The present disclosure relates to metallurgy generally and more specifically to producing aluminum alloys, optionally from recycled scrap, manufacturing aluminum alloy products, and recycling aluminum alloys.
Due to the costs and time associated with producing primary aluminum, many original equipment manufacturers rely on existing aluminum-containing scrap to prepare aluminum alloy materials. However, recyclable scrap can be unsuitable for use in preparing high performance aluminum alloys, as the recyclable scrap can contain high levels of certain undesirable elements. For example, the recyclable scrap can include certain elements in amounts that affect the mechanical properties of the aluminum alloys, such as formability and strength.
Covered embodiments of the invention are defined by the claims, not this summary. This summary is a high-level overview of various aspects of the invention and introduces some of the concepts that are further described in the Detailed Description section below. This summary is not intended to identify key or essential features of the claimed subject matter, nor is it intended to be used in isolation to determine the scope of the claimed subject matter. The subject matter should be understood by reference to appropriate portions of the entire specification, any or all drawings, and each claim.
Described herein are highly formable, recycled aluminum alloys and methods of producing the aluminum alloys. The aluminum alloys described herein comprise about 0.5 to 2.0 wt. % Si, 0.2 to 0.4 wt. % Fe, up to 0.4 wt. % Cu, up to 0.5 wt. % Mg, 0.02 to 0.1 wt. % Mn, 0.01 to 0.1 wt. % Cr, up to 0.15 wt. % Sr, up to 0.15 wt. % total impurities, wherein each impurity is present in an amount of up to about 0.05 wt. %, and Al. In some non-limiting examples, the aluminum alloys comprise about 0.7 to 1.4 wt. % Si, 0.2 to 0.3 wt. % Fe, up to 0.2 wt. % Cu, up to 0.4 wt. % Mg, 0.02 to 0.08 wt. % Mn, 0.02 to 0.05 wt. % Cr, 0.01 to 0.12 wt. % Sr, up to 0.15 wt. % impurities, and Al. In some non-limiting examples, the aluminum alloys comprise about 1.0 to 1.4 wt. % Si, 0.22 to 0.28 wt. % Fe, up to 0.15 wt. % Cu, up to 0.35 wt. % Mg, 0.02 to 0.06 wt. % Mn, 0.02 to 0.04 wt. % Cr, 0.02 to 0.10 wt. % Sr, up to 0.15 wt. % impurities, and Al. Optionally, a combined content of Fe and Cr in the aluminum alloy is from about 0.22 wt. % to about 0.5 wt. %. Also described herein are aluminum alloy products comprising the aluminum alloys as described herein. In some examples, the aluminum alloy products comprise a grain size up to about 35 μm (e.g., from about 25 μm to about 35 μm or from about 28 μm to about 32 μm). Optionally, the aluminum alloy products comprise iron-containing intermetallic particles. In some cases, at least about 36% of the iron-containing intermetallic particles can be spherical. In some non-limiting examples, at least about 36% (e.g., at least about 50% or at least about 75%) of the iron-containing intermetallic particles present in the aluminum alloy products have an equivalent circular diameter (i.e., “ECD”) of about 3 μm or less. Optionally, at least about 36% (e.g., at least about 50%, at least about 70%, or at least about 80%) of the iron-containing intermetallic particles comprise α-AlFe(Mn,Cr)Si intermetallic particles. In some cases, a volume fraction of a cube textural component in the aluminum alloy product comprises at least about 12%. In some cases, the aluminum alloy products comprise a total elongation of at least about 32%. The aluminum alloy product can comprise an automobile body part, among others.
Further described herein are methods of producing an aluminum alloy product. The methods comprise casting an aluminum alloy as described herein to produce a cast aluminum alloy article, homogenizing the cast aluminum alloy article to produce a homogenized cast aluminum alloy article, hot rolling, and cold rolling the homogenized cast aluminum alloy article to produce a final gauge aluminum alloy product, and solution heat treating the final gauge aluminum alloy product. Optionally, the homogenizing is performed at a homogenization temperature of from about 530° C. to about 570° C. Optionally, the aluminum alloy in the casting step comprises a recycled content in an amount of at least about 40 wt. %.
Provided herein are aluminum alloy products having desirable mechanical properties and methods of casting and processing the same. The aluminum alloy products can be recycled as well as produced from recycled material (e.g., post-consumer scrap) and still exhibit desirable mechanical properties, such as good formability without cracking and/or fracture, high elongation before fracture, and good durability.
The aluminum alloy products described herein contain intermetallic particles that have a low aspect ratio (e.g., width to height ratio). In some cases, a low aspect ratio is a ratio of about 4 or less (e.g., about 3 or less, about 2 or less, or about 1.5 or less). In particular, the intermetallic particles are circular or spherical in shape. An aspect ratio of 1 (e.g., close to a circular cross section, i.e., spherical particles) is a preferable Fe-containing intermetallic particle shape for mechanical properties, for example bending, forming, crushing, and/or crash-testing. These intermetallic particles enhance the desirable mechanical properties of the products and result in products exhibiting superior results as compared to aluminum alloy products having intermetallic particles that are elliptical or needle-like in shape.
As used herein, the terms “invention,” “the invention,” “this invention” and “the present invention” are intended to refer broadly to all of the subject matter of this patent application and the claims below. Statements containing these terms should be understood not to limit the subject matter described herein or to limit the meaning or scope of the patent claims below.
In this description, reference is made to alloys identified by aluminum industry designations, such as “series” or “6xxx.” For an understanding of the number designation system most commonly used in naming and identifying aluminum and its alloys, see “International Alloy Designations and Chemical Composition Limits for Wrought Aluminum and Wrought Aluminum Alloys,” or “Registration Record of Aluminum Association Alloy Designations and Chemical Compositions Limits for Aluminum Alloys in the Form of Castings and Ingot,” both published by The Aluminum Association.
