US20220127708A1 - Method for producing a sheet or strip from an aluminium alloy, and a sheet, strip or molded part produced thereby - Google Patents
Method for producing a sheet or strip from an aluminium alloy, and a sheet, strip or molded part produced thereby Download PDFInfo
- Publication number
- US20220127708A1 US20220127708A1 US17/427,460 US202017427460A US2022127708A1 US 20220127708 A1 US20220127708 A1 US 20220127708A1 US 202017427460 A US202017427460 A US 202017427460A US 2022127708 A1 US2022127708 A1 US 2022127708A1
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- United States
- Prior art keywords
- sheet
- strip
- rolling
- optionally
- aluminum alloy
- 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
Links
- 229910000838 Al alloy Inorganic materials 0.000 title claims abstract description 34
- 238000004519 manufacturing process Methods 0.000 title claims abstract description 12
- 238000001816 cooling Methods 0.000 claims abstract description 65
- 238000000137 annealing Methods 0.000 claims abstract description 31
- 238000010438 heat treatment Methods 0.000 claims abstract description 28
- 238000001953 recrystallisation Methods 0.000 claims abstract description 12
- 239000002245 particle Substances 0.000 claims description 57
- 238000005096 rolling process Methods 0.000 claims description 52
- 239000011572 manganese Substances 0.000 claims description 30
- 238000000034 method Methods 0.000 claims description 30
- 239000013078 crystal Substances 0.000 claims description 26
- 238000005097 cold rolling Methods 0.000 claims description 23
- 239000011777 magnesium Substances 0.000 claims description 18
- 239000010949 copper Substances 0.000 claims description 12
- 238000005098 hot rolling Methods 0.000 claims description 12
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims description 8
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 claims description 8
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 claims description 8
- 239000011651 chromium Substances 0.000 claims description 8
- 229910052749 magnesium Inorganic materials 0.000 claims description 8
- 229910052748 manganese Inorganic materials 0.000 claims description 8
- 239000010955 niobium Substances 0.000 claims description 8
- JBQYATWDVHIOAR-UHFFFAOYSA-N tellanylidenegermanium Chemical compound [Te]=[Ge] JBQYATWDVHIOAR-UHFFFAOYSA-N 0.000 claims description 8
- 239000010936 titanium Substances 0.000 claims description 8
- 230000006641 stabilisation Effects 0.000 claims description 7
- 238000011105 stabilization Methods 0.000 claims description 7
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims description 6
- 229910052802 copper Inorganic materials 0.000 claims description 6
- 229910052782 aluminium Inorganic materials 0.000 claims description 5
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 5
- 229910018131 Al-Mn Inorganic materials 0.000 claims description 4
- 229910018461 Al—Mn Inorganic materials 0.000 claims description 4
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 claims description 4
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 claims description 4
- BQCADISMDOOEFD-UHFFFAOYSA-N Silver Chemical compound [Ag] BQCADISMDOOEFD-UHFFFAOYSA-N 0.000 claims description 4
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 claims description 4
- 238000005266 casting Methods 0.000 claims description 4
- 229910052804 chromium Inorganic materials 0.000 claims description 4
- 238000000265 homogenisation Methods 0.000 claims description 4
- 239000012535 impurity Substances 0.000 claims description 4
- 229910052742 iron Inorganic materials 0.000 claims description 4
- 229910052758 niobium Inorganic materials 0.000 claims description 4
- GUCVJGMIXFAOAE-UHFFFAOYSA-N niobium atom Chemical compound [Nb] GUCVJGMIXFAOAE-UHFFFAOYSA-N 0.000 claims description 4
- VSZWPYCFIRKVQL-UHFFFAOYSA-N selanylidenegallium;selenium Chemical compound [Se].[Se]=[Ga].[Se]=[Ga] VSZWPYCFIRKVQL-UHFFFAOYSA-N 0.000 claims description 4
- 229910052710 silicon Inorganic materials 0.000 claims description 4
- 239000010703 silicon Substances 0.000 claims description 4
- 229910052709 silver Inorganic materials 0.000 claims description 4
- 239000004332 silver Substances 0.000 claims description 4
