EP4063530A1 - 7xxx series aluminum alloy or plate, manufacturing method therefor, processing method therefor, and application thereof - Google Patents

7xxx series aluminum alloy or plate, manufacturing method therefor, processing method therefor, and application thereof Download PDF

Info

Publication number
EP4063530A1
EP4063530A1 EP20901677.3A EP20901677A EP4063530A1 EP 4063530 A1 EP4063530 A1 EP 4063530A1 EP 20901677 A EP20901677 A EP 20901677A EP 4063530 A1 EP4063530 A1 EP 4063530A1
Authority
EP
European Patent Office
Prior art keywords
aluminum alloy
series aluminum
sheet
7xxx
quenching
Prior art date
Legal status (The legal status 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 status listed.)
Pending
Application number
EP20901677.3A
Other languages
German (de)
French (fr)
Other versions
EP4063530A4 (en
Inventor
Hao Wu
Cheng Liu
Mingdong Huang
Zhikai ZHENG
Zeyu ZHOU
Ronghui FAN
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Aluminum Corp Of China
Aluminum Corp of China Ltd
Chinalco Materials Application Research Institute Co Ltd
Original Assignee
Aluminum Corp Of China
Aluminum Corp of China Ltd
Chinalco Materials Application Research Institute Co Ltd
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 Aluminum Corp Of China, Aluminum Corp of China Ltd, Chinalco Materials Application Research Institute Co Ltd filed Critical Aluminum Corp Of China
Publication of EP4063530A1 publication Critical patent/EP4063530A1/en
Publication of EP4063530A4 publication Critical patent/EP4063530A4/en
Pending legal-status Critical Current

Links

Images

Classifications

    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C21/00—Alloys based on aluminium
    • C22C21/10—Alloys based on aluminium with zinc as the next major constituent
    • 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
    • C22F1/002—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working by rapid cooling or quenching; cooling agents used therefor
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
    • C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
    • C22F1/04—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon
    • C22F1/053—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon of alloys with zinc as the next major constituent