As used herein, the meaning of “a,” “an,” or “the” includes singular and plural references unless the context clearly dictates otherwise.
As used herein, a plate generally has a thickness of greater than about 15 mm. For example, a plate may refer to an aluminum product having a thickness of greater than about 15 mm, greater than about 20 mm, greater than about 25 mm, greater than about 30 mm, greater than about 35 mm, greater than about 40 mm, greater than about 45 mm, greater than about 50 mm, greater than about 100 mm, or up to about 300 mm.
As used herein, a shate (also referred to as a sheet plate) generally has a thickness of from about 4 mm to about 15 mm. For example, a shate may have a thickness of about 4 mm, about 5 mm, about 6 mm, about 7 mm, about 8 mm, about 9 mm, about 10 mm, about 11 mm, about 12 mm, about 13 mm, about 14 mm, or about 15 mm.
As used herein, a sheet generally refers to an aluminum product having a thickness of less than about 4 mm. For example, a sheet may have a thickness of less than about 4 mm, less than about 3 mm, less than about 2 mm, less than about 1 mm, less than about 0.5 mm, less than about 0.3 mm, or less than about 0.1 mm.
Reference is made in this application to alloy temper or condition. For an understanding of the alloy temper descriptions most commonly used, see “American National Standards (ANSI) H35 on Alloy and Temper Designation Systems.” An F condition or temper refers to an aluminum alloy as fabricated. An O condition or temper refers to an aluminum alloy after annealing. A T1 condition or temper refers to an aluminum alloy cooled from hot working and naturally aged (e.g., at room temperature). A T2 condition or temper refers to an aluminum alloy cooled from hot working, cold worked and naturally aged. A T3 condition or temper refers to an aluminum alloy solution heat treated, cold worked, and naturally aged. A T4 condition or temper refers to an aluminum alloy solution heat treated and naturally aged. A T5 condition or temper refers to an aluminum alloy cooled from hot working and artificially aged (at elevated temperatures). A T6 condition or temper refers to an aluminum alloy solution heat treated and artificially aged. A T7 condition or temper refers to an aluminum alloy solution heat treated and artificially overaged. A T8x condition or temper refers to an aluminum alloy solution heat treated, cold worked, and artificially aged. A T9 condition or temper refers to an aluminum alloy solution heat treated, artificially aged, and cold worked.
As used herein, the meaning of “room temperature” can include a temperature of from about 15° C. to about 30° C., for example about 15° C., about 16° C., about 17° C., about 18° C., about 19° C., about 20° C., about 21° C., about 22° C., about 23° C., about 24° C., about 25° C., about 26° C., about 27° C., about 28° C., about 29° C., or about 30° C.
As used herein, terms such as “cast aluminum alloy article,” “cast metal article,” “cast article,” and the like are interchangeable and refer to a product produced by direct chill casting (including direct chill co-casting) or semi-continuous casting, continuous casting (including, for example, by use of a twin belt caster, a twin roll caster, a block caster, or any other continuous caster), electromagnetic casting, hot top casting, or any other casting method, or any combination thereof.
All ranges disclosed herein are to be understood to encompass any endpoints and any and all subranges subsumed therein. For example, a stated range of “1 to 10” should be considered to include any and all subranges between (and inclusive of) the minimum value of 1 and the maximum value of 10; that is, all subranges beginning with a minimum value of 1 or more, e.g., 1 to 6.1, and ending with a maximum value of 10 or less, e.g., 5.5 to 10.
The following aluminum alloys are described in terms of their elemental composition in weight percentage (wt. %) based on the total weight of the alloy. In certain examples of each alloy, the remainder is aluminum, with a maximum wt. % of 0.15% for the sum of the impurities.
Described herein are novel aluminum alloys and products that exhibit desirable mechanical properties. Among other properties, the aluminum alloys and products described herein display excellent elongation and forming properties and exceptional durability. In some cases, the mechanical properties can be achieved due to the elemental composition of the alloys. For example, the alloys described herein include iron (Fe), manganese (Mn), and chromium (Cr). The presence of at least two of these components, for example Fe and Mn, Fe and Cr, or Fe, Mn, and Cr, in the described amounts results in desirable intermetallic particles. As described below, an Fe content of at least about 0.50 wt. % provides an increased number of intermetallic particles during the casting process. In addition, other elements, such as Mn and/or Cr, influence the size and aspect ratio of the intermetallic particles and result in small, spherical particles having a low aspect ratio. The intermetallic particles, in turn, serve as nucleation sites for new grains, thus resulting in an aluminum alloy product containing small, equiaxial grains rather than coarse, elongated grains. Such aluminum alloy products exhibit desired forming properties. The properties displayed by the aluminum alloy products described herein are unexpected, as a high Fe content of about 0.20 wt. % and greater typically results in a decrease in formability and bendability.
In some cases, an aluminum alloy as described herein can have the following elemental composition as provided in Table 1.
In some examples, the aluminum alloy as described herein can have the following elemental composition as provided in Table 2.
In some examples, the aluminum alloy as described herein can have the following elemental composition as provided in Table 3.
