EP4584413A1 - Rapid annealing and quenching of aluminum alloy products to reduce roping or ludering - Google Patents
Rapid annealing and quenching of aluminum alloy products to reduce roping or luderingInfo
- Publication number
- EP4584413A1 EP4584413A1 EP22783242.5A EP22783242A EP4584413A1 EP 4584413 A1 EP4584413 A1 EP 4584413A1 EP 22783242 A EP22783242 A EP 22783242A EP 4584413 A1 EP4584413 A1 EP 4584413A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- aluminum alloy
- alloy product
- product
- quenching
- rolled
- 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
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Classifications
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
- C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
- C22F1/002—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working by rapid cooling or quenching; cooling agents used therefor
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- 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
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- 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
- C22C—ALLOYS
- C22C21/00—Alloys based on aluminium
- C22C21/12—Alloys based on aluminium with copper 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
- C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
- C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
- C22F1/04—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon
- C22F1/05—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon of alloys of the Al-Si-Mg type, i.e. containing silicon and magnesium in approximately equal proportions
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- 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
-
- 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
- C22F1/057—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 copper as the next major constituent
Definitions
- the present disclosure relates to metallurgy generally and more specifically to aluminum alloys and aluminum alloy products having low roping. In certain aspects, the disclosure also provides methods of making such products.
- Aluminum alloy articles are desirable for use in a number of different applications, such as those where strength and durability are especially desirable.
- aluminum alloys are commonly used for automotive skin panels and structural applications in place of steel. Because aluminum alloys are generally about 2.8 times less dense than steel, the use of such materials reduces the weight of the vehicle and allows for substantial improvements in its fuel economy. Even so, the use of currently available aluminum alloys in automotive and other applications poses certain challenges.
- One such challenge for skin applications relates to forming automotive components with high elongation, improved surface quality (e.g., low roping), and high bendability or hemmability for assembly of the automotive components.
- Roping is a strain-induced roughness or a macroscopic surface roughening defect.
- Roping can be characterized by visible lines that may be several centimeters wide along the rolling direction.
- Roping can result from materials being stretched along a transverse direction. The surface distribution of ridges and valleys can limit the use of the materials for outer panels in vehicle applications.
- the rolled aluminum alloy products may be resistant to roping or Ludering effects upon stretching or forming.
- the methods described may employ a process in which the aluminum alloy product is subjected to a rapid annealing and quenching process during processing to impart desirable properties to the aluminum alloy product.
- the desirable properties can be imparted directly into the aluminum alloy product immediately upon being subjected to rapid annealing and quenching.
- can be imparted and/or carry over into the aluminum alloy product upon subsequent processing which may include rolling processes, solution heat-treatment processes, and/or aging processes, for example.
- a method of this aspect may comprise providing a rolled aluminum alloy product, subjecting the rolled aluminum alloy product to a rapid annealing process to produce an annealed aluminum alloy product, and subjecting the annealed aluminum alloy product to a quenching process to produce a quenched aluminum alloy product.
- the rapid annealing process comprises heating the rolled aluminum alloy product at a rate of up to 100 °C/s to a peak temperature of from 400 °C to 575 °C.
- the quenching process comprises cooling portions of the annealed aluminum alloy at a rate of from -500 °C/s to -2 °C/s.
- additional processing may be performed after the rapid annealing and quenching processes.
- some methods of this aspect may comprise or further comprise subjecting the quenched aluminum alloy product to a cold rolling process to produce a cold-rolled aluminum alloy product.
- some methods of this aspect may comprise or further comprise subjecting the aluminum alloy product to a solution heat-treatment process.
- methods of this aspect may further comprise subjecting the aluminum alloy product to one or more of a cutting process, a forming process, an ageing process.
- the rolled aluminum alloy products used in the methods of this aspect can be any suitable aluminum alloy product.
- the rolled aluminum alloy product may be a hot-rolled aluminum alloy product.
- the rolled aluminum alloy product has a thickness of from 1 mm to 8 mm.
- the rolled aluminum alloy product may be a cold-rolled aluminum alloy product.
- the rolled aluminum alloy product has a thickness of from 0.5 mm to 5 mm.
- the rolled aluminum alloy product is at least partially unrecrystallized or is fully unrecrystallized.
- the annealed aluminum alloy product is at least partially recrystallized or is fully recrystallized.
- the rolled aluminum alloy product comprises a 6xxx series aluminum alloy or a 7xxx series aluminum alloy.
- the rolled aluminum alloy product comprises a 2xxx series aluminum alloy or a 5xxx series aluminum alloy.
- the aluminum alloy product may include, comprise, or exhibit beneficial characteristics.
- the presence of more or larger Mg2Si particles in an aluminum alloy product may result in a lower yield strength or reduced ultimate elongation, so it may be desirable to minimize or reduce the size of Mg2Si particles in the product, such as by processing according to the methods described herein.
