US20070209739A1 - Method for producing Al-Mg-Si alloy sheet excellent in bake-hardenability and hemmability - Google Patents

Method for producing Al-Mg-Si alloy sheet excellent in bake-hardenability and hemmability Download PDF

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US20070209739A1
US20070209739A1 US10/582,272 US58227204A US2007209739A1 US 20070209739 A1 US20070209739 A1 US 20070209739A1 US 58227204 A US58227204 A US 58227204A US 2007209739 A1 US2007209739 A1 US 2007209739A1
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cooling
treatment
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coil
hemmability
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Pizhi Zhao
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Nippon Light Metal Co Ltd
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Nippon Light Metal Co Ltd
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Assigned to NIPPON LIGHT METAL COMPANY, LTD. reassignment NIPPON LIGHT METAL COMPANY, LTD. ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: KOBAYASHI, TAKAYUKI, ANAMI, TOSHIYA, OKAMOTO, ICHIRO, ZHAO, PIZHI
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    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22FCHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
    • C22F1/00Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
    • C22F1/04Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon
    • C22F1/05Changing 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
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22DCASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D11/00Continuous casting of metals, i.e. casting in indefinite lengths
    • B22D11/06Continuous casting of metals, i.e. casting in indefinite lengths into moulds with travelling walls, e.g. with rolls, plates, belts, caterpillars
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22DCASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D11/00Continuous casting of metals, i.e. casting in indefinite lengths
    • B22D11/06Continuous casting of metals, i.e. casting in indefinite lengths into moulds with travelling walls, e.g. with rolls, plates, belts, caterpillars
    • B22D11/0605Continuous casting of metals, i.e. casting in indefinite lengths into moulds with travelling walls, e.g. with rolls, plates, belts, caterpillars formed by two belts, e.g. Hazelett-process
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22DCASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D11/00Continuous casting of metals, i.e. casting in indefinite lengths
    • B22D11/12Accessories for subsequent treating or working cast stock in situ
    • B22D11/124Accessories for subsequent treating or working cast stock in situ for cooling
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C21/00Alloys based on aluminium
    • C22C21/02Alloys based on aluminium with silicon as the next major constituent
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C21/00Alloys based on aluminium
    • C22C21/06Alloys based on aluminium with magnesium as the next major constituent
    • C22C21/08Alloys based on aluminium with magnesium as the next major constituent with silicon

Definitions

  • the present invention relates to a production method for obtaining an Al—Mg—Si alloy sheet that is abundant in hemmability while simultaneously having a high age-hardening ability, by casting a thin slab by continuous casting of an Al—Mg—Si alloy, performing a homogenization treatment, then cold rolling, and performing a solution treatment in a continuous annealing furnace as needed.
  • the present method it is possible to produce, at a low cost as compared to the conventional art, rolled sheets of Al—Mg—Si alloy that are suitable for forming by bending, press forming and the like of automotive parts, household appliances and the like.
  • Al—Mg—Si alloys have the property of increasing in strength when heat is applied during processes such as coating after forming, so that they are well-suited for use in automotive panels or the like. Furthermore, the production of sheets of the alloys by continuous casting and rolling has been proposed to reduce costs by improved productivity.
  • Japanese Patent Application, First Publication No. S62-207851 discloses an aluminum alloy sheet for forming and method of production thereof, obtained by continuous casting of an aluminum alloy melt comprising 0.4-2.5% Si, 0.1-1.2% Mg and one or more among 1.5% or less of Cu, 2.5% or less of Zn, 0.3% or less of Cr, 0.6% or less of Mn and 0.3% or less of Zr, to form a 3-15 mm thick slab, cold rolling, then performing a solution treatment and quenching, characterized in that the maximum size of intermetallic compounds in the matrix is 5 ⁇ m or less.
