EP3690076A1 - 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 - Google Patents
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 Download PDFInfo
- Publication number
- EP3690076A1 EP3690076A1 EP19154632.4A EP19154632A EP3690076A1 EP 3690076 A1 EP3690076 A1 EP 3690076A1 EP 19154632 A EP19154632 A EP 19154632A EP 3690076 A1 EP3690076 A1 EP 3690076A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- weight
- sheet
- strip
- particles
- rolling
- 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.)
- Withdrawn
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- 229910000838 Al alloy Inorganic materials 0.000 title claims abstract description 34
- 238000004519 manufacturing process Methods 0.000 title claims abstract description 14
- 229910052751 metal Inorganic materials 0.000 title claims description 12
- 239000002184 metal Substances 0.000 title claims description 12
- 238000001816 cooling Methods 0.000 claims abstract description 62
- 238000000137 annealing Methods 0.000 claims abstract description 29
- 238000010438 heat treatment Methods 0.000 claims abstract description 25
- 238000001953 recrystallisation Methods 0.000 claims abstract description 11
- 239000002245 particle Substances 0.000 claims description 62
- 238000005096 rolling process Methods 0.000 claims description 39
- 239000011572 manganese Substances 0.000 claims description 35
- 238000000034 method Methods 0.000 claims description 31
- 239000013078 crystal Substances 0.000 claims description 26
- 238000005097 cold rolling Methods 0.000 claims description 23
- 239000011777 magnesium Substances 0.000 claims description 19
- 229910052748 manganese Inorganic materials 0.000 claims description 17
- 239000010949 copper Substances 0.000 claims description 12
- 238000005098 hot rolling Methods 0.000 claims description 12
- 229910052782 aluminium Inorganic materials 0.000 claims description 10
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims description 9
- 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
- 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
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims description 6
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 6
- 229910052802 copper Inorganic materials 0.000 claims description 6
- 230000006641 stabilisation Effects 0.000 claims description 6
- 238000011105 stabilization Methods 0.000 claims description 6
- 239000012535 impurity Substances 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
- 229910015136 FeMn Inorganic materials 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
- 229910052804 chromium Inorganic materials 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
- 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
- 238000005266 casting Methods 0.000 claims description 3
- 238000000265 homogenisation Methods 0.000 claims description 3
- LEONUFNNVUYDNQ-UHFFFAOYSA-N vanadium atom Chemical compound [V] LEONUFNNVUYDNQ-UHFFFAOYSA-N 0.000 claims description 3
- 229910052845 zircon Inorganic materials 0.000 claims 2
- GFQYVLUOOAAOGM-UHFFFAOYSA-N zirconium(iv) silicate Chemical compound [Zr+4].[O-][Si]([O-])([O-])[O-] GFQYVLUOOAAOGM-UHFFFAOYSA-N 0.000 claims 2
- 239000000203 mixture Substances 0.000 abstract description 13
- 229910045601 alloy Inorganic materials 0.000 description 13
- 239000000956 alloy Substances 0.000 description 13
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 11
- 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
- 238000005520 cutting process Methods 0.000 description 6
- 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
- 239000011701 zinc Substances 0.000 description 3
- VSZWPYCFIRKVQL-UHFFFAOYSA-N selanylidenegallium;selenium Chemical compound [Se].[Se]=[Ga].[Se]=[Ga] VSZWPYCFIRKVQL-UHFFFAOYSA-N 0.000 description 2
- 239000011265 semifinished product Substances 0.000 description 2
- 229910000914 Mn alloy Inorganic materials 0.000 description 1
- 238000005275 alloying Methods 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 238000006073 displacement reaction Methods 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
- 230000000087 stabilizing effect Effects 0.000 description 1
- 229910052725 zinc Inorganic materials 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
- 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
-
- 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
Definitions
- the invention relates to a method for producing a sheet or strip from an aluminum alloy and a sheet, strip or molded part produced thereby.
- Al-Mg-Mn alloys are therefore only suitable to a limited extent, for example, for outer skin parts in body construction, where ssf (strech strain free) quality or ffa (low flow figure) quality, i.e. freedom or reduction of type A flow figures, is required.
- the process should be easy to use and reproducible.
