Classifications

• • C—CHEMISTRY; METALLURGY
  • C21—METALLURGY OF IRON
  • C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
  • C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
  • C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
  • C21D8/0221—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the working steps
  • C21D8/0226—Hot rolling
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
  • B21B—ROLLING OF METAL
  • B21B1/00—Metal-rolling methods or mills for making semi-finished products of solid or profiled cross-section; Sequence of operations in milling trains; Layout of rolling-mill plant, e.g. grouping of stands; Succession of passes or of sectional pass alternations
  • B21B1/46—Metal-rolling methods or mills for making semi-finished products of solid or profiled cross-section; Sequence of operations in milling trains; Layout of rolling-mill plant, e.g. grouping of stands; Succession of passes or of sectional pass alternations for rolling metal immediately subsequent to continuous casting
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
  • B21D—WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
  • B21D22/00—Shaping without cutting, by stamping, spinning, or deep-drawing
  • B21D22/02—Stamping using rigid devices or tools
  • B21D22/022—Stamping using rigid devices or tools by heating the blank or stamping associated with heat treatment
• • C—CHEMISTRY; METALLURGY
  • C21—METALLURGY OF IRON
  • C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
  • C21D1/00—General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering
  • C21D1/62—Quenching devices
• • C—CHEMISTRY; METALLURGY
  • C21—METALLURGY OF IRON
  • C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
  • C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
  • C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
  • C21D8/0221—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the working steps
  • C21D8/0236—Cold rolling
• • C—CHEMISTRY; METALLURGY
  • C21—METALLURGY OF IRON
  • C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
  • C21D9/00—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor
  • C21D9/46—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for sheet metals
• • 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
  • C22F1/04—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 present invention relates to a process for manufacturing thin sheets of aluminum alloy 7XXX, which are particularly useful for the automotive industry.
• AA7XXX series aluminum alloys such as the AA7075 alloy, combine interesting chemical and mechanical characteristics such as hardness and corrosion resistance.
• AA7XXX alloys have not yet found wide use in the automotive industry due to the difficulty encountered in shaping and assembling them, while retaining an economical manufacturing process.
• Patent application AT 1 1744 describes for example a process for producing a shaped part from an aluminum alloy sheet of the 7000 series, in which the aluminum sheet is heated and formed in this heated state, then cooled.
• Patent application EP3265595 describes an alloy comprising in% by weight 4 - 15 Zn, 0.1 - 3.5 Cu, 1.0 - 4.0 Mg, 0.05 - 0.50 Fe, 0.05 - 0.30 Si, 0.05 - 0.25 Zr, up to 0.25 Mn, up to 0.20 Cr , up to 0.15 Ti, up to 0.15% of impurities, aluminum residue, which can be used in particular in the automotive industry.
• Patent application WO2016094464 describes a method for achieving the desired strength and elongation with a sheet of aluminum alloy 7xxx having the steps of a) rapidly heating the sheet to a temperature of 450 ° C to 5 lO ° C; b) maintaining the sheet at the temperature of 450 ° C to 5 l O ° C for 20 minutes; c) rapid cooling of the sheet to room temperature above 50 ° C per second; d) heating the sheet to a temperature between about 50 ° C and 150 ° C; e) maintaining the sheet at a temperature between about 50 ° C and 150 ° C for a period of about 0.5 hours to 6 hours.
• Patent application WO2014040939 relates to a method for manufacturing a part of a motor vehicle comprising at least the steps consisting in: (a) providing a bare or composite aluminum alloy produced in sheet metal having a thickness within a range from about 0.5 mm to 4 mm, in which the sheet product comprises at least one layer of an aluminum alloy of the AA7xxx-series, the sheet product having been subjected to a heat treatment in solution and quenching followed by a natural aging period of at least 1 day; (b) subjecting the naturally aged sheet metal product to a reversion annealing treatment, namely a heat treatment at a temperature between 100 ° C and 350 ° C for 0.1 to 60 seconds; (c) optionally subjecting the product of the heated sheet to a forced cooling operation; (d) within 2 hours, preferably within 30 minutes, from the reversion annealing treatment, form the sheet product to obtain a three-dimensional part.