  • Japanese Patent Application, First Publication No. H10-110232 discloses an Al—Mg—Si alloy sheet, obtained by preparing a direct cast rolled sheet of Al alloy comprising 0.2-3.0% Si and 0.2-3.0% Mg, containing one or more of 0.01-0.5% Mn, 0.01-0.5% Cr, 0.01-0.5% Zr and 0.001-0.5% Ti, and further containing 0-2.5% Cu, 0-0.20% Sn and 0-2.0% Zn, with Fe being limited to 1.0% or less and the remainder consisting of Al and unavoidable impurities, and further cold rolling, characterized in that the maximum crystal size in the metallic portion of the sheet is 100 ⁇ m or less and the maximum length of continuous Mg 2 Si compounds on the surface layer portion is 50 ⁇ m or less.
  • Japanese Patent Application, First Publication No. 2001-262264 proposes an Al—Mg—Si alloy sheet excelling in ductility and bendability, the aluminum alloy comprising 0.1-2.0% Si, 0.1-2.0% Mg, 0.1-1.5% Fe or one or more further elements chosen from among 2% or less of Cu, 0.3% or less of Cr, 1.0% or less of Mn, 0.3% or less of Zr, 0.3% or less of V, 0.03% or less of Ti, 1.5% or less of Zn and 0.2% or less of Ag, wherein the maximum size of intermetallic compounds is 5 ⁇ m or less, the maximum aspect ratio is 5 or less and the average crystal grain size is 30 ⁇ m or less.
  • Patent Document 1 Japanese Patent Application, First Publication No. S62-207851
  • Patent Document 2 Japanese Patent Application, First Publication No. Hi0-110232
  • Patent Document 3 Japanese Patent Application, First Publication No. 2001-262264
  • Alloy sheets that are used as outer panels in automotive body sheets or the like require exceptional hemmability and bake-hardenability. For this reason, Al—Mg—Si alloy sheets that excel in bendability and age-harden when heated have been sought. However, sheets produced by continuous casting and rolling have the drawbacks of poor hemmability and insufficient bake-hardenability after coating.
  • the problem to be solved by the present invention is to obtain, at a low cost, an Al—Mg—Si alloy sheet for forming that suppresses GP zones that are deposited during natural ageing when left at room temperature, achieves a high level of bake-hardening due to a reinforcement phase being quickly deposited upon heating during coating and baking, while simultaneously having abundant bendability.
  • a thin slab of Al—Mg—Si alloy is continuously cast by a twin-belt casting machine, the cast thin slab is directly wound, subjected to a homogenization treatment under appropriate conditions, and cold rolled, then combined with a solution treatment in a continuous annealing furnace as needed, thereby fragmenting the compounds and raising the hemmability while simultaneously enabling the procedure to be considerably shortened. Furthermore, microsegregation is reduced by a homogenization treatment, and the cooling rate after the homogenization treatment is raised, thereby reducing the deposition of Mg 2 Si while cooling, to obtain an aluminum sheet for automotive body sheets with excellent bake-hardenabiltiy and hemmability after a final anneal.
  • the present invention which solves the above problem relates to a method of producing aluminum alloy sheets characterized by winding into thin slabs, subjecting to a homogenization treatment, cold rolling, then subjecting to a solution treatment.
  • a method of producing aluminum alloy sheets excelling in bake-hardenability and hemmability comprising steps of casting, by means of a twin-belt casting method, an alloy melt comprising 0.30-1.00 wt % of Mg, 0.30-1.20 wt % of Si, 0.05-0.50 wt % of Fe, 0.05-0.50 wt % of Mn and 0.005-0.10 wt % of Ti, optionally further comprising at least one of 0.05-0.70 wt % of Cu or 0.05-0.40 wt % of Zr, the remainder consisting of Al and unavoidable impurities, to form a 5-15 mm thick slab at a cooling rate of 40-150° C./s at a
  • the homogenization treatment preferably involves heating to 520-580° C. at a heating rate of at least 30° C./h in a batch furnace, then holding at that temperature for 2-24 hours (invention according to claim 2 ).
  • the solution treatment preferably involves heating to 530-560° C. at a heating rate of at least 10° C./s in a continuous annealing line, and holding for 30 seconds or less (invention according to claim 3 ).
  • the solution treatment may be followed by steps of cooling to room temperature at a cooling rate of at least 10° C./s, then subjecting to a restoration treatment by holding for 30 seconds or less at 260-300° C. in a continuous annealing furnace, and cooling to room temperature at a cooling rate of at least 10° C./s (invention according to claim 4 ).