- the quenched aluminum alloy product exhibits a yield stress of from 70 MPa to 160 MPa.
- the quenched aluminum alloy product exhibits a total elongation of from 20% to 30%.
- the quenched aluminum alloy product exhibits an average Mg2Si particle size of less than 2 pm.
- the quenched aluminum alloy product exhibits an electrical conductivity of from 40% IACS to 55% IACS.
- electrical conductivity may be related to or correlate with an amount of dissolved solute (e.g., alloying elements) in the aluminum alloy matrix, including Mg and Si, and so a relatively lower electrical conductivity may indicate a relatively higher amount of dissolved Mg and Si and a relatively lower amount of Mg2Si particles in the aluminum alloy product.
- the dissolution of more Mg and Si into the aluminum matrix may also result in a reduction of average grain size.
- the quenched aluminum alloy product exhibits an average grain size of 10 pm to 35 pm.
- magnetic induction heating may be used for the rapid annealing process.
- the rapid annealing process comprises exposing the annealed aluminum alloy product to a quenching fluid after a heating process.
- the rapid annealing process does not comprise a batch or coil annealing process, such as where an entire coil of a rolled aluminum alloy is heated at the same time, such as in a furnace.
- the quenching process does not comprise a batch or coil cooling process, such as where an entire coil of a rolled aluminum alloy is reduced in temperature from the heated temperature, such as in the annealing furnace.
- subjecting the rolled aluminum alloy product to the rapid annealing process comprises uncoiling the rolled aluminum alloy.
- the rapid annealing process is a continuous heating process that heats only portions of the rolled aluminum alloy product at a time.
- the rapid annealing processes described herein may be performed quickly, such as within a few minutes or within tens of minutes.
- the rolled aluminum alloy product is subjected to temperatures greater than 100 °C during the rapid annealing and quenching processes for at most 5 minutes.
- methods of this aspect may further comprise holding the rolled aluminum alloy product within 20 °C of the peak temperature for up to 1 minute prior to the quenching process.
- an aluminum alloy product comprises a formed or stretched aluminum alloy sheet product comprising a 5xxx series aluminum alloy, a 6xxx series aluminum alloy, or a 7xxx series aluminum alloy, such as having a surface arithmetical mean height (Sa) of the formed or stretched aluminum alloy sheet product of at most 10 pm.
- a thickness of the formed or stretched aluminum alloy sheet product may be from 1.00 mm to 3.5 mm.
- the formed or stretched aluminum alloy sheet product comprises a 6xxx series aluminum alloy.
- the formed or stretched aluminum alloy sheet product is free or substantially free of surface roping bands.
- the formed or stretched aluminum alloy sheet product comprises a 5xxx series aluminum alloy.
- the formed or stretched aluminum alloy sheet product is free or substantially free of surface Luders bands.
- FIG. 1 provides a schematic overview of an example method for making a rolled aluminum alloy product.
- FIG. 3 provides a schematic illustration of rapid annealing and quenching of an aluminum alloy product.
- FIG. 4A, FIG. 4B, FIG. 4C, FIG. 4D, and FIG. 4E provide optical micrographs comparing the grain structure of samples subjected to rapid annealing and quenching with samples subjected to batch annealing.
- FIG. 7 provides data showing yield stress of samples subjected to rapid annealing and quenching and a sample subjected to batch annealing.
- FIG. 8 provides data showing total elongation of samples subjected to rapid annealing and quenching and a sample subjected to batch annealing.
- FIG. 9 shows optical micrographs of a cross section of samples subjected to rapid annealing and quenching and batch annealing.
- FIG. 10 provides 50 pm wide micrograph images of samples subjected to rapid annealing and quenching or batch annealing, showing the amount and size of precipitates.
- FIG. 11 provides data showing the yield stress for annealed, cold rolled, and solution heat treated samples after room temperature aging (T4 temper condition) and artificial aging/paint baking (T81 temper condition).
- FIG. 12 provides data showing the total elongation for annealed, cold rolled, and solution heat treated samples after room temperature aging (T4 temper condition).
- FIG. 13 provides electrical conductivity results for rolled aluminum alloy product samples subjected to rapid annealing and quenching.
- FIG. 17 provides measured yield stress of samples subjected to rapid annealing to different peak temperatures.
- FIG. 18 provides measured maximum axial strain of samples subjected to rapid annealing to different peak temperatures.
- Described herein are methods for preparing rolled aluminum alloy products that are resistant to roping or Ludering effects upon stretching or forming.
- Roping is the development of a series of ridges and valleys of various depths that extend along the rolling direction when certain aluminum alloys, such as 6xxx series alloys or 7xxx series alloys, are stretched in the transverse direction, for example. These ridges and valleys give an undesirable surface appearance to the formed or stretched aluminum alloy products.
- Ludering is another undesirable surface characteristic that develops in certain aluminum alloys, such as 5xxx series alloys or other Mg containing alloys, where dislocations propagate through the aluminum crystal lattice during forming or stretching and create Ludering bands.