In some examples, the aluminum alloy described herein includes silicon (Si) in an amount of from about 0.5% to about 2.0% (e.g., from about 0.7 to about 1.5% or from about 1.0 to about 1.4%) based on the total weight of the alloy. For example, the alloy can include 0.5%, 0.51%, 0.52%, 0.53%, 0.54%, 0.55%, 0.56%, 0.57%, 0.58%, 0.59%, 0.6%, 0.61%, 0.62%, 0.63%, 0.64%, 0.65%, 0.66%, 0.67%, 0.68%, 0.69%, 0.7%, 0.71%, 0.72%, 0.73%, 0.74%, 0.75%, 0.76%, 0.77%, 0.78%, 0.79%, 0.8%, 0.81%, 0.82%, 0.83%, 0.84%, 0.85%, 0.86%, 0.87%, 0.88%, 0.89%, 0.9%, 0.91%, 0.92%, 0.93%, 0.94%, 0.95%, 0.96%, 0.97%, 0.98%, 0.99%, 1.0%, 1.01%, 1.02%, 1.03%, 1.04%, 1.05%, 1.06%, 1.07%, 1.08%, 1.09%, 1.1%, 1.11%, 1.12%, 1.13%, 1.14%, 1.15%, 1.16%, 1.17%, 1.18%, 1.19%, 1.2%, 1.21%, 1.22%, 1.23%, 1.24%, 1.25%, 1.26%, 1.27%, 1.28%, 1.29%, 1.3%, 1.31%, 1.32%, 1.33%, 1.34%, 1.35%, 1.36%1.37%1.38%1.39%, 1.4%, 1.41%, 1.42%, 1.43%, 1.44%, 1.45%, 1.46%, 1.47%, 1.48%, 1.49%, 1.5%, 1.51%, 1.52%, 1.53%, 1.54%, 1.55%, 1.56%, 1.57%, 1.58%, 1.59%, 1.6%, 1.61%, 1.62%, 1.63%, 1.64%, 1.65%, 1.66%, 1.67%, 1.68%, 1.69%, 1.7%, 1.71%, 1.72%, 1.73%, 1.74%, 1.75%, 1.76%, 1.77%, 1.78%, 1.79%, 1.8%, 1.81%, 1.82%, 1.83%, 1.84%, 1.85%, 1.86%, 1.87%, 1.88%, 1.89%, 1.9%, 1.91%, 1.92%, 1.93%, 1.94%, 1.95%, 1.96%, 1.97%, 1.98%, 1.99%, or 2.0% Si. All expressed in wt. %.
In some examples, the aluminum alloy described herein includes iron (Fe) in an amount of from about 0.2% to about 0.4% (e.g., from about 0.2% to about 0.35%, from about 0.2% to about 0.3%, from about 0.2% to about 0.28%, or from about 0.22% to about 0.28%) based on the total weight of the alloy. For example, the alloy can include 0.2%, 0.21%, 0.22%, 0.23%, 0.24%, 0.25%, 0.26%, 0.27%, 0.28%, 0.29%, 0.3%, 0.31%, 0.32%, 0.33%, 0.34%, 0.35%, 0.36%, 0.37%, 0.38%, 0.39%, or 0.4% Fe. All expressed in wt. %.
In some examples, the aluminum alloy described herein includes copper (Cu) in an amount of up to about 0.4% (e.g., from 0.0% to about 0.35% or from 0.0% to about 0.15%) based on the total weight of the alloy. For example, the alloy can include 0.01%, 0.02%, 0.03%, 0.04%, 0.05%, 0.06%, 0.07%, 0.08%, 0.09%, 0.1%, 0.11%, 0.12%, 0.13%, 0.14%, 0.15%, 0.16%, 0.17%, 0.18%, 0.19%, 0.2%, 0.21%, 0.22%, 0.23%, 0.24%, 0.25%, 0.26%, 0.27%, 0.28%, 0.29%, 0.3%, 0.31%, 0.32%, 0.33%, 0.34%, 0.35%, 0.36%, 0.37%, 0.38%, 0.39%, or 0.4% Cu. In some cases, Cu is not present in the alloy (i.e., 0%). All expressed in wt. %.
In some examples, the aluminum alloy described herein includes magnesium (Mg) in an amount of up to about 0.5% (e.g., from 0.0% to about 0.5%, from 0.0% to about 0.4%, from 0.0% to about 0.35%, from about 0.1% to about 0.5%, or from about 0.2% to about 0.35%) based on the total weight of the alloy. For example, the alloy can include 0.01%, 0.02%, 0.03%, 0.04%, 0.05%, 0.06%, 0.07%, 0.08%, 0.09%, 0.1%, 0.11%, 0.12%, 0.13%, 0.14%, 0.15%, 0.16%, 0.17%, 0.18%, 0.19%, 0.2%, 0.21%, 0.22%, 0.23%, 0.24%, 0.25%, 0.26%, 0.27%, 0.28%0.29%, 0.3%, 0.31%, 0.32%, 0.33%, 0.34%, 0.35%, 0.36%, 0.37%, 0.38%, 0.39%, 0.4%, 0.41%, 0.42%, 0.43%, 0.44%, 0.45%, 0.46%, 0.47%, 0.48%, 0.49%, or 0.5% Mg. In some cases, Mg is not present in the alloy (i.e., 0%). All expressed in wt. %.
In some examples, the aluminum alloy described herein includes manganese (Mn) in an amount of from about 0.02% to about 0.1% (e.g., from about 0.02% to about 0.08% or from about 0.02% to about 0.06%) based on the total weight of the alloy. For example, the alloy can include 0.02%, 0.03%, 0.04%, 0.05%, 0.06%, 0.07%, 0.08%, 0.09%, or 0.1% Mn. All expressed in wt. %.
In some examples, the aluminum alloy described herein includes chromium (Cr) in an amount of from about 0.01% to about 0.1% (e.g., from about 0.02 to about 0.1%, from about 0.02% to about 0.08%, or from about 0.02% to about 0.06%) based on the total weight of the alloy. For example, the alloy can include 0.01%, 0.02%, 0.03%, 0.04%, 0.05%, 0.06%, 0.07%, 0.08%, 0.09%, or 0.1% Cr. All expressed in wt. %.
