WO2019083969A1 - Alliages d'aluminium de haute résistance et de haute aptitude au formage leurs procédés de fabrication - Google Patents

Alliages d'aluminium de haute résistance et de haute aptitude au formage leurs procédés de fabrication

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Publication number
WO2019083969A1
WO2019083969A1 PCT/US2018/057054 US2018057054W WO2019083969A1 WO 2019083969 A1 WO2019083969 A1 WO 2019083969A1 US 2018057054 W US2018057054 W US 2018057054W WO 2019083969 A1 WO2019083969 A1 WO 2019083969A1
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WO
WIPO (PCT)
Prior art keywords
aluminum alloy
alloy
alloy product
alloys
stage homogenization
Prior art date
Application number
PCT/US2018/057054
Other languages
English (en)
Inventor
Sazol Kumar DAS
Aude Despois
Rajeev G. Kamat
Original Assignee
Novelis Inc.
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Novelis Inc. filed Critical Novelis Inc.
Priority to JP2020519667A priority Critical patent/JP2020537039A/ja
Priority to EP18797512.3A priority patent/EP3676410B1/fr
Priority to CN201880068803.7A priority patent/CN111247260A/zh
Priority to MX2020003528A priority patent/MX2020003528A/es
Priority to ES18797512T priority patent/ES2955293T3/es
Publication of WO2019083969A1 publication Critical patent/WO2019083969A1/fr
Priority to JP2022136728A priority patent/JP2022172234A/ja
Priority to JP2023181583A priority patent/JP2024010058A/ja

Links

Classifications

    • 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
    • C22F1/043—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 silicon as the next major constituent
    • 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
    • C22C21/02—Alloys based on aluminium with silicon as the next major constituent
    • 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
    • C22C21/02—Alloys based on aluminium with silicon as the next major constituent
    • C22C21/04—Modified aluminium-silicon alloys
    • 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
    • C22C21/06—Alloys based on aluminium with magnesium as the next major constituent
    • C22C21/08—Alloys based on aluminium with magnesium as the next major constituent with silicon
    • 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
    • C22F1/05—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 of the Al-Si-Mg type, i.e. containing silicon and magnesium in approximately equal proportions