- 229910052715 tantalum Inorganic materials 0.000 claims description 4
- GUVRBAGPIYLISA-UHFFFAOYSA-N tantalum atom Chemical compound [Ta] GUVRBAGPIYLISA-UHFFFAOYSA-N 0.000 claims description 4
- 229910052719 titanium Inorganic materials 0.000 claims description 4
- LEONUFNNVUYDNQ-UHFFFAOYSA-N vanadium atom Chemical compound [V] LEONUFNNVUYDNQ-UHFFFAOYSA-N 0.000 claims description 3
- 239000000203 mixture Substances 0.000 abstract description 13
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 10
- 229910045601 alloy Inorganic materials 0.000 description 9
- 239000000956 alloy Substances 0.000 description 9
- 239000011164 primary particle Substances 0.000 description 9
- 239000000047 product Substances 0.000 description 8
- 238000010791 quenching Methods 0.000 description 8
- 230000000171 quenching effect Effects 0.000 description 8
- 239000000126 substance Substances 0.000 description 7
- 238000009864 tensile test Methods 0.000 description 4
- 229910018134 Al-Mg Inorganic materials 0.000 description 3
- 229910018467 Al—Mg Inorganic materials 0.000 description 3
- 238000010276 construction Methods 0.000 description 3
- 238000005275 alloying Methods 0.000 description 2
- 239000011265 semifinished product Substances 0.000 description 2
- 239000011701 zinc Substances 0.000 description 2
- 229910000914 Mn alloy Inorganic materials 0.000 description 1
- 229910001297 Zn alloy Inorganic materials 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 238000009826 distribution Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000001771 impaired effect Effects 0.000 description 1
- 239000011159 matrix material Substances 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
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
- C22C21/06—Alloys based on aluminium with magnesium as the next major constituent
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C21/00—Alloys based on aluminium
- C22C21/06—Alloys based on aluminium with magnesium as the next major constituent
- C22C21/08—Alloys based on aluminium with magnesium as the next major constituent with silicon
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
- C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
- C22F1/04—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon
- C22F1/047—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 magnesium as the next major constituent
Definitions
- the invention relates to a method for producing a sheet or strip from an aluminum alloy and to a sheet, strip, or molded part produced thereby.
- the object of the invention is to create a method for producing a sheet or strip from an aluminum alloy having Mg as one of the main alloying elements and to create a sheet or strip of the type described above that has a comparatively high strength and formability and is of ssf quality or ffa quality.
- the method should also be easy to use and reproducible.
- the sheet or strip in the method is composed of an aluminum alloy, namely with the composition of from 2.0 to 5.5 wt % magnesium (Mg), from 0.2 to 1.2 wt % manganese (Mn), optionally up to 0.45 wt % silicon (Si), optionally up to 0.55 wt % iron (Fe), optionally up to 0.35 wt % chromium (Cr), optionally up to 0.2 wt % titanium (Ti), optionally up to 0.2 wt % silver (Ag), optionally up to 4.0 wt % zinc (Zn), optionally up to 0.8 wt % copper (Cu), optionally up to 0.8 wt % zirconium (Zr), optionally up to 0.3 wt % niobium (Nb), optionally up to 0.25 wt % tantalum (Ta), optionally up to 0.05 wt % vanadium (V), and the remainder comprised of aluminum and inevitable
- the method has the following method steps:
- the method can have the following method steps:
- the sheet or strip that has been cold-rolled to the final thickness has at least one, more particularly primary, intermetallic phase with first particles having an average particle size of 5 ⁇ m to 10 ⁇ m (measured using the ASTM E112 linear intercept method)—this by means of the method steps preceding the heat treatment.
- first particles having an average particle size of 5 ⁇ m to 10 ⁇ m measured using the ASTM E112 linear intercept method
- the sheet or strip has at least one intermetallic phase with first particles having an average particle size of 5 ⁇ m to 10 ⁇ m.