• Patent application WO2012059505 describes a method of manufacturing an aluminum alloy formed part for a motor vehicle, the method comprising: (a) providing a product made of laminated aluminum sheet, in which the aluminum alloy is an AA7000 having a thickness in the range of 0.5 to 4 mm and being subjected to a solution heat treatment and having been cooled, (b) forming the aluminum alloy sheet to obtain a formed part three dimensions, (c) heating said formed part in three dimensions for at least one pre-aging temperature between 50-250 ° C, and (d) subjecting said formed part and the pre-aged motor vehicle component to a cycle of baking paint.
• Patent application EP2514537 describes a method of manufacturing a seal in at least two metal parts which overlap by self-piercing riveting. At least one of the first part and the second part is a sheet material made of an aluminum alloy of the AA7000-series, and a heat treatment is applied to at least the part of said sheet material 7000 of the series within 120 minutes before assembly production and / or at least part of the time during assembly production so as to reduce the tensile strength in the junction zone of at least the part of said sheet material of the 7000 series.
• Patent application EP2479305 relates to a method of manufacturing an aluminum alloy structural part comprising: (a) providing a product made of laminated aluminum sheet, in which the aluminum alloy is of the AA7000 series and has a thickness in the range of 0.5 to 4 mm and being subjected to a heat treatment in solution and having been cooled,
• Patent application EP2440680 describes a method of manufacturing a part of a motor vehicle, having an elastic limit greater than 500 MPa after having been subjected to a paint curing cycle, the method comprising: (a) supplying a product made of laminated aluminum sheet of an AIZnMgCu alloy and having a thickness in the range of 0.5 to 4 mm and being subjected to a heat treatment in solution, and having been quenched and in the microstructure is substantially recrystallized, (b) forming the aluminum alloy sheet to obtain a formed part, (c) assembling the formed part with one or more other metal parts to form an assembly forming a motor vehicle component; (d) subjecting said motor vehicle component to a paint curing cycle and in which the aluminum alloy sheet in the formed part has an elastic limit greater than 500 MPa.
• Patent application WO2009130175 relates to a manufacturing process consisting in forming a structural part from a sheet of aluminum alloy of the 7xxx- series, the process comprising the following steps: (i) cutting the sheet of alloy d aluminum to obtain a blank; (ii) heating the blank to a temperature above 450 ° C; (iii) shaping the blank thus heated; (iv) cool (v) heat treat the structural part that has been cooled and shaped.
• Patent application WO2015132932 relates to a structural aluminum alloy sheet and a method of manufacturing the aluminum alloy sheet, the aluminum alloy sheet containing 7.0 to 12.0% by mass of Zn, 1.5 to 4.5% by mass of Mg, 1.0 to 3.0% by mass of Cu, 0.05-0.30 mass% of Zr, and 0.005-0.5% by mass of Ti and having an Si content reduced to 0.5% by mass or less, an Fe content reduced to 0 , 5% by mass or less, an Mn content reduced to 0.3% by mass or less, and a Cr content reduced to 0.3% by mass or less, the remainder comprising unavoidable impurities and aluminum.
• Patent application WO2017075319 relates to aluminum alloys of the 7xxx series having a high resistance, intended in particular for automotive applications, these alloys comprising, in% by weight, 4 - 15 Zn, 0.1 - 3.5 Cu, 1.0 - 4.0 Mg, 0.05 - 0.50 Fe, 0.05 - 0.30 Si, 0.05 - 0.25 Zr, up to 0.25 Mn, up to 0.20 Cr, up to 0.15 Ti, and up to 0.15 of impurities, aluminum residue.
• laminated products typically 0.5 to 4 mm thick, made of aluminum-zinc-copper-magnesium alloy having improved properties compared to those of known products, in particular in terms of ability to shaping and assembly, while having high mechanical strength and resistance to stress corrosion after curing paints, for the automotive industry. Furthermore, there is a need for a simple and economical process for obtaining these laminated products.
