total volume fraction of A13Zr, A123V4, A17V and AlioV constituent particles does not exceed 0.05%.
In yet another embodiment, the total volume fraction of A13Zr, A123V4, A17V and AlioV
constituent particles does not exceed 0.04%. In another embodiment, the total volume fraction of A13Zr, A123V4, A17V and Al 10V constituent particles does not exceed 0.03%. In yet another embodiment, the total volume fraction of A13Zr, A123V4, A17V and AlioV constituent particles does not exceed 0.02%. In another embodiment, the total volume fraction of A13Zr, A123V4, A17V
and AlioV
constituent particles does not exceed 0.01%. In yet another embodiment, the total volume fraction of A13Zr, A123V4, A17V and AlioV constituent particles does not exceed 0.005%.
In another embodiment, the total amount of vanadium plus zirconium does not exceed 0.20 wt.
% V + Zr. In one embodiment, the total volume fraction of A13Zr, A123V4, A17V
and AlioV
constituent particles does not exceed 0.07%. The total volume fraction of these constituent particles may be determined, for instance, by PandatTM software and the PanAluminum thermodynamic database (CompuTherm LLC, 437 S. Yellowstone Dr. Suite 217, Madison, WI, USA). In one embodiment, the total volume fraction of A13Zr, A123V4, A17V
and AlioV
constituent particles does not exceed 0.06%. In another embodiment, the total volume fraction of A13Zr, A123V4, A17V and AlioV constituent particles does not exceed 0.05%.
In yet another embodiment, the total volume fraction of A13Zr, A123V4, A17V and AlioV
constituent particles does not exceed 0.04%. In another embodiment, the total volume fraction of A13Zr, A123V4, A17V and Al 10V constituent particles does not exceed 0.03%. In yet another embodiment, the total volume fraction of A13Zr, A123V4, A17V and AlioV constituent particles does not exceed 0.02%. In another embodiment, the total volume fraction of A13Zr, A123V4, A17V
and AlioV
constituent particles does not exceed 0.01%. In yet another embodiment, the total volume fraction of A13Zr, A123V4, A17V and AlioV constituent particles does not exceed 0.005%.
[0013] The new wrought 7xxx aluminum alloys generally include from 0.01 to 0.25 wt. %
Ti. In one embodiment, a new wrought 7xxx aluminum alloy includes from 0.01 to 0.15 wt. %
Ti. In another embodiment, a new wrought 7xxx aluminum alloy includes from 0.01 to 0.10 wt.
% Ti. In yet another embodiment, a new wrought 7xxx aluminum alloy includes from 0.01 to 0.08 wt. % Ti. In another embodiment, a new wrought 7xxx aluminum alloy includes from 0.02 to 0.05 wt. % Ti. The titanium may be present (e.g., at least partially present) in the form of TiB2 or TiC.
Ti. In one embodiment, a new wrought 7xxx aluminum alloy includes from 0.01 to 0.15 wt. %
Ti. In another embodiment, a new wrought 7xxx aluminum alloy includes from 0.01 to 0.10 wt.
% Ti. In yet another embodiment, a new wrought 7xxx aluminum alloy includes from 0.01 to 0.08 wt. % Ti. In another embodiment, a new wrought 7xxx aluminum alloy includes from 0.02 to 0.05 wt. % Ti. The titanium may be present (e.g., at least partially present) in the form of TiB2 or TiC.
[0014] In some embodiments, the new wrought 7xxx aluminum alloys may include up to 0.50 wt. % Mn. In embodiments where manganese is utilized, the new wrought 7xxx aluminum alloys generally include from 0.10 to 0.50 wt. % Mn. In one embodiment, a new wrought 7xxx aluminum alloy includes from 0.10 to 0.25 wt. % Mn. In some embodiments, the new wrought 7xxx aluminum alloys are substantially free of manganese, and, in these embodiments, contain less than 0.10 wt. %. Mn (i.e., < 0.09 wt. % Mn), such as < 0.05 wt. % Mn, or < 0.04 wt. % Mn, or < 0.03 wt. % Mn.
[0015] In some embodiments, the new wrought 7xxx aluminum alloys may include up to 0.40 wt. % Cr. In embodiments where chromium is utilized, the new wrought 7xxx aluminum alloys generally include from 0.10 to 0.40 wt. % Cr. In one embodiment, a new wrought 7xxx aluminum alloy includes from 0.10 to 0.35 wt. % Cr. In another embodiment, a new wrought 7xxx aluminum alloy includes from 0.10 to 0.25 wt. % Cr. In some embodiments, the new wrought 7xxx aluminum alloys are substantially free of chromium, and, in these embodiments, contain less than 0.10 wt. %. Cr (i.e., < 0.09 wt. % Cr), such as < 0.05 wt. %
Cr, or < 0.04 wt. %
Cr, or < 0.03 wt. % Cr.
Cr, or < 0.04 wt. %
Cr, or < 0.03 wt. % Cr.
[0016] The new wrought 7xxx aluminum alloys may include iron, up to 0.35 wt. % Fe. In one embodiment, a new wrought 7xxx aluminum alloy includes not greater than 0.25 wt. % Fe.
In another embodiment, a new wrought 7xxx aluminum alloy includes not greater than 0.20 wt.
% Fe. In yet another embodiment, a new wrought 7xxx aluminum alloy includes not greater than 0.15 wt. % Fe. In another embodiment, a new wrought 7xxx aluminum alloy includes not greater than 0.12 wt. % Fe. In yet another embodiment, a new wrought 7xxx aluminum alloy includes not greater than 0.10 wt. % Fe. In yet another embodiment, a new wrought 7xxx aluminum alloy includes not greater than 0.08 wt. % Fe. In one embodiment, a new wrought 7xxx aluminum alloy includes at least 0.01 wt. % Fe.