Definitions

  • the invention relates to the field of nonferrous metals, and particularly relates to a 7xxx series aluminum alloy or sheet.
  • the invention also relates to a process of producing the 7xxx series aluminum alloy or sheet, a process of processing same and use thereof for producing vehicle parts.
  • the weight of the automobile body accounts for about 40% of the total weight of the automobile, such that the lightweight of the automobile body plays a decisive role in the lightweight of the whole automobile.
  • the lightweight of the automobile body is increasingly interested by the automobile producing technology.
  • aluminum alloy sheets commonly used for the automobile body are mainly 5xxx and 6xxx series aluminum alloys with relatively lower strength.
  • the 7xxx series aluminum alloy has high strength but low formability at room temperature, which limits the wide use thereof in vehicle bodies.
  • the integrated hot forming-quenching process is a composite process combining heat treatment and hot forming of aluminum alloy, which combines the forming process and the heat treatment process and realizes forming and controls performance by means of a same set of molds. The process improves the plasticity of the material in the forming process while ensuring the strength of the material.
  • the aluminum alloy sheet after the completion of solid solution treatment is quickly transferred to a water-cooled mold, the mold is quickly closed for forming and kept closed after forming to finish quenching the part in the mold, then the sheet is finally subjected to aging treatment to improve the strength.
  • the process is a novel process with the greatest prospect in the hot forming of high-strength aluminum alloy sheets, which can solve the problems of poor forming plasticity, large resilience and shape distortion during heat treatment.
  • the integrated hot forming-quenching process has been commercialized up to date, it is mainly used on high-strength steel, 5xxx and 6xxx series aluminum alloys, such as AA5754, AA6016, AA6111, and the like.
  • the process improves the formability of the original sheet through an aluminum alloy hot stamping process so as to produce parts with more complex shapes.
  • 5xxx and 6xxx aluminum alloy parts have strength lower than 300 MPa, which cannot satisfy the high strength requirement of vehicle body structural parts.
  • the 7xxx series high-strength aluminum alloy with better mechanical property is mainly used in the field of aerospace but is less used in the vehicle body, so that the related research and application are still in starting stage.
  • the inventors of the present invention have discovered that the integrated hot forming-quenching process has strict requirement on the properties of the 7xxx series aluminum alloy sheet, particularly the short-time solid solubility, low quenching sensitivity, good hot forming and age hardening, and the like. But the present 7xxx series aluminum alloy sheets do not meet all these requirements yet.
  • the inventors of the present invention have found a 7xxx-series aluminum alloy with a specific alloy composition, whose sheet is particularly suitable for the use in an integrated hot forming-quenching process after painstaking research.
  • the present invention has been completed based on this finding.
  • the present invention relates to the following aspects.
  • the term "substantially” means a deviation acceptable or considered as reasonable by a person skilled in the art, such as within ⁇ 5%, within ⁇ 1%, within ⁇ 0.5% or within ⁇ 0.1%.
  • the temperature when describing a process of producing a 7xxx-series aluminum alloy sheet, the temperature generally refers to the temperature of the material itself during the treatment (such as annealing, homogenization or hot rolling), unless particularly specified.
  • the balance being Al means “the balance being Al and unavoidable impurities", unless otherwise specified, as being obvious to those skilled in the art.
  • artificial peak aging may be carried out in any manner known to those skilled in the art, without any particular limitation.
  • the aging may be carried out by maintain the temperature at 100-130 °C for 5-48 h.
  • the baking treatment may be carried out in any manner known to the person skilled in the art, without particular limitation.
  • the treatment may be carried out by maintain the temperature at 170-190 °C for 20-40 min.
  • the method of measuring the yield strength refers to ASTM E8/E8M-16ae1 standard.
  • the method of measuring the ultimate tensile strength refers to ASTM E8/E8M-16ae1 standard.
  • the method of measuring the elongation refers to ASTM E8/E8M-16ae1 standard.
  • the method of measuring the average grain size refers to ASTM E112-13 standard.
  • the invention relates to a 7xxx-series aluminum alloy, in particular a 7xxx-series aluminum alloy in the form of a sheet (i.e. a 7xxx-series aluminum alloy sheet).
  • the 7xxx series aluminum alloy sheet is particularly suitable for integrated hot forming-quenching processing.
  • the aluminum alloy sheet has medium or high strength.
  • the 7xxx series aluminum alloy or sheet has a chemical composition of, by weight, 5.1-10.0% of Zn, 2.0-3.2% of Mg, 1.2-3.0% of Cu, 0-0.5% of Fe, 0-0.4% of Si, 0-0.2% of Ti, 0-0.1% of Cr, 0-0.055% of Zr, 0-0.25% of Mn, 0-0.30% of other grain size controlling element(s), and the balance of Al.
  • grain size controlling element(s) means any trace element (other than Cr, Zr, and Mn) known to those skilled in the art to be useful in adjusting (increasing or decreasing) the grain size of an aluminum alloy.
  • specific examples of other grain size controlling element(s) comprise Er, Sc, Hf, Dy, Gd, and the like. These other grain size controlling element(s) may be used alone or as combination of two or more.
  • the inventors believe that controlling the contents of Fe and Si can reduce the whole costs of preparation and subsequent use of the raw alloy material and has a certain effect on refining the grain structure.
  • the inventors of the invention also think that based on the requirement of the aluminum alloys for the integrated hot forming-quenching process, the contents of main alloy elements Zn, Mg and Cu are strictly controlled to reduce the high-temperature residual Al 2 CuMg phase, such that the residual second phase in the alloy sheet can be quickly dissolved back into the matrix during the heating and short-time heat preservation stages of the integrated hot forming-quenching process and the hot formability as well as the subsequent mechanical property of the alloy can be ensured.
  • the inventors of the invention also think that strict control of the contents of the grain size controlling elements such as Cr, Zr and Mn, and the like, can ensure the alloy sheet has relatively lower quenching sensitivity and simultaneously control the grain size of the alloy. So, the sheet can have relatively larger supersaturation degree of the matrix and finer grain structure after high-temperature solid solution treatment and mold quenching. After subsequent artificial peak aging or baking treatment, the final alloy sheet has a yield strength >400 MPa, a tensile strength >450 MPa, and an elongation >6.5%.
  • the 7xxx-series aluminum alloy or sheet has a chemical composition of, by weight, Zn in 5.4-7.6%, Mg in 2.0-2.7%, Cu in 1.6-2.3%, Fe in 0-0.4%, Si in 0-0.3%, Ti in 0.01-0.15%, Cr in 0-0.05%, Zr in 0-0.05%, Mn in 0-0.25%, and Al in balance.
  • the 7xxx-series aluminum alloy or sheet has a chemical composition of, by weight, Zn in 7.6-9.6%, Mg in 2.1-3.1%, Cu in 1.4-2.6%, Fe in 0-0.4%, Si in 0-0.3%, Ti in 0.01-0.15%, Cr in 0-0.05%, Zr in 0-0.05%, Mn in 0-0.25%, and Al in balance.
  • the 7xxx-series aluminum alloy or sheet has a chemical composition of, by weight, 5.1-6.7% of Zn, 2.0-2.9% of Mg, 1.2-2.6% of Cu, 0-0.5% of Fe, 0-0.4% of Si, 0-0.1% of Cr, 0-0.05% of Zr, 0-0.25% of Mn, and the balance of Al.
  • the 7xxx series aluminum alloy or sheet preferably comprises 5.4-6.5 wt% of Zn, 2.0-2.7 wt% of Mg, 1.6-2.3 wt% of Cu, 0-0.4 wt% of Fe, 0-0.3 wt% of Si, 0-0.05 wt% of Cr, 0-0.05 wt% of Zr, 0-0.15 wt% of Mn and the balance of Al.
  • the 7xxx-series aluminum alloy or sheet comprises 0.05-0.4% of Fe, 0.05-0.3% of Si, 0.001-0.05% of Cr, 0.001-0.04% of Zr, 0.001-0.15% of Mn, and 0-0.15% of other grain size controlling element(s).
  • the 7xxx-series aluminum alloy or sheet comprises 0-0.05% of Cr, 0-0.04% of Zr, 0-0.25% of Mn, and 0-0.15% of other grain size controlling element(s).
  • Cr, Mn, Zr and the other grain size controlling element(s) are each grain size controlling elements, preferably Cr, Mn and Zr. These grain size controlling elements may be used alone or as a combination of two or more. According to an embodiment of the invention, the combined content by weight of these grain size controlling elements (referring to the content by weight of an element for the case of being used alone) is generally ⁇ 0.30%, preferably ⁇ 0.25% or ⁇ 0.15%, when used alone or in combination.
  • the 7xxx series aluminum alloy sheet generally has an average grain size of 10-100 ⁇ m, preferably 15-70 ⁇ m, after maintaining the temperature at 450-510 °C for 5-20 min.
  • the 7xxx-series aluminum alloy sheet generally has a thickness in the range of 0.5-10.0 mm, preferably 1.0-4.0 mm.
  • the 7xxx-series aluminum alloy sheet is particularly suitable for integrated hot forming-quenching processing.
  • the 7xxx aluminum alloy sheet has rapid solid solubility, namely, a solution treatment thereof can be rapidly completed by maintaining the temperature at 450-510 °C for 5-20 min.
  • the 7xxx-series aluminum alloy sheet has a low quenching sensitivity.
  • the 7xxx-series aluminum alloy sheet is in cold-rolled-state, O-state or T4-state.
  • the 7xxx series aluminum alloy sheet generally has a yield strength >400 MPa, preferably >480 MPa, after maintaining the temperature at 450-510 °C for 5-20 min followed by subsequent air quenching, mold quenching or water quenching, and then artificial peak aging or baking treatment.
  • the 7xxx aluminum alloy sheet generally has a ultimate tensile strength of >450MPa, preferably >520 MPa, after maintaining the temperature at 450-510 °C for 5-20 min followed by subsequent air quenching, mold quenching or water quenching, and then artificial peak aging or paint baking treatment.
  • the 7xxx aluminum alloy sheet generally has an elongation of >6.5%, preferably >5.5%, after maintaining the temperature at 450-510 °C for 5-20min followed by subsequent air quenching, mold quenching or water quenching, and then artificial peak aging or paint baking treatment.
  • the invention further relates to a process of producing the 7xxx series aluminum alloy sheet.
  • the process can be used for producing any 7xxx series aluminum alloy sheet of the invention as described above.
  • the producing process comprises the steps of subjecting a 7xxx series aluminum alloy ingot to a homogenization treatment, a hot rolling treatment and a cold rolling treatment to obtain the 7xxx series aluminum alloy sheet.
  • the 7xxx series aluminum alloy ingot is an ingot of any of the 7xxx series aluminum alloys of the present invention as described above.
  • the 7xxx series aluminum alloy ingot has a chemical composition of, by weight, 5.1-10.0% of Zn, 2.0-3.2% of Mg, 1.2-3.0% of Cu, 0-0.5% of Fe, 0-0.4% of Si, 0-0.2% of Ti, 0-0.1% of Cr, 0-0.055% of Zr, 0-0.30% of Mn and the balance of Al.
  • the homogenization treatment may be carried out in any manner known to those skilled in the art, without any particular limitation.
  • the 7xxx series aluminum alloy ingot is heated to 375-460 °C (preferably 400-450 °C) and maintained for 0-15 h (preferably 5-10 h), then heated to 465-490 °C (preferably 470-490 °C or 470-485 °C) and maintained for 10-48 h (preferably 10-36 h or 16-36 h), and then cooled to room temperature by air quenching or being cooled together with the furnace.
  • the homogenization treatment generally has a temperature rising rate of 15-75 °C/h, preferably of 25-75 °C/h or 25-50 °C/h.
  • the hot rolling treatment in the producing process, may be carried out in any manner known to those skilled in the art, without any particular limitation.
  • it is general to conduct hot rough rolling and hot finish rolling to 4-14 mm, preferably to conduct hot rough rolling and hot finish rolling to 4-8 mm or 6-10 mm.
  • the hot rolling treatment has a finishing temperature of 200-460 °C, preferably 250-350 °C, 300-460 °C or 350-450 °C. Then, the hot-rolled sheet was curled and air-quenched to room temperature.
  • the cold rolling treatment in the producing process, may be carried out in any manner known to those skilled in the art, without any particular limitation.
  • it is generally cold-rolled to 0.5-10.0 mm, preferably to 1.0-4.0 mm, to obtain the 7xxx-series aluminum alloy sheet.
  • the 7xxx series aluminum alloy sheet is obtained in cold-rolled state.
  • the producing process further comprises a step of box annealing or continuous annealing the cold-rolled 7xxx-series aluminum alloy sheet to obtain the 7xxx-series aluminum alloy sheet in O-state or T4-state.
  • the box annealing may be carried out in any manner known to those skilled in the art, without any particular limitation.
  • the box annealing can generally have operating conditions of placing the aluminum alloy coil into a box-type annealing furnace to be heated to a temperature of 300-450 °C at a heating rate of 25-50 °C/h, maintaining the temperature for 0.5-3 h, and then cooling.
  • the continuous annealing may be carried out in any manner known to those skilled in the art, without any particular limitation.
  • the continuous annealing can generally have operating conditions of passing a coil of aluminum alloy strip through a continuous annealing furnace with a furnace temperature of 400-500 °C at a speed of 10-80 m/min, then cooling and coiling.
  • the producing process further comprises a step of maintain the temperature of the homogenized ingot at 300-480 °C for 2-30h before the hot rolling treatment.
  • the homogenized ingot is maintained at a temperature of 380-450 °C for 3-20 h.
  • an integrated hot forming-quenching processing process comprising a step of subjecting the 7xxx-series aluminum alloy sheet according to any one of the preceding embodiments or the 7xxx-series aluminum alloy sheet produced by the producing process according to any one of the preceding embodiments to an integrated hot forming-quenching processing.
  • the integrated hot forming-quenching process may be carried out in any manner known to those skilled in the art, without any particular limitation, and thus a detailed description thereof is omitted here.
  • the invention also relates to a vehicle part, in particular an automobile part.
  • the vehicle part may be made of a 7xxx-series aluminum alloy sheet according to any one of the preceding embodiments.
  • the process for producing the vehicle part may be any process known to those skilled in the art, without any particular limitation, and the process may be any process of the integrated hot forming-quenching processes according to any one of the preceding embodiments.
  • the present invention also relates to a vehicle comprising the vehicle part according to any one of the preceding embodiments.
  • the 7xxx aluminum alloy cooling sheet was prepared by a process comprising the following steps. Preparing an alloy cast ingot by an industrial semi-continuous process, wherein the alloy cast ingots were subjected to homogenization treatment according to the characteristics of the trace elements contained in the cast ingots.
  • the homogenization process comprises maintaining the temperature of the alloy cast ingots at 400 °C for 10 hours, followed by maintaining the temperature at 470 °C for 24 hours, with an increasing rate of the temperature of 50 °C/h. Then air quenching the alloy cast ingots to room temperature. Maintaining the temperature of the homogenized blank at 440 °C for 8 hours then carrying out hot rough rolling and hot finish rolling to 6 mm in thickness, with a final rolling temperature at 300 °C.
  • cold rolling-to-intermediate annealing-to-cold rolling process can be selected depending on specific conditions, namely cold rolling the intermediate annealing state, called as a CAC state cold-rolled sheet) on the hot-rolled coil of the alloy to obtain the cold-rolled alloy sheet with a final thickness of 2 mm.
  • the cold-rolled coil can also be optionally subjected to box annealing or continuous annealing to obtain an O-state or T4-state sheet.
  • the alloy composition ranges for Examples A1-A11 were as follows: 5.1-6.7% of Zn, 2.0-2.9% of Mg, 1.2-2.6% of Cu, 0-0.5% of Fe, 0-0.4% of Si, 0-0.1% of Cr, 0-0.05% of Zr, 0-0.25% of Mn, 0-0.25% of other grain size controlling element(s) and the balance of Al.
  • the alloy sheets of Examples A1-A11 and comparative examples C1-C6 were subjected to a fast solution treatment at 480 °C for 5 min (the industrial production can carry out on-line continuous solution treatment) followed by two extreme cooling modes of water quenching (WQ) or air quenching (AQ). Then T6 peak aging (PA) at 120 °C for 24 hours and baking treatment (BH) at 180 °C for 30 min were carried out, respectively.
  • the sheets treated by different processes were subjected to tensile property tests.
  • the alloy sheets of Examples A1-A11 should have yield strength >400 MPa, tensile strength >450 MPa, elongation >6.5%, and yield strength loss coefficients R ⁇ 20%.
  • the property results are shown in Table 2.
  • Table 1 Alloy sheet compositions of Examples A1-A11 and comparative examples C1-C6 Alloy Zn Mg Cu Fe Si Cr Zr Mn Al State A1 (Ex. 1) 5.63 2.73 1.59 0.10 0.02 0.0021 0.0003 0.005 balance 2mm, cold-rolled-state A2 (Ex. 2) 6.11 2.40 2.19 0.09 0.02 0.0027 0.0002 0.004 balance 2mm, cold-rolled-state A3 (Ex. 3) 5.52 2.59 1.72 0.30 0.20 0.0015 0.0003 0.004 balance 2mm, cold-rolled-state A4 (Ex. 4) 5.52 2.53 1.70 0.21 0.12 0.0015 0.0452 0.004 balance 2mm, cold-rolled-state A5 (Ex. 1) 5.63 2.73 1.59 0.10 0.02 0.0021 0.0003 0.005 balance 2mm, cold-rolled-state A2 (Ex. 2) 6.11 2.40 2.19 0.09 0.02 0.0027 0.0002 0.004 balance 2mm, cold-rolled-state A3 (Ex.
  • the alloy sheets of Examples A1-A11 of the invention showed significantly higher tensile properties than those of the comparative examples C1-C6, with yield strength >400 MPa, tensile strength >450 MPa, elongation >6.5% and yield strength loss coefficients R ⁇ 20%.
  • Example A1, Example A2 and Example A3 had substantially similar compositions of main alloy elements, for which the contents of trace elements of Cr, Zr and Mn were substantially zero, resulting in a low quenching sensitivity, and a yield strength loss coefficient R ⁇ 15%.
  • the alloy of Example A1 and the alloy of Example A2 had lower contents of Fe and Si elements than the alloy of Example A3.
  • the comparative example C5 was prepared using high-purity aluminum as a raw material thus had the lowest Fe and Si elements contents in the alloy. However, high contents of Fe and Si can effectively inhibit the growth of the grains in the sheet, which is beneficial to regulate and control the grain structure.
  • the sheets of the A1 alloy, the A3 alloy and the C5 alloy had average grain sizes, of 64 ⁇ m, 61 ⁇ m and 109 ⁇ m, respectively, as shown in Figs. 1-3 .
  • the alloy of Example A4 contained 0.0452% of trace element Zr. Compared with the alloy of example A3 without trace element Zr, the average grain size of the alloy sheet of A4 was greatly reduced to about 37 ⁇ m (as shown in Fig.4 ) after solution treatment, but the quenching sensitivity was increased with yield strength loss coefficient of 6.73% and 12.24% that was significantly higher than those of A3 alloy (4.9% and 5.0%). The results showed that the addition of Zr element would increase the quenching sensitivity of the alloy. For example, the comparative example Cl had higher Zr content of 0.0791%, whose average grain size was further reduced to about 25 ⁇ m (as shown in Fig.
  • Example A4 but the quenching sensitivity was significantly increased compared with Example A4 with R values increased to 22.36% and 34.55%.
  • the strength of air quenched alloys sheets after solution treatment decreased significantly.
  • the addition of trace element Zr was beneficial to control the grain size of the sheet but should be properly controlled, otherwise, the quenching sensitivity would be greatly increased, which might significantly reduce the mechanical property of the alloy.
  • the alloy of Example A5 and the alloys of Examples A7-A11 all contain trace amount of Cr in amounts of no more than about 0.05%.
  • the average grain size of Example A5 was reduced from 61 ⁇ m to 39 ⁇ m.
  • the quenching sensitivity of the corresponding sheet was increased but the yield loss coefficient R was still within 20%.
  • the average grain size of the sheet was reduced with the increase of Cr element, the quenching sensitivity was significantly increased.
  • the average grain sizes of comparative example C2 sheet (0.1241% Cr) and comparative example C3 (0.1811% Cr, being an amount of a conventional 7075 alloy) were respectively reduced to 32 ⁇ m and 27 ⁇ m ( Figs.
  • alloys of Examples A7-A11 had substantially similar compositions, but different preparation processes and sheet thicknesses. Accordingly, the quenching sensitivity of the alloys did not significantly change, and the mechanical properties were substantially similar.
  • the alloy of example A6 contains 0.122% Mn.
  • the addition of a trace amount of Mn effectively reduced the average grain size of the sheet alloy to 24 ⁇ m ( Fig. 9 ), but slightly increased the quenching sensitivity of the alloy sheet compared with example A3, with R values of 10.06% and 10.49%, respectively.
  • the effect of Mn on quenching sensitivity of the alloy was much weaker than Cr in equal amount (as shown in example C2).
  • Increasing the Mn content to 0.263% (comparative example C4 alloy) the quenching sensitivity of the alloy was further increased with larger yield strength loss coefficient R.
  • the alloy showed lower content of main elements Cu and Mg in the alloy leaded to a significantly lower strength than the others Because of the lower content of Cu element, the stability of strengthening phase during high-temperature baking treatment (BH) was poor, resulting in lower strength of the sample after baking treatment. However, due to the absence of trace elements such as Cr, Zr, Mn and the like, comparative example C6 showed lower quenching sensitivity.
  • the alloy composition ranges of Examples A12-A25 were as follows: 7.6 - 9.6% of Zn, 2.1-3.1% of Mg, 1.4-2.6% of Cu, 0-0.4% of Fe, 0-0.3% of Si, 0.01-0.15% of Ti, 0-0.05% of Cr, 0-0.05% of Zr, 0-0.25% of Mn, 0-0.25% of other grain size controlling element(s) and the balance of Al.
  • Table 3 Alloy sheet compositions of Examples A12-A25 and comparative examples C7-C12 Alloy Zn Mg Cu Fe Si Cr Zr Mn Al State A12 (Ex. 12) 7.76 2.13 2.09 0.09 0.03 0.0021 0.0002 0.0022 balance 2mm, cold-rolled-state A13 (Ex. 13) 7.73 2.23 1.93 0.24 0.12 0.0025 0.0002 0.0043 balance 2mm, cold-rolled-state A14 (Ex. 14) 8.18 2.10 1.52 0.09 0.031 0.0057 0.0003 0.0034 balance 2mm, cold-rolled-state A15 (Ex. 15) 9.01 2.38 2.23 0.09 0.032 0.0057 0.0002 0.0036 balance 2mm, cold-rolled-state A16 (Ex.
  • the alloy sheets of Examples A12-A25 and comparative examples C7-C12 were subjected to fast solution treatment at 480 °C for 10 min (the industrial production can carry out on-line continuous solution treatment) followed by water quenching (WQ) or air quenching (AQ). Then T6 peak aging (PA) at 120 °C for 24 hours and baking treatment (BH) at 185°C for 25 min were carried out, respectively.
  • the heat-treated sheets treated were subjected to tensile property tests and the loss coefficients R of the strengths were calculated.
  • Example A12-A27 had yield strength >480 MPa, tensile strength >520 MPa, elongation >5.5%, and yield strength loss coefficient R ⁇ 15%.
  • Table 4 Properties of Examples A12-A25 and comparative examples C7-C12 Treatment Yield Strength, MPa Tensile Strength, MPa Elongation, % (WQ-AQ)/WQ % A12 (Ex. 12) WQ+PA 553 574 16.6 3.80 AQ+PA 532 564 6.3 WQ+BH 558 584 11.0 8.60 AQ+BH 510 537 7.1 A13 (Ex.
  • the alloy sheets of Examples A12-A25 of the invention showed significantly higher tensile properties than those of the alloy sheets of comparative examples C7-C12, with yield strength >480 MPa, tensile strength >520 MPa, elongation >5.5% and yield strength loss coefficient R ⁇ 15%.
  • the comparative examples C7-C12 showed higher quenching sensitivity and significantly larger yield strength loss coefficients R, due to the excessive addition of trace elements such as Cr, Mn and Zr.
  • the alloys of Examples A12-A15 showed relatively low quenching sensitivity with a yield strength loss coefficient less than 8%, due to the absence of trace elements such as Cr, Mn, Zr and the like.
  • Example A16-A21 added about 0.05% of Zr, similar to Example A4, and showed slightly increased yield strength loss coefficients R in the cases of water quenching and air quenching with subsequent baking treatment, indicating that the quenching sensitivity of the alloys was increased with the addition of Zr element. Also, with the increase of Zr contents, the quenching sensitivity increases dramatically, and the strength loses significantly.
  • the comparative examples C7-C9 sheets present significant increase in yield strength loss coefficients, especially for comparative alloy C7 with the highest Zr content whose yield strength loss coefficients was as high as 24.23% and 35.44%. The quenching sensitivity was increased dramatically, and the strength was significant lost.
  • Examples A22 and A23 contained 0.048% and 0.044% Cr. Similar to Examples A16-A21, the yield strength loss coefficients R for the cases of water quenching and air quenching with subsequent baking treatment (i.e., WQ + BH and AQ + BH) were also increased slightly, but with relatively little effect. With the increase of the Cr content, such as comparative examples C10 and C11 with 0.212% and 0.125% Cr, the R values of the alloy sheets were sharply increased up to 30.02%, 41.40%, 27.67% and 38.42%, respectively. The corresponding strengths were sharply decreased, wherein the yield strength for the AQ + PA sample was less than 400 MPa, and the yield strength for the AQ + BH sample was even lower. The excessive addition of the Cr element significantly deteriorates the quenching sensitivity of the alloy.
  • the alloy of Example A24 and the alloy of Example A25 respectively contained 0.131% of Mn element and 0.245% of Mn element, and similarly, the yield strength loss coefficients R for the cases of water quenching and air quenching with subsequent baking treatment (namely WQ + BH and AQ + BH) of the alloy sheets were slightly increased, while the influence on the mechanical property was not very obvious.
  • the quenching sensitivity of the alloy was significantly deteriorated, wherein the corresponding R values of the sheet were increased to 25.32% and 37.13%, and the alloy strength was greatly reduced.
  • Example A15 had relatively cleaner microstructure both the inside the grain and at grain boundary, where no residual second phase existed except for the residual massive Al 7 Cu 2 Fe phase (as shown in Fig. 10 ).
  • trace elements such as Cr, Mn, Zr and the like will form fine dispersed phases that have strong regulation and control effect on the grain structure to reduce the average grain size of the alloy effectively.
  • these elements will also significantly affect the quenching sensitivity of the alloy and have disadvantages to the mechanical property of the alloy.
  • these trace elements should be added in appropriate amounts to regulate the grain structure depending on the actual grain size requirement.