• An object of the invention is a process for manufacturing a laminated product based on aluminum alloy, in particular for the automotive industry in which, successively,
• an aluminum-based liquid metal bath comprising 4 to 7% by weight of Zn, 1.0 to 3.0% by weight of Cu, 1.5 to 3.5% by weight of Mg, at most 0.50% by weight of Fe, at most 0.40% by weight of Si, at least one element chosen from Zr, Mn, Cr, Se, Hf and Ti, the amount of said element, if is chosen, being 0.05 to 0.18% by weight for Zr, 0.1 to 0.6% by weight for Mn, 0.05 to 0.3% by weight for Cr, 0.02 to 0.2 % by weight for Se, 0.05 to 0.5% by weight for Hf and from 0.005 to 0.15% by weight for Ti, the other elements at most 0.05% by weight each and 0.15% by weight in total, the rest of the aluminum;
• said rolling plate is homogenized
• said rolling plate is hot rolled and optionally cold to a sheet, e) said sheet is dissolved and quenched; f) optionally, a leveling is carried out and / or said sheet is pulled in a controlled manner with a cumulative deformation of at least 0.5% and less than 3%,
• Another subject of the invention is a laminated product obtained by the process according to the invention having a combination of RpO, 2 (TL) and A% (TL) properties such as A% (TL)> - 0.05 RpO, 2 (TL) + 40, and A% (TL) is at least 17%.
• Yet another object of the invention is the use of a laminated product capable of being obtained by the process according to the invention or according to the invention for the manufacture of an automobile.
• Figure 1 Relationship between the elongation and the elastic limit Rp02 in the direction TL for sheets obtained by the process according to the invention after 30 days of aging.
• Figure 2 Cross section of the assembly by riveting 1.2 mm thick sheets of AA5182 alloy with a 1.5 mm thick sheet of Example 2 according to the invention.
• Figure 3 Cross section of the assembly by riveting 1.2 mm thick sheets of AA5182 alloy with a 1.5 mm thick sheet of reference example 2. Description of the invention
• the static mechanical characteristics in tension in other words the tensile strength R m , the conventional elastic limit at 0.2% elongation R P o, 2 , and the elongation at break A%, are determined by a tensile test according to standard NF EN ISO 6892-1 (2016), the sampling and the direction of the test being defined by standard EN 485-1 (2016).
• the direction of traction is indicated by the letter L (longitudinal direction) or TL (long through direction).
• the test pieces used have a width of 20 mm and a length of 80 mm, i.e. type 2 according to Table Bl of standard EN ISO 6892-1.
• the mechanical characteristics are measured in full thickness.
• the bendability is quantified using a "ratio r / 1", which is the ratio between the radius of curvature (r) to the sheet thickness (t) , both expressed in mm.
• ratio r / 1 is the ratio between the radius of curvature (r) to the sheet thickness (t) , both expressed in mm.
• the equipment used for the measurement is described for example in Figure 2 of US patent application 2016/0168676.
• the measurements are carried out according to standards ASTM E290-97a and the “Ford Method Laboratory Test” (FLTM) BB1 14-02.
• a granular structure is essentially called recrystallized granular structure such that the recrystallization rate is greater than 70% and preferably greater than 90%.
• the recrystallization rate is defined as the surface fraction on a metallographic section occupied by recrystallized grains.
• the present inventors have obtained sheets having an advantageous compromise between mechanical strength, resistance to stress corrosion, formability and suitability for assembly using the process according to the invention which notably comprises the combination of a 7XXX alloy containing copper and a heat treatment in which said sheet reaches a temperature between 60 and 120 ° C and preferably between 80 and 100 ° C for 8 to 16 hours and preferably from 10 to 14 hours.
• a liquid metal bath comprising 4 to 7% by weight of Zn, 1.0 to 3.0% by weight of Cu, 1.5 to 3.5% by weight of Mg is prepared. , at most 0.50% by weight of Fe, at most 0.40% by weight of Si, at least one element chosen from Zr, Mn, Cr, Se, Hf and Ti, the amount of said element, if it is chosen, being 0.05 to 0.18% by weight for Zr, 0.1 to 0.6% by weight for Mn, 0.05 to 0.3% by weight for Cr, 0.02 to 0.2% by weight for Se, 0.05 to 0.5% by weight for Hf and from 0.005 to 0.15% by weight for Ti, the other elements at most 0.05% by weight each and 0.15% by weight at total, the rest aluminum.
• the zinc content of the products according to the invention is between 4 and 7% by weight. In an advantageous embodiment of the invention the zinc content is at least 5% by weight, preferably at least 5.5% by weight and preferably at least 5.6% by weight. In an advantageous embodiment of the invention, the zinc content is between 5.5 and 6.2% by weight and preferably between 5.6 and 6.1% by weight. In an advantageous embodiment of the invention the zinc content is at most s 6.5% by weight. In one embodiment of the invention the zinc content is at most 6.1% by weight. When the zinc content is too high, the formability and assembly ability may be deteriorated. When the zinc content is too low, the minimum static mechanical characteristics may not be reached.