- the sheet or strip in the process is made of an aluminum alloy with the composition, namely from 2.0 to 5.5% by weight of magnesium (Mg), from 0.2 to 1.2% by weight of manganese (Mn), optionally up to 0.45% by weight silicon (Si), optionally up to 0.55% by weight iron (Fe), optionally up to 0.35% by weight chromium (Cr), optionally up to 0.2% by weight % Titanium (Ti), optionally up to 0.2% by weight silver (Ag), optionally up to 4.0% by weight zinc (Zn), optionally up to 0.8% by weight copper (Cu), optionally up to 0.8% by weight of zirconium (Zr), optionally up to 0.3% by weight of niobium (Nb), optionally up to 0.25% by weight of tantalum (Ta), optionally up to 0.05% by weight of vanadium (V) and the remainder aluminum and production-related inevitable impurities, each with a maximum of 0.05% by weight and a total of at most 0.15% by weight of magnesium (M
- the sheet or strip cold-rolled to the final thickness has at least one intermetallic phase with first particles with an average particle size of 5 ⁇ m to 10 ⁇ m (measured according to the line-cutting method ASTM E112) - by the process steps before the heat treatment.
- the at least casting and the cold rolling in particular after the intermediate annealing, are coordinated with one another in such a way that the sheet or strip has at least one intermetallic phase with first particles with an average particle size of 5 ⁇ m to 10 ⁇ m.
- a sheet or strip with high strength and formability as well as ssf quality or ffa quality can be produced - if this sheet or strip has a mean crystal grain size D of ⁇ 60 ⁇ m after heat treatment (measured according to the ASTM E112 line cutting method) ) and the average crystal grain size D in mm and the number A of the first particles per mm 2 in the aluminum alloy the condition D ⁇ A > 1 , 8th fulfilled - for example in which the recrystallization annealing of the heat treatment is carried out in this way.
- This method is also easy to use and, for example by means of water cooling for accelerated cooling, has the highest level of reproducibility in order to produce a sheet or strip in ssf quality or ffa quality.
- the number of dislocations in the sheet or strip can be increased further in the process if D ⁇ A > 2nd is. Especially if D ⁇ A > 2nd , 5 the sheet or strip can meet comparatively high quality standards without the fear of flow figures, for example Lüders lines of type A, on the surface of the formed sheet or strip, even in the case of comparatively complex geometries or unfavorable plastic deformations.
- the reproducibility of the method can be further improved if, in the heat treatment, the recrystallization annealing is carried out by holding at a temperature of 300 ° C. (degrees Celsius) or more, in particular up to 600 ° C. This can improve further if the recrystallization annealing at 450 ° C to 550 ° C he follows. In addition, this annealing temperature can be sufficient to prestress the structure sufficiently by accelerated cooling in order to produce those dislocations on the first particles which subsequently do not make it necessary to dislodge Lüders lines.
- the heated sheet is accelerated at a cooling rate of at least 10 K / s (Kelvin per second), in particular at least 20 K / s or at least 50 K / s, this accelerated cooling to in particular below 180 ° C. , especially at room temperature.
- K / s Kelvin per second
- the billet is solidified while maintaining a cooling rate (or cooling rate) of ⁇ 2.5 ° C./s.
- a cooling rate or cooling rate
- the cooling rate is ⁇ 2 ° C / s or ⁇ 1 ° C / s or ⁇ 0.75 ° C / s.
- a possible reduction in the average particle size can be absorbed by subsequent process steps, for example by cold rolling, to ensure an average particle size of 5 ⁇ m to 10 ⁇ m before the heat treatment.
- the optional homogenization can be done by holding at 450 ° C to 550 ° C for at least 0.5 h.
- Hot rolling can take place at 280 ° C to 550 ° C.
- the cold rolling to the final thickness can take place with a degree of rolling from 10% to 65%, in particular from 20% to 50%.
- a degree of rolling from 10% to 65%, in particular from 20% to 50%.
- the cold rolling takes place after the intermediate annealing with a rolling degree of 10% to 65%, in particular 20% to 50%, in order to improve the reproducibility of the average particle size from 5 ⁇ m to 10 ⁇ m.
- the optional intermediate annealing can be done by holding at 300 ° C to 500 ° C.
- the optional stabilization can be carried out by 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 be ensured in particular if the product of degree of rolling in% after intermediate annealing and cooling rate in ° C / s meets the condition 10 ⁇ degree of rolling * cooling rate ⁇ 50, in particular 20 ⁇ degree of rolling * Cooling rate ⁇ 45, fulfilled.