In another embodiment, a new wrought 7xxx aluminum alloy includes not greater than 0.20 wt.
% Fe. In yet another embodiment, a new wrought 7xxx aluminum alloy includes not greater than 0.15 wt. % Fe. In another embodiment, a new wrought 7xxx aluminum alloy includes not greater than 0.12 wt. % Fe. In yet another embodiment, a new wrought 7xxx aluminum alloy includes not greater than 0.10 wt. % Fe. In yet another embodiment, a new wrought 7xxx aluminum alloy includes not greater than 0.08 wt. % Fe. In one embodiment, a new wrought 7xxx aluminum alloy includes at least 0.01 wt. % Fe.
17 PCT/US2016/059120 [0017] The new wrought 7xxx aluminum alloys may include silicon, up to 0.25 wt. % Si. In one embodiment, a new wrought 7xxx aluminum alloy includes not greater than 0.20 wt. % Si.
In another embodiment, a new wrought 7xxx aluminum alloy includes not greater than 0.15 wt.
% Si. In yet another embodiment, a new wrought 7xxx aluminum alloy includes not greater than 0.10 wt. % Si. In yet another embodiment, a new wrought 7xxx aluminum alloy includes not greater than 0.08 wt. % Si. In another embodiment, a new wrought 7xxx aluminum alloy includes not greater than 0.05 wt. % Si. In one embodiment, a new wrought 7xxx aluminum alloy includes at least 0.01 wt. % Si.
In another embodiment, a new wrought 7xxx aluminum alloy includes not greater than 0.15 wt.
% Si. In yet another embodiment, a new wrought 7xxx aluminum alloy includes not greater than 0.10 wt. % Si. In yet another embodiment, a new wrought 7xxx aluminum alloy includes not greater than 0.08 wt. % Si. In another embodiment, a new wrought 7xxx aluminum alloy includes not greater than 0.05 wt. % Si. In one embodiment, a new wrought 7xxx aluminum alloy includes at least 0.01 wt. % Si.
[0018] The balance of the new wrought 7xxx aluminum alloy is generally aluminum and unavoidable impurities. In one embodiment, the new wrought 7xxx aluminum alloys contain not more than 0.10 wt. % each of any one impurity (measured on an elemental basis), with the total combined amount of these impurities not exceeding 0.35 wt. % in the new wrought 7xxx aluminum alloy (i.e., < 0.10 wt. % each of any one impurity, and with the total impurities being < 0.35 wt. %). In another embodiment, each one of the impurities, individually, does not exceed 0.05 wt. % in the new wrought 7xxx aluminum alloy, and the total combined amount of the impurities does not exceed 0.15 wt. % in the new wrought 7xxx aluminum alloy (i.e., < 0.05 wt.
% each of any one impurity, and with the total impurities being < 0.15 wt. %).
In another embodiment, each one of these impurities, individually, does not exceed 0.03 wt. % in the new wrought 7xxx aluminum alloy, and the total combined amount of these impurities does not exceed 0.10 wt. % in the new wrought 7xxx aluminum alloys (i.e., < 0.03 wt. %
each of any one impurity, and with the total impurities being < 0.10 wt. %).
% each of any one impurity, and with the total impurities being < 0.15 wt. %).
In another embodiment, each one of these impurities, individually, does not exceed 0.03 wt. % in the new wrought 7xxx aluminum alloy, and the total combined amount of these impurities does not exceed 0.10 wt. % in the new wrought 7xxx aluminum alloys (i.e., < 0.03 wt. %
each of any one impurity, and with the total impurities being < 0.10 wt. %).
[0019] The new wrought 7xxx aluminum alloys described herein may be cast (e.g., as ingot or billet), then homogenized, and then hot worked to an intermediate or final form (e.g., cold working after the hot working when the hot working produces an intermediate form). In one embodiment, the hot working is forging. In one embodiment, the forging produces a shaped product, such as a wheel product. In another embodiment, the hot working is rolling or extruding. After the hot working (and any optional cold working), the new alloy may be tempered, such as by solution heat treating, and then quenching, and then natural aging, followed by artificial aging. Suitable tempers include the T4, T5, T6, and T7 tempers, for instance, as defined in ANSI H35.1 (2009). In one embodiment, the new alloy compositions described herein are processed into a forged wheel product per the processes described in commonly-owned U.S. Patent Application Publication No. 2006/0000094, which is incorporated herein by reference in its entirety. In one embodiment, the new wrought 7xxx aluminum alloys described herein are processed to a T5 temper (e.g., a T53 temper), which may include press quenching the new wrought 7xxx aluminum alloys (e.g., in the form of a forged wheel) after solution heat treatment.
[0020] As mentioned above, the new wrought 7xxx aluminum alloys may realize improved quench insensitivity. Quench insensitivity relates to an aluminum alloy's sensitivity to the quench conditions used after solution heat treatment. One indicator of quench sensitivity is a significant drop in strength with low quench rates as compared to high quench rates. As shown by the below examples, the new wrought 7xxx aluminum alloys described herein may be relatively quench insensitive. For purposes of this application, quench insensitivity is measured by conventionally producing a new wrought 7xxx aluminum alloy as a rolled plate having a final gauge of 1.0 inch (2.54 mm), after which two identical pieces of this plate are solution heat treated, after which one piece is cold water quenched in 77 F (25 C) water and the other piece is boiling water quenched, both for a period of 10 minutes, after which the pieces are allowed to air dry. The two pieces are then both naturally aged for 24 hours and then both two-step artificially aged with a first step of 250 F for 3 hours (with a 2-hour heat up from ambient to 250 F) and a second step of 340 F for 8 hours. The longitudinal (L) tensile yield strengths of these two pieces are then measured at T/2 in accordance with ASTM B557 and E8, using at least duplicate specimens, after which the measured strengths are averaged for each piece. The average TYS(L) of the cold water quenched ("CWQ") piece is then compared to the average TYS(L) of the boiling water quenched (BWQ") TYS. The difference between the two average TYS
values (i.e., CWQ(TYS) - BWQ(TYS)) is the quench insensitivity of the alloy.
values (i.e., CWQ(TYS) - BWQ(TYS)) is the quench insensitivity of the alloy.