- These first and thus primary particles are relatively coarse.
- These particles of the primary phase also have a high stability—even relative to a subsequent recrystallization annealing or relative to a subsequent heat treatment.
- this sheet or strip that has been cold-rolled to the final thickness also has an average crystal grain size D of ⁇ 60 ⁇ m (measured using the ASTM E112 linear intercept method) and the average crystal grain size D in mm and the number A of first particles per mm 2 in the aluminum alloy satisfy the condition ⁇ square root over (D) ⁇ *A>1.8—for example in that the recrystallization annealing of the heat treatment is performed in such a way.
- This method is also easy to use and has an extremely high reproducibility, for example due to a water cooling for the accelerated cooling, for producing a sheet or strip in ssf quality or ffa quality.
- the number of dislocations in the sheet or strip can be further increased in the method if ⁇ square root over (D) ⁇ *A is >2. More particularly, if ⁇ square root over (D) ⁇ *A is >2.5, then the sheet or strip can satisfy comparatively high quality requirements without having to also fear the occurrence of stretcher strain marks such as type A Lüders bands on the surface of the formed sheet or strip, even in the case of comparatively complex geometries or unfavorable plastic deformations.
- the method can be further improved in terms of reproducibility if in the heat treatment, the recrystallization annealing takes place by means of holding at a temperature of 300° C. (degrees Celsius) or more, more particularly up to 600° C. This can improve even more if the recrystallization annealing takes place at 450° C. to 550° C.
- this annealing temperature can be enough to pre-stress the structure by means of an accelerated cooling sufficiently to produce the dislocations at the first particles, which subsequently make Lüders band dislocations unnecessary.
- the heated sheet is cooled in an accelerated manner at a cooling rate of at least 10 K/s (Kelvin per second), more particularly at least 20 K/s or at least 50 K/s, wherein this accelerated cooling can more particularly be carried out to below 180° C., more particularly to room temperature.
- K/s Kelvin per second
- first particles are embodied as large enough in the average particle size if the rolling slab is solidified by maintaining a cooling rate (or cooling speed) of ⁇ 2.5° C./s.
- the cooling rate is ⁇ 2° C./s or ⁇ 1° C./s or ⁇ 0.75° C./s.
- this can counteract a possible reduction in the average particle size by means of subsequent method steps, for example by means of the cold rolling, in order to ensure an average particle size of 5 ⁇ m to 10 ⁇ m before the heat treatment.
- the optional homogenization can take place by means of holding at 450° C. to 550° C. for at least 0.5 h.
- the hot rolling can take place at 280° C. to 550° C.
- the cold rolling to the final thickness can be carried out with a degree of rolling reduction of from 10% to 65%, more particularly from 20% to 50%. More particularly, it can be advantageous if the cold rolling after the intermediate annealing is carried out with a degree of rolling reduction of from 10% to 65%, more particularly from 20% to 50%, in order to improve the reproducibility of the average particle size of 5 ⁇ m to 10 ⁇ m.
- the optional intermediate annealing can take place by means of holding at 300° C. to 500° C.
- the optional stabilization can take place by means of holding at 80° C. to 120° C. for at least 0.5 h.
- An average particle size of 5 ⁇ m to 10 ⁇ m before the heat treatment can more particularly be assured if the product of the degree of rolling reduction in % after the intermediate annealing and the cooling rate in ° C./s satisfies the condition 10 ⁇ degree of rolling reduction*cooling rate ⁇ 50, more particularly 20 ⁇ degree of rolling reduction*cooling rate ⁇ 45.
- the intermetallic phase has an Al—Mn basis, then it is possible to produce the dislocations in the aluminum alloy that enable stretcher strain marks to be avoided in a particularly reliable way.
- the intermetallic phase is of the Al 13 (Mn,Fe) 6 type or of the Al 16 FeMn 3 Si 2 type or of the Al 12 Mn type or of the Al 6 Mn type.