Definitions

  • the present disclosure relates to the fields of material science, materials chemistry, metal manufacturing, aluminum alloys, and aluminum manufacturing.
  • the present disclosure relates to high-strength and highly formable aluminum alloys and methods of making and processing the same.
  • Aluminum alloys can exhibit high strength due, in part, to the elemental content of the alloys.
  • high strength 6xxx series aluminum alloys can be prepared by including high concentrations of certain elements, such as magnesium (Mg), silicon (Si), and/or copper (Cu).
  • Mg magnesium
  • Si silicon
  • Cu copper
  • such aluminum alloys containing high concentrations of these elements display poor formability properties.
  • precipitates can form along grain boundaries in an aluminum matrix. Precipitate formation along grain boundaries can increase strength in the alloy but negatively affect alloy deformation (e.g., reduce bendability, formability, or any suitable desired deformation).
  • the alloys can exhibit reduced yield strength after artificial aging.
  • aluminum alloys comprising about 0.8 - 1.5 wt. % Si, 0.1 - 0.5 wt. % Fe, 0.5 - 1.0 wt. % Cu, 0.5 - 0.9 wt. % Mg, up to 0.1 wt. % Ti, up to 0.5 wt. % Mn, up to 0.5 wt. % Cr, up to 0.5 wt. % Zr, up to 0.5 wt. % V, up to 0.15 wt. % impurities, and Al.
  • the aluminum alloys can comprise about 0.9 - 1.4 wt. % Si, 0.1 - 0.35 wt.
  • the aluminum alloys can comprise about 1.0 - 1.3 wt. % Si, 0.1 - 0.25 wt. % Fe, 0.7 - 0.9 wt. % Cu, 0.6 - 0.8 wt. % Mg, 0.01 - 0.05 wt.
  • the aluminum alloy comprises at least one of Mn, Cr, Zr, and V.
  • a combined content of Mn, Cr, Zr, and/or V is at least about 0.14 wt. % (e.g., from about 0.14 wt. % to about 0.4 wt. % or from about 0.15 wt. % to about 0.25 wt. %).
  • the aluminum alloy comprises about 0.01 - 0.3 wt. % V.
  • the aluminum alloy comprises excess Si and the excess Si content is from about 0.01 to about 1.0.
  • the aluminum alloy products comprising the aluminum alloy as described herein.
  • the aluminum alloy products comprise a rotated cube crystallographic texture at a volume percent of at least about 5 %.
  • the aluminum alloy products can comprise dispersoids.
  • the dispersoids are present in the aluminum alloy in an amount of at least about 1,500,000 dispersoids per mm 2 .
  • the dispersoids occupy an area ranging from about 0.5 % to about 5 % of the aluminum alloy products.
  • the aluminum alloy products comprises Fe-constituents.
  • the Fe-constituents can comprise Al(Fe,X)Si phase particles.
  • the average particle size of the Fe-constituents is up to about 4 ⁇ .
  • the aluminum alloy products can exhibit a yield strength of at least about 300 MPa when in a T6 temper and/or a uniform elongation of at least about 20 % and a minimum bend angle of at least about 120° when in a T4 temper.
  • the methods comprise casting an aluminum alloy as described herein to provide a cast article, homogenizing the cast article in a two-stage homogenization process, hot rolling and cold rolling the cast article to provide a final gauge aluminum alloy product, solution heat treating the final gauge aluminum alloy product, and pre-aging the final gauge aluminum alloy product.
  • the two-stage homogenization process can comprise heating the cast article to a first stage homogenization temperature and holding the cast article at the first stage homogenization temperature for a period of time and further heating the cast article to a second stage homogenization temperature and holding the cast article at the second stage homogenization temperature for a period of time.
  • the first stage homogenization temperature is from about 470 °C to about 530 °C and the second stage homogenization temperature is from about 525 °C to about 575 °C. In some examples, the second stage homogenization temperature is higher than the first stage homogenization temperature.
  • Figure 1 is a graph showing tensile properties of aluminum alloys according to certain aspects of the present disclosure.
  • Figure 2 is a micrograph showing the grain structure of aluminum alloys according to certain aspects of the present disclosure.
  • Figure 3 is a graph showing mechanical properties of aluminum alloys according to certain aspects of the present disclosure.
  • Figure 4 is a graph showing mechanical properties of aluminum alloys according to certain aspects of the present disclosure.
  • Figure 5 is a graph showing mechanical properties of aluminum alloys according to certain aspects of the present disclosure.
  • Figure 6 is a graph showing the distribution of recrystallization textures of aluminum alloys according to certain aspects of the present disclosure.
  • Figure 7 is a series of micrographs of aluminum alloys according to certain aspects of the present disclosure.
  • Figure 8 is a graph showing dispersoid number density and dispersoid area fraction of aluminum alloys according to certain aspects of the present disclosure.
  • Figure 9 is a series of micrographs of aluminum alloys according to certain aspects of the present disclosure.
  • Figure 10 is a graph showing size distribution of Fe-constituents of aluminum alloys according to certain aspects of the present disclosure.
  • Figure 11 is a series of micrographs of aluminum alloys according to certain aspects of the present disclosure.
  • Described herein are novel aluminum alloys and products and methods of preparing the same.
  • the alloys exhibit high strength and high formability.
  • solute elements including Cu, Mg, and Si
  • transition elements e.g., Mn, Cr, Zn, and V
  • the transition elements aid in preventing precipitate formation along grain boundaries in the aluminum alloys, as further described below.
  • the processing methods used to prepare the alloys and products contribute to the high strength and formability exhibited by the alloys and products.
  • alloys identified by aluminum industry designations such as “series” or “AA6xxx .”
  • series or “AA6xxx ”
  • AA6xxx AA6xxx
  • 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.
  • a plate generally has a thickness of greater than about 15 mm.
  • a plate may refer to an aluminum product having a thickness of greater than 15 mm, greater than 20 mm, greater than 25 mm, greater than 30 mm, greater than 35 mm, greater than 40 mm, greater than 45 mm, greater than 50 mm, or greater than 100 mm.
  • a shate (also referred to as a sheet plate) generally has a thickness of from about 4 mm to about 15 mm.
  • a shate may have a thickness of 4 mm, 5 mm, 6 mm, 7 mm, 8 mm, 9 mm, 10 mm, 11 mm, 12 mm, 13 mm, 14 mm, or 15 mm.
  • a sheet generally refers to an aluminum alloy product having a thickness of less than about 4 mm.
  • a sheet may have a thickness of less than 4 mm, less than 3 mm, less than 2 mm, less than 1 mm, less than 0.5 mm, less than 0.3 mm, or less than 0.1 mm.
  • cast metal article As used herein, terms such as "cast metal article,” “cast article,” “cast aluminum alloy,” 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.
  • 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 TI 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.
  • 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.
  • novel aluminum alloys exhibit high strength and high formability. In some cases, the properties of the alloys can be achieved due to the elemental composition of the alloys.
  • the aluminum alloys can be precipitation hardened or precipitation hardenable alloys.
  • the aluminum alloys can be aluminum alloys classified as 2xxx series aluminum alloys (e.g., wherein copper is a predominant alloying element), 6xxx series aluminum alloys (e.g., wherein magnesium and silicon are predominant alloying elements), or 7xxx series aluminum alloys (e.g., wherein zinc is a predominant alloying element). In some cases, the aluminum alloys can be modified 2xxx series, 6xxx series, or 7xxx series aluminum alloys.
  • modified as related to a series of aluminum alloys refers to an alloy composition that would typically be classified within a particular series, but the modification of one or more elements (types or amounts) results in a different predominant alloying element.
  • a modified 6xxx series aluminum alloy can refer to an aluminum alloy in which copper and silicon are the predominant alloying elements rather than magnesium and silicon.
  • an aluminum alloy can have the following elemental composition as provided in Table 1 :
  • the alloy can have the following elemental composition as provided Table 2.
  • the alloy can have the following elemental composition ⁇
  • the alloy described herein includes silicon (Si) in an amount from about 0.8 % to about 1.5 % (e.g., from about 0.9 % to about 1.45 %, from about 0.9 % to about 1.4 %, from about 0.9 % to about 1.35 %, from about 0.9 % to about 1.3 %, from about 0.9 % to about 1.25 %, from about 0.9 % to about 1.2 %, from about 0.95 % to about 1.5 %, from about 0.95 % to about 1.45 %, from about 0.95 % to about 1.4 %, from about 0.95 % to about 1.35 %, from about 0.95 % to about 1.3 %, from about 0.95 % to about 1.25 %, from about 0.95 % to about 1.2 %, from about 1.0 % to about 1.5 %, from about 1.0 % to about 1.45 %, from about 1.0 % to about 1.4 %, from about 1.0 % to about 1.35 %, from
  • the alloy can include 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
  • the alloy described herein includes iron (Fe) in an amount from about 0.1 % to about 0.5 % (e.g., from about 0.1 % to about 0.45 %, from about 0.1 % to about 0.4 %, from about 0.1 % to about 0.35 %, from about 0.1 % to about 0.3 %, from about 0.1 % to about 0.25 %, from about 0.1 % to about 0.2 %, from about 0.15 % to about 0.45 %, from about 0.15 % to about 0.4 %, from about 0.15 % to about 0.35 %, from about 0.15 % to about 0.3 %, from about 0.15 % to about 0.25 %, from about 0.15 % to about 0.2 %, from about 0.2 % to about 0.45 %, from about 0.2 % to about 0.4 %, from about 0.2 % to about 0.35 %, from about 0.2 % to about 0.3 %, from about 0.2 % to about 0.45 %, from
  • the alloy can include 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 % Fe. All expressed in wt. %.