- the present application provides processing techniques for rolled aluminum alloy products that limit roping or Ludering by subjecting the rolled aluminum alloy products to a rapid annealing and quenching process prior to one or more cold rolling processes.
- the rapid annealing and quenching processing described herein can replace batch annealing, commonly used for treating hot-rolled aluminum alloy products prior to cold rolling, and can shorten processing times prior to the cold rolling.
- batch annealing can take many hours (e.g., 20 hours or more) to process, and generally involves placing coils of hot-rolled aluminum alloy products into a furnace and heating them to an annealing temperature and holding for some time before allowing the coils to cool to ambient temperature.
- the rapid annealing and quenching processing described herein can process a coil of a hot-rolled aluminum alloy product very quickly, such as within 1 hour or less.
- the rapid annealing and quenching processing described herein can also or alternatively be used as an interannealing process between cold rolling passes.
- the material can be uncoiled (if coiled), passed through a rapid annealing system and a quenching system and then be re-coiled, optionally, for subsequent processing.
- the rapid annealing process can heat the portion of the aluminum alloy product passing through the rapid annealing system to a desired peak temperature very quickly, such as within a few seconds to a few minutes.
- the rapid annealing and quenching processing can result in modification of the properties of the rolled aluminum alloy product that provide various enhancements.
- the rolled aluminum alloy product can undergo recrystallization, at least in part, where deformed grains of aluminum are replaced by defect-free grains during the annealing process.
- the rolled aluminum alloy product can be at least partially unrecrystallized or fully unrecrystallized prior to rapid annealing and quenching and/or can be at least partially recrystallized or fully recrystallized after rapid annealing and quenching.
- the rapid annealing and quenching process can result in the annealed and quenched aluminum alloy product having a finer grain structure (e.g., smaller average grain size) and more uniform grain structure (e.g., narrower grain size distribution) and different mechanical or strength characteristics as compared to the aluminum alloy product prior to annealing and quenching. These characteristics can propagate through subsequent cold rolling and other processing and into the final product.
- the aluminum alloy product after rapid annealing and quenching, can exhibit an average grain size of 10 pm to 35 pm, such as from 10 pm to 15 pm, 15 pm to 20 pm, 20 pm to 25 pm, 25 pm to 30 pm, or 30 pm to 35 pm.
- the aluminum alloy product after rapid annealing and quenching, can exhibit a yield stress of from 70 MPa to 160 MPa, such as from 70 MPa to 80 MPa, from 80 MPa to 90 MPa, from 90 MPa to 100 MPa, from 100 MPa to 110 MPa, from 110 MPa to 120 MPa, from 120 MPa to 130 MPa, from 130 MPa to 140 MPa, from 140 MPa to 150 MPa, or from 150 MPa to 160 MPa.
- the aluminum alloy product after rapid annealing and quenching, can exhibit a total elongation of from 20% to 30%, such as from 20% to 21%, from 21% to 22%, from 22% to 23%, from 23% to 24%, from 24% to 25%, from 25% to 26%, from 26% to 27%, from 27% to 28%, from 28% to 29%, or from 29% to 30%.
- the rapid annealing and quenching processing can serve to reduce the size of precipitates, such as Mg2Si particles for example, that may be present in the aluminum alloy product prior to annealing and quenching.
- the precipitates can be very coarse, but after the rapid annealing and quenching processing, considerable amounts, or even all or almost all, of the precipitates can be dissolved in the aluminum matrix, impacting electrical conductivity and other properties (e.g., strength). Again, these properties can propagate through subsequent cold rolling and other processing.
- a solution heat treatment process applied after cold rolling can be completed in a shorter amount of time, allowing for increases in line speed of a solutionizing process and higher throughput.
- the rapid annealing and quenching processes described herein are different from and generally do not comprise a batch annealing process, such as where an entire coil of a rolled aluminum product is subjected to annealing while in a coiled configuration.
- the rapid annealing and quenching process provides advantages over batch annealing, including faster annealing and cooling processing times, and differences in grain and precipitate structure.
- the rapid annealing and quenching processing can be useful for controlling various characteristics of the aluminum alloy product, while limiting, reducing, or eliminating the effects of roping or Ludering that may otherwise occur upon forming or stretching of the processed aluminum alloy product in the absence of the rapid annealing and quenching processing.
- surface arithmetical mean height (Sa) may provide a measure characterizing the presence or absence of roping or Ludering.
- Techniques described herein are useful for generating an aluminum alloy product, such as a 5xxx series, 6xxx series, or 7xxx series aluminum alloy sheet product that, after forming or stretching, exhibits a surface arithmetical mean height (Sa) of at most
- invention As used herein, the terms “invention,” “the invention,” “this invention” and “the present invention” are intended to refer broadly to all of the subject matter of this patent application and the claims below. Statements containing these terms should be understood not to limit the subject matter described herein or to limit the meaning or scope of the patent claims below.