  • the solution treatment may be followed by steps of water-cooling to 250° C. or less at a cooling rate of at least 10° C./s, then air-cooling to 60-100° C. at a cooling rate of 1-20° C./s, coiling up, and subjecting to a preliminary ageing treatment by cooling to room temperature (invention according to claim 5 ).
  • the solution treatment may be followed by steps of cooling to room temperature at a cooling rate of at least 10° C./s, then subjecting to a restoration treatment by holding for 30 seconds or less at 260-300° C. in a continuous annealing furnace, cooling to 60-100° C. at a cooling rate of at least 1° C./s, coiling up, and subjecting to a preliminary ageing treatment by cooling to room temperature (invention according to claim 6 ).
  • the aluminum alloy sheet production method of the present invention it is possible to obtain an aluminum alloy sheet with exceptional hemmability and bake-hardenability. Additionally, this production method is capable of obtaining an aluminum alloy sheet in an extremely short procedure and at low cost.
  • the present invention relates to a method of producing a rolled sheet of Al—Mg—Si alloy, characterized by casting a thin slab by a twin-belt casting method, winding the slab directly onto a coil, subjecting to a homogenization treatment, then cold rolling, and further subjecting to a solution treatment.
  • an alloy melt consisting of the aforementioned composition is cast into a slab 5-15 mm thick at a cooling rate of 40-150° C./s at a quarter thickness of the slab, using a twin-belt casting method, and after winding into a coil, it is subjected to a homogenization treatment and cooled to 250° C. or less at a cooling rate of at least 500° C./s, then cold rolled, and subsequently subjected to a solution treatment.
  • the twin-belt casting method is a method of casting thin slabs by pouring a melt between water-cooled rotating belts that oppose each other from above and below, so as to harden the melt by cooling through the belt surfaces.
  • slabs that are 5-15 mm thick are cast by the twin-belt casting method. If the slab thickness exceeds 15 mm, it becomes difficult to wind the thin slabs into coils, and if the slab thickness is less than 5 mm, there is a loss in productivity and it becomes difficult to cast the thin slabs.
  • the cooling rate 40-150° C./s at a quarter thickness of the slab.
  • the cooling rate is computed by measuring the DAS (Dendrite Arm Spacing) by a line intersection method from observations of the microstructure in the slab at quarter thickness.
  • the cooling rate is less than 40° C./s, the cast structure formed in the central portion of the slab during hardening becomes coarse, thus reducing the hemmability, while if the cooling rate exceeds 150° C./s, Al—Fe—Si crystals and Al—(Fe.Mn)—Si crystals become 1 ⁇ m or less and the size of recrystallized grains becomes coarse at 30 ⁇ m or more.
  • this coil After winding a thin slab, this coil is subjected to a homogenization treatment under appropriate conditions to fragment the Al—Fe—Si crystals and Al—(Fe.Mn)—Si crystals that have an adverse effect on hemmability, thus improving the hemmability. Furthermore, it is possible to obtain thin slabs in a state where relatively small Mg 2 Si crystals that reside in the cast structure are completely dissolved into the matrix, thus raising the effectiveness of the solid solution treatment after the cold rolling process.
  • the reason that the cooling after the homogenization treatment is performed at a rate of at least 500° C./s and to 250° C. or less is in order to suppress the deposition of relatively coarse Mg 2 Si as much as possible, and to dissolve the Mg and Si into the matrix in an oversaturated state.
  • the coil After winding the thin slab, the coil is inserted into a batch furnace, and heated at a rate of at least 30° C./h to 520-580° C., at which temperature it is held for 2-24 hours to perform a homogenization treatment, after which the coil may be extracted from the batch furnace and forcibly air-cooled to room temperature at a cooling rate of at least 500° C./h.
  • This cooling can be performed, for example, by a fan while unwinding the coil.
  • the reason the heating rate to the homogenization temperature is limited to at least 30° C./h for the homogenization treatment following winding of the thin slab is that if the heating rate is less than 30° C./h, at least 16 hours will be required to reach the predetermined homogenization temperature, thus raising costs.