  • the alloy described herein includes copper (Cu) in an amount from about 0.5 % to about 1.0 % (e.g., from about 0.55 % to about 1.0 %, from about 0.6 % to about 1.0 %, from about 0.65 % to about 1.0 %, from about 0.7 % to about 1.0 %, from about 0.75 % to about 1.0 %, from about 0.8 % to about 1.0 %, from about 0.5 % to about 0.95 %, from about 0.55 % to about 0.95 %, from about 0.6 % to about 0.95 %, from about 0.65 % to about 0.95 %, from about 0.7 % to about 0.95 %, from about 0.75 % to about 0.95 %, from about 0.8 % to about 0.95 %, from about 0.5 % to about 0.9 %, from about 0.55 % to about 0.9 %, from about 0.6 % to about 0.9 %, from about 0.65 % to about 0.9 %, from about
  • 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 %,
  • the alloy described herein includes magnesium (Mg) in an amount from about 0.5 % to about 0.9 % (e.g., from about 0.55 % to about 0.9 %, from about 0.6 % to about 0.9 %, from about 0.65 % to about 0.9 %, from about 0.7 % to about 0.9 %, from about 0.75 % to about 0.9 %, from about 0.8 % to about 0.9 %, from about 0.5 % to about 0.85 %, from about 0.55 % to about 0.85 %, from about 0.6 % to about 0.85 %, from about 0.65 % to about 0.85 %, from about 0.7 % to about 0.85 %, from about 0.75 % to about 0.85 %, from about 0.8 % to about 0.85 %, from about 0.5 % to about 0.8 %, from about 0.55 % to about 0.8 %, from about 0.6 % to about 0.8 %, from about 0.65 % to about 0.8 %, from
  • 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 %, or 0.9 % Mg. All expressed in wt. %.
  • the alloy described herein includes titanium (Ti) in an amount up to about 0.1 % (e.g., from about 0.01 % to about 0.09 %, from about 0.02 % to about 0.09 %, from about 0.03 % to about 0.09 %, from about 0.04 % to about 0.09 %, from about 0.05 % to about 0.09 %, from about 0.01 % to about 0.08 %, from about 0.02 % to about 0.08 %, from about 0.03 % to about 0.08 %, from about 0.04 % to about 0.08 %, from about 0.05 % to about 0.08 %, from about 0.01 % to about 0.07 %, from about 0.02 % to about 0.07 %, from about 0.03 % to about 0.07 %, from about 0.04 % to about 0.07 %, from about 0.05 % to about 0.07 %, from about 0.01 % to about 0.06 %, from about 0.02 % to about 0.06 %, from about 0.02 %
  • 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 % Ti.
  • Ti is not present in the alloy (i.e., 0 % Ti). All expressed in wt. %.
  • the alloy described herein includes manganese (Mn) in an amount up to about 0.5 % (e.g., from about 0.01 % to about 0.5 %, from about 0.01 % to about 0.4 %, from about 0.01 % to about 0.3 %, from about 0.01 % to about 0.2 %, from about 0.01 % to about 0.1 %, from about 0.06 % to about 0.5 %, from about 0.06 % to about 0.4 %, from about 0.06 % to about 0.3 %, from about 0.06 % to about 0.2 %, from about 0.06 % to about 0.1 %, from about 0.1 % to about 0.5 %, from about 0.1 % to about 0.4 %, from about 0.1 % to about 0.3 %, or from about 0.1 % to about 0.2 %) based on the total weight of the alloy.
  • Mn manganese
  • 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
  • the alloy described herein includes chromium (Cr) in an amount up to about 0.5 % (e.g., from about 0.01 % to about 0.5 %, from about 0.01 % to about 0.4 %, from about 0.01 % to about 0.3 %, from about 0.01 % to about 0.2 %, from about 0.01 % to about 0.1 %, from about 0.06 % to about 0.5 %, from about 0.06 % to about 0.4 %, from about 0.06 % to about 0.3 %, from about 0.06 % to about 0.2 %, from about 0.06 % to about 0.1 %, from about 0.1 % to about 0.5 %, from about 0.1 % to about 0.4 %, from about 0.1 % to about 0.3 %, or from about 0.1 % to about 0.2 %) based on the total weight of the alloy.
  • Cr chromium
  • 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
  • the alloy described herein includes zirconium (Zr) in an amount up to about 0.5 % (e.g., from about 0.01 % to about 0.5 %, from about 0.01 % to about 0.4 %, from about 0.01 % to about 0.3 %, from about 0.01 % to about 0.2 %, from about 0.01 % to about 0.1 %, from about 0.06 % to about 0.5 %, from about 0.06 % to about 0.4 %, from about 0.06 % to about 0.3 %, from about 0.06 % to about 0.2 %, from about 0.06 % to about 0.1 %, from about 0.1 % to about 0.5 %, from about 0.1 % to about 0.4 %, from about 0.1 % to about 0.3 %, or from about 0.1 % to about 0.2 %) based on the total weight
  • 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
  • the alloy described herein includes vanadium (V) in an amount up to about 0.5 % (e.g., from about 0.01 % to about 0.5 %, from about 0.01 % to about 0.4 %, from about 0.01 % to about 0.3 %, from about 0.01 % to about 0.2 %, from about 0.01 % to about 0.1 %, from about 0.06 % to about 0.5 %, from about 0.06 % to about 0.4 %, from about 0.06 % to about 0.3 %, from about 0.06 % to about 0.2 %, from about 0.06 % to about 0.1 %, from about 0.1 % to about 0.5 %, from about 0.1 % to about 0.4 %, from about 0.1 % to about 0.3 %, or from about 0.1 % to about 0.2 %) based on the total weight of the alloy.
  • V vanadium
  • 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
  • the alloy compositions can further include other minor elements, sometimes referred to as impurities, in amounts of about 0.05 % or below, 0.04 % or below, 0.03 % or below, 0.02 % or below, or 0.01 % or below each.
  • impurities may include, but are not limited to, Ni, Sc, Sn, Ga, Ca, Hf, Sr, or combinations thereof. Accordingly, Ni, Sc, Sn, Ga, Ca, Hf, or Sr may be present in an alloy in amounts of 0.05 % or below, 0.04 % or below, 0.03 % or below, 0.02 % or below, or 0.01 % or below. In certain aspects, the sum of all impurities does not exceed 0.15 % (e.g., 0.1 %). All expressed in wt. %.
  • the alloy composition also includes aluminum. In certain aspects, the remaining percentage of the alloy is aluminum.
  • a suitable alloy includes 1.20 % Si, 0.18 % Fe, 0.80 % Cu, 0.70 % Mg, 0.02 % Ti, 0.13 % Mn, 0.07 % Cr, and up to 0.15 % total impurities, with the remainder Al.
  • another non-limiting example of a suitable alloy includes 1.20 % Si, 0.18 % Fe, 0.80 % Cu, 0.70 % Mg, 0.02 % Ti, 0.14 % Cr, and up to 0.15 % total impurities, with the remainder Al.
  • another non-limiting example of a suitable alloy includes 1.20 % Si, 0.18 % Fe, 0.80 % Cu, 0.70 % Mg, 0.02 % Ti, 0.07 % Cr, 0.11 % Zr, and up to 0.15 % total impurities, with the remainder Al.
  • another non-limiting example of a suitable alloy includes 1.20 % Si, 0.18 % Fe, 0.80 % Cu, 0.70 % Mg, 0.02 % Ti, 0.08 % Cr, 0.11 % V, and up to 0.15 % total impurities, with the remainder Al.
  • another non-limiting example of a suitable alloy includes 1.20 % Si, 0.18 % Fe, 0.80 % Cu, 0.70 % Mg, 0.02 % Ti, 0.09 % Zr, 0.10 % V, and up to 0.15 % total impurities, with the remainder Al.
  • another non-limiting example of a suitable alloy includes 1.20 % Si, 0.18 % Fe, 0.80 % Cu, 0.70 % Mg, 0.02 % Ti, 0.09 % Mn, 0.10 % V, and up to 0.15 % total impurities, with the remainder Al.
  • the Si, Mg, and Cu content and ratios are controlled to enhance strength and formability.
  • the transition element e.g., Mn, Cr, Zr, and/or V
  • the transition element e.g., Mn, Cr, Zr, and/or V
  • the alloy described herein includes excess Si.
  • the Si and Mg content are controlled such that excess Si is present in the alloy as described herein.
  • Excess Si content can be calculated according to the method described in U.S. Patent No. 4,614,552, col. 4, lines 49-52, which is incorporated herein by reference. Briefly, Mg and Si combine as Mg 2 Si, imparting a considerable strength improvement after age-hardening.
  • Si-containing constituents, such as Al(FeMn)Si can form. Excess Si is present when the Si content is above the stoichiometric ratio of Mg 2 Si and above the amount included in Al(FeMn)Si constituents.
  • the excess Si content can be calculated by subtracting from the total Si content the Si needed for Mg 2 Si (Mg/1.73) and the Fe-containing phase (Fe/3).
  • the excess Si content can be 1.0 or less (e.g., from about 0.01 to about 1.0, from about 0.1 to about 0.9, or from about 0.5 to 0.8).
  • the excess Si content can be 0.01, 0.02, 0.03, 0.04, 0.05, 0.06, 0.07, 0.08, 0.09, 0.10, 0.15, 0.20, 0.25, 0.30, 0.35, 0.40, 0.45, 0.50, 0.55, 0.60, 0.65, 0.70, 0.75, 0.80, 0.85, 0.90, 0.95, 1.0, or anywhere in between.
  • the alloys described herein include at least one transition element (e.g., at least one of Mn, Cr, Zr, and/or V).
  • the combined content of the transition elements in the alloys described herein is at least about 0.14 wt. %.
  • the combined content of Mn, Cr, Zr, and/or V can be from about 0.14 wt. % to about 0.40 wt. % (e.g., from about 0.15 wt. % to about 0.35 wt. % or from about 0.25 wt. % to about 0.30 wt. %).
  • the combined content of Mn, Cr, Zr, and/or V is about 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 %.
  • one or more of the transition elements may not be present, as long as the total weight percentage of the present transition elements is at least 0.14 wt. %.
  • the presence of one or more of the transition elements, such as Mn, Cr, Zr, and/or V, can advantageously form dispersoids during the processing methods described herein, such as during the homogenization step.
  • the dispersoids can function as heterogeneous nucleation sites for precipitates during processing steps, such as during the solution heat treatment step.
  • grain boundary (GB) precipitation occurs due to GB misorientation that is favorable for precipitate nucleation.
  • the dispersoids reduce or eliminate GB precipitates and also reduce strain localization, thus diffusing strain distribution during deformation.
  • the reduced or eliminated GB precipitates and/or the diffused strain distribution during deformation result in an improved bendability of the resulting alloys and alloy products.
  • the dispersoids described herein can contain Al and one or more of the alloying elements found in the alloy composition as described above.
  • the dispersoids can have a composition according to one or more of the following formulae: A1X, A1XX, AlXSi, Al(Fe,X), Al(Fe,X)Si, or the like, wherein each X is selected from the group consisting of Fe, Si, Mn, Cr, V, or Zr.
  • the dispersoid average size and distribution are important factors that result in the desirable strength and formability properties displayed by the alloys and alloy products described herein.
  • the size and distribution are influenced by the presence of transition elements, as described above, and also by the methods of processing the alloys, as further described below.
  • the dispersoids can be present in the aluminum alloy in an average amount of at least about 1,500,000 dispersoids per square millimeter (mm 2 ).