- a plate generally has a thickness of greater than about 15 mm.
- a plate may refer to an aluminum product having a thickness of greater than about 15 mm, greater than about 20 mm, greater than about 25 mm, greater than about 30 mm, greater than about 35 mm, greater than about 40 mm, greater than about 45 mm, greater than about 50 mm, or greater than about 100 mm.
- a sheet generally refers to an aluminum product having a thickness of less than about 4 mm.
- a sheet may have a thickness of less than about 4 mm, less than about 3 mm, less than about 2 mm, less than about 1 mm, less than about 0.5 mm, or less than about 0.3 mm (e.g., about 0.2 mm).
- a T1 condition or temper refers to an aluminum alloy cooled from hot working and naturally aged (e.g., at room temperature).
- a T2 condition or temper refers to an aluminum alloy cooled from hot working, cold worked and naturally aged.
- a T3 condition or temper refers to an aluminum alloy solution heat treated, cold worked, and naturally aged.
- a T4 condition or temper refers to an aluminum alloy solution heat treated and naturally aged.
- a T5 condition or temper refers to an aluminum alloy cooled from hot working and artificially aged (at elevated temperatures).
- a T6 condition or temper refers to an aluminum alloy solution heat treated and artificially aged.
- a T7 condition or temper refers to an aluminum alloy solution heat treated and artificially overaged.
- a T8x condition or temper refers to an aluminum alloy solution heat treated, cold worked, and artificially aged.
- a T9 condition or temper refers to an aluminum alloy solution heat treated, artificially aged, and cold worked.
- a W condition or temper refers to an aluminum alloy after solution heat treatment.
- cast metal product As used herein, terms such as “cast metal product,” “cast product,” “cast aluminum alloy product,” and the like are interchangeable and refer to a product produced by direct chill casting (including direct chill co-casting) or semi-continuous casting, continuous casting (including, for example, by use of a twin belt caster, a twin roll caster, a block caster, or any other continuous caster), electromagnetic casting, hot top casting, or any other casting method.
- Unavoidable impurities including materials or elements may be present in an alloy in minor amounts due to inherent properties of aluminum or leaching from contact with processing equipment. Some alloys, as described, may contain no more than about 0.25 wt.% of any element besides the alloying elements, incidental elements, and unavoidable impurities.
- a cast product may be heated to a temperature ranging from about 400 °C to about 600 °C.
- the cast product can be heated to a temperature of about 400 °C, about 410 °C, about 420 °C, about 430 °C, about 440 °C, about 450 °C, about 460 °C, about 470 °C, about 480 °C, about 490 °C, about 500 °C, about 510 °C, about 520 °C, about 530 °C, about 540 °C, about 550 °C, about 560 °C, about 570 °C, about 580 °C, about 590 °C, or about 600 °C.
- the product may then be allowed to soak (i.e., held at the indicated temperature) for a period of time to form a homogenized product.
- the total time for the homogenization step can be up to 24 hours.
- the product can be heated up to 500 °C to 600 °C, and soaked, for a total time of up to 18 hours for the homogenization step.
- the product can be heated to below 490 °C and soaked, for a total time of greater than 18 hours for the homogenization step.
- the homogenization step comprises multiple processes.
- the homogenization step includes heating a cast product to a first temperature for a first period of time followed by heating to a second temperature for a second period of time.
- a cast product can be heated to about 465 °C for about 3.5 hours and then heated to about 480 °C for about 6 hours.
- a hot rolling step can be optionally performed.
- the homogenized product Prior to the start of hot rolling, can be allowed to cool to a temperature between 300 °C to 450 °C.
- the homogenized product can be allowed to cool to a temperature of between 325 °C to 425 °C or from 350 °C to 400 °C.
- the homogenized product can then be hot rolled at a temperature between 300 °C to 450 °C to form a hot rolled plate, a hot rolled shate or a hot rolled sheet having a gauge between 3 mm and 200 mm (e.g., 3 mm, 4 mm, 5 mm, 6 mm, 7 mm, 8 mm, 9 mm, 10 mm, 15 mm, 20 mm, 25 mm, 30 mm, 35 mm, 40 mm, 45 mm, 50 mm, 55 mm, 60 mm, 65 mm, 70 mm, 75 mm, 80 mm, 85 mm, 90 mm, 95 mm, 100 mm, 110 mm, 120 mm, 130 mm, 140 mm, 150 mm, 160 mm, 170 mm, 180 mm, 190 mm, 200 mm, or anywhere in between).
- the cast product can be a continuously cast product that can be allowed to cool to a temperature between 300 °C to 450 °C.
- the continuously cast product can be allowed to cool to a temperature of between 325 °C to 425 °C or from 350 °C to 400 °C.
- Cast, homogenized, or hot-rolled products can be optionally cold rolled using cold rolling mills into thinner products, such as a cold rolled sheet.