In some examples, the aluminum alloy described herein includes strontium (Sr) in an amount of up to about 0.15% (e.g., from 0.0% to about 0.15%, from about 0.02% to about 0.15%, from about 0.02% to about 0.10%, or from about 0.02% to about 0.14%) based on the total weight of the alloy. For example, the alloy can include 0.01%, 0.02%, 0.03%, 0.04%, 0.05%, 0.06%, 0.07%, 0.08%, 0.09%, 0.1%, 0.11%, 0.12%, 0.13%, 0.14%, or 0.15% Sr. In some cases, Sr is not present in the alloy (i.e., 0%). All expressed in wt. %. In some cases, adding Sr to the aluminum alloy described herein can further increase the formability and ductility of the material. Not to be bound by theory, the increase in formability can be due to the eutectic modification of the intermetallic particles that can reduce the lamellar spacing within the eutectic component during casting and solidification of the aluminum alloy. Thus, Sr modification of the eutectic component can allow the intermetallic particles to break apart into smaller and/or finer intermetallic particles during, for example, a hot rolling process. Finally, the finer intermetallic particles can reduce the tendency of the aluminum alloy to undergo internal damage during deformation (e.g., forming), thereby improving the formability of the aluminum alloy.
Optionally, the aluminum alloy described herein can include one or both of titanium (Ti) and zinc (Zn). In some examples, the aluminum alloy described herein includes Ti in an amount up to about 0.1% (e.g., from about 0.001% to about 0.08% or from about 0.005% to about 0.06%) based on the total weight of the alloy. For example, the alloy can include 0.001%, 0.002%, 0.003%, 0.004%, 0.005%, 0.006%, 0.007%, 0.008%, 0.009%, 0.01%, 0.02%, 0.03%, 0.04%, 0.05%, 0.06%, 0.07%, 0.08%, 0.09%, or 0.1% Ti. In some cases, Ti is not present in the alloy (i.e., 0%). In some examples, the aluminum alloy described herein includes Zn in an amount up to about 0.1% (e.g., from about 0.001% to about 0.08% or from about 0.005% to about 0.06%) based on the total weight of the alloy. For example, the alloy can include 0.001%, 0.002%, 0.003%, 0.004%, 0.005%, 0.006%, 0.007%, 0.008%, 0.009%, 0.01%, 0.02%, 0.03%, 0.04%, 0.05%, 0.06%, 0.07%, 0.08%, 0.09%, or 0.1% Zn. In some cases, Zn is not present in the alloy (i.e., 0%). All expressed in wt. %.
As described above, the presence of Fe in an amount of at least about 0.2 wt. % and in combination with Cr is a factor that results in the desirable properties exhibited by aluminum alloy products described herein. Optionally, the combined content of Fe and Cr is at least about 0.22 wt. %. In some cases, the combined content of Fe and Cr can be from about 0.22 wt. % to about 0.5 wt. %, from about 0.22 wt. % to about 0.4 wt. %, or from about 0.25 wt. % to about 0.35 wt. %. For example, the combined content of Fe and Cr can be 0.22%, 0.23%, 0.24%, 0.25%, 0.26%, 0.27%0.28%0.29%, 0.3%, 0.31%, 0.32%, 0.33%, 0.34%, 0.35%, 0.36%, 0.37%, 0.38%, 0.39%, 0.4%, 0.41%, 0.42%, 0.43%, 0.44%, 0.45%, 0.46%, 0.47%, 0.48%, 0.49%, or 0.5%. All expressed in wt. %.
Optionally, the aluminum alloys described herein can further include other minor elements, sometimes referred to as impurities, in amounts of 0.05% or below, 0.04% or below, 0.03% or below, 0.02% or below, or 0.01% or below. These impurities may include, but are not limited to V, Ni, Sc, Hf, Zr, Sn, Ga, Ca, Bi, Na, Pb, or combinations thereof. Accordingly, V, Ni, Sc, Hf, Zr, Sn, Ga, Ca, Bi, Na, or Pb may be present in alloys in amounts of 0.05% or below, 0.04% or below, 0.03% or below, 0.02% or below, or 0.01% or below. The sum of all impurities does not exceed 0.15% (e.g., 0.1%). All expressed in wt. %. The remaining percentage of each alloy is aluminum.
The aluminum alloy products described herein include iron-containing intermetallic particles. In some cases, the iron-containing intermetallic particles are spherical. For example, at least about 36% of the iron-containing intermetallic particles are spherical (e.g., at least about 40%, at least about 50%, at least about 60%, at least about 70%, at least about 80%, or at least about 90% of the iron-containing intermetallic particles are spherical). At least about 36% of the particles present in the aluminum alloy products have a particle size, measured by equivalent circular diameter (i.e., “ECD”), of about 3 μm or less (e.g., about 2.5 μm or less, about 2.0 μm or less, about 1.5 μm or less, or about 1.2 μm or less). The ECD can be determined by imposing an estimated circular cross-section on a non-spherical measured object. For example, the iron-containing intermetallic particles present in the aluminum alloy products can have an ECD of 3 μm or less, 2.9 μm or less, 2.8 μm or less, 2.7 μm or less, 2.6 μm or less, 2.5 μm or less, 2.4 μm or less, 2.3 μm or less, 2.2 μm or less, 2.1 μm or less, 2 μm or less, 1.9 μm or less, 1.8 μm or less, 1.7 μm or less, 1.6 μm or less, 1.5 μm or less, 1.4 μm or less, 1.3 μm or less, 1.2 μm or less, 1.1 μm or less, 1 μm or less, 0.9 μm or less, 0.8 μm or less, 0.7 μm or less, 0.6 μm or less, 0.5 μm or less, 0.4 μm or less, 0.3 μm or less, 0.2 μm or less, 0.1 μm or less, or anywhere in between. In some cases, at least 45%, at least 50%, at least 55%, at least 60%, at least 65%, at least 70%, at least 75%, at least 80%, at least 85%, at least 90%, at least 95%, or at least 99% of the particles present in the aluminum alloy products have an ECD of 3 μm or less.