  • the dispersoids can be present in an amount of at least about 1,600,000 dispersoids per mm 2 , at least about 1,700,000 dispersoids per mm 2 , at least about 1,800,000 dispersoids per mm 2 , at least about 1,900,000 dispersoids per mm 2 , at least about 2,000,000 dispersoids per mm 2 , at least about 2,100,000 dispersoids per mm 2 , at least about 2,200,000 dispersoids per mm 2 , at least about 2,300,000 dispersoids per mm 2 , at least about 2,400,000 dispersoids per mm 2 , at least about 2,500,000 dispersoids per mm 2 , at least about 2,600,000 dispersoids per mm 2 , at least about 2,700,000 dispersoids per mm 2 , at least about 2,800,000 dispersoids per mm 2 , at least about 2,900,000 dispersoids per mm 2 , or at least about 3,000,000 dispersoids per mm 2 .
  • the average number of dispersoids present in the aluminum alloy can be from about 1,500,000 dispersoids per mm 2 to about 5,000,000 dispersoids per mm 2 (e.g., from about 1,750,000 dispersoids per mm 2 to about 4,750,000 dispersoids per mm 2 or from about 2,000,000 dispersoids per mm 2 to about 4,500,000 dispersoids per mm 2 ).
  • the dispersoids in the aluminum alloy can occupy an area ranging from about 0.5 % to about 5 % of the alloy (e.g., from about 1 % to about 4 % or from about 1.5 % to about 2.5 % of the alloy).
  • the dispersoids can have an average diameter of from about 10 nm to about 600 nm (e.g., from about 50 nm to about 500 nm, from about 100 nm to about 450 nm, from about 200 nm to about 400 nm, from about 10 nm to about 200 nm, or from about 500 nm to about 600 nm).
  • the dispersoids can have a diameter of about 10 nm, 20 nm, 30 nm, 40 nm, 50 nm, 60 nm, 70 nm, 80 nm, 90 nm, 100 nm, 110 nm, 120 nm, 130 nm, 140 nm, 150 nm, 160 nm, 170 nm, 180 nm, 190 nm, 200 nm, 210 nm, 220 nm, 230 nm, 240 nm, 250 nm, 260 nm, 270 nm, 280 nm, 290 nm, 300 nm, 310 nm, 320 nm, 330 nm, 340 nm, 350 nm, 360 nm, 370 nm, 380 nm, 390 nm, 400 nm, 410 nm, 420 nm, 430 nm, 440 nm, 100
  • the alloys described herein also include Fe-constituents, which are also referred to herein as Fe-containing particles.
  • the Fe-constituents can include one or more of Al, Mn, Si, Cu, Ti, Zr, Cr, and/or Mg.
  • the Fe-constituents can be Al(Fe,X)Si phase particles, wherein X can be Mn, Cr, Zr, and/or V, and/or AlFeSi phase particles.
  • the Fe-constituents can include one or more of Al 3 Fe, Al x (Fe,Mn), Al 3 Fe, Ali 2 CFe,Mn) 3 Si, Al 7 Cu 2 Fe, Al(Fe,Mn) 2 Si 3 , Al x (Mn,Fe), and Ah 2 ( 7,Fe) 3 Si.
  • the presence of the transition elements described herein results in the transformation of AlFeSi particles into Al(Fe,X)Si particles.
  • the number of Al(Fe,X)Si phase particles, which are spheroid particles is greater than the number of AlFeSi phase particles, which are flake or needle type particles.
  • At least 50 % of the Fe-constituents are present as Al(Fe,X)Si particles (e.g., at least 55 %, at least 60 %, at least 65 %, at least 70 %, at least 75 %, at least 80 %, at least 85 %, at least 90 %, or at least 95 % of the Fe-constituents are present as Al(Fe,X)Si particles).
  • the Fe-constituents can have an average particle size of up to about 4 ⁇ .
  • the Fe-constituents, on average can range in size from about 0.1 ⁇ to about 4 ⁇ (e.g., from about 0.5 ⁇ to about 3.5 ⁇ or from about 1 ⁇ to about 3 ⁇ ).
  • a ratio of Cr to Mn (also referred to herein as the Cr/Mn ratio) can be from about 0.15:1 to about 0.7:1 (e.g., from about 0.3:1 to about 0.6:1 or from about 0.4:1 to about 0.55:1).
  • the Cr/Mn ratio can be about 0.15:1, 0.16:1, 0.17:1, 0.18:1, 0.19:1, 0.20:1, 0.21:1, 0.22:1, 0.23:1, 0.24:1, 0.25:1, 0.26:1, 0.27:1, 0.28:1, 0.29:1, 0.30:1, 0.31:1, 0.32:1, 0.33:1, 0.34:1, 0.35:1, 0.36:1, 0.37:1, 0.38:1, 0.39:1, 0.40:1, 0.41:1, 0.42:1, 0.43:1, 0.44:1, 0.45:1, 0.46:1, 0.47:1, 0.48:1, 0.49:1, 0.50:1, 0.51:1, 0.52:1, 0.53:1, 0.54:1, 0.55:1, 0.56:1, 0.57:1, 0.58:1, 0.59:1, 0.60:1, 0.61:1, 0.62:1, 0.63:1, 0.64:1, 0.65:1, 0.66:1, 0.67:1, 0.68:1, 0.69:1, or0.70:l.
  • a ratio of Cr to V (also referred to herein as the Cr/V ratio) can be from about 0.5:1 to about 1.5:1 (e.g., from about 0.6:1 to about 1.4:1 or from about 0.7:1 to about 1.3:1).
  • the Cr/V ratio can be about 0.50:1, 0.51:1, 0.52:1, 0.53:1, 0.54:1, 0.55:1, 0.56:1, 0.57:1, 0.58:1, 0.59:1, 0.60:1, 0.61:1, 0.62:1, 0.63:1, 0.64:1, 0.65:1, 0.66:1, 0.67:1, 0.68:1, 0.69:1, 0.70:1, 0.71:1, 0.72:1, 0.73:1, 0.74:1, 0.75:1, 0.76:1, 0.77:1, 0.78:1, 0.79:1, 0.80:1, 0.81:1, 0.82:1, 0.83:1, 0.84:1, 0.85:1, 0.86:1, 0.87:1, 0.88:1, 0.89:1, 0.90:1, 0.91:1, 0.92:1, 0.93:1, 0.94:1, 0.95:1, 0.96:1, 0.97:1, 0.98:1, 0.99:1, 1.0:1, 1.1:1, 1.2:1, 1.3:1, 1.4:1, or 1.5:1.
  • a ratio of Cr to Zr (also referred to herein as the Cr/Zr ratio) can be from about 0.5:1 to about 1.5:1 (e.g., from about 0.6:1 to about 1.4:1 or from about 0.7:1 to about 1.3:1).
  • the Cr/Zr ratio can be about 0.50:1, 0.51:1, 0.52:1, 0.53:1, 0.54:1, 0.55:1, 0.56:1, 0.57:1, 0.58:1, 0.59:1, 0.60:1, 0.61:1, 0.62:1, 0.63:1, 0.64:1, 0.65:1, 0.66:1, 0.67:1, 0.68:1, 0.69:1, 0.70:1, 0.71:1, 0.72:1, 0.73:1, 0.74:1, 0.75:1, 0.76:1, 0.77:1, 0.78:1, 0.79:1, 0.80:1, 0.81:1, 0.82:1, 0.83:1, 0.84:1, 0.85:1, 0.86:1, 0.87:1, 0.88:1, 0.89:1, 0.90:1, 0.91:1, 0.92:1, 0.93:1, 0.94:1, 0.95:1, 0.96:1, 0.97:1, 0.98:1, 0.99:1, 1.0:1, 1.1:1, 1.2:1, 1.3:1, 1.4:1, or 1.5:1.
  • a ratio of V to Mn (also referred to herein as the V/Mn ratio) can be from about 0.8:1 to about 1.4: 1 (e.g., from about 0.9: 1 to about 1.3 : 1 or from about 0.9:1 to about 1.2:1).
  • the V/Mn ratio can be about 0.80:1, 0.81:1, 0.82:1, 0.83:1, 0.84:1, 0.85:1, 0.86:1, 0.87:1, 0.88:1, 0.89:1, 0.90:1, 0.91:1, 0.92:1, 0.93:1, 0.94:1, 0.95:1,
  • a ratio of V to Zr (also referred to herein as the V/Zr ratio) can be from about 0.8: 1 to about 1.4: 1 (e.g., from about 0.9: 1 to about 1.3 : 1 or from about 0.9:1 to about 1.2:1).
  • the V/Zr ratio can be about 0.80:1, 0.81:1, 0.82:1, 0.83:1,
  • a ratio of V to Cr (also referred to herein as the V/Cr ratio) can be from about 0.8:1 to about 1.4: 1 (e.g., from about 0.9: 1 to about 1.3 : 1 or from about 0.9:1 to about 1.2:1).
  • the V/Cr ratio can be about 0.80:1, 0.81:1, 0.82:1, 0.83:1,
  • the mechanical properties of the aluminum alloy can be controlled by various aging conditions depending on the desired use.
  • the alloy can be produced (or provided) in a T4 temper or a T6 temper.
  • the proposed alloy has very high formability and bendability in the T4 temper and very high strength in the T6 temper.
  • the aluminum alloy may have a T4 yield strength ranging from about
  • 150 MPa to about 250 MPa e.g., about 150 MPa, about 160 MPa, about 170 MPa, about 180
  • the yield strength is from about 185 MPa to about
  • the alloy in the T4 temper provides a uniform elongation of at least about 20 % (e.g., from about 20% to about 30% or from about 22 % to about 26%).
  • the uniform elongation can be about 20 %, about 21 %, about 22 %, about 23 %, about 24 %, about 25 %, about 26 %, about 27 %, about 28 %, about 29 %, or about 30 %.
  • the uniform elongation is measured in the longitudinal (L) direction.
  • the alloy in the T4 temper provides a bend angle, as tested according to VDA 238-100, of at least 120°.
  • the bend angle can be from about 120° to about 140° (e.g., 120°, 121°, 122°, 123°, 124°, 125°, 126°, 127 ⁇ 128 ⁇ 129°, 130°, 131°, 132°, 133°, 134°, 135°, 136°, 137 ⁇ 138 ⁇ 139°, or 140°).
  • including V can improve the formability of the alloys.
  • alloys that include V exhibit an increase in bend angle of up to 10° (e.g., showing an improvement of at least about 5°, at least about 6°, at least about 7°, at least about 8°, at least about 9°, at least about 10°, or anywhere in between) as compared to alloys that do not contain V.
  • the aluminum alloy may have a T6 yield strength of at least about 200 MPa.
  • the yield strength is at least about 200 MPa, at least about 210 MPa, at least about 220 MPa, at least about 230 MPa, at least about 240 MPa, at least about 250 MPa, at least about 260 MPa, at least about 270 MPa, at least about 280 MPa, at least about 290 MPa, or at least about 300 MPa, at least about 310 MPa, at least about 320 MPa, at least about 330 MPa, at least about 340 MPa, at least about 350 MPa, at least about 360 MPa, at least about 370 MPa, or at least about 375 MPa.
  • the yield strength is from about 200 MPa to about 400 MPa (e.g., about 200 MPa, about 210 MPa, about 220 MPa, about 230 MPa, about 240 MPa, about 250 MPa, about 260 MPa, about 270 MPa, about 280 MPa, about 290 MPa, about 300 MPa, about 310 MPa, about 320 MPa, about 330 MPa, about 340 MPa, about 350 MPa, about 360 MPa, about 370 MPa, or about 375 MPa).
  • MPa to about 400 MPa e.g., about 200 MPa, about 210 MPa, about 220 MPa, about 230 MPa, about 240 MPa, about 250 MPa, about 260 MPa, about 270 MPa, about 280 MPa, about 290 MPa, about 300 MPa, about 310 MPa, about 320 MPa, about 330 MPa, about 340 MPa, about 350 MPa, about 360 MPa, about 370 MPa, or about 375 MPa
  • the alloy in the T6 temper provides a uniform elongation of at least about 5 % (e.g., from about 5 % to about 10 % or from about 6 % to about 9 %).
  • the uniform elongation can be about 5 %, about 6 %, about 7 %, about 8 %, about 9 %, or about 10 %.
  • the uniform elongation is measured in the longitudinal (L) direction.
  • the alloy products also include recrystallization texture components at a surface of the alloy products.
  • the alloy products include one or more of the following recrystallization texture components: cube, goss, brass, S, Cu, and rotated cube (referred to as "RC").
  • RC rotated cube
  • at least about 5 volume % of the rotated cube texture component is present in the alloy product (e.g., from about 5 vol. % to about 20 vol. %, from about 6 vol. % to about 18 vol. %, from about 8 vol. % to about 15 vol. %, from about 10 vol. % to about 13 vol. %, or from about 5 vol. % to about 6 vol. %).
  • Such a rotated cube texture component can result in desirable bending in the alloy product.
  • aluminum alloy properties are partially determined by the formation of microstructures during the alloy's preparation.
  • the method of preparation for an alloy composition may influence or even determine whether the alloy will have properties adequate for a desired application.
  • the alloy described herein can be cast into a cast article using any suitable casting method.
  • the casting process can include a direct chill (DC) casting process.