• the copper content of the products according to the invention is between 1.0 and 3.0% by weight. In an advantageous embodiment of the invention the copper content is at least 1.1% by weight, preferably at least 1.2% by weight and preferably at least 1.3% by weight. In an advantageous embodiment of the invention, the copper content is between 1.2 and 2.0% by weight and preferably between 1.4 and 1.6% by weight. In an advantageous embodiment of the invention, the copper content is at most 2.5% by weight and preferably at most 2.0% by weight. In one embodiment of the invention, the copper content is at most 1.8% by weight. When the copper content is too high, the formability and assembly ability may be deteriorated. When the copper content is too low, the minimum static mechanical characteristics are not reached and the corrosion resistance is insufficient.
• the magnesium content of the products according to the invention is between 1.5 and 3.5% by weight. In an advantageous embodiment of the invention the magnesium content is at least 1.8% by weight, preferably at least 2.0% by weight and preferably at least 2.2% by weight. In an advantageous embodiment of the invention, the magnesium content is between 2.2 and 3.0% by weight and preferably between 2.4 and 2.8% by weight. In an advantageous embodiment of the invention the magnesium content is at most 3.2% by weight and preferably at most 3.0% by weight. In one embodiment of the invention the magnesium content is at most 2.8% by weight. When the magnesium content is too high, the formatting and assembly skills can be deteriorated. When the magnesium content is too low, the minimum static mechanical characteristics are not reached and the corrosion resistance is insufficient.
• the iron and silicon contents are each at most 0.5% by weight and 0.4% by weight, respectively. In an advantageous embodiment of the invention, the iron and silicon contents are at most 0.2% and preferably at most 0.15% by weight. In an advantageous embodiment of the invention, the iron content is between 0.05 and 0.25% by weight and preferably between 0.15 and 0.20% by weight. In an advantageous embodiment of the invention, the silicon content is between 0.03 and 0.15% by weight and preferably between 0.06 and 0.12% by weight An iron and silicon content controlled and limited contributes to the improvement of the property compromise.
• the alloy of the products according to the invention contains at least one element chosen from Zr, Mn, Cr, Se, Hf and Ti, the amount of said element, if it is chosen, being 0.05 to 0.18% by weight for Zr, 0.1 to 0.6% by weight for Mn, 0.05 to 0.3% by weight for Cr, 0.02 to 0.2% by weight for Se, 0.05 to 0.5% by weight for Hf and from 0.005 to 0.15% by weight for Ti.
• the elements chosen are chromium and titanium, the chromium content being between 0.15 and 0.25% by weight, preferably between 0.17 and 0.23% by weight and preferably between 0.18 and 0.22% by weight and the titanium content being between 0.01 and 0.10% by weight, preferably between 0.02 and 0.06% by weight.
• the addition of titanium, possibly combined with boron and / or carbon, contributes to controlling the granular structure, in particular during casting.
• the elements chosen are zirconium and titanium, the zirconium content being between 0.07 and 0.15% by weight, preferably between 0.08 and 0.13% by weight and preferably between 0.09 and 0.12% by weight and the titanium content being between 0.01 and 0.10% by weight, preferably between 0.02 and 0.06% by weight.
• the other elements are unavoidable impurities which are maintained at a content less than or equal to 0.05% by weight each and 0.15% by weight in total.
• the alloy is chosen from AA7010, AA7012, AA7022, AA7122, AA7023, AA7032, AA7033, AA7040, AA7140, AA7050, AA7050A, AA7150, AA7250, AA7075, AA7175, AA7475, and preferably AA7010, AA7050, AA7075, AA7175 and AA7475.
• the method of manufacturing thin sheets according to the invention then comprises stages of casting, optionally homogenization, hot rolling and optionally cold, dissolution, quenching, optionally leveling and / or controlled traction, heat treatment and aging.
• the bath of liquid metal produced is poured in the form of a rolling plate.
• the laminating plate is then optionally homogenized at a temperature between 450 ° C and 500 ° C.
• the homogenization time is between 5 and 60 hours.
• the homogenization temperature is at least 460 ° C. In one embodiment, the homogenization temperature is less than 490 ° C.