  • the reason the homogenization temperature is within the range of 520-580° C. is that if the temperature is less than 520° C., the fragmentation of Al—Fe—Si crystals and Al—(Fe.Mn)—Si crystals is inadequate, and not enough to dissolve the Mg 2 Si that crystallized during casting into the matrix, and if the temperature exceeds 580° C., the metals with low melting points will melt and cause burning.
  • the reason that the homogenization treatment time is set to within the range of 2-24 hours is because if the treatment time is less than 2 hours, the fragmentation of Al—Fe—Si crystals and Al—(Fe.Mn)—Si crystals is inadequate, and not enough to dissolve the Mg 2 Si that crystallized during casting into the matrix, and if the treatment time exceeds 24 hours, the Mg 2 Si that crystallized during casting is well-dissolved into the matrix, and the Mg and Si become saturated, resulting in cost increases.
  • the invention is characterized by further cold rolling this coil and performing a solution treatment.
  • This solution treatment is preferably performed in a normal continuous annealing line (CAL).
  • CAL normal continuous annealing line
  • a continuous annealing line is an installation for performing continuous solution treatments and the like of coils, characterized by comprising inductive heating devices for performing heat treatments, water tanks for water-cooling, air nozzles for air-cooling, and the like.
  • the solution treatment it should preferably be performed by heating at a rate of at least 10° C./s to 530-560° C. by means of a continuous annealing line, and holding for 30 seconds or less.
  • the reason the heating rate to the solution treatment temperature is limited to at least 10° C./s in the solution treatment is that if the heating rate is less than 10° C./s, the coil advancing speed becomes too slow, as a result of which the processing time becomes long and the cost mounts.
  • the reason the solution treatment temperature is set to be within the range of 530-560° C. is that if the temperature is less than 530° C., it is not sufficient to cause Mg 2 Si that crystallized while casting or precipitated while being cooled after homogenization to be dissolved into the matrix, and if the temperature exceeds 560° C., the metals with low melting points will melt and cause burning.
  • the reason the solution treatment time is restricted to be within 30 seconds is that in the case of treatment times exceeding 30 seconds, Mg 2 Si that crystallized while casting or precipitated while being cooled after homogenization is well-dissolved into the matrix, and the Mg and Si become saturated, thereby slowing the coil advancement speed, as a result of which the processing time is increased and the costs mount.
  • the invention is characterized by cooling to room temperature at a rate of at least 10° C./s after the solution treatment.
  • the reason the cooling rate after the solution treatment is at least 10° C./s is that if the cooling rate is less than 10° C./s, Si is deposited in the crystal grain boundary during the cooling step, thus reducing the hemmability.
  • the thin slab After performing the aforementioned homogenization treatment on the thin slab, it is further cold rolled, subjected to a solution treatment and cooled to room temperature at a rate of at least 10° C./s, and after the coil is left at room temperature, it may be held for 30 seconds or less at 260-300° C. in a continuous annealing line, then cooled to room temperature at 10° C./s.
  • a continuous annealing line is an installation for performing continuous solution treatments and the like of coils, characterized by comprising inductive heating devices for performing heat treatments, water tanks for water-cooling, air nozzles for air-cooling, and the like. Due to the restoration treatment, it is possible to re-dissolve GP zones that appear due to natural ageing when left at room temperature after a solution treatment, thus enabling adequate strength to be obtained after heating for coating and baking.
  • the reason the time over which the restoration treatment temperature is held is restricted to within 30 seconds is that if the treatment time exceeds 30 seconds, it is not possible to adequately re-dissolve the GP zones that appear due to natural ageing when left at room temperature after the solution treatment, in addition to which the coil advancement speed is too slow, as a result of which the treatment time is long and the costs mount.
  • first cooling rate water-cooled to 250° C. or less at a cooling rate (first cooling rate) of at least 10° C./s, then air-cooled to 60-100° C. at a cooling rate (second cooling rate) of 1-20° C./s, coiled up and cooled to room temperature.
  • This heat solution treatment and subsequent cooling are preferably performed in a normal continuous annealing line (CAL).