In some non-limiting examples, the iron-containing intermetallic particles described herein comprise α-AlFe(Mn,Cr)Si intermetallic particles. The a-AlFe(Mn,Cr)Si intermetallic particles can be spherical particles. The aluminum alloys described herein having such spherical type intermetallic particles are amenable to forming (e.g., bending, shaping, stamping, or any suitable forming method) when compared to aluminum alloys that predominantly include β-AlFeSi intermetallic particles. The β-AlFeSi intermetallic particles typically have an elongated, needle-like shape. Such needle-like intermetallic particles are detrimental to forming and thus problematic when creating aluminum alloy parts from recycled aluminum alloys.
Introducing Cr in the concentrations described above (e.g., from about 0.01 wt. % to about 0.1 wt. %) into the aluminum alloy in a molten stage during production of a primary aluminum alloy) and/or recycling (e.g., by melting scrap aluminum alloys and optionally adding primary aluminum alloys) can allow the Cr to interact with any excess Fe found in the aluminum alloy (e.g., the molten alloy containing the primary aluminum alloy and the molten scrap) and provide the α-AlFe(Mn,Cr)Si intermetallic particles, thus replacing the β-AlFeSi intermetallic particles. Accordingly, replacing β-AlFeSi intermetallic particles with α-AlFe(Mn,Cr)Si intermetallic particles provides aluminum alloys that demonstrate high formability and durability. In some cases, at least about 36% of the iron-containing intermetallic particles in the aluminum alloys described herein are α-AlFe(Mn,Cr)Si intermetallic particles. For example, at least 36%, at least 40%, at least 45%, at least 50%, at least 55%, at least 60%, at least 65%, at least 70%, at least 75%, at least 80%, at least 85%, at least 90%, at least 95%, or at least 99% of the iron-containing intermetallic particles in the aluminum alloys described herein are α-AlFe(Mn,Cr)Si intermetallic particles.
In some cases, adding Cr as described herein can increase an amount of recycled content when providing the aluminum alloys. The aluminum alloys described herein can contain at least about 40 wt. % recycled content. For example, the aluminum alloys can contain at least about 45 wt. %, at least about 50 wt. %, at least about 60 wt. %, at least about 70 wt. %, at least about 80 wt. %, at least about 90 wt. %, or at least about 95 wt. % recycled content.
In some examples, the iron-containing intermetallic particles can be present in the aluminum alloy in an average amount of at least about 2000 to about 3000 particles per square millimeter (mm2). For example, the average amount of iron-containing intermetallic particles can be about 2000 particles/mm2, 2100 particles/mm2, 2200 particles/mm2, 2300 particles/mm2, 2400 particles/mm2, 2500 particles/mm2, 2600 particles/mm2, 2700 particles/mm2, 2800 particles/mm2, 2900 particles/mm2, 3000 particles/mm2, or anywhere in between.
As described above, the intermetallic particles in the aluminum alloys can serve as nucleation sites for grains. The aluminum alloys and products including the aluminum alloys can include grains having an average grain size of up to about 35 μm (e.g., from about 5 μm to about 35 μm, from about 25 μm to about 35 μm, or from about 28 μm to about 32 μm). For example, the average grain size can be about 1 μm, 5 μm, 10 μm, 15 μm, 20 μm, 25 μm, 30 μm, 35 μm, or anywhere in between.
In some cases, the aluminum alloy products can have a total elongation of at least about 27% and up to about 40% when in, for example, a T4 temper. For example, the aluminum alloy products can have a total elongation of about 27%, 28%, 29%, 30%, 31%, 32%, 33%, 34%, 35%, 36%, 37%, 38%, 39%, or 40%, or anywhere in between.
In some cases, the aluminum alloy products can have a uniform elongation of at least about 20% and up to about 30% when in, for example, a T4 temper. For example, the aluminum alloy products can have a uniform elongation of about 20%, 21%, 22%, 23%, 24%, 25%, 26%, 27%, 28%, 29%, or 30%, or anywhere in between.
In some examples, the aluminum alloy products have a yield strength of about 100 MPa or greater when in, for example, a T4 temper. For example, the aluminum alloy products can have a yield strength of 105 MPa or greater, 110 MPa or greater, 115 MPa or greater, 120 MPa or greater, 125 MPa or greater, 130 MPa or greater, 135 MPa or greater, 140 MPa or greater, 145 MPa or greater, or 150 MPa or greater. In some cases, the yield strength is from about 100 MPa to about 150 MPa (e.g., from about 105 MPa to about 145 MPa, from about 110 MPa to about 140 MPa, or from about 115 MPa to about 135 MPa).
In some examples, the aluminum alloy products have an ultimate tensile strength of about 200 MPa or greater when in, for example, a T4 temper. For example, the aluminum alloy products can have an ultimate tensile strength of 205 MPa or greater, 210 MPa or greater, 215 MPa or greater, 220 MPa or greater, 225 MPa or greater, 230 MPa or greater, 235 MPa or greater, 240 MPa or greater, 245 MPa or greater, or 250 MPa or greater. In some cases, the ultimate tensile strength is from about 200 MPa to about 250 MPa (e.g., from about 205 MPa to about 245 MPa, from about 210 MPa to about 240 MPa, or from about 215 MPa to about 235 MPa).
The aluminum alloy products include at least a first surface portion having a plurality of crystallographic texture components. The crystallographic texture components can include recrystallization texture components (e.g., a GOSS component, a Cube component, and Rotated Cube (RC) components including an RCRD1 component, an RCRD2 component, an RCRN1 component, and an RCRN2 component). The crystallographic texture components can also include deformation texture components (e.g., a Brass (Bs) component, an S component, a Copper component, a Shear 1 component, a Shear 2 component, a Shear 3 component, a P component, a Q component, and an R component).
In some examples, the aluminum alloy products can include a Cube component. Optionally, a volume fraction of the Cube component in the aluminum alloy products can be at least about 12% (e.g., at least about 13%, at least about 14%, at least about 15%, at least about 16%, at least about 17%, or at least about 18%). In some examples, the volume fraction of the Cube component in the aluminum alloy products is up to about 20% (e.g., up to about 15% or up to about 10%). For example, the volume fraction of the Cube component in the aluminum alloy products can range from about 12% to about 20% (e.g., from about 13% to about 20% or from about 16% to about 18%).