[0021] In one embodiment, a new wrought 7xxx aluminum alloy realizes a quench insensitivity (as defined above) of not greater than 7 ksi (i.e., CWQ(TYS) -BWQ(TYS) < 7 ksi).
In another embodiment, a new wrought 7xxx aluminum alloy realizes a quench insensitivity of not greater than 6 ksi. In yet another embodiment, a new wrought 7xxx aluminum alloy realizes a quench insensitivity of not greater than 5 ksi. In another embodiment, a new wrought 7xxx aluminum alloy realizes a quench insensitivity of not greater than 4 ksi. In yet another embodiment, a new wrought 7xxx aluminum alloy realizes a quench insensitivity of not greater than 3 ksi. In another embodiment, a new wrought 7xxx aluminum alloy realizes a quench insensitivity of not greater than 2 ksi. In yet another embodiment, a new wrought 7xxx aluminum alloy realizes a quench insensitivity of not greater than 1 ksi. In another embodiment, a new wrought 7xxx aluminum alloy realizes a quench insensitivity of not greater than 0 ksi, meaning the boiling water quenched alloy realizes at least equivalent strength to the cold water quenched alloy. In yet another embodiment, a new wrought 7xxx aluminum alloy realizes a quench insensitivity of not greater than -1 ksi, meaning the boiling water quenched alloy realizes higher strength than the cold water quenched alloy. In another embodiment, a new wrought 7xxx aluminum alloy realizes a quench insensitivity of not greater than -2 ksi. In another embodiment, a new wrought 7xxx aluminum alloy realizes a quench insensitivity of not greater than -3 ksi. In another embodiment, a new wrought 7xxx aluminum alloy realizes a quench insensitivity of not greater than -4 ksi. In another embodiment, a new wrought 7xxx aluminum alloy realizes a quench insensitivity of not greater than -5 ksi. In another embodiment, a new wrought 7xxx aluminum alloy realizes a quench insensitivity of not greater than -6 ksi. In another embodiment, a new wrought 7xxx aluminum alloy realizes a quench insensitivity of not greater than -7 ksi. In another embodiment, a new wrought 7xxx aluminum alloy realizes a quench insensitivity of not greater than -8 ksi. In another embodiment, a new wrought 7xxx aluminum alloy realizes a quench insensitivity of not greater than -9 ksi, or more.
In another embodiment, a new wrought 7xxx aluminum alloy realizes a quench insensitivity of not greater than 6 ksi. In yet another embodiment, a new wrought 7xxx aluminum alloy realizes a quench insensitivity of not greater than 5 ksi. In another embodiment, a new wrought 7xxx aluminum alloy realizes a quench insensitivity of not greater than 4 ksi. In yet another embodiment, a new wrought 7xxx aluminum alloy realizes a quench insensitivity of not greater than 3 ksi. In another embodiment, a new wrought 7xxx aluminum alloy realizes a quench insensitivity of not greater than 2 ksi. In yet another embodiment, a new wrought 7xxx aluminum alloy realizes a quench insensitivity of not greater than 1 ksi. In another embodiment, a new wrought 7xxx aluminum alloy realizes a quench insensitivity of not greater than 0 ksi, meaning the boiling water quenched alloy realizes at least equivalent strength to the cold water quenched alloy. In yet another embodiment, a new wrought 7xxx aluminum alloy realizes a quench insensitivity of not greater than -1 ksi, meaning the boiling water quenched alloy realizes higher strength than the cold water quenched alloy. In another embodiment, a new wrought 7xxx aluminum alloy realizes a quench insensitivity of not greater than -2 ksi. In another embodiment, a new wrought 7xxx aluminum alloy realizes a quench insensitivity of not greater than -3 ksi. In another embodiment, a new wrought 7xxx aluminum alloy realizes a quench insensitivity of not greater than -4 ksi. In another embodiment, a new wrought 7xxx aluminum alloy realizes a quench insensitivity of not greater than -5 ksi. In another embodiment, a new wrought 7xxx aluminum alloy realizes a quench insensitivity of not greater than -6 ksi. In another embodiment, a new wrought 7xxx aluminum alloy realizes a quench insensitivity of not greater than -7 ksi. In another embodiment, a new wrought 7xxx aluminum alloy realizes a quench insensitivity of not greater than -8 ksi. In another embodiment, a new wrought 7xxx aluminum alloy realizes a quench insensitivity of not greater than -9 ksi, or more.
[0022] The quench insensitivity of the new wrought 7xxx aluminum alloys may facilitate improved strength. Likewise, when using a hot quench media, a new wrought 7xxx aluminum alloy may realize less distortion.
[0023] The new wrought 7xxx aluminum alloys may be post-solution heat treatment quenched with any applicable fluid or media. In one embodiment, a new wrought 7xxx aluminum alloy is water quenched (cold water quenched, hot water quenched, or boiling water quenched). In one embodiment, the new wrought 7xxx aluminum alloy is hot or boiling water quenched. A hot water quench is a quenching using water having a temperature of from 150 F to boiling (212 F at standard temperature and pressure). A boiling water quench uses boiling water.