  • CAL normal continuous annealing line
  • the thin slab After subjecting the thin slab to a homogenization treatment and further cold rolling, it may be subjected to a solution treatment by heating to 530-560° C. at a rate of at least 10° C./s, then holding for 30 seconds or less, then cooled to room temperature at a rate of at least 10° C./s, thereafter subjected to a restoration treatment by holding within a range of 260-300° C. for 30 seconds, then cooled to 60-100° C. at a cooling rate of at least 1° C./s, coiled up and subjected to a preliminary ageing treatment by cooling to room temperature.
  • a solution treatment by heating to 530-560° C. at a rate of at least 10° C./s, then holding for 30 seconds or less, then cooled to room temperature at a rate of at least 10° C./s, thereafter subjected to a restoration treatment by holding within a range of 260-300° C. for 30 seconds, then cooled to 60-100° C. at
  • This solution treatment and subsequent cooling, and restoration treatment and subsequent cooling are preferably performed in a normal continuous annealing line (CAL).
  • CAL normal continuous annealing line
  • the essential element Mg is dissolved in the matrix after the heat solution treatment, and is deposited as a reinforcing phase together with Si upon heating for coating and baking, thereby improving the strength.
  • the reason the Mg content is limited to 0.30-1.00 wt % is that the effect is small if less than 0.30 wt %, and if more than 1.00 wt %, the hemmability after the solution treatment is reduced.
  • a more preferable range for the Mg content is 0.30-0.70 wt %.
  • the essential element Si is deposited together with Mg as an intermediary phase of Mg 2 Si known as ⁇ ′′ or an analogous reinforcing phase upon being heated for coating and baking, thereby increasing the strength.
  • the reason the Si content is limited to 0.30-1.20 wt % is that if less than 0.30 wt %, its effects are minimal, and if more than 1.20 wt %, the hemmability is reduced after the heat solution treatment.
  • a more preferable range of Si content is 0.60-1.20 wt %.
  • the essential element Fe when coexisting with Si and Mn, generates many Al—Fe—Si crystals and Al—(Fe.Mn)—Si crystals of a size of 5 ⁇ m or less upon casting, so that re-crystallized nuclei are increased, as a result of which the recrystallized grains are refined and sheets of exceptional formability are obtained. If the Fe content is less than 0.05 wt %, the effects are not very remarkable.
  • the preferable range of Fe content is 0.05-0.50 wt %.
  • a more preferable range of Fe content is 0.05-0.30 wt %.
  • the essential element Mn is added as an element to refine the re-crystallized grains.
  • the size of the re-crystallized grains By keeping the size of the re-crystallized grains relatively small at 10-25 ⁇ m, it is possible to form sheets with exceptional formability. If the Mn content is less than 0.05 wt %, the effect is not adequate, and if it exceeds 0.50 wt %, coarse Al—Fe—Si crystals and Al—(Fe.Mn)—Si crystals are formed upon casting, thus not only reducing the hemmability but also reducing the amount of Si dissolved in the thin slabs, as a result of which the bake-hardenability of the final sheets is reduced. Therefore, the preferable range of Mn content is 0.05-0.50 wt %. A more preferable range of Mn content is 0.05-0.30 wt %.
  • the essential element Ti will not inhibit the effects of the present invention if it is contained at 0.10 wt % or less, and it can function as a crystal grain refiner for the thin slabs, so as to reliably prevent casting defects of the slabs such as cracks or the like. If the Ti content is less than 0.005 wt %, the effects are not adequate, and if the Ti content exceeds 0.10 wt %, coarse intermetallic compounds such as TiAl 3 and the like are formed during casting, thus greatly reducing the hemmability. Therefore, the preferable range of Ti content is 0.005-0.10 wt %. A more preferable range for the Ti content is 0.005-0.05 wt %.
  • the optional element Cu is an element that promotes age-hardening and raises the bake-hardenability. If the Cu content is less than 0.05 wt %, the effect is small, and if it exceeds 0.70 wt %, the yield strength of the sheets becomes high after a preliminary ageing treatment, and not only does the hemmability decrease, but the reduction in corrosion resistance is also marked. Therefore, the Cu content is preferably within a range of 0.05-0.70 wt %. The Cu content is more preferably 0.10-0.60 wt %.