- These first particles of the primary phase are a particularly stable phase. It is also conceivable for the primary phase to constitute the intermetallic phase in order, in combination with the heat treatment of the sheet or strip, to produce a sufficient number of dislocations.
- the method can achieve high strength and formability while avoiding orange peel and stretcher strain marks if the aluminum alloy (with an Al—Mg—Mn basis) has from 4.0 to 5.0 wt % magnesium (Mg) and/or from 0.2 to 0.5 wt % manganese (Mn).
- the aluminum alloy also has from 2.0 to 4.0 wt % zinc (Zn) (Al—Mg—Zn basis).
- this aluminum alloy can also have up to 0.8 wt % copper (Cu).
- the sheet or strip is composed of an aluminum alloy, namely with the alloy contents from 2.0 to 5.5 wt % magnesium (Mg), from 0.2 to 1.2 wt % manganese (Mn), optionally up to 0.45 wt % silicon (Si), optionally up to 0.55 wt % iron (Fe), optionally up to 0.35 wt % chromium (Cr), optionally up to 0.2 wt % titanium (Ti), optionally up to 0.2 wt % silver (Ag), optionally up to 4.0 wt % zinc (Zn), optionally up to 0.8 wt % copper (Cu), optionally up to 0.8 wt % zirconium (Zr), optionally up to 0.3 wt % niobium (Nb), optionally up to 0.25 wt % tantalum (Ta), and the remainder comprised of aluminum and inevitable production-related impurities, with up to at most 0.05 wt % of each and all together
- the formed sheet or strip can be achieved if this sheet or strip has an average crystal grain size D of ⁇ 60 ⁇ m (measured using the ASTM E112 linear intercept method) and at least one, more particularly primary, intermetallic phase with first particles having an average particle size of 5 ⁇ m to 10 ⁇ m (measured using the ASTM E112 linear intercept method) and the average crystal grain size D in mm and the number A of first particles per mm 2 in the aluminum alloy satisfy the condition ⁇ square root over (D) ⁇ *A>1.8.
- the sheet or strip It is also necessary for the sheet or strip to have been subjected to a heat treatment, including recrystallization annealing with subsequent accelerated cooling and optionally a stabilization of the sheet or strip that has undergone accelerated cooling. As a result, dislocations are produced at the first particles in the structure of the sheet or strip. These first and thus primary particles are also stable relative to the heat treatment that is used to further adjust the microstructure of the sheet or strip.
- the average crystal grain size D of ⁇ 60 ⁇ m according to the invention results in the fact that the comparatively fine crystal grain of the sheet or strip enables achievement of a high strength and formability.
- the first particles that are present in the sheet or strip have a limited average particle size of 5 ⁇ m to 10 ⁇ m and the average crystal grain size D in mm and the number A of first particles per mm 2 in the aluminum alloy satisfy the condition ⁇ square root over (D) ⁇ *A>1.8.
- this can ensure a sufficiently high number of dislocations in the sheet or strip. This prevents the formation of Lüders band dislocations even with complex geometries.
- this produces a sheet or strip composed of an aluminum alloy, preferably with an Al—Mg basis (or with Mg as one of the main alloying elements) in ssf quality or ffa quality, which due to its sufficient strength and formability can also excel when used, for example, for outer shell components in vehicle body construction.
- the number of dislocations in the sheet or strip can be further increased if ⁇ square root over (D) ⁇ *A is >2. More particularly, if ⁇ square root over (D) ⁇ *A is >2.5, then the sheet or strip can satisfy comparatively high quality requirements without having to also fear the occurrence of stretcher strain marks such as type A Lüders bands on the surface of the formed sheet or strip, even in the case of comparatively complex geometries or unfavorable plastic deformations.
- a sufficient number of dislocations in order to avoid stretcher strain marks in the formed sheet or strip can be achieved if the crystal structure has more than 200, more particularly more than 400, dislocations at each first particle. This can be achieved if the sheet or strip has been heat treated by heating and subsequent accelerated cooling in such a way that the crystal structure has more than 200, more particularly more than 400, dislocations at each first particle.