• the rolling plate After homogenization, the rolling plate is generally cooled to room temperature before being preheated to be deformed when hot.
• the purpose of preheating is to reach a hot rolling inlet temperature preferably between 350 and 450 ° C. allowing deformation by hot rolling. Hot rolling is carried out so as to obtain a sheet typically 3 to 8 mm thick.
• the sheet obtained After hot rolling, it is optionally possible to cold roll the sheet obtained in particular to obtain a final thickness of between 0.4 and 4 mm.
• the final thickness is at most 3.0 mm and preferably at most 2.5 mm.
• the final thickness is at least 0.5 mm and preferably at least 0.8 mm.
• the sheet thus obtained is then placed in solution between 450 and 515 ° C.
• the dissolution can be carried out sheet to sheet in an oven, the duration of dissolution in this embodiment is advantageously between 1 minute to 1 hour.
• the dissolution is carried out on a continuous treatment line, the duration of dissolution in this embodiment is advantageously between 5 seconds and one minute.
• the sheet thus dissolved is then quenched.
• the quenching is carried out with water whose temperature is between 20 and 60 ° C and preferably between 30 and 50 ° C.
• the sheet can then undergo cold deformation by leveling and / or controlled traction with a permanent deformation of at least 0.5% and less than 3%.
• a heat treatment in which said sheet reaches a temperature between 60 and 120 ° C for 8 to 16 hours and preferably between 80 and 100 ° C for 10 to 14 hours is then carried out; the temperatures of 120 ° C and 100 ° C mentioned being the maximum temperatures which can be reached by the sheet during the heat treatment.
• the maximum temperature reached by the sheet is 110 ° C or 105 ° C or 95 ° C or 90 ° C.
• the heat treatment is carried out at the outlet of a solution treatment line and continuous quenching.
• the sheet after quenching, the sheet is heated to a sufficient temperature so that after winding, the sheet reaches a temperature between 60 and 120 ° C for 8 to 16 hours and preferably between 80 and 100 ° C for 10 to 14 h, advantageously, the sheet is cooled after quenching to a temperature between 20 and 40 ° C and reheated to a temperature between 70 and 90 ° C and then cooled slowly so that the temperature is maintained at a temperature of at least 60 ° C for at least 10 hours. Finally, the product thus heat treated is aged for at least 30 days at room temperature. The present inventors have found that if the heat treatment is too short and / or if its temperature is insufficient, the mechanical properties of the sheet are too unstable.
• the evolution of RpO, 2 (TL) during the aging step is less than 15 MPa, preferably less than 10 MPa and preferably less than 7 MPa.
• the present inventors have found that if the heat treatment is too short and / or if its temperature is insufficient, the mechanical properties of the sheet do not allow satisfactory shaping, especially when cold. If the heat treatment is too long and / or if its temperature is too high, the mechanical properties of the sheet are stable, but the mechanical strength is too high and / or the formability too low to allow satisfactorily to carry out the operations of shaping and assembly.
• the sheet metal thus formed is assembled on a white automobile body, preferably by welding or riveting,
• baking is carried out in which said sheet reaches a temperature between 160 and 200 ° C and preferably between 170 and 190 ° C for 15 minutes to 1 hour.
• the shaping operation is carried out by stamping at a temperature between 150 and 250 ° C. This embodiment is particularly advantageous with regard to shaping in which the deformation is significant, typically reaching locally at least 5%.
• the shaping operation is carried out by rolling or folding or stamping at ambient temperature, which is advantageous in particular when the deformation is smaller, typically reaching locally less than 5%.
• the products obtained by the process according to the invention are particularly suitable for riveting operations with other products, in particular aluminum.
• the rolled products capable of being obtained by the process according to the invention have a combination of properties R p o , 2 (TL) and A% (TL) such that A% (TL)> - 0.05 R p o , 2 (TL) + 40 and A% (TL) is at least 17% and preferably at least 18%.
• the test pieces used have a width of 20 mm and a length of 80 mm, ie type 2 according to Table B. l of standard EN ISO 6892-1, the elongation can also be noted A80% (TL).
• the ratio r / t in the direction TL which is the ratio between the radius of curvature (r) determined according to the standards ASTM E290-97a and FLTM BB1 14-02 and the sheet thickness (t), expressed in mm, is at most 2.25 and preferably at most 2.0 for the rolled products according to the invention.