- the intermetallic phase has an Al-Mn base, those dislocations can be created in the aluminum alloy on the basis of which flow figures can be avoided in a particularly stable manner.
- the intermetallic phase is preferably of the Al 13 (Mn, Fe) 6 or Al 15 FeMn 3 Si 2 or Al 12 Mn or Al 6 Mn type. It is also conceivable that the primary phase forms the intermetallic phase in order to create a sufficient number of dislocations in cooperation with the heat treatment of the sheet or strip.
- the aluminum alloy (with an Al-Mg-Mn base) is from 4.0 to 5.0% by weight of magnesium (Mg) and / or Has 0.2 to 0.5 wt .-% manganese (Mn).
- the aluminum alloy additionally contains 2.0 to 4.0% by weight of zinc (Zn) (Al-Mg-Zn base).
- This aluminum alloy can optionally have up to 0.8% by weight of copper (Cu).
- the invention achieves the stated object with regard to the sheet or strip by the features of claim 8.
- zirconium (Zr) optionally up to 0.3% by weight of niobium (Nb), optionally up to 0.25% by weight of tantalum (Ta) and the rest aluminum and Due to production-related unavoidable impurities with a maximum of 0.05% by weight and a total of at most 0.15% by weight, an alloy composition is available with which sufficiently high strength and formability, an
- the mean crystal grain size D according to the invention of 60 60 ⁇ m leads to the fact that the comparatively fine crystal grain of the sheet or strip enables high strength and formability.
- the first particles present in the sheet or strip have a limited average particle size of 5 ⁇ m to 10 ⁇ m, the average crystal grain size D in mm and the number A of the first Particles in the aluminum alloy per mm 2 the condition D ⁇ A > 1 , 8th Fulfills.
- a sheet or strip made of an aluminum alloy preferably with an Al-Mg base (or Mg as one of the main alloy elements) in ssf-quality or ffa-quality, is created, which also has sufficient strength and formability, for example for outer skin parts in body construction can award.
- the number of dislocations in the sheet or strip can be increased further if D ⁇ A > 2nd is. Especially if D ⁇ A > 2nd , 5 the sheet or strip can meet comparatively high quality standards without the fear of flow figures, for example Lüders lines of type A, 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 flow figures on the formed sheet or strip can result if the crystal structure has more than 200, in particular more than 400, dislocations on each first particle. This can be achieved if the sheet or strip has been heat-treated by heating and then accelerated cooling such that the crystal structure has more than 200, in particular more than 400, dislocations for each first particle.
- the number A of the first particles is preferably 10 10 particles / mm 2 , which can enable a sufficient distribution of the dislocations in the sheet metal or strip to avoid flow figures. This is particularly the case if the number A of the first particles is 25 25 particles / mm 2 , preferably 35 35 particles / mm 2 .
- the intermetallic phase has an Al-Mn base, those dislocations can be created in the aluminum alloy that can be used to avoid stable flow figures.
- the intermetallic phase is preferably of the Al 13 (Mn, Fe) 6 or Al 15 FeMn 3 Si 2 or Al 12 Mn or Al 6 Mn type. It is also conceivable that the primary phase forms the intermetallic phase in order to create a sufficient number of dislocations through the subsequent heat treatment of the sheet or strip.
- the aluminum alloy contains 4.0 to 5.0% by weight of magnesium (Mg) and / or 0.2 to 0.5% by weight of manganese (Mn ) having.
- the aluminum alloy additionally contains 2.0 to 4.0% by weight of zinc (Zn) (with an Al-Mg-Zn base).
- This aluminum alloy can optionally have up to 0.8% by weight of copper (Cu).
- the sheet or strip according to the invention can also be particularly suitable for producing a molded part, in particular a vehicle part, preferably a body part, by sheet metal forming.
- a plate is preferably produced from the sheet or strip in order to be able to carry out a sheet metal forming process.
- the aluminum alloy preferably has an Al-Mg base.
- 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 rate) ⁇ 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 separated into a split strip or into sheet metal or else cut off from the sheet or strip in order to form these semi-finished products, for example to form sheet metal.
- Forming can be deep drawing, roll profiling, etc.