- the number A of first particles is ⁇ 10 particles/mm 2 , which can enable a sufficient distribution of the dislocations in the sheet or strip in order to avoid stretcher strain marks. This is more particularly the case if the number A of first particles is ⁇ 25 particles/mm 2 , preferably ⁇ 35 particles/mm 2 .
- the intermetallic phase has an Al—Mn basis, then it is possible to produce the dislocations in the aluminum alloy that enable stretcher strain marks to be avoided in a particularly reliable way.
- the intermetallic phase is of the Al 13 (Mn,Fe) 6 type or of the Al 16 FeMn 3 Si 2 type or of the Al 12 Mn type or of the Al 6 Mn type.
- These first particles of the primary phase are a particularly stable phase. It is also conceivable for the primary phase to constitute the intermetallic phase in order, through the subsequent heat treatment of the sheet or strip, to achieve a sufficient number of dislocations.
- the method can achieve high strength and formability while avoiding orange peel and stretcher strain marks if the aluminum alloy has from 4.0 to 5.0 wt % magnesium (Mg) and/or from 0.2 to 0.5 wt % manganese (Mn).
- the aluminum alloy also has from 2.0 to 4.0 wt % zinc (Zn) (with an Al—Mg—Zn basis).
- this aluminum alloy can also have up to 0.8 wt % copper (Cu).
- the sheet or strip according to the invention can also be particularly well-suited for producing a molded part, more particularly a vehicle part, preferably a vehicle body part, by means of sheet-metal-forming.
- the sheet or strip is used to produce a sheet bar in order to be able to perform a sheet-metal-forming process.
- the average crystal grain size and the average particle size are measured using the ASTM E112 linear intercept method.
- the aluminum alloy has an Al—Mg basis.
- the sheet or strip can have an average crystal grain size D of ⁇ 50 ⁇ m, ⁇ 40 ⁇ m, or ⁇ 30 ⁇ m.
- the cooling rate (or cooling speed) can be ⁇ 2.4° C./s, ⁇ 2.3° C./s, ⁇ 2.2° C./s, ⁇ 2.1° C./s, ⁇ 2.0° C./s, ⁇ 1.9° C./s, ⁇ 1.8° C./s, ⁇ 1.7° C./s, ⁇ 1.6° C./s, ⁇ 1.5° C./s, ⁇ 1.4° C./s, ⁇ 1.3° C./s, ⁇ 1.2° C./s, ⁇ 1.1° C./s, ⁇ 1.0° C./s, ⁇ 0.9° C./s, ⁇ 0.8° C./s, ⁇ 0.7° C./s, or ⁇ 0.6° C./s.
- the strip can be cut into a slit strip or cut into sheets or also sheet bars can be cut out from the sheet or strip in order to form these semi-finished products, for example by means of sheet-metal-forming.
- the forming can be a deep-drawing, roll profiling, etc.
- the aluminum alloy can, for example, be of the EN AW-5083 or EN AW-5086 or EN AW-5182 or EN AW-5454 or EN AW-5457 or EN AW-5754 type.
- cold-rolled semi-finished products namely thin sheets composed of an aluminum alloy with an Al—Mg—Mn basis and thin sheets composed of and aluminum alloy with an Al—Mg—Zn—Mn basis were produced.
- the following aluminum alloys were used, which were composed of
- sheet bars i.e. sheet blanks
- sheet-metal-formed specifically deep-drawn
- An alloy of the AA5182 type (Al—Mg—Mn basis) with the chemical composition C1 was used to produce a thin sheet A1 with a sheet thickness of 1.2 mm.
- the rolling slab was solidified at a comparatively reduced cooling rate (or cooling speed) and the rolling steps in the hot rolling and cold rolling were carried out in accordance with the standard scheme.
- the last rolling reduction pass in the cold rolling amounted to 63% (from 3.25 mm to 1.2 mm) and the final heat treatment was carried out at 500° C. with subsequent water quenching.