In some examples, the aluminum alloy products can include a Brass component, an S component, a Copper component, and a GOSS component. Optionally, a volume fraction of any one of the Brass, S, Copper, or GOSS components in the aluminum alloy products can be lower than about 5% (e.g., lower than about 4%, lower than about 3%, lower than about 2%, or lower than about 1%). For example, the volume fraction of any one of the Brass, S, Copper, or GOSS components in the aluminum alloy products can be from about 1% to about 5%, from about 1.5% to about 4.5%, or from about 2% to about 4%.
Aluminum alloy properties are partially determined by the formation of microstructures during the alloy's preparation. In certain aspects, the method of preparation for an alloy composition may influence or even determine whether the alloy will have properties adequate for a desired application.
Casting
The aluminum alloys as described herein can be cast into a cast aluminum alloy article using any suitable casting method. For example, the casting process can include a direct chill (DC) casting process or a continuous casting (CC) process. In some non-limiting examples, the aluminum alloys for use in the casting step can be a primary material produced from raw materials (e.g., purified aluminum and additional alloying elements). In some further examples, the aluminum alloys for use in the casting step can be a recycled material, produced at least in part by aluminum scrap and optionally in combination with a primary material. In some cases, aluminum alloys for use in the casting step can contain at least about 40% of recycled content. For example, the aluminum alloy for use in the casting step can contain at least about 45%, at least about 50%, at least about 60%, at least about 70%, at least about 80%, at least about 90%, or at least about 95% of recycled content.
The cast aluminum alloy article can then be subjected to further processing steps. For example, the processing methods as described herein can include the steps of homogenizing, hot rolling, cold rolling, and/or solution heat treating to form an aluminum alloy product.
Homogenization
The homogenization step as described herein was designed for the aluminum alloys described above. The aluminum alloys described herein have a high Si content (i.e., from 0.5 to 2.0 wt. %), which can lead to localized melting within the aluminum alloy matrix when homogenized at temperatures greater than about 550° C. (e.g., 560° C. and greater). Such localized melting can cause fracturing during downstream thermal processing steps. The homogenization step described herein is effective in dissolving any elemental Si and concurrently avoiding localized melting.
The homogenization step can include heating the cast aluminum alloy article to attain a temperature of about, or up to about, 570° C. (e.g., up to about 560° C., up to about 550° C., up to about 540° C., up to about 530° C., up to about 520° C., up to about 510° C., up to about 500° C., up to about 490° C., up to about 480° C., up to about 470° C., or up to about 460° C.). For example, the cast aluminum alloy article can be heated to a temperature of from about 460° C. to about 570° C. (e.g., from about 465° C. to about 570° C., from about 470° C. to about 570° C., from about 480° C. to about 570° C., from about 490° C. to about 570° C., from about 500° C. to about 570° C., from about 510° C. to about 570° C., from about 520° C. to about 570° C., from about 530° C. to about 570° C., from about 540° C. to about 570° C., or from about 550° C. to about 570° C.). In some cases, the heating rate can be about 100° C./hour or less, 75° C./hour or less, 50° C./hour or less, 40° C./hour or less, 30° C./hour or less, 25° C./hour or less, 20° C./hour or less, or 15° C./hour or less. In other cases, the heating rate can be from about 10° C./min to about 100° C./min (e.g., from about 10° C./min to about 90° C./min, from about 10° C./min to about 70° C./min, from about 10° C./min to about 60° C./min, from about 20° C./min to about 90° C./min, from about 30° C./min to about 80° C./min, from about 40° C./min to about 70° C./min, or from about 50° C./min to about 60° C./min).
The cast aluminum alloy article is then allowed to soak for a period of time. According to one non-limiting example, the cast aluminum alloy article is allowed to soak for up to about 15 hours (e.g., from about 20 minutes to about 15 hours or from about 5 hours to about 10 hours, inclusively). For example, the cast aluminum alloy article can be soaked at a temperature of from about 500° C. to about 550° C. for about 20 minutes, about 30 minutes, about 45 minutes, about 1 hour, about 1.5 hours, about 2 hours, about 3 hours, about 4 hours, about 5 hours, about 6 hours, about 7 hours, about 8 hours, about 9 hours, about 10 hours, about 11 hours, about 12 hours, about 13 hours, about 14 hours, about 15 hours, or anywhere in between.
Hot Rolling
Following the homogenization step, a hot rolling step can be performed. In certain cases, the cast aluminum alloy articles are laid down and hot-rolled with an entry temperature range of about 500° C. to 560° C. (e.g., from about 510° C. to about 550° C. or from about 520° C. to about 540° C.). The entry temperature can be, for example, about 505° C., 510° C., 515° C., 520° C., 525° C., 530° C., 535° C., 540° C., 545° C., 550° C., 555° C., 560° C., or anywhere in between. In certain cases, the hot roll exit temperature can range from about 200° C. to about 290° C. (e.g., from about 210° C. to about 280° C. or from about 220° C. to about 270° C.). For example, the hot roll exit temperature can be about 200° C., 205° C., 210° C., 215° C., 220° C., 225° C., 230° C., 235° C., 240° C., 245° C., 250° C., 255° C., 260° C., 265° C., 270° C., 275° C., 280° C., 285° C., 290° C., or anywhere in between.
In certain cases, the cast aluminum alloy article is hot rolled to an about 4 mm to about 15 mm gauge (e.g., from about 5 mm to about 12 mm gauge), which is referred to as a hot band. For example, the cast article can be hot rolled to a 15 mm gauge, a 14 mm gauge, a 13 mm gauge, a 12 mm gauge, a 11 mm gauge, a 10 mm gauge, a 9 mm gauge, an 8 mm gauge, a 7 mm gauge, a 6 mm gauge, a 5 mm gauge, or a 4 mm gauge. The temper of the as-rolled hot band is referred to as F-temper.