• the laminated products according to the invention have an elastic limit R p o, 2 (TL) of at least 370 MPa and preferably at least 380 MPa, and an elongation at break A% (TL) of at least 19% and preferably at least 20%.
• the laminated products according to the invention have an elastic limit R p o, 2 (TL) of at least 430 MPa and preferably at least 440 MPa, and an elongation at break A % (TL) of at least 18% and preferably at least 19%.
• the mechanical characteristics of the laminated products according to the invention are obtained following an aging of 30 days at room temperature after the heat treatment.
• the mechanical properties of the products according to the invention after the firing step are particularly advantageous.
• the products according to the invention have, after baking, an elastic limit Rpo, 2 (TL) of at least 450 MPa, preferably of at least 470 MPa and preferably of at least 490 MPa, and a resistance at break R m (TL) of at least 510 MPa, preferably of at least 530 MPa and preferably of at least 540 MPa.
• Rpo, 2 TL
• TL resistance at break R m
• the resistance to stress corrosion after curing of the laminated products according to the invention is high. Corrosion under stress is typically evaluated with a test in which the stress is obtained by 4-point bending at 75% of the elastic limit and the conditions are defined by ASTM G85.
• the products according to the invention after curing do not exhibit any stress corrosion breakage before 15 days and preferably before 30 days.
• laminated products capable of being obtained by the method according to the invention or according to the invention for the manufacture of an automobile is advantageous, in particular for structural parts, typically anti-intrusion structural parts.
• an alloy liquid metal bath was prepared, the composition of which is given in table 1.
• a rolling plate was cast from this liquid metal bath.
• Said rolling plate was hot and cold rolled into a sheet of thickness 1.5 mm.
• the sheet thus obtained was dissolved at 480 ° C for 10 minutes and then quenched.
• the static mechanical properties were characterized in the TL direction (long beam) and are given in Table 2.
• the test pieces used were 20 mm wide and 80 mm long, ie type 2 according to Table Bl of the standard. EN ISO 6892-1.
• a liquid metal alloy bath was prepared, the composition of which is given in table 4.
• a rolling plate was cast from this liquid metal bath. The rolling plate was homogenized for 19 hours at 475 ° C.
• a heat treatment was then carried out by heating the sheet to a temperature of 80 ° C before rolling it up in the form of a coil and maintaining a temperature above 60 ° C for 10 hours, then measuring the mechanical properties after waiting from 4 to 62 days. After this wait, a baking treatment of 20 minutes at 185 ° C., simulating the baking of paint, was carried out and the mechanical properties were also measured.
• the static mechanical properties have been characterized in the TL direction and are given in Table 5.
• the test specimens used had a width of 20 mm and a length of 80 mm, that is to say type 2 according to Table Bl of standard EN ISO 6892- 1.
• the assembly by riveting of 1.2 mm thick sheets of AA5182 alloy was tested with a 1.5 mm thick sheet of Example 2.
• the sheet was subjected to a treatment of 1 minute at 200 ° C. to simulate a shaping operation by stamping.
• the assembly was also tested with a sheet of AA7075 alloy having undergone a 24 hour heat treatment at 120 ° C.
• the configuration 5182 0 1.2 mm / Invention 1.5 mm with the rivet described above has no cracks and has good static strength, in particular greater than 150 daN during cross tests.

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• Chemical & Material Sciences (AREA)
• Engineering & Computer Science (AREA)
• Mechanical Engineering (AREA)
• Organic Chemistry (AREA)
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• Metallurgy (AREA)
• Thermal Sciences (AREA)
• Physics & Mathematics (AREA)
• Crystallography & Structural Chemistry (AREA)
• Metal Rolling (AREA)
• Laminated Bodies (AREA)
• Continuous Casting (AREA)
• Heat Treatment Of Articles (AREA)

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• 2018
  • 2018-07-17 FR FR1856613A patent/FR3084087B1/fr active Active
• 2019
  • 2019-07-11 CN CN201980047355.7A patent/CN112424387A/zh active Pending
  • 2019-07-11 EP EP19758427.9A patent/EP3824110A1/de active Pending
  • 2019-07-11 KR KR1020217004048A patent/KR20210032429A/ko unknown
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  • 2019-07-11 US US17/259,341 patent/US20210292861A1/en active Pending
  • 2019-07-11 JP JP2020571507A patent/JP2021529882A/ja active Pending
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