  • the optional element Zr is added as an element for refining the re-crystallized grains. If the Zr content is less than 0.05 wt %, the effect is not adequate, and if it exceeds 0.40 wt %, coarse Al—Zr crystals are created during slab casting, thus reducing the hemmability. Therefore, the Zr content is preferably within a range of 0.05-0.40 wt %. The Zr content is more preferably within a range of 0.05-0.30 wt %.
  • the present invention allows an Al—Mg—Si alloy sheet for use in automotive body sheets having exceptional bake-hardenablitiy and hemmability after a final anneal to be produced at low cost. While a restoration treatment or high-temperature winding is required to suppress natural ageing as with conventional methods, the steps such as facing, hot rolling and the like that precede these steps can be largely simplified, thus greatly reducing the total production cost.
  • the samples after cold rolling are not coils but all cut sheets. Therefore, in order to simulate the step of continuous annealing of a coil in a continuous annealing line (CAL), a solution treatment of the samples in a salt bath and a cold water quench or 85° C. water quench were employed.
  • CAL continuous annealing line
  • Table 2 shows the results for cases in which the homogenization conditions and cooling rate after the homogenization treatment were changed.
  • the slabs were cold rolled to a thickness of 1 mm, these cold rolled sheets were subjected to a solution treatment by holding for 15 seconds at a predetermined temperature by means of a salt bath, then quenched with 85° C. water, and immediately inserted into an annealer with an atmospheric temperature of 85° C. to perform a preliminary ageing of 8 hours.
  • Those falling within the scope of conditions of the present invention (1-7) had exceptional bake-hardenability and hemmability.
  • Those that did not undergo a homogenization treatment (8, 10) had poor bake-hardenability and hemmability.
  • those which had a slow cooling rate after the homogenization treatment had poor bake-hardenability (9).
  • B twin-belt/7 50 560 6 1700
  • B twin-belt/7 50 550 5 500
  • C twin-belt/7 30 530 10 1000
  • D twin-belt/7 40 530 10 1000
  • E twin-belt/7 40 530 10 1000 7 F twin-belt/7 50 550 6 1000 Comp.
  • Table 3 shows the results when the temperatures/times of the homogenization treatment are changed.
  • the slabs were cold rolled to a thickness of 1 mm, these cold rolled sheets were subjected to a solution treatment by holding for 15 seconds at a predetermined temperature by means of a salt bath, then quenched in 85° C. water and immediately entered into an annealer with an atmospheric temperature of 85° C. to perform a preliminary ageing of 8 hours.
  • Those falling within the scope of conditions of the present invention (11-14) had exceptional bake-hardenability and hemmability.
  • Rate Temp Time Rate ID No. (mm) (° C./h) (° C.) (h) (° C./h) Present 11 B twin-belt/7 30 560 5 1500 Invention 12 B twin-belt/7 50 560 6 1500 13 C twin-belt/7 50 550 5 1500 14 C twin-belt/7 30 530 10 1500 Comp. 15 B twin-belt/7 50 500 6 1500 Example 16 B twin-belt/7 50 560 1 1500 Cold Roll Sol. Yield Str. Bake- Sheet Treat. Prelim. before/after Hard. ID Thick. Temp.
  • Table 4 shows the results when the homogenization conditions and restoration conditions were changed.
  • the slabs were cold rolled to a thickness of 1 mm, these cold rolled sheets are subjected to a solution treatment by holding for 15 seconds at a predetermined temperature by means of a salt bath, then quenched in cold water, and after leaving at room temperature for 24 hours, subjected to a restoration treatment by holding for 15 seconds at a predetermined temperature.
  • Those falling within the scope of conditions of the present invention (17-20) had exceptional bake-hardenability and hemmability.
  • Those that had a low restoration temperature (reheating temperature) (21) had poor bake-hardenability.