Coil Cooling
Optionally, the hot band can be coiled into a hot band coil (i.e., an intermediate gauge aluminum alloy product coil) upon exit from the hot mill. In some examples, the hot band is coiled into a hot band coil upon exit from the hot mill resulting in F-temper. In some further examples, the hot band coil is cooled in air. The air cooling step can be performed at a rate of about 12.5° C./hour (° C./h) to about 3600° C./h. For example, the coil cooling step can be performed at a rate of about 12.5° C./h, 25° C./h, 50° C./h, 100° C./h, 200° C./h, 400° C./h, 800° C./h, 1600° C./h, 3200° C./h, 3600° C./h, or anywhere in between. In some still further examples, the air cooled coil is stored for a period of time. In some examples, the intermediate coils are maintained at a temperature of about 100° C. to about 350° C. (for example, about 200° C. or about 300° C.).
Cold Rolling
A cold rolling step can optionally be performed before the solution heat treating step. In certain aspects, the hot band is cold rolled to a final gauge aluminum alloy product (e.g., a sheet). In some examples, the final gauge aluminum alloy sheet has a thickness of 4 mm or less, 3 mm or less, 2 mm or less, 1 mm or less, 0.9 mm or less, 0.8 mm or less, 0.7 mm or less, 0.6 mm or less, 0.5 mm or less, 0.4 mm or less, 0.3 mm or less, 0.2 mm or less, or 0.1 mm.
Optional Inter-Annealing
In some non-limiting examples, an optional inter-annealing step can be performed during cold rolling. For example, the hot band can be cold rolled to an intermediate cold roll gauge, annealed, and subsequently cold rolled to a final gauge. In some aspects, the optional inter-annealing can be performed in a batch process (i.e., a batch inter-annealing step). The inter-annealing step can be performed at a temperature of from about 300° C. to about 450° C. (e.g., about 310° C., about 320° C., about 330° C., about 340° C., about 350° C., about 360° C., about 370° C., about 380° C., about 390° C., about 400° C., about 410° C., about 420° C., about 430° C., about 440° C., or about 450° C.).
Solution Heat Treating
The solution heat treating step can include heating the final gauge aluminum alloy product from room temperature to a peak metal temperature. Optionally, the peak metal temperature can be from about 530° C. to about 570° C. (e.g., from about 535° C. to about 560° C., from about 545° C. to about 555° C., or about 540° C.). The final gauge aluminum alloy product can soak at the peak metal temperature for a period of time. In certain aspects, the final gauge aluminum alloy product is allowed to soak for up to approximately 2 minutes (e.g., from about 10 seconds to about 120 seconds inclusively). For example, the final gauge aluminum alloy product can be soaked at the temperature of from about 530° C. to about 570° C. for 10 seconds, 15 seconds, 20 seconds, 25 seconds, 30 seconds, 35 seconds, 40 seconds, 45 seconds, 50 seconds, 55 seconds, 60 seconds, 65 seconds, 70 seconds, 75 seconds, 80 seconds, 85 seconds, 90 seconds, 95 seconds, 100 seconds, 105 seconds, 110 seconds, 115 seconds, 120 seconds, or anywhere in between. After solution heat treating, the final gauge aluminum alloy product can be quenched from the peak metal temperature at a rate of at least about 75° C. per second (° C./s). For example, the final gauge aluminum alloy product can be quenched at a rate of about 75° C./s, 100° C./s, 125° C./s, 150° C./s, 175° C./s, 200° C./s, or anywhere in between.
Optionally, the aluminum alloy product can then be naturally aged and/or artificially aged. In some non-limiting examples, the aluminum alloy product can be naturally aged to a T4 temper by storing at room temperature (e.g., about 15° C., about 20° C., about 25° C., or about 30° C.) for at least 72 hours. For example, the aluminum alloy product can be naturally aged for 72 hours, 84 hours, 96 hours, 108 hours, 120 hours, 132 hours, 144 hours, 156 hours, 168 hours, 180 hours, 192 hours, 204 hours, 216 hours, 240 hours, 264 hours, 288 hours, 312 hours, 336 hours, 360 hours, 384 hours, 408 hours, 432 hours, 456 hours, 480 hours, 504 hours, 528 hours, 552 hours, 576 hours, 600 hours, 624 hours, 648 hours, 672 hours, or anywhere in between.
The alloys and methods described herein can be used in automotive and/or transportation applications, including motor vehicle, aircraft, and railway applications, or any other desired application. In some examples, the alloys and methods can be used to prepare motor vehicle body part products, such as safety cages, bodies-in-white, crash rails, bumpers, side beams, roof beams, cross beams, pillar reinforcements (e.g., A-pillars, B-pillars, and C-pillars), inner panels, outer panels, side panels, inner hoods, outer hoods, or trunk lid panels. The aluminum alloys and methods described herein can also be used in aircraft or railway vehicle applications, to prepare, for example, external and internal panels.
The alloys and methods described herein can also be used in electronics applications, to prepare, for example, external and internal encasements. For example, the alloys and methods described herein can also be used to prepare housings for electronic devices, including mobile phones and tablet computers. In some examples, the alloys can be used to prepare housings for the outer casing of mobile phones (e.g., smart phones) and tablet bottom chassis.
Illustration 1 is an aluminum alloy, comprising about 0.5 to 2.0 wt. % Si, 0.2 to 0.4 wt. % Fe, up to 0.4 wt. % Cu, up to 0.5 wt. % Mg, 0.02 to 0.1 wt. % Mn, 0.01 to 0.1 wt. % Cr, up to 0.15 wt. % Sr, up to 0.15 wt. % impurities, and Al.