- the cold rolled product can have a gauge between about 0.5 to 10 mm, e.g., between about 0.7 to 6.5 mm.
- the cold rolled product can have a gauge of 0.5 mm, 1.0 mm, 1.5 mm, 2.0 mm, 2.5 mm, 3.0 mm, 3.5 mm, 4.0 mm, 4.5 mm, 5.0 mm, 5.5 mm, 6.0 mm, 6.5 mm, 7.0 mm, 7.5 mm, 8.0 mm, 8.5 mm, 9.0 mm, 9.5 mm, or 10.0 mm.
- the hot product is cooled at a quench rate of above 200 °C/second at temperatures between 450 °C and 200 °C.
- the cooling rates can be faster in other cases.
- the temperature can be lower in other cases.
- the hot product is cooled at a quench rate of above 200 °C/second at temperatures between 450 °C and 200 °C.
- the heat-treated product can optionally undergo a pre-aging treatment by reheating before coiling.
- the pre-aging treatment can be performed at a temperature of from about 70 °C to about 125 °C for a period of time of up to 6 hours.
- the pre-aging treatment can be performed at a temperature of about 70 °C, about 75 °C, about 80 °C, about 85 °C, about 90 °C, about 95 °C, about 100 °C, about 105 °C, about 110 °C, about 115 °C, about 120 °C, or about 125 °C.
- the pre-aging treatment can be performed for about 30 minutes, about 1 hour, about 2 hours, about 3 hours, about 4 hours, about 5 hours, or about 6 hours.
- the pre-aging treatment can be carried out by passing the heat-treated product through a heating device, such as a device that emits radiant heat, convective heat, induction heat, infrared heat, or the like.
- the aluminum alloy products and methods described herein can also be used in electronics applications.
- the aluminum alloy products and methods described herein can be used to prepare housings for electronic devices, including mobile phones and tablet computers.
- the aluminum alloy products can be used to prepare housings for the outer casing of mobile phones (e.g., smart phones), tablet bottom chassis, and other portable electronics.
- the aluminum alloy product may optionally be subjected to a solution heat treatment process 235, where the temperature of the aluminum alloy product is increased to a temperature above a threshold temperature, such as a temperature at which precipitated components in the aluminum alloy product dissolve into a solid solution, and held above the threshold temperature for a period of time.
- a threshold temperature such as a temperature at which precipitated components in the aluminum alloy product dissolve into a solid solution
- the aluminum alloy product may be subjected to a quenching process 240, where dissolved components are fixed into place by rapidly reducing the temperature of the aluminum alloy by a quenching process.
- a quenching process 240 may involve exposing the aluminum alloy product to a solution, such as a quench solution including water, an aqueous solution, or a gas solution.
- the rapid annealing and quenching process 225 may allow for a hold time during solution heat treatment process 235 to be reduced compared to solution heat treatment of an aluminum alloy product that is not subjected to rapid annealing and quenching process 225.
- the processes overviewed in FIG. 2 may be performed discretely or as part of one or more continuous processing lines where the aluminum alloy product may be transported as a coil, a film, or a web of material between processing stages.
- the aluminum alloy product may be transported between stages by rolling the aluminum alloy product, which may be under tension, over or between one or more rollers, or by transporting the aluminum alloy product on one or more conveyors, for example.
- other stages not explicitly identified may be included before, between, and/or after any stage identified in FIG. 2.
- Other example stages include, but are not limited to, a washing stage, a chemical treatment stage, or a finishing stage.
- FIG. 3 provides a schematic illustration of an example rapid annealing and quenching system 300 for treatment of an aluminum alloy product 305.
- Aluminum alloy product 305 can comprise any suitable aluminum alloy product, such as a hot-rolled aluminum alloy product or a cold-rolled aluminum alloy product.
- Aluminum alloy product 305 can comprise any aluminum alloy described herein, but particularly may comprise a 2xxx series aluminum alloy, a 5xxx series aluminum alloy, a 6xxx series aluminum alloy, or a 7xxx series aluminum alloy.
- Aluminum alloy product 305 can have any suitable thickness, such as a thickness of from 1 mm to 8 mm, or a thickness of from 0.5 mm to 5 mm.
- aluminum alloy product has a thickness of from 1.0 mm to 1.1 mm, from 1.1 mm to 1.2 mm, from 1.2 mm to 1.3 mm, from 1.3 mm to 1.4 mm, from 1.4 mm to 1.5 mm, from
- rapid annealing system 310 can comprise a series of permanent magnetic rotors 320 that are used to heat the aluminum alloy product 305 by way of magnetic induction heating.
- Permanent magnetic rotors 320 may be provided in any suitable arrangement of individual permanent magnetic rotors 320 or pairs of permanent magnetic rotors 320. Further details of an exemplary magnetic rotor-based magnetic induction heating system are described in U.S. Patent Application Publication No. 2018/0091263, which is hereby incorporated by reference in its entirety.