- the average crystal grain size or final grain size of the thin sheet A1 was 15 ⁇ m (measured using the ASTM E112 linear intercept method) and in the primary intermetallic phase, there were 44 first particles per mm 2 having an average particle size of 5 ⁇ m to 10 ⁇ m (measured using the ASTM E112 linear intercept method). These primary particles were also embodied as comparatively coarse. In addition, with the product of the cooling rate after the intermediate annealing and the degree of rolling reduction of 44, the condition 10 ⁇ degree of rolling reduction*cooling rate ⁇ 50 is satisfied.
- An alloy of the AA5182 type with the chemical composition C2 was used to produce a thin sheet A2 with a sheet thickness of 1.2 mm.
- the rolling slab was solidified at a cooling rate (or cooling speed) of 1.8° C./s and the rolling steps in the hot rolling and cold rolling were carried out in accordance with the standard scheme.
- the last rolling reduction pass in the cold rolling amounted to 15% (from 1.41 mm to 1.2 mm) and the final heat treatment was carried out at 500° C. with subsequent water quenching.
- the condition 10 ⁇ degree of rolling reduction*cooling rate ⁇ 50 is satisfied.
- the average crystal grain size or final grain size of the thin sheet A1 after the heat treatment was 35 ⁇ m and in the primary intermetallic phase, there were 12 first particles per mm 2 having an average particle size of 5 ⁇ m to 10 ⁇ m. With a ⁇ D*A value of 2.24, the criterion ( ⁇ D*A>1.8) is satisfied. A tensile test did not show any Lüders bands on the surface of the thin sheet A2.
- the intermetallic phase according to the invention with the first or primary particles was therefore able to provide a sufficient number of dislocations to prevent the occurrence of Lüders bands during the forming.
- An alloy of the AA5182 type with the chemical composition C3 was used to produce a thin sheet A3 with a sheet thickness of 1.2 mm.
- the rolling slab was solidified at a cooling rate (or cooling speed) of 1.8° C./s and the rolling steps in the hot rolling and cold rolling were carried out in accordance with the standard scheme.
- the last rolling reduction pass in the cold rolling amounted to 18% (from 1.46 mm to 1.2 mm) and the final heat treatment was carried out at 500° C. with subsequent water quenching.
- the average crystal grain size or final grain size was 29 ⁇ m and in the primary intermetallic phase, there were 14 first particles per mm 2 having an average particle size of 5 ⁇ m to 10 ⁇ m.
- the condition 10 ⁇ degree of rolling reduction*cooling rate ⁇ 50 is satisfied.
- An alloy of the AA5182 type with the chemical composition C4 was used to produce two thin sheets A4.1 and A4.2 with a sheet thickness of 1.2 mm.
- the rolling slab was solidified at a cooling rate (or cooling speed) of 1.8° C./s and the rolling steps in the hot rolling and cold rolling were carried out in accordance with the standard scheme.
- the last rolling reduction pass in the cold rolling amounted to 25% from 1.60 mm to 1.2 mm).
- the final heat treatment of the thin sheet A4.1 was carried out at 500° C. with subsequent water quenching.
- the final heat treatment of the thin sheet A4.2 was carried out at 370° C. with subsequent cooling in stationary air.
- the average crystal grain size or final grain size of both of the thin sheets A4.1 and A4.2 was 32 ⁇ m and in their primary intermetallic phase, there were 12 first particles per mm 2 having an average particle size of 5 ⁇ m to 10 ⁇ m. With a ⁇ D*A value of 2.14, the criterion ( ⁇ D*A>1.8) is satisfied by both thin sheets A4.1 and A4.2.
- the thin sheet A4.2 exhibits Lüders bands after the deep-drawing.
- the thin sheet A4.2 despite having the same composition and microstructure, because of the slower cooling in stationary air, it was not possible for a sufficient number of dislocations in the structure to form in order to prevent the occurrence of Lüders bands.