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Shaping Metal By Deep-Drawing, Or The Like (AREA)
  • Metal Rolling (AREA)
  • Heat Treatment Of Sheet Steel (AREA)

Abstract

The invention relates to a 7xxx series aluminum alloy or sheet. The 7xxx series aluminum alloy or sheet comprise, by weight, Zn in 5.1-10.0%, Mg in 2.0-3.2%, Cu in 1.2-3.0%, Fe in 0-0.5%, Si in 0-0.4%, Ti in 0-0.2%, Cr in 0-0.1%, Zr in 0-0.055%, Mn in 0-0.25%, other grain size controlling element(s) in 0-0.30%, and Al in balance. The 7xxx series aluminum alloy sheet is particularly suitable for integrated hot forming-quenching processing. The invention also relates to a process of producing and a process of processing the 7xxx series aluminum alloy or sheet and use of the 7xxx series aluminum alloy or sheet in producing vehicle parts.

Description

    Technical Field
  • The invention relates to the field of nonferrous metals, and particularly relates to a 7xxx series aluminum alloy or sheet. The invention also relates to a process of producing the 7xxx series aluminum alloy or sheet, a process of processing same and use thereof for producing vehicle parts.
    • Background
  • In recent years, the automobile industry has been rapidly developed, and the demand for lightweight automobiles is also greatly influenced by energy, environment and the like. The weight of the automobile body accounts for about 40% of the total weight of the automobile, such that the lightweight of the automobile body plays a decisive role in the lightweight of the whole automobile. The lightweight of the automobile body is increasingly interested by the automobile producing technology. Currently, aluminum alloy sheets commonly used for the automobile body are mainly 5xxx and 6xxx series aluminum alloys with relatively lower strength. The 7xxx series aluminum alloy has high strength but low formability at room temperature, which limits the wide use thereof in vehicle bodies.
  • In the traditional hot forming process, in order to ensure the formability and the strength of parts, a sheet blank is heated to the required temperature and then transferred into a die for hot forming, and then the formed parts are subjected to conventional solid solution treatment and aging strengthening treatment to obtain parts with final properties. The process has the disadvantages of complicated procedures, long duration, being difficult to ensure the dimensional accuracy of the parts after heat treatment and relatively high production cost. The integrated hot forming-quenching process is a composite process combining heat treatment and hot forming of aluminum alloy, which combines the forming process and the heat treatment process and realizes forming and controls performance by means of a same set of molds. The process improves the plasticity of the material in the forming process while ensuring the strength of the material. The aluminum alloy sheet after the completion of solid solution treatment is quickly transferred to a water-cooled mold, the mold is quickly closed for forming and kept closed after forming to finish quenching the part in the mold, then the sheet is finally subjected to aging treatment to improve the strength. The process is a novel process with the greatest prospect in the hot forming of high-strength aluminum alloy sheets, which can solve the problems of poor forming plasticity, large resilience and shape distortion during heat treatment.
  • Although the integrated hot forming-quenching process has been commercialized up to date, it is mainly used on high-strength steel, 5xxx and 6xxx series aluminum alloys, such as AA5754, AA6016, AA6111, and the like. The process improves the formability of the original sheet through an aluminum alloy hot stamping process so as to produce parts with more complex shapes. It is known that 5xxx and 6xxx aluminum alloy parts have strength lower than 300 MPa, which cannot satisfy the high strength requirement of vehicle body structural parts. The 7xxx series high-strength aluminum alloy with better mechanical property is mainly used in the field of aerospace but is less used in the vehicle body, so that the related research and application are still in starting stage.
    • Summary of Invention
  • The inventors of the present invention have discovered that the integrated hot forming-quenching process has strict requirement on the properties of the 7xxx series aluminum alloy sheet, particularly the short-time solid solubility, low quenching sensitivity, good hot forming and age hardening, and the like. But the present 7xxx series aluminum alloy sheets do not meet all these requirements yet.
  • The inventors of the present invention have found a 7xxx-series aluminum alloy with a specific alloy composition, whose sheet is particularly suitable for the use in an integrated hot forming-quenching process after painstaking research. The present invention has been completed based on this finding.
  • Specifically, the present invention relates to the following aspects.
    1. 1. A 7xxx series aluminum alloy (preferably sheet) comprising, by weight, Zn in 5.1-10.0%, Mg in 2.0-3.2%, Cu in 1.2-3.0%, Fe in 0-0.5%, Si in 0-0.4%, Ti in 0-0.2%, Cr in 0-0.1%, Zr in 0-0.055%, Mn in 0-0.25%, other grain size controlling element(s) in 0-0.30%, and Al in balance.
    2. 2. The 7xxx-series aluminum alloy (preferably sheet) according to any of the preceding or subsequent aspects, having a chemical composition, by weight, of Zn in 5.4 - 7.6%, Mg in 2.0-2.7%, Cu in 1.6 - 2.3%, Fe in 0-0.4%, Si in 0-0.3%, Ti in 0.01-0.15%, Cr in 0-0.05%, Zr in 0-0.05%, Mn in 0-0.25%, other grain size controlling element(s) in 0-0.25%, and Al in balance.
    3. 3. The 7xxx-series aluminum alloy (preferably sheet) according to any one of the preceding or subsequent aspects, having a chemical composition, by weight, of Zn in 7.6-9.6%, Mg in 2.1-3.1%, Cu in 1.4-2.6%, Fe in 0-0.4%, Si in 0-0.3%, Ti in 0.01-0.15%, Cr in 0-0.05%, Zr in 0-0.05%, Mn in 0-0.25%, other grain size controlling element(s) in 0-0.25%, and Al in balance.
    4. 4. The 7xxx series aluminum alloy (preferably sheet) according to any of the preceding or subsequent aspects, having a chemical composition, by weight, of Zn in 5.1-6.7%, Mg in 2.0-2.9%, Cu in 1.2-2.6%, Fe in 0-0.5%, Si in 0-0.4%, Cr in 0-0.1%, Zr in 0-0.05%, Mn in 0-0.25%, and Al in balance.
    5. 5. The 7xxx series aluminum alloy (preferably sheet) according to any of the preceding or subsequent aspects, having a chemical composition, by weight, of Zn in 5.4 - 6.5%, Mg in 2.0-2.7%, Cu in 1.6 - 2.3%, Fe in 0-0.4%, Si in 0-0.3%, Cr in 0-0.05%, Zr in 0-0.05%, Mn in 0-0.15%, and Al in balance.
    6. 6. The 7xxx series aluminum alloy (preferably sheet) according to any one of the preceding or subsequent aspects, comprising Fe in 0.05-0.4%, Si in 0.05-0.3%, Cr in 0.001-0.05%, Zr in 0.001-0.04%, Mn in 0.001-0.15%, and other grain size controlling element(s) in 0-0.15%.
    7. 7. The 7xxx-series aluminum alloy (preferably sheet) according to any one of the preceding or subsequent aspects, comprising Cr in 0-0.05%, Zr in 0-0.04%, Mn in 0-0.15%, and other grain size controlling element(s) in 0-0.15%, and/or having a combined content by weight of Cr, Mn, Zr and other grain size controlling element(s) (preferably Cr, Mn, and Zr, such as present alone, or present as a mixture of two or more) of ≤ 0.25% (preferably ≤ 0.20% or ≤ 0.15%).
    8. 8. The 7xxx series aluminum alloy sheet according to any one of the preceding or subsequent aspects, having an average grain size of 10-100 µm (preferably 15-70 µm) and/or a thickness of 0.5-10.0 mm (preferably 1.0-4.0 mm), after maintaining the temperature at 450-510 °C for 5-20 min.
    9. 9. The 7xxx series aluminum alloy sheet according to any one of the preceding or subsequent aspects, having at least one of the following properties:
      1. (1) being suitable for an integrated hot forming-quenching process,
      2. (2) being able of completing the solid solution treatment at 450-510 °C within 5-20 min,
      3. (3) low quenching sensitivity, and
      4. (4) being in the cold-rolled-state, O-state or T4-state sheet.
    10. 10. The 7xxx series aluminum alloy sheet according to any one of the preceding or subsequent aspects, having a yield strength >400 MPa (preferably >480 MPa), a tensile strength >450 MPa (preferably >520 MPa) and an elongation >6.5% (preferably >5.5%), after maintaining the temperature at 450-510 °C for 5-20 min, followed by an air quenching, a mold quenching or a water quickening and then an artificial peak aging or a paint-baking treatment.
    11. 11. A process of producing a 7xxx series aluminum alloy sheet, comprising the steps of carrying out homogenization treatment, hot rolling treatment and cold rolling treatment on a 7xxx series aluminum alloy cast ingot, to obtain the 7xxx series aluminum alloy sheet, wherein the 7xxx series aluminum alloy cast ingot has a chemical composition of, by weight, 5.1-10.0% of Zn, 2.0-3.2% of Mg, 1.2-3.0% of Cu, 0-0.5% of Fe, 0-0.4% of Si, 0-0.2% of Ti, 0-0.1% of Cr, 0-0.055% of Zr, 0-0.30% of Mn and the balance of Al.
    12. 12. The process according to any one of the preceding or subsequent aspects, wherein the homogenization treatment comprises: heating the 7xxx series aluminum alloy ingot to 375-460 °C (preferably 400-450 °C), maintaining the temperature for 0-15 hours (preferably 5-10 hours), then heating to 465-490 °C (preferably 470-490 °C or 470-485 °C), maintaining the temperature for 10-48 hours (preferably 10-36 hours or 16-36 hours), then cooling to room temperature by air quenching or being cooled together with the furnace, wherein the heating rate is 15-75 °C/h (preferably 25-75 °C/h or 25-50 °C/h). And/or the hot rolling treatment comprises hot rough rolling and hot finish rolling to 4-14 mm (preferably 4-8 mm or 6-10 mm), at a final rolling temperature of 200-460 °C (preferably 250-350 °C, 300-460 °C or 350-450 °C), and coiling followed by air quenching to room temperature. And/or the cold rolling treatment comprises cold rolling to 0.5-10.0 mm (preferably 1.0-4.0 mm) to obtain the 7xxx series aluminum alloy sheet (in a cold-rolled-state). And/or the process further comprises a step of box annealing or continuous annealing of the 7xxx series aluminum alloy sheet in the cold-rolled-state to obtain an O-state or a T4-state alloy sheet. And/or the process further comprises a step of maintaining the temperature of the homogenized ingot at 300-480 °C (preferably 380-460 °C) for 2-30 hours (preferably 3-20 hours) before the hot rolling treatment.
    13. 13. An integrated hot forming-quenching processing process, comprising a step of subjecting a 7xxx-series aluminum alloy sheet according to any one of the preceding or subsequent aspects or a 7xxx-series aluminum alloy sheet produced by the process according to any one of the preceding or subsequent aspects to an integrated hot forming-quenching processing.
    14. 14. A vehicle part (particularly an automobile part), made of the 7xxx-series aluminum alloy sheet according to any one of the preceding or subsequent aspects or produced by the processing process according to any one of the preceding or subsequent aspects.
    15. 15. A vehicle provided with the vehicle part according to any one of the preceding or subsequent aspects.
    Technical effects
  • The aluminum alloy sheet provided by the invention has one of the following beneficial effects or a combination thereof:
    1. (1) being suitable for an integrated hot forming-quenching process;
    2. (2) excellent short-time solid solubility;
    3. (3) excellent quenching sensitivity;
    4. (4) excellent age hardening or paint bake hardening; and
    5. (5) excellent hot formability.
    Description of Drawings
    • FIG. 1 shows the grain structure of the alloy sheet of Example A1 after solid solution treatment at 480 °C for 5 min.
    • FIG. 2 shows the grain structure of the alloy sheet of Example A3 after solid solution treatment at 480 °C for 5 min.
    • FIG. 3 shows the grain structure of the alloy sheet of comparative example C5 after solid solution treatment at 480 °C for 5 min.
    • FIG. 4 shows the grain structure of the alloy sheet of Example A4 after solid solution treatment at 480 °C for 5 min.
    • FIG. 5 shows the grain structure of the C1 alloy sheet of comparative example after solid solution treatment at 480 °C for 5 min.
    • FIG. 6 shows the grain structure of the alloy sheet of Example A5 after solid solution treatment at 480 °C for 5 min.
    • FIG. 7 shows the grain structure of the alloy sheet of comparative example C2 after solid solution treatment at 480 °C for 5 min.
    • FIG. 8 shows the grain structure of the alloy sheet of comparative example C3 after solid solution treatment at 480 °C for 5 min.
    • FIG. 9 shows the grain structure of the alloy sheet of Example A6 after solid solution treatment at 480 °C for 5 min.