- cooling rates below -500 °C/s can be used.
- a cooling rate of -5 °C/s refers to the temperature of an aluminum alloy product being decreased by 5 °C in one second.
- quenching system 315 can comprise a series of spray nozzles 325 that are used to apply a quenching fluid to the aluminum alloy product 305.
- Example quenching fluids can comprise a gas, air, water, an aqueous solution, oil, or other suitable quenching fluids.
- Example hold times include from 0 seconds to 5 seconds, from 5 seconds to 10 seconds, from 10 seconds to 15 seconds, from 15 seconds to 20 seconds, from 20 seconds to 25 seconds, from 25 seconds to 30 seconds, from 30 seconds to 35 seconds, from 35 seconds to 40 seconds, from 40 seconds to 45 seconds, from 45 seconds to 50 seconds, from 50 seconds to 55 seconds, or from 55 seconds to 1 minute. Hold times in excess of 1 minute may be applied in some cases.
- rapid heating and quenching system 300 can be used to anneal and quench aluminum alloy product 305 very quickly, such as in 5 minutes or less.
- a portion of the aluminum alloy product 305 can enter the rapid annealing system 310, exit the rapid annealing system 310, enter the quenching system 315, and exit the quenching system 315 in 5 minutes or less.
- any portion of the aluminum alloy product is subjected to temperatures greater than or about 100 °C during rapid annealing and quenching for at most 5 minutes.
- these times can be from 5 seconds to 5 minutes, such as from 15 seconds to 30 seconds, from 30 seconds to 45 seconds, from 45 seconds to 1 minute, from 1 minute to 1.25 minutes, from 1.25 minutes to 1.5 minutes, from 1.5 minutes to 1.75 minutes, from 1.75 minutes to 2 minutes, from 2 minutes to 2.25 minutes, from 2.25 minutes to 2.5 minutes, from 2.5 minutes to 2.75 minutes, from 2.75 minutes to 3 minutes, from 3 minutes to 3.25 minutes, from 3.25 minutes to 3.5 minutes, from 3.5 minutes to 3.75 minutes, from 3.75 minutes to 4 minutes, from 4 minutes to 4.25 minutes, from 4.25 minutes to 4.5 minutes, from 4.5 minutes to 4.75 minutes, or from 4.75 minutes to 5 minutes.
- 5 seconds to 5 minutes such as from 15 seconds to 30 seconds, from 30 seconds to 45 seconds, from 45 seconds to 1 minute, from 1 minute to 1.25 minutes, from 1.25 minutes to 1.5 minutes, from 1.5 minutes to 1.75 minutes, from 1.75 minutes to 2 minutes, from 2 minutes to 2.25 minutes, from 2.25 minutes to 2.5 minutes, from 2.5 minutes to 2.75 minutes, from
- the rapid heating and quenching system 300 can have any suitable heating power and line capacity.
- the line capacity may be a function of the heating power, incoming temperature for aluminum alloy product 305, and peak temperature to raise the aluminum alloy product 305 to.
- rapid heating and quenching system 300 can have a heating power of from 1 MW to 10 MW, or more.
- Example powers include, but are not limited to, 1 MW, 1.5 MW, 2 MW, 2.5 MW, 3 MW, 3.5 MW, 4 MW, 4.5 MW, 5 MW, 5.5 MW, 6 MW, 6.5 MW, 7 MW, 7.5 MW, 8 MW, 8.5 MW, 9 MW, 9.5 MW, or 10 MW.
- the temperature of the aluminum alloy product 305 prior to or at entry into the rapid heating and quenching system 300 can be any suitable temperature, such as from about 25 °C to about 400 °C, such as from 25 °C to 50 °C, from 50 °C to 75 °C, from 75 °C to 100 °C, from 100 °C to 125 °C, from 125 °C to 150 °C, from 150 °C to 175 °C, from 175 °C to 200 °C, from 200 °C to 225 °C, from 225 °C to 250 °C, from 250 °C to 275 °C, from 275 °C to 300 °C, from 300 °C to 325 °C, from 325 °C to 350 °C, from 350 °C to 375 °C, or from 375 °C to 400 °C.
- the line capacity of rapid heating and quenching system may range from about 40 kTa to about 400 kTa, such as from 40 kTa to 50 kTa, from 50 kTa to 75 kTa, from 75 kTa to 100 kTa, from 100 kTa to 125 kTa, from 125 kTa to 150 kTa, from 150 kTa to 175 kTa, from 175 kTa to 200 kTa, from 200 kTa to 225 kTa, from 225 kTa to 250 kTa, from 250 kTa to 275 kTa, from 275 kTa to 300 kTa, from 300 kTa to 325 kTa, from 325 kTa to 350 kTa, from 350 kTa to 375 kTa, or from 375 kTa to 400 kTa.
- Line capacity may be higher still, such as if heating power is
- the aluminum alloy product subjected to rapid annealing and quenching can comprise any suitable alloy and have any suitable dimensions.