A boiling water quench is a species of the hot water quench genus. As shown by the below data, use of a hot water quench (including a boiling water quench) may facilitate improved SCC
resistance. In another embodiment, a new wrought 7xxx aluminum alloy is air quenched (e.g., via a forced air quench). In yet another embodiment, a new wrought 7xxx aluminum alloy is press-quenched. In one embodiment, the quenching step results in an average cooling rate of from 1 F to 25 F per second as measured during the first 60 seconds of the quench. In another embodiment, the quenching step results in an average cooling rate of not greater than 22.5 F per second as measured during the first 60 seconds of the quench. In yet another embodiment, the quenching step results in an average cooling rate of not greater than 20 F per second as measured during the first 60 seconds of the quench. In another embodiment, the quenching step results in an average cooling rate of not greater than 17.5 F per second as measured during the first 60 seconds of the quench. In yet another embodiment, the quenching step results in an average cooling rate of not greater than 15 F per second as measured during the first 60 seconds of the quench. In another embodiment, the quenching step results in an average cooling rate of not greater than 12.5 F per second as measured during the first 60 seconds of the quench. In yet another embodiment, the quenching step results in an average cooling rate of not greater than F per second as measured during the first 60 seconds of the quench. In another embodiment, the quenching step results in an average cooling rate of not greater than 9.0 F per second as measured during the first 60 seconds of the quench. In yet another embodiment, the quenching step results in an average cooling rate of not greater than 8.0 F per second as measured during the first 60 seconds of the quench. In another embodiment, the quenching step results in an average cooling rate of not greater than 7.0 F per second as measured during the first 60 seconds of the quench. In yet another embodiment, the quenching step results in an average cooling rate of not greater than 6.0 F per second as measured during the first 60 seconds of the quench.
BRIEF DESCRIPTION OF THE DRAWINGS
A boiling water quench is a species of the hot water quench genus. As shown by the below data, use of a hot water quench (including a boiling water quench) may facilitate improved SCC
resistance. In another embodiment, a new wrought 7xxx aluminum alloy is air quenched (e.g., via a forced air quench). In yet another embodiment, a new wrought 7xxx aluminum alloy is press-quenched. In one embodiment, the quenching step results in an average cooling rate of from 1 F to 25 F per second as measured during the first 60 seconds of the quench. In another embodiment, the quenching step results in an average cooling rate of not greater than 22.5 F per second as measured during the first 60 seconds of the quench. In yet another embodiment, the quenching step results in an average cooling rate of not greater than 20 F per second as measured during the first 60 seconds of the quench. In another embodiment, the quenching step results in an average cooling rate of not greater than 17.5 F per second as measured during the first 60 seconds of the quench. In yet another embodiment, the quenching step results in an average cooling rate of not greater than 15 F per second as measured during the first 60 seconds of the quench. In another embodiment, the quenching step results in an average cooling rate of not greater than 12.5 F per second as measured during the first 60 seconds of the quench. In yet another embodiment, the quenching step results in an average cooling rate of not greater than F per second as measured during the first 60 seconds of the quench. In another embodiment, the quenching step results in an average cooling rate of not greater than 9.0 F per second as measured during the first 60 seconds of the quench. In yet another embodiment, the quenching step results in an average cooling rate of not greater than 8.0 F per second as measured during the first 60 seconds of the quench. In another embodiment, the quenching step results in an average cooling rate of not greater than 7.0 F per second as measured during the first 60 seconds of the quench. In yet another embodiment, the quenching step results in an average cooling rate of not greater than 6.0 F per second as measured during the first 60 seconds of the quench.
BRIEF DESCRIPTION OF THE DRAWINGS
[0024] FIG 1 is a table illustrating various embodiments of new 7xxx wrought aluminum alloy compositions.
DETAILED DESCRIPTION
Example 1
DETAILED DESCRIPTION
Example 1
[0025] Several 7xxx aluminum alloys having the compositions shown in Table 1, below, were cast as lab-scale, 2.5 inch (6.35 cm) thick ingots (nominal). The ingots were then scalped, homogenized, and hot rolled to a final gauge of 1.25 inch (3.175 cm). After hot rolling, the plates were metallographically inspected. The inspection revealed that plates 2, 14, 15, 17 and 18 contained a high volume fraction of constituent particles due to excess V +
Zr + Ti content relative to the amount of Zn+Mg+Cu content of those alloys.
Zr + Ti content relative to the amount of Zn+Mg+Cu content of those alloys.
[0026] The hot rolled plates were then solution heat treated, cold water quenched, and then allowed to naturally age for about 24-hours. After natural aging, the plates were then two-step artificially aged at 250 F for 3 hours and then 340 F for 8 hours. Several of the alloy samples in the naturally aged condition were also artificially aged at 250 F for 3 hours and then 340 F for 16 hours. The longitudinal (L) mechanical properties of the artificially aged plates were then measured at T/2 and in accordance with ASTM B557 and E8, the results of which are shown in Table 2, below (average of duplicate specimens).