    • FIG. 10 shows the microstructure of the alloy sheet according to Example A15 observed by SEM after solid solution treatment at 480 °C for 10 min.
    • FIG. 11 shows the microstructure of the alloy sheet according to comparative example C7 observed by SEM after solid solution treatment at 480 °C for 10 min.
    • FIG. 12 shows the microstructure of the alloy sheet according to comparative example C10 observed by SEM after solid solution treatment at 480 °C for 10 min.
    • FIG. 13 shows the microstructure of the alloy sheet according to comparative example C12 observed by SEM after solid solution treatment at 480 °C for 10 min.
    Embodiments of the Invention
  • The embodiments of the present invention will be illustrated in more detail below, but it should be understood that the scope of the invention is not limited by the embodiments but is defined by the claims appended.
  • All publications, patent applications, patents, and other references mentioned in this specification are herein incorporated by reference in their entirety. Unless defined otherwise, all technical and scientific terms used herein are understood same as the meanings commonly known to those skilled in the art. In case of conflict, definitions according to the present specification will control.
  • When the specification introduces materials, substances, processes, steps, devices, components, or the like initiated with "known to those ordinary skill in the art", "prior art", or the like, it is intended that the subject matter so initiated encompass not only those conventionally used in the art at the time of filing this application, but also those may not be so commonly used at the present time, but will become known in the art as being suitable for a similar purpose.
  • In the context of this specification, the term "substantially" means a deviation acceptable or considered as reasonable by a person skilled in the art, such as within ± 5%, within ± 1%, within ± 0.5% or within ± 0.1%.
  • In the context of the present specification, when describing a process of producing a 7xxx-series aluminum alloy sheet, the temperature generally refers to the temperature of the material itself during the treatment (such as annealing, homogenization or hot rolling), unless particularly specified.
  • In the context of the present specification, the expression "the balance being Al" means "the balance being Al and unavoidable impurities", unless otherwise specified, as being obvious to those skilled in the art.
  • In the context of the present specification, artificial peak aging may be carried out in any manner known to those skilled in the art, without any particular limitation. For example, the aging may be carried out by maintain the temperature at 100-130 °C for 5-48 h.
  • In the context of the present specification, the baking treatment may be carried out in any manner known to the person skilled in the art, without particular limitation. For example, the treatment may be carried out by maintain the temperature at 170-190 °C for 20-40 min.
  • In the context of the present specification, the method of measuring the yield strength refers to ASTM E8/E8M-16ae1 standard.
  • In the context of the present specification, the method of measuring the ultimate tensile strength refers to ASTM E8/E8M-16ae1 standard.
  • In the context of the present specification, the method of measuring the elongation refers to ASTM E8/E8M-16ae1 standard.
  • In the context of this specification, the method of measuring the average grain size refers to ASTM E112-13 standard.
  • All percentages, parts, ratios, etc. involved in this specification are calculated by weight, and pressures are gauge pressures, unless explicitly indicated.
  • In the context of this specification, any two or more embodiments of the invention may be combined in any manner, and the resulting solution is a part of the original disclosure of this specification and is within the scope of the invention.
  • According to an embodiment of the invention, the invention relates to a 7xxx-series aluminum alloy, in particular a 7xxx-series aluminum alloy in the form of a sheet (i.e. a 7xxx-series aluminum alloy sheet). The 7xxx series aluminum alloy sheet is particularly suitable for integrated hot forming-quenching processing. Generally, the aluminum alloy sheet has medium or high strength.
  • According to an embodiment of the invention, the 7xxx series aluminum alloy or sheet has a chemical composition of, by weight, 5.1-10.0% of Zn, 2.0-3.2% of Mg, 1.2-3.0% of Cu, 0-0.5% of Fe, 0-0.4% of Si, 0-0.2% of Ti, 0-0.1% of Cr, 0-0.055% of Zr, 0-0.25% of Mn, 0-0.30% of other grain size controlling element(s), and the balance of Al.
  • In the context of this specification, "other grain size controlling element(s)" means any trace element (other than Cr, Zr, and Mn) known to those skilled in the art to be useful in adjusting (increasing or decreasing) the grain size of an aluminum alloy. Specific examples of other grain size controlling element(s) comprise Er, Sc, Hf, Dy, Gd, and the like. These other grain size controlling element(s) may be used alone or as combination of two or more.
  • Without being limited by any theory, the inventors believe that controlling the contents of Fe and Si can reduce the whole costs of preparation and subsequent use of the raw alloy material and has a certain effect on refining the grain structure. In addition, the inventors of the invention also think that based on the requirement of the aluminum alloys for the integrated hot forming-quenching process, the contents of main alloy elements Zn, Mg and Cu are strictly controlled to reduce the high-temperature residual Al2CuMg phase, such that the residual second phase in the alloy sheet can be quickly dissolved back into the matrix during the heating and short-time heat preservation stages of the integrated hot forming-quenching process and the hot formability as well as the subsequent mechanical property of the alloy can be ensured. Moreover, the inventors of the invention also think that strict control of the contents of the grain size controlling elements such as Cr, Zr and Mn, and the like, can ensure the alloy sheet has relatively lower quenching sensitivity and simultaneously control the grain size of the alloy. So, the sheet can have relatively larger supersaturation degree of the matrix and finer grain structure after high-temperature solid solution treatment and mold quenching. After subsequent artificial peak aging or baking treatment, the final alloy sheet has a yield strength >400 MPa, a tensile strength >450 MPa, and an elongation >6.5%.
  • According to an embodiment of the invention, the 7xxx-series aluminum alloy or sheet has a chemical composition of, by weight, Zn in 5.4-7.6%, Mg in 2.0-2.7%, Cu in 1.6-2.3%, Fe in 0-0.4%, Si in 0-0.3%, Ti in 0.01-0.15%, Cr in 0-0.05%, Zr in 0-0.05%, Mn in 0-0.25%, and Al in balance.
  • According to an embodiment of the invention, the 7xxx-series aluminum alloy or sheet has a chemical composition of, by weight, Zn in 7.6-9.6%, Mg in 2.1-3.1%, Cu in 1.4-2.6%, Fe in 0-0.4%, Si in 0-0.3%, Ti in 0.01-0.15%, Cr in 0-0.05%, Zr in 0-0.05%, Mn in 0-0.25%, and Al in balance.
  • According to an embodiment of the invention, the 7xxx-series aluminum alloy or sheet has a chemical composition of, by weight, 5.1-6.7% of Zn, 2.0-2.9% of Mg, 1.2-2.6% of Cu, 0-0.5% of Fe, 0-0.4% of Si, 0-0.1% of Cr, 0-0.05% of Zr, 0-0.25% of Mn, and the balance of Al.
  • According to an embodiment of the invention, conforming to the requirements by the integrated hot forming-quenching process on the solid solubility and quenching sensitivity of aluminum alloy sheet, the 7xxx series aluminum alloy or sheet preferably comprises 5.4-6.5 wt% of Zn, 2.0-2.7 wt% of Mg, 1.6-2.3 wt% of Cu, 0-0.4 wt% of Fe, 0-0.3 wt% of Si, 0-0.05 wt% of Cr, 0-0.05 wt% of Zr, 0-0.15 wt% of Mn and the balance of Al.
  • According to an embodiment of the present invention, the 7xxx-series aluminum alloy or sheet comprises 0.05-0.4% of Fe, 0.05-0.3% of Si, 0.001-0.05% of Cr, 0.001-0.04% of Zr, 0.001-0.15% of Mn, and 0-0.15% of other grain size controlling element(s).
  • According to an embodiment of the present invention, the 7xxx-series aluminum alloy or sheet comprises 0-0.05% of Cr, 0-0.04% of Zr, 0-0.25% of Mn, and 0-0.15% of other grain size controlling element(s).
  • According to the invention, Cr, Mn, Zr and the other grain size controlling element(s) are each grain size controlling elements, preferably Cr, Mn and Zr. These grain size controlling elements may be used alone or as a combination of two or more. According to an embodiment of the invention, the combined content by weight of these grain size controlling elements (referring to the content by weight of an element for the case of being used alone) is generally ≤0.30%, preferably ≤0.25% or ≤0.15%, when used alone or in combination.
  • According to an embodiment of the invention, the 7xxx series aluminum alloy sheet generally has an average grain size of 10-100 µm, preferably 15-70 µm, after maintaining the temperature at 450-510 °C for 5-20 min.
  • According to an embodiment of the invention, the 7xxx-series aluminum alloy sheet generally has a thickness in the range of 0.5-10.0 mm, preferably 1.0-4.0 mm.
  • According to an embodiment of the invention, the 7xxx-series aluminum alloy sheet is particularly suitable for integrated hot forming-quenching processing.
  • According to an embodiment of the invention, the 7xxx aluminum alloy sheet has rapid solid solubility, namely, a solution treatment thereof can be rapidly completed by maintaining the temperature at 450-510 °C for 5-20 min.
  • According to an embodiment of the invention, the 7xxx-series aluminum alloy sheet has a low quenching sensitivity.
  • According to an embodiment of the invention, the 7xxx-series aluminum alloy sheet is in cold-rolled-state, O-state or T4-state.
  • According to an embodiment of the invention, the 7xxx series aluminum alloy sheet generally has a yield strength >400 MPa, preferably >480 MPa, after maintaining the temperature at 450-510 °C for 5-20 min followed by subsequent air quenching, mold quenching or water quenching, and then artificial peak aging or baking treatment.
  • According to an embodiment of the invention, the 7xxx aluminum alloy sheet generally has a ultimate tensile strength of >450MPa, preferably >520 MPa, after maintaining the temperature at 450-510 °C for 5-20 min followed by subsequent air quenching, mold quenching or water quenching, and then artificial peak aging or paint baking treatment.
  • According to an embodiment of the invention, the 7xxx aluminum alloy sheet generally has an elongation of >6.5%, preferably >5.5%, after maintaining the temperature at 450-510 °C for 5-20min followed by subsequent air quenching, mold quenching or water quenching, and then artificial peak aging or paint baking treatment.
  • According to an embodiment of the invention, the invention further relates to a process of producing the 7xxx series aluminum alloy sheet. The process can be used for producing any 7xxx series aluminum alloy sheet of the invention as described above.
  • According to an embodiment of the present invention, the producing process comprises the steps of subjecting a 7xxx series aluminum alloy ingot to a homogenization treatment, a hot rolling treatment and a cold rolling treatment to obtain the 7xxx series aluminum alloy sheet. Here, the 7xxx series aluminum alloy ingot is an ingot of any of the 7xxx series aluminum alloys of the present invention as described above. For example, the 7xxx series aluminum alloy ingot has a chemical composition of, by weight, 5.1-10.0% of Zn, 2.0-3.2% of Mg, 1.2-3.0% of Cu, 0-0.5% of Fe, 0-0.4% of Si, 0-0.2% of Ti, 0-0.1% of Cr, 0-0.055% of Zr, 0-0.30% of Mn and the balance of Al.
  • According to an embodiment of the present invention, in the producing process, the homogenization treatment may be carried out in any manner known to those skilled in the art, without any particular limitation. For example, the 7xxx series aluminum alloy ingot is heated to 375-460 °C (preferably 400-450 °C) and maintained for 0-15 h (preferably 5-10 h), then heated to 465-490 °C (preferably 470-490 °C or 470-485 °C) and maintained for 10-48 h (preferably 10-36 h or 16-36 h), and then cooled to room temperature by air quenching or being cooled together with the furnace. Here, the homogenization treatment generally has a temperature rising rate of 15-75 °C/h, preferably of 25-75 °C/h or 25-50 °C/h.
  • According to an embodiment of the present invention, in the producing process, the hot rolling treatment may be carried out in any manner known to those skilled in the art, without any particular limitation. For example, it is general to conduct hot rough rolling and hot finish rolling to 4-14 mm, preferably to conduct hot rough rolling and hot finish rolling to 4-8 mm or 6-10 mm. Here, the hot rolling treatment has a finishing temperature of 200-460 °C, preferably 250-350 °C, 300-460 °C or 350-450 °C. Then, the hot-rolled sheet was curled and air-quenched to room temperature.