- the aluminum alloy can be of the type, for example, EN AW-5083 or EN AW-5086 or EN AW-5182 or EN AW-5454 or EN AW-5457 or EN AW-5754.
- a fine sheet A1 with a sheet thickness of 1.2 mm was produced from an alloy of the type AA5182 (Al-Mg-Mn base) with the chemical composition C1.
- the production of the billet was solidified with a comparatively reduced cooling rate (or cooling rate), the rolling steps for hot and cold rolling were carried out according to the standard scheme.
- the last rolling pass during cold rolling was 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 mean crystal grain size or final grain size of the thin sheet A1 was 15 ⁇ m (measured according to the line-cutting method ASTM E112) and in the intermetallic phase 44, the first having a mean particle size of 5 ⁇ m to 10 ⁇ m (measured according to the line-cutting method ASTM E112) Particles per mm 2 . These first particles were also comparatively rough.
- the condition 10 ⁇ degree of rolling * cooling rate ⁇ 50 is met.
- the criterion ( ⁇ D * A> 1.8) is met with a ⁇ D * A value of 5.4.
- a tensile test showed no lines of Lüders on the surface of the sheet A1.
- the intermetallic phase according to the invention with the first particles could therefore ensure a sufficient number of dislocations in order to prevent Lüders lines from being formed.
- a sheet A2 with a sheet thickness of 1.2 mm was made from an alloy of type AA5182 with the chemical composition C2.
- the billet was solidified at a cooling rate (or cooling rate) of 1.8 ° C / s and the rolling steps during hot and cold rolling were carried out according to the standard scheme.
- the last rolling pass during cold rolling was 15% (from 1.41 mm to 1.2 mm), the final heat treatment was carried out at 500 ° C subsequent water quenching.
- the condition 10 ⁇ degree of rolling * cooling rate ⁇ 50 is met.
- the average crystal grain size or final grain size of the fine sheet A1 after the heat treatment was found to be 35 ⁇ m and in the 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 met. A tensile test showed no lines of Lüders on the surface of the sheet A2. The intermetallic phase according to the invention with the first particles could therefore ensure a sufficient number of dislocations in order to prevent Lüders lines from being formed.
- a sheet A3 with a sheet thickness of 1.2 mm was made from an alloy of type AA5182 with the chemical composition C3.
- the ingot was solidified at a cooling rate (or cooling rate) of 1.8 ° C / s and the rolling steps in hot and cold rolling were carried out according to the standard scheme.
- the last rolling pass during cold rolling was 18% (from 1.46 mm to 1.2 mm), 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 intermetallic phase 14 first particles per mm 2 were found having an average particle size of 5 ⁇ m to 10 ⁇ m.
- the condition 10 ⁇ degree of rolling * cooling rate ⁇ 50 is met.
- Two sheets A4.1 and A4.2 with a sheet thickness of 1.2 mm were made from an alloy of type AA5182 with the chemical composition C4.
- the rolling ingot was solidified at a cooling rate (or cooling rate) of 1.8 ° C./s, and the rolling steps during hot and cold rolling were carried out according to the standard scheme.
- the last rolling pass during cold rolling was 25% (from 1.60 mm to 1.2 mm).
- the final heat treatment was carried out on sheet A4.1 at 500 ° C with subsequent water quenching.
- the sheet A4.2 was finally heat-treated at 370 ° C with subsequent cooling in still air.
- the average crystal grain size or final grain size of the two fine sheets A4.1 and A4.2 was 32 ⁇ m and in their 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 met by both thin sheets A4.1 and A4.2.
- Lüders lines appear on A4.2 thin sheet after deep drawing.
- the slower cooling in still air did not allow a sufficient number of dislocations to form on the sheet A4.2 to prevent lines of wear.
- the accelerated water cooling of the sheet A4.1 therefore meant that the intermetallic phase with the first particles could provide a sufficient number of dislocations to prevent Lüders lines from being formed.
- a sheet A5 with a sheet thickness of 1.2 mm was made from an alloy of type AA5182 with the chemical composition C4.
- the billet was solidified at a cooling rate (or cooling rate) of 1.8 ° C / s and the rolling steps during hot and cold rolling were carried out according to the standard scheme.
- the last rolling pass during cold rolling was 63% (from 3.25 mm to 1.2mm), 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 intermetallic phase there were 12 first particles per mm 2 having an average particle size of 5 ⁇ m to 10 ⁇ m.