Illustration 2 is the aluminum alloy of any preceding or subsequent illustration, comprising about 0.7 to 1.4 wt. % Si, 0.2 to 0.3 wt. % Fe, up to 0.2 wt. % Cu, up to 0.4 wt. % Mg, 0.02 to 0.08 wt. % Mn, 0.02 to 0.05 wt. % Cr, 0.01 to 0.12 wt. % Sr, up to 0.15 wt. % impurities, and Al.
Illustration 3 is the aluminum alloy of any preceding or subsequent illustration, comprising about 1.0 to 1.4 wt. % Si, 0.22 to 0.28 wt. % Fe, up to 0.15 wt. % Cu, up to 0.35 wt. % Mg, 0.02 to 0.06 wt. % Mn, 0.02 to 0.04 wt. % Cr, 0.02 to 0.10 wt. % Sr, up to 0.15 wt. % impurities, and Al.
Illustration 4 is the aluminum alloy of any preceding or subsequent illustration, wherein a combined content of Fe and Cr is from about 0.22 wt. % to 0.50 wt. %.
Illustration 5 is an aluminum alloy product, comprising the aluminum alloy according to any preceding or subsequent illustration.
Illustration 6 is the aluminum alloy product of any preceding or subsequent illustration, wherein the aluminum alloy product comprises a grain size of up to about 35 μm.
Illustration 7 is the aluminum alloy product of any preceding or subsequent illustration, wherein the grain size is from about 25 μm to about 35 μm.
Illustration 8 is the aluminum alloy product of any preceding or subsequent illustration, comprising iron-containing intermetallic particles.
Illustration 9 is the aluminum alloy product of any preceding or subsequent illustration, wherein at least about 36% of the iron-containing intermetallic particles are spherical.
Illustration 10 is the aluminum alloy product of any preceding or subsequent illustration, wherein at least about 36% of the iron-containing intermetallic particles present in the aluminum alloy product have an equivalent circular diameter of about 3 μm or less.
Illustration 11 is the aluminum alloy product of any preceding or subsequent illustration, wherein at least about 50% of the iron-containing intermetallic particles present in the aluminum alloy product have an equivalent circular diameter of about 3 μm or less.
Illustration 12 is the aluminum alloy product of any preceding or subsequent illustration, wherein at least about 75% of the iron-containing intermetallic particles present in the aluminum alloy product have an equivalent circular diameter of about 3 μm or less.
Illustration 13 is the aluminum alloy product of any preceding or subsequent illustration, wherein at least about 36% of the iron-containing intermetallic particles comprise α-AlFe(Mn,Cr)Si intermetallic particles.
Illustration 14 is the aluminum alloy product of any preceding or subsequent illustration, wherein at least about 50% of the iron-containing intermetallic particles comprise α-AlFe(Mn,Cr)Si intermetallic particles.
Illustration 15 is the aluminum alloy product of any preceding or subsequent illustration, wherein at least about 80% of the iron-containing intermetallic particles comprise α-AlFe(Mn,Cr)Si intermetallic particles.
Illustration 16 is the aluminum alloy product of any preceding or subsequent illustration, wherein a volume fraction of a cube textural component in the aluminum alloy product comprises at least about 12%.
Illustration 17 is the aluminum alloy product of any preceding or subsequent illustration, wherein the aluminum alloy product comprises a total elongation of at least about 32%.
Illustration 18 is the aluminum alloy product of any preceding or subsequent illustration, wherein the aluminum alloy product comprises an automobile body part.
Illustration 19 is a method of producing an aluminum alloy product, comprising: casting an aluminum alloy according to any preceding or subsequent illustration to produce a cast aluminum alloy article; homogenizing the cast aluminum alloy article to produce a homogenized cast aluminum alloy article; hot rolling and cold rolling the homogenized cast aluminum alloy article to produce a final gauge aluminum alloy product; and solution heat treating the final gauge aluminum alloy product.
Illustration 20 is the method of any preceding or subsequent illustration, wherein the homogenizing is performed at a homogenization temperature of from about 530° C. to about 570° C.
Illustration 21 is the method of any preceding illustration, wherein the aluminum alloy in the casting comprises a recycled content in an amount of at least about 40 wt. %.
The following examples will serve to further illustrate the present invention without, however, constituting any limitation thereof. On the contrary, it is to be clearly understood that resort may be had to various embodiments, modifications, and equivalents thereof which, after reading the description herein, may suggest themselves to those skilled in the art without departing from the spirit of the invention.
Aluminum alloy products were prepared having the compositions as shown in Table 4:
In Table 4, all values are weight percent (wt. %) of the whole. The alloys can contain up to 0.15 wt. % total impurities and the remainder is aluminum. Alloy 1 is a highly recyclable aluminum alloy as described herein, containing 0.26 wt. % Fe and 0.025 wt. % Cr. Alloy 2, Alloy 3, and Alloy 4 are comparative 6xxx series aluminum alloys.
Alloy 1 and Alloy 2 were each processed by a method without a batch inter-annealing step (referred to herein as “no BA”), with a batch inter-annealing step (referred to herein as “BA”), and by a process with a coil cooling step (referred to herein as “CC”).
All patents, publications, and abstracts cited above are incorporated herein by reference in their entireties. Various embodiments of the invention have been described in fulfillment of the various objectives of the invention. It should be recognized that these embodiments are merely illustrative of the principles of the present invention. Numerous modifications and adaptions thereof will be readily apparent to those skilled in the art without departing from the spirit and scope of the present invention as defined in the following claims.
The present application claims priority to and filing benefit of U.S. Provisional Patent Application No. 62/701,977, filed on Jul. 23, 2018, and U.S. Provisional Patent Application No. 62/810,585, filed on Feb. 26, 2019, which are incorporated herein by reference in their entireties.
Number | Date | Country | |
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62701977 | Jul 2018 | US | |
62810585 | Feb 2019 | US |