  • According to an embodiment of the present invention, in the producing process, the cold rolling treatment may be carried out in any manner known to those skilled in the art, without any particular limitation. For example, it is generally cold-rolled to 0.5-10.0 mm, preferably to 1.0-4.0 mm, to obtain the 7xxx-series aluminum alloy sheet. In this case, the 7xxx series aluminum alloy sheet is obtained in cold-rolled state.
  • According to an embodiment of the invention, the producing process further comprises a step of box annealing or continuous annealing the cold-rolled 7xxx-series aluminum alloy sheet to obtain the 7xxx-series aluminum alloy sheet in O-state or T4-state. Here, the box annealing may be carried out in any manner known to those skilled in the art, without any particular limitation. For example, the box annealing can generally have operating conditions of placing the aluminum alloy coil into a box-type annealing furnace to be heated to a temperature of 300-450 °C at a heating rate of 25-50 °C/h, maintaining the temperature for 0.5-3 h, and then cooling. The continuous annealing may be carried out in any manner known to those skilled in the art, without any particular limitation. For example, the continuous annealing can generally have operating conditions of passing a coil of aluminum alloy strip through a continuous annealing furnace with a furnace temperature of 400-500 °C at a speed of 10-80 m/min, then cooling and coiling.
  • According to an embodiment of the invention, the producing process further comprises a step of maintain the temperature of the homogenized ingot at 300-480 °C for 2-30h before the hot rolling treatment. Preferably, the homogenized ingot is maintained at a temperature of 380-450 °C for 3-20 h.
  • According to an embodiment of the present invention, there is also provided an integrated hot forming-quenching processing process, comprising a step of subjecting the 7xxx-series aluminum alloy sheet according to any one of the preceding embodiments or the 7xxx-series aluminum alloy sheet produced by the producing process according to any one of the preceding embodiments to an integrated hot forming-quenching processing. Here, the integrated hot forming-quenching process may be carried out in any manner known to those skilled in the art, without any particular limitation, and thus a detailed description thereof is omitted here.
  • According to an embodiment of the invention, the invention also relates to a vehicle part, in particular an automobile part. Here, the vehicle part may be made of a 7xxx-series aluminum alloy sheet according to any one of the preceding embodiments. The process for producing the vehicle part may be any process known to those skilled in the art, without any particular limitation, and the process may be any process of the integrated hot forming-quenching processes according to any one of the preceding embodiments.
  • According to an embodiment of the present invention, the present invention also relates to a vehicle comprising the vehicle part according to any one of the preceding embodiments.
    • Examples
  • The present invention will be described in further detail below for examples and comparative examples, but the present invention is not limited to the following examples.
  • The 7xxx aluminum alloy cooling sheet was prepared by a process comprising the following steps. Preparing an alloy cast ingot by an industrial semi-continuous process, wherein the alloy cast ingots were subjected to homogenization treatment according to the characteristics of the trace elements contained in the cast ingots. The homogenization process comprises maintaining the temperature of the alloy cast ingots at 400 °C for 10 hours, followed by maintaining the temperature at 470 °C for 24 hours, with an increasing rate of the temperature of 50 °C/h. Then air quenching the alloy cast ingots to room temperature. Maintaining the temperature of the homogenized blank at 440 °C for 8 hours then carrying out hot rough rolling and hot finish rolling to 6 mm in thickness, with a final rolling temperature at 300 °C. Then coiling and air quenching the hot-rolled coil of the alloy to room temperature. Finally, carrying out cold rolling (a cold rolling-to-intermediate annealing-to-cold rolling process can be selected depending on specific conditions, namely cold rolling the intermediate annealing state, called as a CAC state cold-rolled sheet) on the hot-rolled coil of the alloy to obtain the cold-rolled alloy sheet with a final thickness of 2 mm. The cold-rolled coil can also be optionally subjected to box annealing or continuous annealing to obtain an O-state or T4-state sheet.
  • The alloy composition ranges for Examples A1-A11 were as follows: 5.1-6.7% of Zn, 2.0-2.9% of Mg, 1.2-2.6% of Cu, 0-0.5% of Fe, 0-0.4% of Si, 0-0.1% of Cr, 0-0.05% of Zr, 0-0.25% of Mn, 0-0.25% of other grain size controlling element(s) and the balance of Al. The specific chemical compositions of the alloys of Examples A1-A11 and comparative examples C1-C6, as well as the corresponding sheet states, were shown in Table 1.
  • Based on the characteristics of the integrated hot forming-quenching process, the alloy sheets of Examples A1-A11 and comparative examples C1-C6 were subjected to a fast solution treatment at 480 °C for 5 min (the industrial production can carry out on-line continuous solution treatment) followed by two extreme cooling modes of water quenching (WQ) or air quenching (AQ). Then T6 peak aging (PA) at 120 °C for 24 hours and baking treatment (BH) at 180 °C for 30 min were carried out, respectively. The sheets treated by different processes were subjected to tensile property tests. Meanwhile, a loss coefficient R of the yield strengths of the alloy sheet obtained respectively by the air quenching and the water quenching aging was introduced, namely: ((yield strength obtained by water quenched sample)-(yield strength obtained by air quenched sample))/(yield strength obtained by water quenched sample), and the corresponding calculation equation was R = (WQ-AQ)/WQ, calculated in %. Through the tensile test and calculation, the alloy sheets of Examples A1-A11 should have yield strength >400 MPa, tensile strength >450 MPa, elongation >6.5%, and yield strength loss coefficients R ≤ 20%. The property results are shown in Table 2. Table 1: Alloy sheet compositions of Examples A1-A11 and comparative examples C1-C6
    Alloy Zn Mg Cu Fe Si Cr Zr Mn Al State
    A1 (Ex. 1) 5.63 2.73 1.59 0.10 0.02 0.0021 0.0003 0.005 balance 2mm, cold-rolled-state
    A2 (Ex. 2) 6.11 2.40 2.19 0.09 0.02 0.0027 0.0002 0.004 balance 2mm, cold-rolled-state
    A3 (Ex. 3) 5.52 2.59 1.72 0.30 0.20 0.0015 0.0003 0.004 balance 2mm, cold-rolled-state
    A4 (Ex. 4) 5.52 2.53 1.70 0.21 0.12 0.0015 0.0452 0.004 balance 2mm, cold-rolled-state
    A5 (Ex. 5) 5.69 2.66 1.69 0.23 0.13 0.0442 0.0002 0.005 balance 2mm, cold-rolled-state
    A6 (Ex. 6) 5.73 2.72 1.82 0.25 0.12 0.0024 0.0003 0.122 balance 2mm, cold-rolled-state
    A7 (Ex. 7) 5.71 2.68 1.79 0.24 0.11 0.0481 0.0001 0.004 balance 1mm, cold-rolled-state
    A8 (Ex. 8) 5.65 2.70 1.73 0.21 0.14 0.0425 0.0003 0.003 balance 4mm, cold-rolled-state
    A9 (Ex. 9) 5.70 2.68 1.64 0.24 0.11 0.0441 0.0002 0.005 balance 2mm CAC state
    A10 (Ex. 10) 5.69 2.63 1.67 0.23 0.13 0.0472 0.0003 0.004 balance 2mm O-state
    A11 (Ex. 11) 5.59 2.71 1.70 0.26 0.14 0.0435 0.0001 0.003 balance 2mm T4-state
    C1 (C.Ex. 1) 5.60 2.60 1.60 0.10 0.03 0.0032 0.0791 0.004 balance 2mm, cold-rolled-state
    C2 (C.Ex. 2) 5.75 2.65 1.72 0.24 0.12 0.1241 0.0006 0.004 balance 2mm, cold-rolled-state
    C3 (C.Ex. 3) 5.71 2.56 1.60 0.10 0.03 0.1811 0.0002 0.004 balance 2mm, cold-rolled-state
    C4 (C.Ex. 4) 5.71 2.73 1.79 0.21 0.13 0.0019 0.0003 0.263 balance 2mm, cold-rolled-state
    C5 (C.Ex. 5) 5.67 2.54 1.52 0.02 0.01 0.0054 0.0001 0.003 balance 2mm, cold-rolled-state
    C6 (C.Ex. 6) 5.49 1.42 0.28 0.25 0.12 0.0011 0.0002 0.003 balance 2mm, cold-rolled-state
    Table 2: Properties of alloy sheets of Examples A1-A11 and comparative examples C1-C6
    Treatment Yield Strength, MPa Tensile Strength, MPa Elongation, % (WQ-AQ)/WQ %
    A1 (Ex. 1) WQ+PA 493 553 16.6 3.45
    AQ+PA 476 523 7.1
    WQ+BH 460 507 12.5 8.04
    AQ+BH 423 479 9.5
    A2 (Ex. 2) WQ+PA 503 568 17.3 2.78
    AQ+PA 489 539 9.4
    WQ+BH 477 546 13.7 12.6
    AQ+BH 417 481 9.2
    A3 (Ex. 3) WQ+PA 490 546 14.7 4.90
    AQ+PA 466 534 9.7
    WQ+BH 460 513 13.8 5.00
    AQ+BH 437 506 12.9
    A4 (Ex. 4) WQ+PA 505 564 15.4 6.73
    AQ+PA 471 527 6.5
    WQ+BH 482 532 12.5 12.24
    AQ+BH 423 490 12.38
    A5 (Ex. 5) WQ+PA 535 586 14.2 14.58
    AQ+PA 457 506 10.1
    WQ+BH 497 550 12.5 17.30
    AQ+BH 411 478 11.0
    A6 (Ex. 6) WQ+PA 507 571 16.0 10.06
    AQ+PA 456 524 9.6
    WQ+BH 467 521 11.8 10.49
    AQ+BH 418 499 14.2
    A7 (Ex. 7) WQ+PA 543 589 13.4 14.92
    AQ+PA 462 511 9.6
    WQ+BH 489 530 13.5 14.93
    AQ+BH 416 476 11.7
    A8 (Ex. 8) WQ+PA 536 576 14.6 12.87
    AQ+PA 467 516 9.4
    WQ+BH 496 546 12.9 16.73
    AQ+BH 413 471 11.4
    A9 (Ex. 9) WQ+PA 528 576 14.7 12.50
    AQ+PA 462 511 9.8
    WQ+BH 494 541 12.9 17.21
    AQ+BH 409 481 11.3
    A10 (Ex. 10) WQ+PA 537 588 14.1 12.66
    AQ+PA 469 517 10.5
    WQ+BH 498 538 12.7 17.07
    AQ+BH 413 485 11.1
    A11 (Ex. 11) WQ+PA 531 578 13.7 10.36
    AQ+PA 476 527 9.6
    WQ+BH 494 529 12.5 14.78
    AQ+BH 421 491 10.5
    C1 (C.Ex. 1) WQ+PA 474 538 18.9 22.36
    AQ+PA 368 465 14.5
    WQ+BH 437 495 14.4 34.55
    AQ+BH 286 404 19.9
    C2 (C.Ex. 2) WQ+PA 533 589 14.0 34.90
    AQ+PA 347 456 10.1
    WQ+BH 497 550 12.5 38.63
    AQ+BH 305 425 11.8
    C3 (C.Ex. 3) WQ+PA 492 560 17.2 46.54
    AQ+PA 263 416 18.6
    WQ+BH 442 515 14.0 53.85
    AQ+BH 204 362 15.4
    C4 (C.Ex. 4) WQ+PA 507 571 16.0 10.06
    AQ+PA 456 524 9.6
    WQ+BH 467 521 11.8 16.70
    AQ+BH 389 468 15.1
    C5 (C.Ex. 5) WQ+PA 470 512 18.6 12.77
    AQ+PA 410 448 6.4
    WQ+BH 451 502 12.5 17.30
    AQ+BH 373 431 8.5
    C6 (C.Ex. 6) WQ+PA 369 417 16.3 -
    AQ+PA 385 429 15.0
    WQ+BH 188 309 20.8 3.72
    AQ+BH 181 276 20.2
  • As seen from Table 2, the alloy sheets of Examples A1-A11 of the invention showed significantly higher tensile properties than those of the comparative examples C1-C6, with yield strength >400 MPa, tensile strength >450 MPa, elongation >6.5% and yield strength loss coefficients R ≤ 20%.
  • The Example A1, Example A2 and Example A3 had substantially similar compositions of main alloy elements, for which the contents of trace elements of Cr, Zr and Mn were substantially zero, resulting in a low quenching sensitivity, and a yield strength loss coefficient R ≤ 15%.
  • The alloy of Example A1 and the alloy of Example A2 had lower contents of Fe and Si elements than the alloy of Example A3. The comparative example C5 was prepared using high-purity aluminum as a raw material thus had the lowest Fe and Si elements contents in the alloy. However, high contents of Fe and Si can effectively inhibit the growth of the grains in the sheet, which is beneficial to regulate and control the grain structure. After solution treatment, the sheets of the A1 alloy, the A3 alloy and the C5 alloy had average grain sizes, of 64 µm, 61 µm and 109 µm, respectively, as shown in Figs. 1-3. Meanwhile, although the yield strength loss coefficient R of comparative example C5 was less than 20%, the strength of the C5 alloy sheet was significantly lower than those of the Example A1 alloy, Example A2 alloy and Example A3 alloy treated by the corresponding processes due to larger grain size of the alloy sheet.
  • The alloy of Example A4 contained 0.0452% of trace element Zr. Compared with the alloy of example A3 without trace element Zr, the average grain size of the alloy sheet of A4 was greatly reduced to about 37 µm (as shown in Fig.4) after solution treatment, but the quenching sensitivity was increased with yield strength loss coefficient of 6.73% and 12.24% that was significantly higher than those of A3 alloy (4.9% and 5.0%). The results showed that the addition of Zr element would increase the quenching sensitivity of the alloy. For example, the comparative example Cl had higher Zr content of 0.0791%, whose average grain size was further reduced to about 25 µm (as shown in Fig. 5) but the quenching sensitivity was significantly increased compared with Example A4 with R values increased to 22.36% and 34.55%. The strength of air quenched alloys sheets after solution treatment decreased significantly. The addition of trace element Zr was beneficial to control the grain size of the sheet but should be properly controlled, otherwise, the quenching sensitivity would be greatly increased, which might significantly reduce the mechanical property of the alloy.