Table 1 - Composition of the Example 1 Alloys (all values in weight percent)*
Alloy # Si Fe Zn Mg Cu V Zr V+Zr 1** 0.056 0.087 4.25 1.59 0.57 0.079 0.10 0.179 2 0.059 0.094 4.83 1.67 0.65 0.120 0.19 0.310 3** 0.057 0.095 5.20 1.60 0.64 0.082 0.10 0.182 4** 0.056 0.094 6.02 1.57 0.64 0.086 0.10 0.186 0.057 0.085 3.65 1.66 0.62 0.080 0.11 0.190 6 0.059 0.092 2.83 1.61 0.60 0.080 0.10 0.180 7** 0.064 0.093 4.39 1.99 0.62 0.088 0.10 0.188 8** 0.057 0.092 4.38 2.37 0.61 0.089 0.10 0.189 9 0.052 0.072 4.53 1.20 0.55 0.083 0.10 0.183 0.050 0.080 4.40 0.85 0.60 0.080 0.10 0.180 11** 0.058 0.084 4.41 1.63 0.88 0.084 0.10 0.184 12** 0.054 0.088 4.38 1.64 1.26 0.083 0.10 0.183 13** 0.055 0.088 4.35 1.63 0.42 0.082 0.12 0.202 14 0.059 0.092 4.44 1.67 0.61 0.200 0.10 0.300 0.059 0.086 4.46 1.62 0.61 0.160 0.11 0.270 16** 0.058 0.100 4.41 1.55 0.64 0.056 0.10 0.156 17 0.057 0.089 4.39 1.65 0.61 0.088 0.15 0.238 18 0.059 0.092 4.44 1.61 0.62 0.086 0.19 0.276 19** 0.054 0.084 4.36 1.62 0.59 0.086 0.06 0.146 0.056 0.088 4.31 1.6 0.61 0.078 0 0.078 * = The balance of the alloys was Ti, Al and impurities; all alloys contained 0.02 - 0.03 wt. % Ti, except alloy 2 which contained 0.055 wt. % Ti ; all alloys contained < 0.03 wt.
% of any one impurity and < 0.10 wt. % in total of all impurities; impurities included Mn and Cr in this example.
** = invention alloy Table 2 - Measured Mechanical Properties of the Example 1 Alloys All # Artificial Aging TYS UTS Elong.
oy Practice (MPa) (MPa) (%
1 250F/3hrs + 340F/8hrs 332.5 395.3 17.0 1 250F/3hrs + 340F/16hrs 323.8 389.3 16.0 3 250F/3hrs + 340F/8hrs 399.0 447.5 17.0 3 250F/3hrs + 340F/16hrs 371.3 428.3 18.0 4 250F/3hrs + 340F/16hrs 416.3 459.0 16.5 250F/3hrs + 340F/8hrs 285.8 365.3 17.5 5 250F/3hrs + 340F/16hrs 299.0 378.5 18.0 6 250F/3hrs + 340F/16hrs 224.5 317.0 21.5 7 250F/3hrs + 340F/8hrs 383.3 440.3 16.0 7 250F/3hrs + 340F/16hrs 383.8 444.0 15.5 8 250F/3hrs + 340F/16hrs 399.8 455.3 13.5 9 250F/3hrs + 340F/8hrs 304.5 360.5 15.0 9 250F/3hrs + 340F/16hrs 275.0 340.0 15.0 250F/3hrs + 340F/16hrs 231.0 298.0 19.5 11 250F/3hrs + 340F/8hrs 344.3 411.0 15.5 11 250F/3hrs + 340F/16hrs 358.3 424.8 16.0 12 250F/3hrs + 340F/16hrs 357.5 433.0 15.0 13 250F/3hrs + 340F/8hrs 332.8 391.3 17.0 13 250F/3hrs + 340F/16hrs 333.3 397.3 17.0 16 250F/3hrs + 340F/8hrs 368.8 424.8 16.5 16 250F/3hrs + 340F/16hrs 325.8 392.0 14.5 19 250F/3hrs + 340F/8hrs 336.5 393.8 17.0 19 250F/3hrs + 340F/16hrs 326.5 389.0 16.0 250F/3hrs + 340F/8hrs 345.3 399.8 16.0 20 250F/3hrs + 340F/16hrs 337.0 396.5 13.0
Table 1 - Composition of the Example 1 Alloys (all values in weight percent)*
Alloy # Si Fe Zn Mg Cu V Zr V+Zr 1** 0.056 0.087 4.25 1.59 0.57 0.079 0.10 0.179 2 0.059 0.094 4.83 1.67 0.65 0.120 0.19 0.310 3** 0.057 0.095 5.20 1.60 0.64 0.082 0.10 0.182 4** 0.056 0.094 6.02 1.57 0.64 0.086 0.10 0.186 0.057 0.085 3.65 1.66 0.62 0.080 0.11 0.190 6 0.059 0.092 2.83 1.61 0.60 0.080 0.10 0.180 7** 0.064 0.093 4.39 1.99 0.62 0.088 0.10 0.188 8** 0.057 0.092 4.38 2.37 0.61 0.089 0.10 0.189 9 0.052 0.072 4.53 1.20 0.55 0.083 0.10 0.183 0.050 0.080 4.40 0.85 0.60 0.080 0.10 0.180 11** 0.058 0.084 4.41 1.63 0.88 0.084 0.10 0.184 12** 0.054 0.088 4.38 1.64 1.26 0.083 0.10 0.183 13** 0.055 0.088 4.35 1.63 0.42 0.082 0.12 0.202 14 0.059 0.092 4.44 1.67 0.61 0.200 0.10 0.300 0.059 0.086 4.46 1.62 0.61 0.160 0.11 0.270 16** 0.058 0.100 4.41 1.55 0.64 0.056 0.10 0.156 17 0.057 0.089 4.39 1.65 0.61 0.088 0.15 0.238 18 0.059 0.092 4.44 1.61 0.62 0.086 0.19 0.276 19** 0.054 0.084 4.36 1.62 0.59 0.086 0.06 0.146 0.056 0.088 4.31 1.6 0.61 0.078 0 0.078 * = The balance of the alloys was Ti, Al and impurities; all alloys contained 0.02 - 0.03 wt. % Ti, except alloy 2 which contained 0.055 wt. % Ti ; all alloys contained < 0.03 wt.
% of any one impurity and < 0.10 wt. % in total of all impurities; impurities included Mn and Cr in this example.