  • the casting process can include a continuous casting (CC) process.
  • the cast article can then be subjected to further processing steps.
  • the processing methods as described herein can include the steps of homogenizing, hot rolling, cold rolling, and solutionizing. In some cases, the processing methods can also include a pre-aging step and/or an artificial aging step.
  • the homogenization step can include a two-stage heating process.
  • a cast article prepared from an alloy composition described herein can be heated to a first stage homogenization temperature (e.g., the dispersoid nucleation temperature).
  • the first stage homogenization temperature can be from about 470 °C to about 530 °C (e.g., about 470 °C, about 480 °C, about 490 °C, about 500 °C, about 510 °C, about 520 °C, about 530 °C, or anywhere in between).
  • a heating rate to the first stage homogenization temperature can be about 100 °C/hour or less, about 75 °C/hour or less, about 50 °C/hour or less, about 40 °C/hour or less, about 30 °C/hour or less, about 25 °C/hour or less, about 20 °C/hour or less, or about 15 °C/hour or less.
  • the heating rate to the first stage homogenization temperature can be from about 10 °C/min to about 100 °C/min (e.g., from about 15 °C/min to about 90 °C/min, from about 20 °C/min to about 80 °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 45 °C/min to about 65 °C/min).
  • the cast article is then allowed to soak (i.e., held at the indicated temperature) for a period of time.
  • the cast article is allowed to soak for up to about 6 hours (e.g., from about 30 minutes to about 6 hours, inclusively).
  • the cast article can be soaked at a temperature of from about 470 °C to about 530 °C for 30 minutes, 1 hour, 2 hours, 3 hours, 4 hours, 5 hours, 6 hours, or anywhere in between.
  • the temperature of the cast article is increased to a temperature higher than the temperature used for the first stage of the homogenization process.
  • the cast article temperature can be increased, for example, to a temperature at least 5 °C higher than the aluminum alloy cast article temperature during the first stage of the homogenization process.
  • the cast article can be further heated to a second stage homogenization temperature (e.g., a dispersoid coarsening temperature) of from about 525 °C to about 575 °C (e.g., from about 530 °C to about 570 °C or from about 535 °C to about 565 °C).
  • the second stage homogenization temperature can be about 525 °C, about 530 °C, about 535 °C, about 540 °C, about 545 °C, about 550 °C, about 555 °C, about 560 °C, about 565 °C, about 570 °C, about 575 °C, or anywhere in between) in a second homogenization step.
  • a heating rate to the second stage homogenization temperature can be about 50 °C/hour or less, 30 °C/hour or less, or 25 °C/hour or less.
  • the cast article is then allowed to soak for a period of time during the second stage.
  • the cast article is allowed to soak for up to about 5 hours (e.g., from about 20 minutes to about 5 hours, inclusively).
  • the cast article can be soaked at a temperature of from about 525 °C to about 575 °C for about 15 minutes, 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, or anywhere in between. Hot Rolling
  • a hot rolling step can be performed.
  • the cast 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.
  • the hot roll exit temperature can range from about 250 °C to about 380 °C (e.g., from about 275 °C to about 370 °C or from about 300 °C to about 360 °C).
  • the hot roll exit temperature can be about 255 °C, 260 °C, 265 °C, 270 °C, 275 °C, 280 °C, 285 °C, 290 °C, 295 °C, 300 °C, 305 °C, 310 °C, 315 °C, 320 °C, 325 °C, 330 °C, 335 °C, 340 °C, 345 °C, 350 °C, 355 °C, 360 °C, 365 °C, 370 °C, 375 °C, or 380 °C.
  • the cast 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.
  • the cast article can be hot rolled to a 15 mm gauge, a 14 mm gauge, a 13 mm gauge, a 12 mm gauge, an 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.
  • a cold rolling step can optionally be performed before the solutionizing step.
  • the hot band is cold rolled to a final gauge aluminum alloy sheet.
  • 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.
  • the solutionizing step can include heating the aluminum alloy sheet or other rolled article from room temperature to a peak metal temperature.
  • the peak metal temperature can be from about 520 °C to about 590 °C (e.g., from about 520 °C to about 580 °C, from about 530 °C to about 570 °C, from about 545 °C to about 575 °C, from about 550 °C to about 570 °C, from about 555 °C to about 565 °C, from about 540 °C to about 560 °C, from about 560 °C to about 580 °C, or from about 550 °C to about 575 °C).
  • the aluminum alloy sheet can soak at the peak metal temperature for a period of time.
  • the aluminum alloy sheet is allowed to soak for up to approximately 2 minutes (e.g., from about 10 seconds to about 120 seconds inclusively).
  • the sheet can be soaked at the temperature of from about 520 °C to about 590 °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.
  • the aluminum alloy sheet can optionally undergo a pre-aging heat treatment.
  • pre-aging can include heating the aluminum alloy sheet to a temperature of from about 80 °C to about 120 °C (e.g., about 80 °C, about 85 °C, about 90 °C, about 95 °C, about 100 °C, about 105 °C, about 110 °C, about 115 °C, about 120 °C, or anywhere in between) and coiling the aluminum alloy sheet.
  • the coiled aluminum alloy sheet can be cooled (i.e., coil cooling is performed) for a period of up to about 24 hours (e.g., about 1 hour, about 2 hours, about 6 hours, about 12 hours, about 18 hours, about 24 hours, or anywhere in between).
  • the aluminum alloy sheet can then be naturally aged and/or artificially aged.
  • the aluminum alloy sheet can be naturally aged for a period of time to result in a T4 temper.
  • the aluminum alloy sheet can be naturally aged for 1 week or more, 2 weeks or more, 3 weeks or more, or 4 weeks or more.
  • the aluminum alloy sheet in the T4 temper can be artificially aged at a temperature of from about 180 °C to about 225 °C (e.g., 185 °C, 190 °C, 195 °C, 200 °C, 205 °C, 210 °C, 215 °C, 220 °C, or 225 °C) for a period of time to result in a T6 temper.
  • the aluminum alloy sheet can be artificially aged for a period from about 15 minutes to about 3 hours (e.g., 15 minutes, 30 minutes, 60 minutes, 90 minutes, 105 minutes, 2 hours, 2.5 hours, 3 hours, or anywhere in between) to result in a T6 temper.
  • the alloys, products, and methods described herein can be used in automotive, electronics, and transportation applications, such as commercial vehicle, aircraft, or railway applications.
  • the alloys can be used for chassis, cross-member, and intra-chassis components (encompassing, but not limited to, all components between the two C channels in a commercial vehicle chassis) to gain strength, serving as a full or partial replacement of high- strength steels.
  • the alloys can be used in F, T4, T6, or T8x tempers.
  • the alloys are used with a stiffener to provide additional strength.
  • the alloys are useful in applications where the processing and operating temperature is approximately 150 °C or lower.
  • the alloys and methods can be used to prepare motor vehicle body part products.
  • the disclosed alloys and methods can be used to prepare automobile body parts, such as bumpers, side beams, roof beams, cross beams, pillar reinforcements (e.g., A-pillars, B-pillars, and C-pillars), inner panels, side panels, floor panels, tunnels, structure panels, reinforcement panels, inner hoods, or trunk lid panels.
  • pillar reinforcements e.g., A-pillars, B-pillars, and C-pillars
  • inner panels e.g., side panels, floor panels, tunnels, structure panels, reinforcement panels, inner hoods, or trunk lid panels.
  • the disclosed aluminum alloys and methods can also be used in aircraft or railway vehicle applications, to prepare, for example, external and internal panels.
  • the described alloys and methods can also be used to prepare housings for electronic devices, including mobile phones and tablet computers.
  • the alloy can be used to prepare housings for the outer casing of mobile phones (e.g., smart phones) and tablet bottom chassis, with or without anodizing.
  • Exemplary consumer electronic products include mobile phones, audio devices, video devices, cameras, laptop computers, desktop computers, tablet computers, televisions, displays, household appliances, video playback and recording devices, and the like.
  • Exemplary consumer electronic product parts include outer housings (e.g., facades) and inner pieces for the consumer electronic products.
  • Illustration 1 is an aluminum alloy, comprising about 0.8 - 1.5 wt. % Si, 0.1 - 0.5 wt. % Fe, 0.5 - 1.0 wt. % Cu, 0.5 - 0.9 wt. % Mg, up to 0.1 wt. % Ti, up to 0.5 wt. % Mn, up to 0.5 wt. % Cr, up to 0.5 wt. % Zr, up to 0.5 wt. % V, up to 0.15 wt. % impurities, and Al.
  • Illustration 2 is the aluminum alloy of any preceding or subsequent illustration, comprising about 0.9 - 1.4 wt. % Si, 0.1 - 0.35 wt. % Fe, 0.6 - 0.9 wt. % Cu, 0.6 - 0.9 wt. % Mg, 0.01 - 0.09 wt. % Ti, up to 0.3 wt. % Mn, up to 0.3 wt. % Cr, up to 0.3 wt. % Zr, up to 0.3 wt. % V, up to 0.15 wt. % impurities, and Al.
  • Illustration 3 is the aluminum alloy of any preceding or subsequent illustration, comprising about 1.0 - 1.3 wt. % Si, 0.1 - 0.25 wt. % Fe, 0.7 - 0.9 wt. % Cu, 0.6 - 0.8 wt. % Mg, 0.01 - 0.05 wt. % Ti, up to 0.2 wt. % Mn, up to 0.2 wt. % Cr, up to 0.2 wt. % Zr, up to 0.2 wt. % V, up to 0.15 wt. % impurities, and Al.
  • Illustration 4 is the aluminum alloy of any preceding or subsequent illustration, wherein the aluminum alloy comprises at least one of Mn, Cr, Zr, and V.
  • Illustration 5 is the aluminum alloy of any preceding or subsequent illustration, wherein a combined content of Mn, Cr, Zr, and/or V is at least about 0.14 wt. %.
  • Illustration 6 is the aluminum alloy of any preceding or subsequent illustration, wherein the combined content of Mn, Cr, Zr, and/or V is from about 0.14 wt. % to about 0.4 wt. %.
  • Illustration 7 is the aluminum alloy of any preceding or subsequent illustration, wherein the combined content of Mn, Cr, Zr, and/or V is from about 0.15 wt. % to about 0.25 wt. %.
  • Illustration 8 is the aluminum alloy of any preceding or subsequent illustration, wherein the aluminum alloy comprises about 0.01 - 0.3 wt. % V.