  • The alloy of Example A5 and the alloys of Examples A7-A11 all contain trace amount of Cr in amounts of no more than about 0.05%. As shown in Fig. 6, compared with the alloy of Example A3 without Cr, the average grain size of Example A5 was reduced from 61 µm to 39 µm. The quenching sensitivity of the corresponding sheet was increased but the yield loss coefficient R was still within 20%. Although the average grain size of the sheet was reduced with the increase of Cr element, the quenching sensitivity was significantly increased. For example, the average grain sizes of comparative example C2 sheet (0.1241% Cr) and comparative example C3 (0.1811% Cr, being an amount of a conventional 7075 alloy) were respectively reduced to 32 µm and 27 µm (Figs. 7 and 8), while the yield strength loss coefficients R were significantly increased to 34.9% and 38.63 for C2, and 46.54% and 53.85% for C3, respectively. The strength of air quenched alloys sheets after solution treatment decreased significantly. Therefore, the addition of trace element Cr should also be cautious, wherein an appropriate amount of Cr element could effectively control the grain structure of the sheet, otherwise, the quenching sensitivity of the alloy might be increased significantly, leading to the reduce of alloy strength.
  • In addition, the alloys of Examples A7-A11 had substantially similar compositions, but different preparation processes and sheet thicknesses. Accordingly, the quenching sensitivity of the alloys did not significantly change, and the mechanical properties were substantially similar.
  • The alloy of example A6 contains 0.122% Mn. Similarly, the addition of a trace amount of Mn effectively reduced the average grain size of the sheet alloy to 24 µm (Fig. 9), but slightly increased the quenching sensitivity of the alloy sheet compared with example A3, with R values of 10.06% and 10.49%, respectively. However, the effect of Mn on quenching sensitivity of the alloy was much weaker than Cr in equal amount (as shown in example C2). Increasing the Mn content to 0.263% (comparative example C4 alloy), the quenching sensitivity of the alloy was further increased with larger yield strength loss coefficient R.
  • Compare the comparative example C6 with examples A1-A11, the alloy showed lower content of main elements Cu and Mg in the alloy leaded to a significantly lower strength than the others Because of the lower content of Cu element, the stability of strengthening phase during high-temperature baking treatment (BH) was poor, resulting in lower strength of the sample after baking treatment. However, due to the absence of trace elements such as Cr, Zr, Mn and the like, comparative example C6 showed lower quenching sensitivity.
  • The alloy composition ranges of Examples A12-A25 were as follows: 7.6 - 9.6% of Zn, 2.1-3.1% of Mg, 1.4-2.6% of Cu, 0-0.4% of Fe, 0-0.3% of Si, 0.01-0.15% of Ti, 0-0.05% of Cr, 0-0.05% of Zr, 0-0.25% of Mn, 0-0.25% of other grain size controlling element(s) and the balance of Al. The specific chemical compositions of the alloys of Examples A12-A25 and comparative examples C7-C12, as well as the corresponding sheet states, were shown in Table 3. Table 3: Alloy sheet compositions of Examples A12-A25 and comparative examples C7-C12
    Alloy Zn Mg Cu Fe Si Cr Zr Mn Al State
    A12 (Ex. 12) 7.76 2.13 2.09 0.09 0.03 0.0021 0.0002 0.0022 balance 2mm, cold-rolled-state
    A13 (Ex. 13) 7.73 2.23 1.93 0.24 0.12 0.0025 0.0002 0.0043 balance 2mm, cold-rolled-state
    A14 (Ex. 14) 8.18 2.10 1.52 0.09 0.031 0.0057 0.0003 0.0034 balance 2mm, cold-rolled-state
    A15 (Ex. 15) 9.01 2.38 2.23 0.09 0.032 0.0057 0.0002 0.0036 balance 2mm, cold-rolled-state
    A16 (Ex. 16) 8.37 2.55 1.95 0.17 0.084 0.0060 0.0450 0.0058 balance 2mm, cold-rolled-state
    A17 (Ex. 17) 8.98 2.86 1.99 0.17 0.081 0.0059 0.0490 0.0060 balance 1mm, cold-rolled-state
    A18 (Ex. 18) 9.22 2.91 1.96 0.17 0.076 0.0061 0.0430 0.0056 balance 4mm, cold-rolled-state
    A19 (Ex. 19) 8.70 2.69 2.50 0.18 0.076 0.0067 0.0400 0.0059 balance 2mm CAC state
    A20 (Ex. 20) 8.94 2.77 1.54 0.18 0.076 0.0061 0.0480 0.0060 balance 2mm O-state
    A21 (Ex. 21) 8.91 2.14 2.02 0.19 0.073 0.0059 0.0460 0.0058 balance 2mm T4-state
    A22 (Ex. 22) 8.99 2.83 2.19 0.17 0.082 0.0480 0.0003 0.0060 balance 2mm, cold-rolled-state
    A23 (Ex. 23) 8.95 2.73 1.98 0.16 0.078 0.0440 0.0004 0.0055 balance 2mm, cold-rolled-state
    A24 (Ex. 24) 9.19 2.53 2.09 0.15 0.081 0.0052 0.0002 0.1310 balance 2mm, cold-rolled-state
    A25 (Ex. 25) 8.91 2.59 1.98 0.16 0.078 0.0050 0.0003 0.2450 balance 2mm, cold-rolled-state
    C7 (C.Ex. 7) 8.95 2.13 2.21 0.18 0.083 0.0053 0.1210 0.0051 balance 2mm, cold-rolled-state
    C8 (C.Ex. 8) 9.01 2.09 2.11 0.16 0.081 0.0051 0.0920 0.0051 balance 2mm, cold-rolled-state
    C9 (C.Ex. 9) 8.93 2.19 2.22 0.19 0.083 0.0049 0.0750 0.0051 balance 2mm, cold-rolled-state
    C10 (C.Ex. 10) 8.99 2.10 2.13 0.15 0.075 0.212 0.0003 0.0056 balance 2mm, cold-rolled-state
    C11 (C.Ex. 11) 9.11 2.23 2.19 0.18 0.080 0.125 0.0004 0.0061 balance 2mm, cold-rolled-state
    C12 (C.Ex. 12) 8.83 1.98 2.22 0.17 0.073 0.0049 0.0005 0.3360 balance 2mm, cold-rolled-state
  • Based on the characteristics of the integrated hot forming-quenching process, the alloy sheets of Examples A12-A25 and comparative examples C7-C12 were subjected to fast solution treatment at 480 °C for 10 min (the industrial production can carry out on-line continuous solution treatment) followed by water quenching (WQ) or air quenching (AQ). Then T6 peak aging (PA) at 120 °C for 24 hours and baking treatment (BH) at 185°C for 25 min were carried out, respectively. The heat-treated sheets treated were subjected to tensile property tests and the loss coefficients R of the strengths were calculated. Through test and calculation, the alloy sheets of Examples A12-A27 had yield strength >480 MPa, tensile strength >520 MPa, elongation >5.5%, and yield strength loss coefficient R ≤ 15%. The property results are shown in Table 4. Table 4: Properties of Examples A12-A25 and comparative examples C7-C12
    Treatment Yield Strength, MPa Tensile Strength, MPa Elongation, % (WQ-AQ)/WQ %
    A12 (Ex. 12) WQ+PA 553 574 16.6 3.80
    AQ+PA 532 564 6.3
    WQ+BH 558 584 11.0 8.60
    AQ+BH 510 537 7.1
    A13 (Ex. 13) WQ+PA 549 563 10.2 5.46
    AQ+PA 519 559 6.8
    WQ+BH 528 554 11.1 6.44
    AQ+BH 494 521 9.2
    A14 (Ex. 14) WQ+PA 544 580 16.8 4.04
    AQ+PA 522 553 6.4
    WQ+BH 518 544 9.9 4.25
    AQ+BH 496 537 5.8
    A15 (Ex. 15) WQ+PA 545 608 13.1 0.92
    AQ+PA 540 592 5.94
    WQ+BH 549 589 9.9 7.65
    AQ+BH 507 549 5.8
    A16 (Ex. 16) WQ+PA 553 619 13.2 2.53
    AQ+PA 539 600 8.6
    WQ+BH 570 604 8.4 6.67
    AQ+BH 532 567 5.8
    A17 (Ex. 17) WQ+PA 561 622 10.9 0.89
    AQ+PA 556 591 6.1
    WQ+BH 601 637 8.5 13.14
    AQ+BH 522 534 6.0
    A18 (Ex. 18) WQ+PA 545 612 13.3 1.28
    AQ+PA 538 583 5.7
    WQ+BH 565 598 9.6 11.5
    AQ+BH 500 544 5.9
    A19 (Ex. 19) WQ+PA 564 630 13.2 2.83
    AQ+PA 548 583 6.6
    WQ+BH 570 605 9.6 9.30
    AQ+BH 517 545 6.6
    A20 (Ex. 20) WQ+PA 544 616 15.2 2.02
    AQ+PA 533 583 7.8
    WQ+BH 558 598 10.2 11.83
    AQ+BH 492 537 10.6
    A21 (Ex. 21) WQ+PA 520 587 16.7 -
    AQ+PA 522 571 7.3
    WQ+BH 546 574 12.5 10.26
    AQ+BH 490 523 6.1
    A22 (Ex. 22) WQ+PA 521 577 16.2 2.11
    AQ+PA 510 559 7.6
    WQ+BH 541 564 12.3 9.80
    AQ+BH 488 520 6.3
    A23 (Ex. 23) WQ+PA 512 581 15.2 0.20
    AQ+PA 511 570 7.6
    WQ+BH 540 570 13.8 7.78
    AQ+BH 498 521 6.8
    A24 (Ex. 24) WQ+PA 511 565 15.2 0.20
    AQ+PA 510 550 6.6
    WQ+BH 542 563 13.5 9.78
    AQ+BH 489 525 6.2
    A25 (Ex. 25) WQ+PA 509 555 15.5 1.57
    AQ+PA 501 545 7.7
    WQ+BH 541 558 13.9 11.28
    AQ+BH 480 513 6.8
    C7 (C.Ex. 7) WQ+PA 553 619 13.2 24.23
    AQ+PA 419 486 17.8
    WQ+BH 570 604 8.4 35.44
    AQ+BH 368 456 6.5
    C8 (C.Ex. 8) WQ+PA 552 610 12.8 21.74
    AQ+PA 432 488 16.7
    WQ+BH 566 599 8.7 33.57
    AQ+BH 376 460 6.9
    C9 (C.Ex. 9) WQ+PA 549 611 13.1 18.94
    AQ+PA 445 494 17.5
    WQ+BH 568 602 9.0 31.87
    AQ+BH 387 466 7.3
    C10 (C.Ex. 10) WQ+PA 553 619 13.2 30.02
    AQ+PA 387 456 17.9
    WQ+BH 570 604 8.4 41.40
    AQ+BH 334 427 5.5
    C11 (C.Ex. 11) WQ+PA 553 619 13.2 27.67
    AQ+PA 400 441 18.2
    WQ+BH 570 604 8.4 38.42
    AQ+BH 351 452 5.3
    C12 (C.Ex. 12) WQ+PA 553 619 13.2 25.32
    AQ+PA 413 478 17.3
    WQ+BH 570 604 8.4 37.13
    AQ+BH 358 459 5.6
  • As seen from Table 4, the alloy sheets of Examples A12-A25 of the invention showed significantly higher tensile properties than those of the alloy sheets of comparative examples C7-C12, with yield strength >480 MPa, tensile strength >520 MPa, elongation >5.5% and yield strength loss coefficient R ≤ 15%. On the other hand, the comparative examples C7-C12 showed higher quenching sensitivity and significantly larger yield strength loss coefficients R, due to the excessive addition of trace elements such as Cr, Mn and Zr.
  • The alloys of Examples A12-A15 showed relatively low quenching sensitivity with a yield strength loss coefficient less than 8%, due to the absence of trace elements such as Cr, Mn, Zr and the like.
  • The alloys of Example A16-A21 added about 0.05% of Zr, similar to Example A4, and showed slightly increased yield strength loss coefficients R in the cases of water quenching and air quenching with subsequent baking treatment, indicating that the quenching sensitivity of the alloys was increased with the addition of Zr element. Also, with the increase of Zr contents, the quenching sensitivity increases dramatically, and the strength loses significantly. For example, the comparative examples C7-C9 sheets present significant increase in yield strength loss coefficients, especially for comparative alloy C7 with the highest Zr content whose yield strength loss coefficients was as high as 24.23% and 35.44%. The quenching sensitivity was increased dramatically, and the strength was significant lost.
  • Examples A22 and A23 contained 0.048% and 0.044% Cr. Similar to Examples A16-A21, the yield strength loss coefficients R for the cases of water quenching and air quenching with subsequent baking treatment (i.e., WQ + BH and AQ + BH) were also increased slightly, but with relatively little effect. With the increase of the Cr content, such as comparative examples C10 and C11 with 0.212% and 0.125% Cr, the R values of the alloy sheets were sharply increased up to 30.02%, 41.40%, 27.67% and 38.42%, respectively. The corresponding strengths were sharply decreased, wherein the yield strength for the AQ + PA sample was less than 400 MPa, and the yield strength for the AQ + BH sample was even lower. The excessive addition of the Cr element significantly deteriorates the quenching sensitivity of the alloy.
  • The alloy of Example A24 and the alloy of Example A25 respectively contained 0.131% of Mn element and 0.245% of Mn element, and similarly, the yield strength loss coefficients R for the cases of water quenching and air quenching with subsequent baking treatment (namely WQ + BH and AQ + BH) of the alloy sheets were slightly increased, while the influence on the mechanical property was not very obvious. However, with the increase of Mn content to 0.336%, the quenching sensitivity of the alloy was significantly deteriorated, wherein the corresponding R values of the sheet were increased to 25.32% and 37.13%, and the alloy strength was greatly reduced.
  • The microstructures (characterized by SEM) of solution treated (480 °C, 10min) and air quenched sheets of Example A15 (containing no trace elements), C7 (containing 0.121% Zr), C10 (containing 0.212% Cr) and C12 (containing 0.336% Mn) were shown in Fig. 10-13, respectively. Obviously, Example A15 had relatively cleaner microstructure both the inside the grain and at grain boundary, where no residual second phase existed except for the residual massive Al7Cu2Fe phase (as shown in Fig. 10). However, in the cases of comparative examples C7, C10 and C12 added with trace elements Cr, Zr and Mn, the quenching sensitivity of the alloy sheets was increased, and fine second phase particles were present in the microstructure rather than the remaining Al7Cu2Fe phase (see Figs. 11 to 13).
  • Therefore, the addition of trace elements such as Cr, Mn, Zr and the like will form fine dispersed phases that have strong regulation and control effect on the grain structure to reduce the average grain size of the alloy effectively. However, these elements will also significantly affect the quenching sensitivity of the alloy and have disadvantages to the mechanical property of the alloy. As a result, these trace elements should be added in appropriate amounts to regulate the grain structure depending on the actual grain size requirement.
  • The preferred embodiments of the present invention are illustrated above, while it should be noted that, for those skilled in the art, many modifications and optimization could be made without departing from the principle of the present invention, and these modifications and optimization should also be regarded as the protection scope of the present invention.