** = invention alloy Table 2 - Measured Mechanical Properties of the Example 1 Alloys All # Artificial Aging TYS UTS Elong.
oy Practice (MPa) (MPa) (%
1 250F/3hrs + 340F/8hrs 332.5 395.3 17.0 1 250F/3hrs + 340F/16hrs 323.8 389.3 16.0 3 250F/3hrs + 340F/8hrs 399.0 447.5 17.0 3 250F/3hrs + 340F/16hrs 371.3 428.3 18.0 4 250F/3hrs + 340F/16hrs 416.3 459.0 16.5 250F/3hrs + 340F/8hrs 285.8 365.3 17.5 5 250F/3hrs + 340F/16hrs 299.0 378.5 18.0 6 250F/3hrs + 340F/16hrs 224.5 317.0 21.5 7 250F/3hrs + 340F/8hrs 383.3 440.3 16.0 7 250F/3hrs + 340F/16hrs 383.8 444.0 15.5 8 250F/3hrs + 340F/16hrs 399.8 455.3 13.5 9 250F/3hrs + 340F/8hrs 304.5 360.5 15.0 9 250F/3hrs + 340F/16hrs 275.0 340.0 15.0 250F/3hrs + 340F/16hrs 231.0 298.0 19.5 11 250F/3hrs + 340F/8hrs 344.3 411.0 15.5 11 250F/3hrs + 340F/16hrs 358.3 424.8 16.0 12 250F/3hrs + 340F/16hrs 357.5 433.0 15.0 13 250F/3hrs + 340F/8hrs 332.8 391.3 17.0 13 250F/3hrs + 340F/16hrs 333.3 397.3 17.0 16 250F/3hrs + 340F/8hrs 368.8 424.8 16.5 16 250F/3hrs + 340F/16hrs 325.8 392.0 14.5 19 250F/3hrs + 340F/8hrs 336.5 393.8 17.0 19 250F/3hrs + 340F/16hrs 326.5 389.0 16.0 250F/3hrs + 340F/8hrs 345.3 399.8 16.0 20 250F/3hrs + 340F/16hrs 337.0 396.5 13.0
[0027] As shown, alloys 5-6 and 9-10 with low zinc (alloys 5-6) or low magnesium (9-10) have low strength, not achieving a tensile yield strength (TYS) of at least 320 MPa in combination with an elongation of at least 12%.
[0028] Rotating beam fatigue testing in accordance with ISO 1143 was also conducted on alloy plates 1, 13, 16 and 20, the results of which are shown in Table 3, below. The stress level for the test was 15 ksi, with R = -1 and with the RPM being 10,000. Three test specimens per alloy were used, and the number of cycles to failure was measured for each specimen. The test run-out was 10,000,000 cycles.
Table 3 - Measured Fatigue Life of Alloys 1, 13, 16 and 20 Alloy # Artificial Aging Cycles to Failure**
Practice Specimen 1 Specimen 2 Specimen 3 250F/3 hrs +
340F/8hrs 10,000,000 10,000,000 10,000,000 250F/3 hrs +
340F/8hrs 10,000,000 1,174,446 10,000,000 250F/3 hrs +
340F/8hrs 10,000,000 10,000,000 10,000,000 250F/3 hrs +
340F/8hrs 2,281,864 2,664,481 1,562,425
Table 3 - Measured Fatigue Life of Alloys 1, 13, 16 and 20 Alloy # Artificial Aging Cycles to Failure**
Practice Specimen 1 Specimen 2 Specimen 3 250F/3 hrs +
340F/8hrs 10,000,000 10,000,000 10,000,000 250F/3 hrs +
340F/8hrs 10,000,000 1,174,446 10,000,000 250F/3 hrs +
340F/8hrs 10,000,000 10,000,000 10,000,000 250F/3 hrs +
340F/8hrs 2,281,864 2,664,481 1,562,425
[0029] As shown, alloy 20 with no zirconium realizes worse fatigue properties relative to alloys 1, 13 and 16.
Example 2
Example 2
[0030] Three 7xxx aluminum alloys having the compositions shown in Table 4, below, were cast as industrial-scale billet. From these billets, 3" x 7.75" x 7.75"
samples were obtained from D/2 by machining. The samples were then hot rolled to a final gauge of about 1.0 inch (2.54 cm). The hot rolled plates were then solution heat treated, and then either cold water (CW) or boiling water (BW) quenched, and then allowed to naturally age for about 24-hours. Cold water quenched means the use of ambient temperature water. Boiling-water quench means the use of boiling water. After natural aging, the plates were then two-step artificially aged with a first step of 250 F for 3 hours (with a 2-hour heat up from ambient to 250 F) and a second step of 340 F
for 8 hours. The longitudinal (L) mechanical properties of the plates were then measured at T/2 and in accordance with ASTM B557 and E8, the results of which are shown in Table 5, below (average of duplicate specimens). SCC results were also measured in accordance with ASTM
G103-97(2011), the "Standard Practice for Evaluating Stress-Corrosion Cracking Resistance of Low Copper 7XXX Series Al-Zn-Mg-Cu Alloys in Boiling 6% Sodium Chloride Solution," at 25 ksi and 35 ksi stress levels, the results of which are shown in Table 6, below.
Table 4 - Composition of the Example 2 Alloys (all values in weight percent)*
Alloy # Si Fe Zn Mg Cu V Zr A 0.062 0.065 4.38 1.54 0.63 0.06 0.08 0.078 0.061 4.60 1.72 0.61 0.01 0.11 0.060 0.068 4.43 1.71 0.89 0.01 0.10 * = The balance of the alloys was Ti, Al and impurities; all alloys contained 0.02 - 0.03 wt. % Ti; all alloys contained < 0.03 wt. % of any one impurity and < 0.10 wt.