- the accelerated water cooling of the thin sheet A4.1 resulted in the fact that the intermetallic phase with the first or primary particles was able to provide a sufficient number of dislocations to prevent the occurrence of Lüders bands during the forming.
- An alloy of the AA5182 type with the chemical composition C4 was used to produce a thin sheet A5 with a sheet thickness of 1.2 mm.
- the rolling slab was solidified at a cooling rate (or cooling speed) of 1.8° C./s and the rolling steps in the hot rolling and cold rolling were carried out in accordance with the standard scheme.
- the last rolling reduction pass in the cold rolling amounted to 63% (from 3.25 mm to 1.2 mm) and the final heat treatment was carried out at 500° C. with subsequent water quenching.
- the average crystal grain size or final grain size was 10 ⁇ m and in the primary intermetallic phase, there were 12 first particles per mm 2 having an average particle size of 5 ⁇ m to 10 ⁇ m.
- An alloy with an Al—Mg—Zn—Mn basis and the chemical composition D1 was used to produce a thin sheet A6.1 with a sheet thickness of 1.2 mm.
- the rolling slab was solidified at a cooling rate (or cooling speed) of 1.8° C./s and the rolling steps in the hot rolling and cold rolling were carried out in accordance with the standard scheme.
- the last rolling reduction pass in the cold rolling amounted to 18% (from 1.46 mm to 1.2 mm).
- the final heat treatment was carried out at 500° C. with subsequent water quenching. After the accelerated cooling, a stabilization was carried out at 100° C. for 3 h.
- the average crystal grain size or final grain size was 28 ⁇ m and in the primary intermetallic phase, there were 14 first particles per mm 2 having an average particle size of 5 ⁇ m to 10 ⁇ m. With a ⁇ D*A value of 2.34, the criterion ( ⁇ D*A>1.8) is satisfied. In addition, with the product of the cooling rate after the intermediate annealing and the degree of rolling reduction of 32, the condition 10 ⁇ degree of rolling reduction*cooling rate ⁇ 50 is satisfied.
- a tensile test did not show any Lüders bands on the surface of the thin sheet A6.1.
- the intermetallic phase according to the invention with the first or primary particles was therefore able to provide a sufficient number of dislocations to prevent the occurrence of Lüders bands during the forming.
- An alloy with an Al—Mg—Zn—Mn basis and the chemical composition D1 was used to produce a thin sheet A6.2 with a sheet thickness of 1.2 mm.
- the rolling slab was solidified at a cooling rate (or cooling speed) of 1.8° C./s and the rolling steps in the hot rolling and cold rolling were carried out in accordance with the standard scheme.
- the last rolling reduction pass in the cold rolling amounted to 63% (from 3.25 mm to 1.2 mm) and the final heat treatment was carried out at 500° C. with subsequent water quenching.
- the average crystal grain size or final grain size was 10 ⁇ m and in the primary intermetallic phase, there were 14 first particles per mm 2 having an average particle size of 5 ⁇ m to 10 ⁇ m.
- Lüders bands were detected.
- the intermetallic phase with the first or primary particles was therefore not able to provide a sufficiently high number of dislocations to prevent the occurrence of Lüders bands during the forming.
- All of the exemplary embodiments according to the invention namely A1, A2, A3, A4.1, and A6.1 share the fact that their crystal structure has more than 200, more particularly more than 400, dislocations at each first particle.
- German expression “ably” can be translated into English as “more particularly.”
- a feature that is preceded by “more particularly” is to be considered an optional feature that can be omitted and therefore does not constitute a limitation, for example of the claims.