  • Illustration 9 is the aluminum alloy of any preceding or subsequent illustration, wherein the aluminum alloy comprises excess Si and wherein an excess Si content is from about 0.01 to about 1.0.
  • Illustration 10 is an aluminum alloy product, comprising the aluminum alloy of any preceding or subsequent illustration.
  • Illustration 11 is the aluminum alloy product of any preceding or subsequent illustration, wherein the aluminum alloy product comprises a rotated cube crystallographic texture at a volume percent of at least about 5 %.
  • Illustration 12 is the aluminum alloy product of any preceding or subsequent illustration, wherein the aluminum alloy product comprises dispersoids in an amount of at least about 1,500,000 dispersoids per mm 2 .
  • Illustration 13 is the aluminum alloy product of any preceding or subsequent illustration, wherein the dispersoids occupy an area ranging from about 0.5 % to about 5 % of the aluminum alloy.
  • Illustration 14 is the aluminum alloy product of any preceding or subsequent illustration, wherein the aluminum alloy product comprises Fe-constituents.
  • Illustration 15 is the aluminum alloy product of any preceding or subsequent illustration, wherein the Fe-constituents comprise Al(Fe,X)Si phase particles.
  • Illustration 16 is the aluminum alloy product of any preceding or subsequent illustration, wherein an average particle size of the Fe-constituents is up to about 4 ⁇ .
  • Illustration 17 is the aluminum alloy product of any preceding or subsequent illustration, wherein the aluminum alloy product comprises a yield strength of at least about 300 MPa when in a T6 temper.
  • Illustration 18 is the aluminum alloy product of any preceding or subsequent illustration, wherein the aluminum alloy product comprises a uniform elongation of at least about 20 % and a minimum bend angle of at least about 120° when in a T4 temper.
  • Illustration 19 is a method producing an aluminum alloy product according to any preceding or subsequent illustration, comprising: casting an aluminum alloy according to Illustration 1 to provide a cast article; homogenizing the cast article in a two-stage homogenization process, wherein the two-stage homogenization process comprises heating the cast article to a first stage homogenization temperature and holding the cast article at the first stage homogenization temperature for a period of time and further heating the cast article to a second stage homogenization temperature and holding the cast article at the second stage homogenization temperature for a period of time; hot rolling and cold rolling to provide a final gauge aluminum alloy product; solution heat treating the final gauge aluminum alloy product; and pre-aging the final gauge aluminum alloy product.
  • Illustration 20 is the method of any preceding illustration, wherein the first stage homogenization temperature is from about 470 °C to about 530 °C and the second stage homogenization temperature is from about 525 °C to about 575 °C, and wherein the second stage homogenization temperature is higher than the first stage homogenization temperature.
  • Alloys were prepared for strength and formability testing.
  • the compositions for these alloys are provided in Table 4 below. In each of the alloy compositions in Table 4, the remainder is Al.
  • the alloys were prepared by DC casting the components into ingots and homogenizing the ingots in a two-step homogenization step as described herein.
  • the first step provided nucleation of a maximum amount of fine dispersoids (e.g., dispersoids having a diameter of less than about 10 nm).
  • the second step coarsened the fine dispersoids.
  • the homogenized ingots were then laid down and hot rolled according to the methods as described herein to a 10 mm gauge.
  • the hot band was coiled and cooled and was then cold rolled to a 2 mm gauge.
  • a solution heat treatment step was then performed at 560 °C for 35 seconds.
  • a pre-aging step was performed by heating the sheet to 100 °C and soaking for 1 hour (e.g., to simulate coil cooling as described above), followed by natural aging to achieve the T4 temper.
  • the T6 temper was then achieved by aging the T4 alloys at 200 °C for 30 minutes.
  • the properties of the D 1 - D6 alloys in T4 temper were determined.
  • Tensile testing was performed according to ASTM B557 in three directions relative to a rolling direction of the alloy sheets to evaluate anisotropic properties that can occur during recrystallization.
  • Yield strength (referred to as “YS” and indicated by histograms) and uniform elongation (referred to as "UE” and indicated by points) are shown in Figure 1 for a longitudinal direction along the rolling direction (referred to as "L” and indicated by vertical stripes), a transverse direction 90° to the rolling direction (referred to as "T” and indicated by horizontal stripes), and a diagonal direction 45° to the rolling direction (referred to as "D” and indicated by cross-hatching).
  • the alloys exhibited isotropic behavior in all three directions subjected to tensile testing even with elongated recrystallized grain structures as observed in Figure 2.
  • the uniform elongation values ranged from 24 % to 26 % and the yield strengths were from 185 MPa to 195 MPa.
  • Figure 3 shows the yield strengths and uniform elongations for alloys Dl - D6 in T4 and T6 tempers.
  • the composition had a negligible effect on yield strength and uniform elongation.
  • the composition had a negligible effect on uniform elongation and a decrease in yield strength of about 10 MPa for alloys including V in the composition.
  • the decrease in yield strength can be attributed to solute loss (e.g., Si, Mg, and/or Cu) during solutionizing by heterogeneous nucleation of solute precipitates on V-containing dispersoids.
  • Figure 4 is a graph showing bend angle test results for alloys Dl - D6 in a T4 temper.
  • Addition of Cr and V produced a large number of fine dispersoids which improves bending by diffusing strain distribution during deformation (e.g., bending, forming, stamping, or any suitable deformation process).
  • Mn combined with Fe and Si to form and spheroidize Fe- constituents, rather than forming dispersoids, due to the high diffusivity of Mn as compared to Zr, Cr, and/or V.
  • Spheroidization of the Fe-constituents improved bending by eliminating elongated (i.e., needle-like) particulates that can initiate cracking during deformation.
  • V-containing alloys e.g., alloys D4 - D6
  • Figure 5 compares yield strength (YS) and bend angle (VDA) for alloys Dl - D6 in T4 and T6 tempers.
  • FIG 6 shows recrystallization texture components for alloys Dl - D6, including cube, goss, brass, S, Cu, and rotated cube (referred to as "RC").
  • Each alloy Dl - D6 exhibited a similar distribution of texture components, and composition had a negligible effect on recrystallization texture.
  • each alloy exhibited a relatively high amount of rotated cube texture, resulting in the significantly improved bending angles shown in Figure 4 and Figure 5.
  • Figure 7 shows transmission electron microscopy (TEM) images of alloys Dl - D6 in T4 temper. Evident in the TEM images is dispersoid formation (shown as bright white particulates) in each alloy. Alloy D4 (including Cr and V) exhibited a higher dispersoid amount due to the relatively low diffusivities of Cr and V. Likewise, alloys D5 and D6 exhibited a lower number of dispersoids due to the relatively higher diffusivities of Mn and Zr. Accordingly, alloy D6 exhibited a lesser amount of dispersoids attributed to an affinity of Mn to be incorporated in Fe-constituents and to not solely form Mn dispersoids.
  • TEM transmission electron microscopy
  • Figure 8 shows dispersoid number density (histograms) and area fraction (open circles) for alloys Dl - D6 in T4 temper. Alloys not containing V (alloys Dl - D3) exhibited similar dispersoid number density. Alloy D2 (incorporating only Cr as a transition metal alloying element) exhibited a higher dispersoid area fraction compared to alloys Dl and D3 (incorporating Mn and Cr (Dl) and Zr and Cr (D3)). Alloy D4 (incorporating Cr and V) exhibited the highest dispersoid number density and the highest dispersoid area fraction.
  • FIG 9 shows scanning electron microscopy (SEM) images of alloys Dl - D6 in a T4 temper.
  • SEM scanning electron microscopy
  • Fe-constituent formation shown as bright white elongated particulates.
  • Each of the alloys Dl - D6 exhibited similar amounts of Fe-constituent formation, and similar Fe-constituent particle size distribution as shown in Figure 10.
  • employing transition metal alloying elements reduced the formation of Fe- constituents (e.g., AlFeSi) by replacing a portion of the Fe, thus forming spherical Al(Fe,X)Si constituents.
  • Each alloy continued to exhibit AlFeSi (elongated particulates) due to the presence of excess Si and processing at a low homogenization temperature (e.g., about 500 °C), with a reduced size and size distribution in alloys not employing the transition metal alloying elements.
  • the AlFeSi constituents in alloys not containing the transition metal alloying elements exhibited a larger size than the AlFeSi constituents observed in the alloys containing the transition metal alloying elements.
  • Fe-constituent size and size distribution was evaluated at a depth of about 0.5 mm from a surface of the aluminum alloy sheet (referred to as quarter thickness, indicated "QT" in the graph).
  • Figure 1 1 shows optical microscopy (referred to as "OM”) and SEM images of alloy
  • Alloy Dl was subjected to a one-step homogenization after casting, including a thermal ramp of 50 °C per hour to 560 °C, soaked for 2 hours, and subsequently hot rolled, cold rolled, solutionized, pre-aged, and naturally aged as described above.
  • Evident in the OM images is incipient and/or eutectic melting of Mg 2 Si in alloy Dl (shown as dark areas).
  • SEM images show the dark areas are voids that formed in the alloy during homogenization.
  • Energy dispersive X-ray spectroscopy (EDXS) showed Fe-constituents present in the voids (shown as bright particulates).
  • Employing the exemplary two-step homogenization as described herein can eliminate the incipient and/or eutectic melting when transition metal alloying elements are incorporated in the aluminum alloy compositions.