% in total of all impurities; impurities included Mn and Cr in this example.
Table 5 - Measured Mechanical Properties of the Example 2 Alloys Alto # Quench TYS UTS Elong.
y (MPa) (MPa) (%
A CW 362.8 417.5 17.0 A BW 370.5 423.0 16.5 CW 391.0 441.8 16.0 BW 400.8 448.3 15.8 CW 390.5 446.0 16.0 BW 401.3 450.5 16.3 Table 6 - SCC Properties of the Example 2 Alloys Stress (ST) Days to Failure Alloy #Quench (ksi) Specimen 1 Specimen 2 Specimen 3 A
25 2.12 01(7 0K7 CW
35 6.06 3.01 2.12 A BW
25 0.65 1.07 0.65 CW
35 0.65 0.65 0.65 25 5.08 01(7 0K7 BW
35 0.65 1.7 1.07 25 0K7 0K7 7.0 CW
35 3.01 0.65 2.12 25 3.01 01(7 5.08 BW
35 2.67 2.12 01(7 0K7 = Passed the SCC test for the full 7 days 7.0 = failed on the 7th day
samples were obtained from D/2 by machining. The samples were then hot rolled to a final gauge of about 1.0 inch (2.54 cm). The hot rolled plates were then solution heat treated, and then either cold water (CW) or boiling water (BW) quenched, and then allowed to naturally age for about 24-hours. Cold water quenched means the use of ambient temperature water. Boiling-water quench means the use of boiling water. After natural aging, the plates were then two-step artificially aged with a first step of 250 F for 3 hours (with a 2-hour heat up from ambient to 250 F) and a second step of 340 F
for 8 hours. The longitudinal (L) mechanical properties of the plates were then measured at T/2 and in accordance with ASTM B557 and E8, the results of which are shown in Table 5, below (average of duplicate specimens). SCC results were also measured in accordance with ASTM
G103-97(2011), the "Standard Practice for Evaluating Stress-Corrosion Cracking Resistance of Low Copper 7XXX Series Al-Zn-Mg-Cu Alloys in Boiling 6% Sodium Chloride Solution," at 25 ksi and 35 ksi stress levels, the results of which are shown in Table 6, below.
Table 4 - Composition of the Example 2 Alloys (all values in weight percent)*
Alloy # Si Fe Zn Mg Cu V Zr A 0.062 0.065 4.38 1.54 0.63 0.06 0.08 0.078 0.061 4.60 1.72 0.61 0.01 0.11 0.060 0.068 4.43 1.71 0.89 0.01 0.10 * = The balance of the alloys was Ti, Al and impurities; all alloys contained 0.02 - 0.03 wt. % Ti; all alloys contained < 0.03 wt. % of any one impurity and < 0.10 wt.
% in total of all impurities; impurities included Mn and Cr in this example.
Table 5 - Measured Mechanical Properties of the Example 2 Alloys Alto # Quench TYS UTS Elong.
y (MPa) (MPa) (%
A CW 362.8 417.5 17.0 A BW 370.5 423.0 16.5 CW 391.0 441.8 16.0 BW 400.8 448.3 15.8 CW 390.5 446.0 16.0 BW 401.3 450.5 16.3 Table 6 - SCC Properties of the Example 2 Alloys Stress (ST) Days to Failure Alloy #Quench (ksi) Specimen 1 Specimen 2 Specimen 3 A
25 2.12 01(7 0K7 CW
35 6.06 3.01 2.12 A BW
25 0.65 1.07 0.65 CW
35 0.65 0.65 0.65 25 5.08 01(7 0K7 BW
35 0.65 1.7 1.07 25 0K7 0K7 7.0 CW
35 3.01 0.65 2.12 25 3.01 01(7 5.08 BW
35 2.67 2.12 01(7 0K7 = Passed the SCC test for the full 7 days 7.0 = failed on the 7th day
[0031] As shown, Alloy A realizes a superior combination of strength, elongation and SCC
resistance properties. As shown, Alloy A is generally quench insensitive, realizing about 8 ksi higher tensile yield strength when boiling water quenched.
resistance properties. As shown, Alloy A is generally quench insensitive, realizing about 8 ksi higher tensile yield strength when boiling water quenched.
[0032] While various embodiments of the present disclosure have been described in detail, it is apparent that modifications and adaptations of those embodiments will occur to those skilled in the art. However, it is to be expressly understood that such modifications and adaptations are within the spirit and scope of the present disclosure.
Claims (4)
1. A wrought 7xxx aluminum alloy consisting of:
(a) from 3.75 to 8.0 wt. % Zn;
(b) from 1.25 to 3.0 wt. % Mg;
(c) from 0.35 to 1.35 wt. % Cu;
(d) from 0.04 to 0.20 wt. % V;
(e) from 0.06 to 0.20 wt. % Zr;
wherein V + Zr < 0.23 wt. %;
(f) from 0.01 to 0.25 wt. % Ti;
(g) up to 0.50 wt. % Mn;
(h) up to 0.40 wt. % Cr;
(i) up to 0.35 wt. % Fe; and (j) up to 0.25 wt. % Si;
(k) the balance being aluminum and impurities, wherein the wrought 7xxx aluminum alloy wrought 7xxx aluminum alloy includes not greater than 0.10 wt. % each of any one impurity, and wherein the wrought 7xxx aluminum alloy includes not greater than 0.35 wt. % in total of the impurities.