- the alloy product can have a thickness of from 1 mm to 8 mm.
- the aluminum alloy product can comprise a 6xxx series aluminum alloy, a 7xxx series aluminum alloy, a 2xxx series aluminum alloy, or a 5xxx series aluminum alloy.
- a series of tests were performed to evaluate the properties of rolled aluminum alloy products subjected to rapid annealing and quenching as described herein. Initial tests were performed using a Gleeble thermomechanical simulator to evaluate mechanical properties, degree of recrystallization, and precipitate coarsening as a function of annealing temperature and quenching rate and aid in defining processing conditions for subsequent tests. Coupons of a hot-rolled 6xxx series aluminum alloy with 5 mm thickness were heated to peak temperatures from 325 °C to 500 °C using rapid heating (about 10-20 °C/s) and subjected to immediate air quenching upon reaching the peak temperature, air quenching 10 seconds after reaching the peak temperature, or non-quenched cooling with a temperature profile similar to coil cooling. The air quenching rate was about -40 °C/s.
- FIG. 4A, FIG. 4B, FIG. 4C, FIG. 4D, and FIG. 4E provides optical micrographs comparing the grain structure of samples of a 6xxx series aluminum alloy product subjected to rapid heating to different peak temperatures followed immediately by air quenching, samples of a 6xxx series aluminum alloy product subjected to rapid heating to different peak temperatures followed by air quenching after 10 seconds, and samples subjected to batch annealing for 2 hours followed by coil type cooling in the batch annealing furnace.
- the samples subjected to rapid heating to 500 °C show full recrystallization and smaller and more equiaxed grains than the comparable product subjected to batch annealing.
- FIG. 14A shows micrographs illustrating the through thickness grain structure (transverse cross section, perpendicular to rolling direction) of samples annealed to a peak temperature of 460 °C, showing no significant impact of heating rate on grain size.
- FIG. 14C shows micrographs illustrating the through thickness grain structure (transverse cross section, perpendicular to rolling direction) of samples annealed to a peak temperature of 530 °C, showing no significant impact of heating rate on grain size.
- FIG. 15A and FIG. 15B provide micrograph images of samples subjected to rapid annealing to peak temperatures of 460 °C and 530 °C at different heating rates to show the amount and size of Mg2Si precipitates (dark spots in images). In general, the particle content appears to be similar at the different heating rates, though the higher peak temperature of 530 appears to reduce particle numbers.
- FIG. 16 provides electrical conductivity data of samples subjected to rapid annealing to different peak temperatures, showing measured conductivity values at different positions in terms of % IACS (International Annealed Copper Standard). These values are significantly lower than those observed for batch annealed reference samples, which exhibited an electrical conductivity of about 56.8 % IACS.
- FIG. 17 provides measured yield stress of samples subjected to rapid annealing to different peak temperatures. These values are significantly higher than those observed for batch annealed reference samples, which exhibited a yield strength of about 51-52 MPa.
- FIG. 18 provides measured maximum axial strain of samples subjected to rapid annealing to different peak temperatures. These values are significantly lower than those observed for batch annealed reference samples, which exhibited a maximum axial strain of about 32-36 MPa.
- any reference to a series of aspects e.g., “Aspects 1-4” or nonenumerated group of aspects (e.g., “any previous or subsequent aspect”) is to be understood as a reference to each of those aspects disjunctively (e.g., “Aspects 1-4” is to be understood as “Aspects 1, 2, 3, or 4 ”).
- Aspect 1 is a method comprising: providing a rolled aluminum alloy product; subjecting the rolled aluminum alloy product to a rapid annealing process to produce an annealed aluminum alloy product, wherein the rapid annealing process comprises heating the rolled aluminum alloy product at a rate of up to 100 °C/s to a peak temperature of from 400 °C to 575 °C; and subjecting the annealed aluminum alloy product to a quenching process to produce a quenched aluminum alloy product, wherein the quenching process comprises cooling portions of the annealed aluminum alloy product at a rate of from -500 °C/s to -2 °C/s.
- Aspect 5 is the method of any previous or subsequent aspect, wherein the rolled aluminum alloy product is a hot-rolled aluminum alloy product.
- Aspect 6 is the method of any previous or subsequent aspect, wherein the quenched aluminum alloy product exhibits an average Mg2Si particle size of less than 2 pm.
- Aspect 7 is the method of any previous or subsequent aspect, wherein the quenched aluminum alloy product exhibits an electrical conductivity of from 40% IACS to 55% IACS.
- Aspect 8 is the method of any previous or subsequent aspect, wherein the quenched aluminum alloy product exhibits a yield stress of from 70 MPa to 160 MPa.
- Aspect 9 is the method of any previous or subsequent aspect, wherein the quenched aluminum alloy product exhibits a total elongation of from 20% to 30%.