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- 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)
- Metal Rolling (AREA)
- Continuous Casting (AREA)
- Heat Treatment Of Sheet Steel (AREA)
- Manufacturing Of Steel Electrode Plates (AREA)
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP19154632.4A EP3690076A1 (fr) | 2019-01-30 | 2019-01-30 | Procédé de fabrication d'une tôle ou d'une bande d'un alliage d'aluminium ainsi que tôle, bande ou pièce moulée fabriqués selon ledit procédé |
EP19154632.4 | 2019-01-30 | ||
PCT/EP2020/052375 WO2020157246A1 (fr) | 2019-01-30 | 2020-01-30 | Procédé de fabrication d'une tôle ou d'un feuillard en un alliage d'aluminium ainsi que tôle, feuillard ou pièce façonnée produit-e par ce procédé |
Publications (1)
Publication Number | Publication Date |
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US20220127708A1 true US20220127708A1 (en) | 2022-04-28 |
Family
ID=65268872
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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US17/427,460 Pending US20220127708A1 (en) | 2019-01-30 | 2020-01-30 | Method for producing a sheet or strip from an aluminium alloy, and a sheet, strip or molded part produced thereby |
Country Status (7)
Country | Link |
---|---|
US (1) | US20220127708A1 (fr) |
EP (2) | EP3690076A1 (fr) |
JP (1) | JP2022519238A (fr) |
CN (1) | CN113474479B (fr) |
CA (1) | CA3128294A1 (fr) |
MX (1) | MX2021009093A (fr) |
WO (1) | WO2020157246A1 (fr) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
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EP3848476A1 (fr) * | 2020-01-07 | 2021-07-14 | AMAG rolling GmbH | Tôle ou bande en alliage d'aluminium durcissable, pièce de véhicule fabriquée à partir de celle-ci, utilisation et procédé de fabrication de tôle ou de bande |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CH638243A5 (de) * | 1978-07-05 | 1983-09-15 | Alusuisse | Verfahren zur herstellung von magnesium- und zinkhaltigen aluminium-legierungs-blechen. |
JPH0668146B2 (ja) * | 1986-09-09 | 1994-08-31 | スカイアルミニウム株式会社 | アルミニウム合金圧延板の製造方法 |
NL9100565A (nl) | 1991-04-02 | 1992-11-02 | Hoogovens Aluminium Nv | Aluminium plaat en werkwijze voor het vervaardigen daarvan. |
DE10231422A1 (de) | 2001-08-13 | 2003-02-27 | Corus Aluminium Nv | Aluminium-Magnesium-Legierungserzeugnis |
SE530437C2 (sv) * | 2006-10-13 | 2008-06-03 | Sapa Heat Transfer Ab | Rankmaterial med hög hållfasthet och högt saggingmotstånd |
CN107787376A (zh) * | 2015-06-25 | 2018-03-09 | 海德鲁铝业钢材有限公司 | 高强度且成形优良的AlMg带材及其生产方法 |
CN106834825B (zh) * | 2016-11-16 | 2018-08-31 | 广西南南铝加工有限公司 | 5182铝合金 |
-
2019
- 2019-01-30 EP EP19154632.4A patent/EP3690076A1/fr not_active Withdrawn
-
2020
- 2020-01-30 EP EP20706105.2A patent/EP3918102A1/fr active Pending
- 2020-01-30 CN CN202080011029.3A patent/CN113474479B/zh active Active
- 2020-01-30 JP JP2021544421A patent/JP2022519238A/ja active Pending
- 2020-01-30 MX MX2021009093A patent/MX2021009093A/es unknown
- 2020-01-30 US US17/427,460 patent/US20220127708A1/en active Pending
- 2020-01-30 CA CA3128294A patent/CA3128294A1/fr active Pending
- 2020-01-30 WO PCT/EP2020/052375 patent/WO2020157246A1/fr unknown
Also Published As
Publication number | Publication date |
---|---|
EP3690076A1 (fr) | 2020-08-05 |
MX2021009093A (es) | 2021-10-22 |
WO2020157246A1 (fr) | 2020-08-06 |
CA3128294A1 (fr) | 2020-08-06 |
EP3918102A1 (fr) | 2021-12-08 |
CN113474479A (zh) | 2021-10-01 |
JP2022519238A (ja) | 2022-03-22 |
CN113474479B (zh) | 2023-06-06 |
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