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Abstract

Cette invention concerne des alliages d'aluminium de haute résistance et de haute aptitude au formage et des procédés de fabrication et de traitement de tels alliages. Les alliages d'aluminium selon l'invention contiennent des éléments d'alliage de métaux de transition pour fournir une haute résistance et une haute aptitude au formage. Le procédé de traitement comprend une homogénéisation à étapes multiples, un laminage à chaud et à froid, et des étapes de mise en solution. L'invention concerne en outre les procédés d'utilisation des alliages d'aluminium.
PCT/US2018/057054 2017-10-23 2018-10-23 Alliages d'aluminium de haute résistance et de haute aptitude au formage leurs procédés de fabrication WO2019083969A1 (fr)

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EP18797512.3A EP3676410B1 (fr) 2017-10-23 2018-10-23 Alliages d'aluminium de haute résistance et de haute aptitude au formage leurs procédés de fabrication
CN201880068803.7A CN111247260A (zh) 2017-10-23 2018-10-23 高强度高度可成型的铝合金及其制作方法
MX2020003528A MX2020003528A (es) 2017-10-23 2018-10-23 Aleaciones de aluminio de alta resistencia, altamente formables y metodos para su fabricacion.
ES18797512T ES2955293T3 (es) 2017-10-23 2018-10-23 Aleaciones de aluminio de alta resistencia, altamente conformables y métodos para su fabricación
JP2022136728A JP2022172234A (ja) 2017-10-23 2022-08-30 高強度で高度に成形可能なアルミニウム合金およびその作製方法
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Publication number Priority date Publication date Assignee Title
BR112022012186A2 (pt) * 2019-12-23 2022-09-13 Alcoa Usa Corp Ligas de extrusão 6xxx de alta resistência
CN111876700B (zh) * 2020-06-08 2021-12-03 中南大学 一种粉末冶金铝合金冷轧板材的热处理工艺
CA3205192A1 (fr) * 2021-01-29 2022-08-04 Lynette M. Karabin Nouveaux alliages d'aluminium 6xxx
CN116179904A (zh) * 2022-10-13 2023-05-30 烟台南山学院 一种低Sc、低Zn/Mg比的铝合金板材及其时效工艺