- Aspect 10 is the method of any previous or subsequent aspect, wherein the quenched aluminum alloy product exhibits an average grain size of 10 pm to 35 pm.
- Aspect 11 is the method of any previous or subsequent aspect, wherein the rolled aluminum alloy product has a thickness of from 1 mm to 8 mm.
- Aspect 13 is the method of any previous or subsequent aspect, wherein the rolled aluminum alloy product is at least partially unrecrystallized or is fully unrecrystallized.
- Aspect 22 is the method of any previous or subsequent aspect, wherein the rapid annealing process comprises passing the rolled aluminum alloy product through a heating system at a rate of from 5 m/min to 600 m/min; or wherein the quenching process comprises passing the annealed aluminum alloy product through a quenching system at a rate of from 5 m/min to 600 m/min.
- Aspect 23 is the method of any previous or subsequent aspect, wherein the rolled aluminum alloy product is subjected to temperatures greater than 100 °C during the rapid annealing and quenching processes for at most 5 minutes.
- Aspect 24 is the method of any previous or subsequent aspect, further comprising holding the rolled aluminum alloy product within 20 °C of the peak temperature for up to 1 minute prior to the quenching process.
- Aspect 25 is an aluminum alloy prepared using the method of any of any previous or subsequent aspect.
- Aspect 26 is an aluminum alloy product comprising: a formed or stretched aluminum alloy sheet product comprising a 5xxx series aluminum alloy, a 6xxx series aluminum alloy, or a 7xxx series aluminum alloy, wherein a surface arithmetical mean height (Sa) of the formed or stretched aluminum alloy sheet product is at most 10 pm, and wherein a thickness of the formed or stretched aluminum alloy sheet product is from 1.00 mm to 3.5 mm.
- a surface arithmetical mean height (Sa) of the formed or stretched aluminum alloy sheet product is at most 10 pm
- a thickness of the formed or stretched aluminum alloy sheet product is from 1.00 mm to 3.5 mm.
- Aspect 27 is the aluminum alloy product of any previous or subsequent aspect, wherein the formed or stretched aluminum alloy sheet product comprises a 6xxx series aluminum alloy, and wherein the formed or stretched aluminum alloy sheet product is free or substantially free of surface roping bands.
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Abstract
Description
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| PCT/US2022/076177 WO2024054235A1 (en) | 2022-09-09 | 2022-09-09 | Rapid annealing and quenching of aluminum alloy products to reduce roping or ludering |
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| EP (1) | EP4584413A1 (en) |
| JP (1) | JP2025530811A (en) |
| KR (1) | KR20250040036A (en) |
| CN (1) | CN119855934A (en) |
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| JP2000001730A (en) * | 1998-06-17 | 2000-01-07 | Furukawa Electric Co Ltd:The | Aluminum alloy plate for can body and method for producing the same |
| JP2004043938A (en) * | 2002-07-16 | 2004-02-12 | Furukawa Sky Kk | Manufacturing method of aluminum alloy annealed sheet with excellent appearance performance |
| JP4178518B2 (en) * | 2003-10-14 | 2008-11-12 | 新東工業株式会社 | Method for producing 6000 series aluminum alloy plate |
| AU2014200219B2 (en) * | 2004-02-19 | 2016-10-13 | Arconic Technologies Llc | In-line method of making heat-treated and annealed aluminum alloy sheet |
| JP2007031819A (en) * | 2005-07-29 | 2007-02-08 | Nippon Light Metal Co Ltd | Method for producing aluminum alloy plate |
| JP5406745B2 (en) * | 2009-03-19 | 2014-02-05 | 株式会社神戸製鋼所 | Aluminum alloy sheet with excellent ridging marks during molding |
| CA2971618C (en) * | 2015-01-12 | 2020-08-25 | Novelis Inc. | Highly formable automotive aluminum sheet with reduced or no surface roping and a method of preparation |
| WO2016161579A1 (en) | 2015-04-08 | 2016-10-13 | Telefonaktiebolaget Lm Ericsson (Publ) | A wireless device and method therein for performing aretransmission of data in a device-to-device, d2d, communication |
| CN109628803B (en) * | 2018-11-30 | 2020-08-25 | 郑州明泰实业有限公司 | Aluminum alloy checkered plate in 4017-H2X state and preparation method thereof |
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2022
- 2022-09-09 CN CN202280099859.5A patent/CN119855934A/en active Pending
- 2022-09-09 EP EP22783242.5A patent/EP4584413A1/en active Pending
- 2022-09-09 KR KR1020257005233A patent/KR20250040036A/en active Pending
- 2022-09-09 CA CA3264350A patent/CA3264350A1/en active Pending
- 2022-09-09 JP JP2025513658A patent/JP2025530811A/en active Pending
- 2022-09-09 WO PCT/US2022/076177 patent/WO2024054235A1/en not_active Ceased
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| JP2025530811A (en) | 2025-09-17 |
| KR20250040036A (en) | 2025-03-21 |
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