(a) from 3.75 to 8.0 wt. % Zn;
(b) from 1.25 to 3.0 wt. % Mg;
(c) from 0.35 to 1.35 wt. % Cu;
(d) from 0.04 to 0.20 wt. % V;
(e) from 0.06 to 0.20 wt. % Zr;
wherein V + Zr < 0.23 wt. %;
(f) from 0.01 to 0.25 wt. % Ti;
(g) up to 0.50 wt. % Mn;
(h) up to 0.40 wt. % Cr;
(i) up to 0.35 wt. % Fe; and (j) up to 0.25 wt. % Si;
(k) the balance being aluminum and impurities, wherein the wrought 7xxx aluminum alloy wrought 7xxx aluminum alloy includes not greater than 0.10 wt. % each of any one impurity, and wherein the wrought 7xxx aluminum alloy includes not greater than 0.35 wt. % in total of the impurities.
2. The wrought 7xxx aluminum alloy of claim 1, wherein the wrought 7xxx aluminum alloy is a forged wheel product.
3. The wrought 7xxx aluminum alloy of claim 1, wherein the wrought 7xxx aluminum alloy is a forged wheel product in the T5 temper.
4. The wrought 7xxx aluminum alloy of claim 1, wherein the wrought 7xxx aluminum alloy is a forged wheel product in the T5 temper, and wherein the wrought 7xxx aluminum alloy realizes a quench insensitivity of not greater than 7 ksi.
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| CN107619976B (en) * | 2017-08-09 | 2019-04-16 | 中车青岛四方机车车辆股份有限公司 | A kind of Al-Zn-Mg alloy and preparation method thereof |
| EP3704279A4 (en) | 2017-10-31 | 2021-03-10 | Howmet Aerospace Inc. | Improved aluminum alloys, and methods for producing the same |
| BR112021004434B1 (en) * | 2018-11-12 | 2024-01-02 | Novelis Koblenz Gmbh | 7XXX SERIES ALUMINUM ALLOY PRODUCT |
| EP3927860A4 (en) * | 2019-02-20 | 2022-11-23 | Howmet Aerospace Inc. | Improved aluminum-magnesium-zinc aluminum alloys |
| US20210172044A1 (en) * | 2019-12-05 | 2021-06-10 | Kaiser Aluminum Fabricated Products, Llc | High Strength Press Quenchable 7xxx alloy |
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| JPS58213852A (en) * | 1982-06-05 | 1983-12-12 | Kobe Steel Ltd | High strength aluminum alloy having superior stress corrosion cracking resistance at flash butt weld zone |
| JPS5928555A (en) * | 1982-08-06 | 1984-02-15 | Sumitomo Light Metal Ind Ltd | High tensile aluminum alloy good in extrudability and excellent in strength and toughness |
| US5135713A (en) * | 1984-03-29 | 1992-08-04 | Aluminum Company Of America | Aluminum-lithium alloys having high zinc |
| US4867805A (en) * | 1988-02-03 | 1989-09-19 | Agrawal Suphal P | Superplastic aluminum alloys, alloy processes and component part formations thereof |
| JPH03122245A (en) * | 1989-10-06 | 1991-05-24 | Furukawa Alum Co Ltd | High strength aluminum alloy for welding excellent in stress corrosion cracking resistance |
| US20050034794A1 (en) * | 2003-04-10 | 2005-02-17 | Rinze Benedictus | High strength Al-Zn alloy and method for producing such an alloy product |
| US20060000009A1 (en) * | 2004-07-01 | 2006-01-05 | Fleming Michael P | Protective helmet for children in automobiles |
| US20060000094A1 (en) | 2004-07-01 | 2006-01-05 | Garesche Carl E | Forged aluminum vehicle wheel and associated method of manufacture and alloy |
| WO2007020041A2 (en) * | 2005-08-16 | 2007-02-22 | Aleris Aluminum Koblenz Gmbh | High strength weldable al-mg alloy |
| US7914646B2 (en) * | 2006-07-21 | 2011-03-29 | Nalco Company | Compositions and processes for paper production |
| CN101484603B (en) * | 2006-07-07 | 2011-09-21 | 阿勒里斯铝业科布伦茨有限公司 | Aa7000-series aluminium alloy products and a method of manufacturing thereof |
| WO2009156283A1 (en) * | 2008-06-24 | 2009-12-30 | Aleris Aluminum Koblenz Gmbh | Al-zn-mg alloy product with reduced quench sensitivity |
| JP2010221256A (en) * | 2009-03-24 | 2010-10-07 | Furukawa-Sky Aluminum Corp | Tube joining method |
| US9347558B2 (en) * | 2010-08-25 | 2016-05-24 | Spirit Aerosystems, Inc. | Wrought and cast aluminum alloy with improved resistance to mechanical property degradation |
| KR101883021B1 (en) * | 2010-09-08 | 2018-07-27 | 아르코닉 인코포레이티드 | Improved 7xxx aluminum alloys, and methods for producing the same |
| US11103919B2 (en) | 2014-04-30 | 2021-08-31 | Alcoa Usa Corp. | 7xx aluminum casting alloys, and methods for making the same |
| JP5928555B2 (en) * | 2014-10-30 | 2016-06-01 | キヤノンマーケティングジャパン株式会社 | Information processing system, information processing method, and computer program |
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- 2016-10-27 EP EP16860785.1A patent/EP3368702B1/en active Active
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| EP3368702A1 (en) | 2018-09-05 |
| CN108291280B (en) | 2021-05-11 |
| US20170121795A1 (en) | 2017-05-04 |
| EP3368702C0 (en) | 2023-08-16 |
| HUE063975T2 (en) | 2024-02-28 |
| EP3368702A4 (en) | 2019-07-17 |
| CN108291280A (en) | 2018-07-17 |
| WO2017075217A1 (en) | 2017-05-04 |
| EP3368702B1 (en) | 2023-08-16 |
| CA3003158C (en) | 2020-07-07 |
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