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4614552A (en) 1983-10-06 1986-09-30 Alcan International Limited Aluminum alloy sheet product
JPH07166285A (ja) * 1993-06-08 1995-06-27 Shinko Alcoa Yuso Kizai Kk 焼付硬化型Ａｌ合金板及びその製造方法
JPH09202933A (ja) * 1996-01-25 1997-08-05 Nippon Steel Corp 焼入性に優れた高強度アルミニウム合金
US20170175239A1 (en) * 2015-12-18 2017-06-22 Novelis Inc. High strength 6xxx aluminum alloys and methods of making the same

Family Cites Families (34)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH06136478A (ja) * 1992-10-23 1994-05-17 Kobe Steel Ltd 成形加工性に優れた焼付硬化型Ａｌ合金板及びその製造方法
JP2626958B2 (ja) * 1993-03-16 1997-07-02 スカイアルミニウム株式会社 成形性および焼付硬化性に優れたアルミニウム合金板の製造方法
US5522950A (en) * 1993-03-22 1996-06-04 Aluminum Company Of America Substantially lead-free 6XXX aluminum alloy
JP3351087B2 (ja) * 1994-03-17 2002-11-25 株式会社神戸製鋼所 Ａｌ−Ｍｇ−Ｓｉ系合金板の製法
JPH07252570A (ja) * 1994-03-17 1995-10-03 Kobe Steel Ltd 自動車パネル用Ａｌ−Ｍｇ−Ｓｉ系合金板
JPH0978210A (ja) * 1995-09-07 1997-03-25 Mitsubishi Materials Corp アルミ合金製車両ホイールの製造方法および車両ホイール
JPH11350058A (ja) * 1998-06-12 1999-12-21 Shinko Alcoa Yuso Kizai Kk 成形性及び焼き付け硬化性に優れるアルミニウム合金板及びその製造方法
JP2000282163A (ja) * 1999-03-30 2000-10-10 Kobe Steel Ltd 張出し成形性及び曲げ成形性に優れたＡｌ−Ｍｇ−Ｓｉ系合金板
JP4045326B2 (ja) * 1999-11-09 2008-02-13 株式会社神戸製鋼所 プレス成形性に優れたＡｌ−Ｍｇ−Ｓｉ系Ａｌ合金板
JP2001262265A (ja) * 2000-03-22 2001-09-26 Kobe Steel Ltd 高成形性アルミニウム合金板の熱間圧延材
JP4603134B2 (ja) * 2000-07-21 2010-12-22 株式会社神戸製鋼所 表面光沢度に優れた輸送機パネル材用アルミニウム合金板
JP4708555B2 (ja) * 2000-12-13 2011-06-22 株式会社神戸製鋼所 成形性と平坦度に優れたアルミニウム合金圧延薄板の連続溶体化焼き入れ処理方法
JP2003268475A (ja) * 2002-03-12 2003-09-25 Sky Alum Co Ltd 成形加工用アルミニウム合金板およびその製造方法
BR0312098A (pt) * 2002-06-24 2005-03-29 Corus Aluminium Walzprod Gmbh Método para a produção de liga de al-mg-si balanceada de alta resistência e produto desta liga capaz de ser soldado
JP2004211177A (ja) * 2003-01-07 2004-07-29 Nippon Steel Corp 成形性、塗装焼付け硬化性及び形状に優れたアルミニウム合金板並びに製造方法
JP2004211176A (ja) * 2003-01-07 2004-07-29 Nippon Steel Corp 成形性、塗装焼付け硬化性及び耐食性に優れたアルミニウム合金板並びに製造方法
TW200536946A (en) * 2003-12-11 2005-11-16 Nippon Light Metal Co Method for producing Al-Mg-Si alloy excellent in bake-hardenability and hemmability
JP2007169740A (ja) * 2005-12-22 2007-07-05 Kobe Steel Ltd 成形性に優れたアルミニウム合金板およびその製造方法
JP4939093B2 (ja) * 2006-03-28 2012-05-23 株式会社神戸製鋼所 ヘム曲げ性およびベークハード性に優れる自動車パネル用６０００系アルミニウム合金板の製造方法
JP4944474B2 (ja) * 2006-03-30 2012-05-30 株式会社神戸製鋼所 伸びフランジ性に優れたアルミニウム合金板およびその製造方法
JP2009173973A (ja) * 2008-01-22 2009-08-06 Kobe Steel Ltd 成形時のリジングマーク性に優れたアルミニウム合金板
JP2009173972A (ja) * 2008-01-22 2009-08-06 Kobe Steel Ltd 成形時のリジングマーク性に優れたアルミニウム合金板
JP5203772B2 (ja) * 2008-03-31 2013-06-05 株式会社神戸製鋼所 塗装焼付け硬化性に優れ、室温時効を抑制したアルミニウム合金板およびその製造方法
JP5385025B2 (ja) * 2009-06-18 2014-01-08 株式会社神戸製鋼所 成形性に優れた高強度ボルト用アルミニウム合金線棒材およびその製造方法、高強度フランジボルトおよびその製造方法
JP5400510B2 (ja) * 2009-07-15 2014-01-29 株式会社Ｕａｃｊ 深絞り性と曲げ加工性に優れた成形加工用アルミニウム合金板
CN101643869B (zh) * 2009-09-04 2011-04-06 河池学院 高强度汽车铝合金轮辋
JP5758676B2 (ja) * 2011-03-31 2015-08-05 株式会社神戸製鋼所 成形加工用アルミニウム合金板およびその製造方法
CN102337429B (zh) * 2011-08-18 2013-12-25 苏州有色金属研究院有限公司 高强度Al-Mg-Si-Cu合金及其制备方法
CN103757507B (zh) * 2014-02-25 2016-04-27 北京科技大学 一种汽车车身外板用高烤漆硬化铝合金材料及其制备方法
JP5901738B2 (ja) * 2014-03-27 2016-04-13 株式会社神戸製鋼所 アルミニウム合金鍛造材およびその製造方法
CN104630556B (zh) * 2015-02-06 2016-08-17 中南大学 一种超高强高韧高耐蚀CuNiSiNbSn系弹性铜合金及其制备方法
JP6445958B2 (ja) * 2015-12-14 2018-12-26 株式会社神戸製鋼所 自動車用アルミニウム合金鍛造材
JP2017155251A (ja) * 2016-02-29 2017-09-07 株式会社神戸製鋼所 強度と延性に優れたアルミニウム合金鍛造材およびその製造方法
WO2017170835A1 (fr) * 2016-03-30 2017-10-05 株式会社神戸製鋼所 Feuille d'alliage d'aluminium et procédé de fabrication de feuille d'alliage d'aluminium

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4614552A (en) 1983-10-06 1986-09-30 Alcan International Limited Aluminum alloy sheet product
JPH07166285A (ja) * 1993-06-08 1995-06-27 Shinko Alcoa Yuso Kizai Kk 焼付硬化型Ａｌ合金板及びその製造方法
JPH09202933A (ja) * 1996-01-25 1997-08-05 Nippon Steel Corp 焼入性に優れた高強度アルミニウム合金
US20170175239A1 (en) * 2015-12-18 2017-06-22 Novelis Inc. High strength 6xxx aluminum alloys and methods of making the same

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
MURAYAMA M ET AL: "The effect of Cu additions on the precipitation kinetics in an Al-Mg-Si alloy with excess Si", METALLURGICAL AND MATERIALS TRANSACTIONS A, SPRINGER-VERLAG, NEW YORK, vol. 32, no. 2, 1 February 2001 (2001-02-01), pages 239 - 246, XP019693766, ISSN: 1543-1940 *

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