Claims (15)

  1. A 7xxx series aluminum alloy (preferably sheet) comprising, by weight, Zn in 5.1-10.0%, Mg in 2.0-3.2%, Cu in 1.2-3.0%, Fe in 0-0.5%, Si in 0-0.4%, Ti in 0-0.2%, Cr in 0-0.1%, Zr in 0-0.055%, Mn in 0-0.25%, other grain size controlling element(s) in 0-0.30%, and Al in balance.
  2. The 7xxx-series aluminum alloy (preferably sheet) according to claim 1, having a chemical composition, by weight, of Zn in 5.4 - 7.6%, Mg in 2.0-2.7%, Cu in 1.6 - 2.3%, Fe in 0-0.4%, Si in 0-0.3%, Ti in 0.01-0.15%, Cr in 0-0.05%, Zr in 0-0.05%, Mn in 0-0.25%, other grain size controlling element(s) in 0-0.25%, and Al in balance.
  3. The 7xxx-series aluminum alloy (preferably sheet) according to claim 1, having a chemical composition, by weight, of Zn in 7.6-9.6%, Mg in 2.1-3.1%, Cu in 1.4-2.6%, Fe in 0-0.4%, Si in 0-0.3%, Ti in 0.01-0.15%, Cr in 0-0.05%, Zr in 0-0.05%, Mn in 0-0.25%, other grain size controlling element(s) in 0-0.25%, and Al in balance.
  4. The 7xxx series aluminum alloy (preferably sheet) according to any one of claims 1-3, having a chemical composition, by weight, of Zn in 5.1-6.7%, Mg in 2.0-2.9%, Cu in 1.2-2.6%, Fe in 0-0.5%, Si in 0-0.4%, Cr in 0-0.1%, Zr in 0-0.05%, Mn in 0-0.25%, and Al in balance.
  5. The 7xxx series aluminum alloy (preferably sheet) according to any one of claims 1-4, having a chemical composition, by weight, of Zn in 5.4 - 6.5%, Mg in 2.0-2.7%, Cu in 1.6 - 2.3%, Fe in 0-0.4%, Si in 0-0.3%, Cr in 0-0.05%, Zr in 0-0.05%, Mn in 0-0.15%, and Al in balance.
  6. The 7xxx series aluminum alloy (preferably sheet) according to any one of claims 1-5, comprising Fe in 0.05-0.4%, Si in 0.05-0.3%, Cr in 0.001-0.05%, Zr in 0.001-0.04%, Mn in 0.001-0.15%, and other grain size controlling element(s) in 0-0.15%.
  7. The 7xxx-series aluminum alloy (preferably sheet) according to any one of claims 1-6, comprising Cr in 0-0.05%, Zr in 0-0.04%, Mn in 0-0.15%, and other grain size controlling element(s) in 0-0.15%, and/or having a combined content by weight of Cr, Mn, Zr and other grain size controlling element(s) (preferably Cr, Mn, and Zr, such as present alone, or present as a mixture of two or more) of ≤ 0.25% (preferably ≤ 0.20% or ≤ 0.15%).
  8. The 7xxx series aluminum alloy sheet according to any one of claims 1-7, having an average grain size of 10-100 µm (preferably 15-70 µm) and/or a thickness of 0.5-10.0 mm (preferably 1.0-4.0 mm), after maintaining the temperature at 450-510 °C for 5-20 min.
  9. The 7xxx series aluminum alloy sheet according to any one of claims 1-8, having at least one of the following properties:
    (1) being suitable for an integrated hot forming-quenching process,
    (2) being able of completing the solid solution treatment at 450-510 °C within 5-20 min,
    (3) low quenching sensitivity, and
    (4) being in the cold-rolled-state, O-state or T4-state sheet.
  10. The 7xxx series aluminum alloy sheet according to any one of claims 1-9, having a yield strength >400 MPa (preferably >480 MPa), a tensile strength >450 MPa (preferably >520 MPa) and an elongation >6.5% (preferably >5.5%), after maintaining the temperature at 450-510 °C for 5-20 min, followed by an air quenching, a mold quenching or a water quenching and then an artificial peak aging or a paint-baking treatment.
  11. A process of producing a 7xxx series aluminum alloy sheet, comprising the steps of carrying out homogenization treatment, hot rolling treatment and cold rolling treatment on a 7xxx series aluminum alloy cast ingot, to obtain the 7xxx series aluminum alloy sheet, wherein the 7xxx series aluminum alloy cast ingot has a chemical composition of, by weight, 5.1-10.0% of Zn, 2.0-3.2% of Mg, 1.2-3.0% of Cu, 0-0.5% of Fe, 0-0.4% of Si, 0-0.2% of Ti, 0-0.1% of Cr, 0-0.055% of Zr, 0-0.30% of Mn and the balance of Al.
  12. The process according to claim 11, wherein the homogenization treatment comprises: heating the 7xxx series aluminum alloy ingot to 375-460 °C (preferably 400-450 °C), maintaining the temperature for 0-15 hours (preferably 5-10 hours), then heating to 465-490 °C (preferably 470-490 °C or 470-485 °C), maintaining the temperature for 10-48 hours (preferably 10-36 hours or 16-36 hours), then cooling to room temperature by air quenching or being cooled together with the furnace, wherein the heating rate is 15-75 °C/h (preferably 25-75 °C/h or 25-50 °C/h). And/or the hot rolling treatment comprises: hot rough rolling and hot finish rolling to 4-14 mm (preferably 4-8 mm or 6-10 mm), at a final rolling temperature of 200-460 °C (preferably 250-350 °C, 300-460 °C or 350-450 °C), and coiling followed by air quenching to room temperature, and/or the cold rolling treatment comprises: cold rolling to 0.5-10.0 mm (preferably 1.0-4.0 mm) to obtain the 7xxx series aluminum alloy sheet (in a cold-rolled-state), and/or the process further comprises a step of box annealing or continuous annealing of the 7xxx series aluminum alloy sheet in the cold-rolled-state to obtain an O-state or a T4-state alloy sheet, and/or the process further comprises a step of maintaining the temperature of the homogenized ingot at 300-480 °C (preferably 380-450 °C) for 2-30 hours (preferably 3-20 hours) before the hot rolling treatment.
  13. An integrated hot forming-quenching processing process, comprising a step of subjecting a 7xxx-series aluminum alloy sheet according to any one of claims 1-10 or a 7xxx-series aluminum alloy sheet produced by the process according to claim 11 or 12 to an integrated hot forming-quenching processing.
  14. A vehicle part (particularly an automobile part), made of the 7xxx-series aluminum alloy sheet according to any one of claims 1-10 or produced by the processing process according to claim 13.
  15. A vehicle provided with the vehicle part according to claim 14.
EP20901677.3A 2019-12-17 2020-12-17 7xxx series aluminum alloy or plate, manufacturing method therefor, processing method therefor, and application thereof Pending EP4063530A4 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
CN201911301001.9A CN110885942B (en) 2019-12-17 2019-12-17 Medium-strength 7xxx series aluminum alloy plate suitable for hot stamping forming-quenching integrated process
PCT/CN2020/137405 WO2021121343A1 (en) 2019-12-17 2020-12-17 7xxx series aluminum alloy or plate, manufacturing method therefor, processing method therefor, and application thereof