- a sheet A6.1 with a sheet thickness of 1.2 mm was made from an alloy with an Al-Mg-Zn-Mn base with chemical composition D1.
- the billet was solidified at a cooling rate (or cooling rate) of 1.8 ° C / s and the rolling steps during hot and cold rolling were carried out according to the standard scheme.
- the last roll pass during cold rolling was 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, stabilization was carried out at 100 ° C for 3 h (hours).
- the mean crystal grain size or final grain size was 28 ⁇ m and in the intermetallic phase there were 14 first particles per mm 2 having an average particle size of 5 ⁇ m to 10 ⁇ m.
- the criterion ( ⁇ D * A> 1.8) is met with a ⁇ D * A value of 2.34.
- the condition 10 ⁇ degree of rolling * cooling rate ⁇ 50 is met.
- a tensile test showed no lines of Lüders on the surface of the sheet A6.1.
- the intermetallic phase according to the invention with the first particles could therefore ensure a sufficient number of dislocations in order to prevent Lüders lines from being formed.
- a sheet A6.2 with a sheet thickness of 1.2 mm was made from an alloy with an Al-Mg-Zn-Mn base of chemical composition D1.
- the billet was solidified at a cooling rate (or cooling rate) of 1.8 ° C / s and the rolling steps during hot and cold rolling were carried out according to the standard scheme.
- the last rolling pass during cold rolling was 63% (from 3.25 mm to 1.2 mm), 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 intermetallic phase there were 14 first particles per mm 2 having an average particle size of 5 ⁇ m to 10 ⁇ m.
- All of the exemplary embodiments according to the invention namely A1, A2, A3, A4.1 and A6.1, have in common that their crystal structure has more than 200, in particular more than 400, dislocations on each first particle.
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- Chemical & Material Sciences (AREA)
- Mechanical Engineering (AREA)
- Organic Chemistry (AREA)
- Metallurgy (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Crystallography & Structural Chemistry (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Metal Rolling (AREA)
- Continuous Casting (AREA)
- Heat Treatment Of Sheet Steel (AREA)
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Priority Applications (8)
| 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 |
| JP2021544421A JP2022519238A (ja) | 2019-01-30 | 2020-01-30 | アルミニウム合金製の板または帯の製造方法ならびにそれにより製造された板、帯または成形品 |
| US17/427,460 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 |
| CN202080011029.3A CN113474479B (zh) | 2019-01-30 | 2020-01-30 | 由铝合金制造板材或带材的方法和由此制成的板材、带材或成形件 |
| CA3128294A CA3128294A1 (fr) | 2019-01-30 | 2020-01-30 | Procede de fabrication d'une tole ou d'un feuillard en un alliage d'aluminium ainsi que tole, feuillard ou piece faconnee produit-e par ce procede |
| EP20706105.2A EP3918102A1 (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 |
| MX2021009093A MX2021009093A (es) | 2019-01-30 | 2020-01-30 | Metodo para producir una lamina o tira a partir de una aleacion de aluminio y una lamina, tira o parte formada producida de esta manera. |
| 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 |
Applications Claiming Priority (1)
| 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 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| EP3690076A1 true EP3690076A1 (fr) | 2020-08-05 |
Family
ID=65268872
Family Applications (2)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP19154632.4A Withdrawn 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 |
| EP20706105.2A Pending EP3918102A1 (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 |
Family Applications After (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP20706105.2A Pending EP3918102A1 (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 |