Publications (2)

Publication Number Publication Date
EP4063530A1 true EP4063530A1 (en) 2022-09-28
EP4063530A4 EP4063530A4 (en) 2023-07-19

Family

ID=69752221

Family Applications (1)

Application Number Title Priority Date Filing Date
EP20901677.3A Pending EP4063530A4 (en) 2019-12-17 2020-12-17 7xxx series aluminum alloy or plate, manufacturing method therefor, processing method therefor, and application thereof

Country Status (3)

Country Link
EP (1) EP4063530A4 (en)
CN (2) CN110885942B (en)
WO (1) WO2021121343A1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN119736530A (en) * 2024-12-24 2025-04-01 广东齐力澳美高新材料股份有限公司 Middle-high temperature resistant 7-series aluminum alloy section bar and preparation method and application thereof

Families Citing this family (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110885942B (en) * 2019-12-17 2021-05-07 中铝材料应用研究院有限公司 Medium-strength 7xxx series aluminum alloy plate suitable for hot stamping forming-quenching integrated process
CN111876639A (en) * 2020-08-06 2020-11-03 北部湾大学 A kind of manufacturing method of 7000 series aluminum alloy for automobile column and its plate
CN114807696A (en) * 2021-01-28 2022-07-29 宝山钢铁股份有限公司 Aluminum alloy plate, preparation method thereof and automobile component
CN114807794B (en) * 2021-01-28 2023-04-11 宝山钢铁股份有限公司 Aluminum alloy product, manufacturing method thereof and automobile structural part
CN113337760B (en) * 2021-06-04 2022-08-02 河南明晟新材料科技有限公司 Method for improving O-state conductivity of 5754 alloy
CN113667867A (en) * 2021-07-30 2021-11-19 宁波吉胜铸业有限公司 High-strength connecting piece
CN117305733B (en) * 2022-06-20 2025-10-14 宝山钢铁股份有限公司 A method for manufacturing an Al-Zn-Mg-Cu series aluminum alloy plate and an aluminum alloy plate
CN115094277B (en) * 2022-07-11 2023-01-24 上海交通大学 Mixed crystal structure aluminum alloy and preparation method and application thereof
CN115449675A (en) * 2022-07-28 2022-12-09 广西南南铝加工有限公司 Al-Zn-Mg ultrahigh-strength aluminum alloy and preparation method thereof
CN115652151B (en) * 2022-12-14 2023-04-07 中铝材料应用研究院有限公司 6xxx series aluminum alloy plate suitable for hot stamping forming formability integrated process, and preparation method and application thereof
CN116083765B (en) * 2023-01-17 2024-07-23 上海交通大学 Hafnium-containing aluminum alloy and preparation method and application thereof
TWI852413B (en) * 2023-03-20 2024-08-11 中國鋼鐵股份有限公司 Aluminum alloy plate, method of forming the same and aluminum component for car structure
CN116287906A (en) * 2023-03-28 2023-06-23 中铝瑞闽股份有限公司 Aluminum alloy strip for light ultra-high strength shield and preparation method thereof
CN117144212A (en) * 2023-09-27 2023-12-01 北京科技大学 An ultra-high-strength, high-toughness, stress-corrosion-resistant aluminum alloy and its preparation method
CN117583420A (en) * 2023-10-27 2024-02-23 中国航发北京航空材料研究院 A preparation process for 750MPa ultra-high-strength aluminum alloy sheets
CN117127130B (en) * 2023-10-27 2024-02-20 中铝材料应用研究院有限公司 Multistage homogenization treatment method for aluminum alloy and aluminum alloy
CN117949279B (en) * 2024-03-26 2024-06-21 有研工程技术研究院有限公司 Method for evaluating homogenization effect of 2xxx aluminum alloy cast ingot
CN118422020B (en) * 2024-05-07 2025-06-20 沈阳工程学院 Al-Zn-Mg-Cu series high-strength aluminum alloy and forming method
CN119571149B (en) * 2024-11-19 2026-01-16 东北轻合金有限责任公司 Manufacturing method of Al-Zn-Mg-Cu aluminum alloy flat ingot
CN119220915B (en) * 2024-11-28 2025-02-18 中国航发北京航空材料研究院 Method for improving toughness of aluminum alloy sheet and reducing manufacturing cost
CN119736531B (en) * 2024-12-26 2025-11-04 东北轻合金有限责任公司 A large-size high-strength rare-earth aluminum alloy ingot and its preparation method

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2017075319A1 (en) 2015-10-30 2017-05-04 Novelis Inc. High strength 7xxx aluminum alloys and methods of making the same

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB476930A (en) * 1936-03-16 1937-12-16 Tennyson Fraser Bradbury A new aluminium alloy
FR2510231A1 (en) * 1981-07-22 1983-01-28 Gerzat Metallurg METHOD FOR MANUFACTURING HOLLOW BODIES UNDER PRESSURE OF ALUMINUM ALLOYS
JPH07252573A (en) * 1994-03-17 1995-10-03 Kobe Steel Ltd Al-zn-mg-cu alloy excellent in toughness and its production
US6315842B1 (en) * 1997-07-21 2001-11-13 Pechiney Rhenalu Thick alznmgcu alloy products with improved properties
US7214281B2 (en) * 2002-09-21 2007-05-08 Universal Alloy Corporation Aluminum-zinc-magnesium-copper alloy extrusion
WO2009156283A1 (en) * 2008-06-24 2009-12-30 Aleris Aluminum Koblenz Gmbh Al-zn-mg alloy product with reduced quench sensitivity
CN105543592B (en) * 2009-06-12 2018-08-14 阿勒里斯铝业科布伦茨有限公司 Structural partsof automobiles and its manufacturing method made of AlZnMgCu alloy products
WO2015132932A1 (en) * 2014-03-06 2015-09-11 株式会社Uacj Structural aluminum alloy and process for producing same
EP3018226A1 (en) * 2014-11-05 2016-05-11 Constellium Valais SA (AG, Ltd) Ultra high strength products forged from 6xxx aluminium alloys having excellent corrosion resistance
WO2017062225A1 (en) * 2015-10-08 2017-04-13 Novelis Inc. Optimization of aluminum hot working
CN108220698B (en) * 2018-01-12 2019-10-22 北京科技大学 A kind of preparation method of high formability aluminum alloy composite plate for car body outer panel
CN108546858A (en) * 2018-05-29 2018-09-18 广西南南铝加工有限公司 A kind of 7xxx line aluminium alloys plank and its preparation process
CN108994135B (en) * 2018-07-11 2020-01-21 北京航星机器制造有限公司 Thermoforming and quenching integrated forming method
CN109457150A (en) * 2018-12-05 2019-03-12 天津忠旺铝业有限公司 A kind of container 7 line aluminium alloys and its processing technology
CN110305719A (en) * 2019-06-20 2019-10-08 湖北永喆热冲压零部件有限公司 Drop stamping is with lubricator and the quenching integrated technique of high-strength aluminum alloy drop stamping
CN110885942B (en) * 2019-12-17 2021-05-07 中铝材料应用研究院有限公司 Medium-strength 7xxx series aluminum alloy plate suitable for hot stamping forming-quenching integrated process

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2017075319A1 (en) 2015-10-30 2017-05-04 Novelis Inc. High strength 7xxx aluminum alloys and methods of making the same

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN119736530A (en) * 2024-12-24 2025-04-01 广东齐力澳美高新材料股份有限公司 Middle-high temperature resistant 7-series aluminum alloy section bar and preparation method and application thereof

Also Published As

Publication number Publication date
CN114929913A (en) 2022-08-19
CN110885942B (en) 2021-05-07
CN110885942A (en) 2020-03-17
EP4063530A4 (en) 2023-07-19
WO2021121343A1 (en) 2021-06-24

Similar Documents

Publication Publication Date Title
EP4063530A1 (en) 7xxx series aluminum alloy or plate, manufacturing method therefor, processing method therefor, and application thereof
EP3532219B1 (en) High strength 6xxx series aluminum alloys and methods of making the same
EP3303649B1 (en) An automotive body part comprising an aluminium alloy and a method for producing the automotive body part
KR20160021749A (en) Aluminum alloy material suitable for manufacturing of automobile sheet, and preparation method therefor
EP3183373B1 (en) Aa6xxx aluminum alloy sheet with high anodized quality and method for making same
CN107532247B (en) High strength aluminum alloy plate
EP3662091A1 (en) 6xxxx-series rolled sheet product with improved formability
EP4617392A1 (en) 6xxx-series aluminum alloy plate suitable for hot stamping forming and formability integrated process, and preparation method therefor and use thereof
CN105593392B (en) Bendability and the excellent high-strength aluminium alloy plate of shape freezing and its manufacture method
EP0480402B1 (en) Process for manufacturing aluminium alloy material with excellent formability, shape fixability and bake hardenability
WO2019167469A1 (en) Al-mg-si system aluminum alloy material
EP3191611B1 (en) Alloys for highly shaped aluminum products and methods of making the same
CN104975207A (en) Al-Mg-Si aluminum alloy material, aluminum alloy plate, and preparation methods of Al-Mg-Si aluminum alloy material and aluminum alloy plate
KR20210024575A (en) High formability, recycled aluminum alloy and its manufacturing method
CN112626386A (en) High-strength corrosion-resistant Al-Mg-Si-Cu aluminum alloy and preparation method and application thereof
TW202033775A (en) Method for manufacturing aluminum-manganese alloy
JP2004238657A (en) Method of manufacturing aluminum alloy plate for outer panel
JP3871462B2 (en) Method for producing aluminum alloy plate for can body
JPH06340940A (en) Aluminum alloy sheet excellent in press formability and baking hardenability and its production
JPH0543974A (en) Aluminum alloy sheet excellent in baking hardenability of coating material and press formability and its production
JP2026508834A (en) Method for manufacturing aluminum alloy sheet material and aluminum alloy sheet material
JPH07166285A (en) Hardened al alloy sheet by baking and production thereof
JPH05331588A (en) Aluminum alloy plate having excellent flange formability for forming and method for producing the same
CN114086034B (en) Al-Mg-Si series aluminum alloy plate
JP2024509070A (en) Variants of high-strength 5XXX aluminum alloys and their preparation method

Legal Events

Date Code Title Description
STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE INTERNATIONAL PUBLICATION HAS BEEN MADE

PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: REQUEST FOR EXAMINATION WAS MADE

17P Request for examination filed

Effective date: 20220624

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

DAV Request for validation of the european patent (deleted)
DAX Request for extension of the european patent (deleted)
A4 Supplementary search report drawn up and despatched

Effective date: 20230616

RIC1 Information provided on ipc code assigned before grant

Ipc: C22F 1/053 20060101ALI20230612BHEP

Ipc: C22C 21/10 20060101AFI20230612BHEP

TPAC Observations filed by third parties

Free format text: ORIGINAL CODE: EPIDOSNTIPA