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) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| 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 |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2025539857A (ja) * | 2022-12-12 | 2025-12-09 | アーコニック テクノロジーズ エルエルシー | 新規の5xxxアルミニウム合金及びその製造方法 |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2024861A (en) * | 1978-07-05 | 1980-01-16 | Alusuisse | Method fo manufacture of aluminium alloy sheets containingmagnesium and zine |
| EP0259700A1 (fr) * | 1986-09-09 | 1988-03-16 | Sky Aluminium Co., Ltd. | Procédé de production d'une feuille laminée en alliage à base d'aluminium |
| EP0507411A1 (fr) | 1991-04-02 | 1992-10-07 | Hoogovens Aluminium N.V. | Tôle en aluminium et procédé pour sa fabrication |
Family Cites Families (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP3062274B2 (ja) * | 1991-03-28 | 2000-07-10 | 住友軽金属工業株式会社 | 深絞り性に優れた成形加工用アルミニウム合金板材の製造法 |
| NL1003453C2 (nl) * | 1996-06-28 | 1998-01-07 | Hoogovens Aluminium Nv | Aluminiumplaat van het AA5000-type en een werkwijze voor het vervaardigen daarvan. |
| JPH10219412A (ja) * | 1997-02-04 | 1998-08-18 | Shinko Alcoa Yuso Kizai Kk | 成形加工後の外観性が優れたアルミニウム合金圧延板の製造方法 |
| DE10231422A1 (de) | 2001-08-13 | 2003-02-27 | Corus Aluminium Nv | Aluminium-Magnesium-Legierungserzeugnis |
| JP4109600B2 (ja) * | 2003-10-10 | 2008-07-02 | 株式会社神戸製鋼所 | アルミニウム合金板およびその製造方法 |
| SE530437C2 (sv) * | 2006-10-13 | 2008-06-03 | Sapa Heat Transfer Ab | Rankmaterial med hög hållfasthet och högt saggingmotstånd |
| JP5416433B2 (ja) * | 2008-04-09 | 2014-02-12 | 株式会社神戸製鋼所 | 缶胴用アルミニウム合金板およびその製造方法 |
| JP5342201B2 (ja) * | 2008-09-26 | 2013-11-13 | 株式会社神戸製鋼所 | 成形性に優れたアルミニウム合金板 |
| JP5723245B2 (ja) * | 2010-10-19 | 2015-05-27 | 株式会社神戸製鋼所 | アルミニウム合金板 |
| CN103320729B (zh) * | 2013-05-31 | 2015-07-22 | 浙江巨科铝业股份有限公司 | 一种汽车车身用Al-Mg合金板的制备方法 |
| EP3205734B1 (fr) * | 2014-10-09 | 2018-12-12 | UACJ Corporation | Plaque d'alliage d'aluminium à formage superplastique et son procédé de production |
| CN104313413B (zh) * | 2014-10-24 | 2016-08-24 | 北京科技大学 | 一种Al-Mg-Zn系合金及其合金板材的制备方法 |
| CA2990303C (fr) * | 2015-06-25 | 2019-12-17 | Hydro Aluminium Rolled Products Gmbh | Bande almg a haute resistance aisement faconnable et procede de production de celle-ci |
| 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 JP JP2021544421A patent/JP2022519238A/ja active Pending
- 2020-01-30 CA CA3128294A patent/CA3128294A1/fr active Pending
- 2020-01-30 CN CN202080011029.3A patent/CN113474479B/zh not_active Expired - Fee Related
- 2020-01-30 WO PCT/EP2020/052375 patent/WO2020157246A1/fr not_active Ceased
- 2020-01-30 MX MX2021009093A patent/MX2021009093A/es unknown
- 2020-01-30 EP EP20706105.2A patent/EP3918102A1/fr active Pending
- 2020-01-30 US US17/427,460 patent/US20220127708A1/en active Pending
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2024861A (en) * | 1978-07-05 | 1980-01-16 | Alusuisse | Method fo manufacture of aluminium alloy sheets containingmagnesium and zine |
| EP0259700A1 (fr) * | 1986-09-09 | 1988-03-16 | Sky Aluminium Co., Ltd. | Procédé de production d'une feuille laminée en alliage à base d'aluminium |
| EP0507411A1 (fr) | 1991-04-02 | 1992-10-07 | Hoogovens Aluminium N.V. | Tôle en aluminium et procédé pour sa fabrication |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| 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 |
| US12480186B2 (en) | 2020-01-07 | 2025-11-25 | Amag Rolling Gmbh | Sheet or strip made of a hardenable aluminum alloy, a vehicle part made therefrom, a use, and a method for producing the sheet or strip |
Also Published As
| Publication number | Publication date |
|---|---|
| CA3128294A1 (fr) | 2020-08-06 |
| WO2020157246A1 (fr) | 2020-08-06 |
| CN113474479A (zh) | 2021-10-01 |
| EP3918102A1 (fr) | 2021-12-08 |
| MX2021009093A (es) | 2021-10-22 |
| JP2022519238A (ja) | 2022-03-22 |
| US20220127708A1 (en) | 2022-04-28 |
| CN113474479B (zh) | 2023-06-06 |
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