  • Example 22 1 mm 550° C. 310 127/229 102 X 23 1 mm 550° C. 290 97/197 100 X 24 1 mm 550° C. 280 90/160 70 X 25 1 mm 550° C. 290 95/145 50 ⁇
  • Table 5 shows the results when the homogenization conditions and cooling pattern after the solution treatment were changed.
  • the cooling rate after the solution treatment was divided into two stages, with the cooling rate from the solution temperature to an intermediate temperature being defined as the first cooling rate and the cooling rate from the intermediate temperature to the coil-up temperature being defined as the second cooling rate.
  • the slabs were cold rolled to a thickness of 1 mm, and these cold rolled sheets were subjected to a solution treatment by holding for 15 seconds at a predetermined temperature by means of a salt bath, after which they were cooled to the intermediate temperature at the first cooling rate, then cooled to the coil-up temperature at the second cooling rate, and thereafter cooled to room temperature at 5° C./h.
  • Table 6 shows the results when the restoration treatment temperature (reheating temperature) after the solution treatment and coil-up temperature were changed.
  • the slabs were cold rolled to a thickness of 1 mm, these cold rolled sheets are subjected to a solution treatment by holding for 15 seconds at a predetermined temperature by means of a salt bath, then quenched in cold water, and after leaving at room temperature for 24 hours, held for 15 seconds at a predetermined temperature (preheating temperature) and cooled to a predetermined coil-up temperature at 10° C./s, then further cooled to room temperature at 10° C./h.
  • preheating temperature a predetermined temperature
  • rolled sheets of Al—Mg—Si alloy that are suitable for forming by bending, press forming and the like of automotive parts, household appliances and the like can be produced at a low cost relative to the conventional art.

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US10/582,272 2003-12-11 2004-12-13 Method for producing Al-Mg-Si alloy sheet excellent in bake-hardenability and hemmability Abandoned US20070209739A1 (en)

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JP2003-413885 2003-12-11
JP2003413885 2003-12-11
PCT/JP2004/018581 WO2005056859A1 (fr) 2003-12-11 2004-12-13 Procede de production d'un alliage al-mg-si excellent en matiere de trempabilite et d'aptitude a ourler

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US (1) US20070209739A1 (fr)
EP (1) EP1702995A1 (fr)
JP (1) JP4577218B2 (fr)
KR (1) KR20060133996A (fr)
CN (1) CN1914348A (fr)
CA (1) CA2548788A1 (fr)
TW (1) TW200536946A (fr)
WO (1) WO2005056859A1 (fr)

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US20120055591A1 (en) * 2010-09-08 2012-03-08 Alcoa Inc. 6xxx aluminum alloys, and methods for producing the same
US20120135261A1 (en) * 2009-05-28 2012-05-31 Bluescope Steel Limited Metal-coated steel strip
US20120152416A1 (en) * 2008-09-19 2012-06-21 Alistair Foster Process for forming aluminium alloy sheet components
US20120298513A1 (en) * 2009-12-22 2012-11-29 Showa Denko K.K. Aluminum alloy for anodization and aluminum alloy component
CN103305779A (zh) * 2013-06-18 2013-09-18 常州大学 一种6000系铝合金的形变热处理方法
CN103343304A (zh) * 2013-06-18 2013-10-09 常州大学 一种提高6000系铝合金薄板拉伸性能的形变热处理方法
US20170306466A1 (en) * 2014-12-11 2017-10-26 Aleris Aluminum Duffel Bvba Method of continuously heat-treating 7000-series aluminium alloy sheet material
US20190119800A1 (en) * 2016-07-14 2019-04-25 Uacj Corporation Method for producing aluminum alloy rolled material for molding having excellent bending workability and ridging resistance and comprising aluminum alloy
US10294553B2 (en) * 2014-09-12 2019-05-21 Aleris Aluminum Duffel Bvba Method of annealing aluminium alloy sheet material
US20200095664A1 (en) * 2015-12-18 2020-03-26 Novelis Inc. High-strength 6xxx aluminum alloys and methods of making the same
US10913107B2 (en) 2016-10-27 2021-02-09 Novelis Inc. Metal casting and rolling line
US20220077420A1 (en) * 2020-09-09 2022-03-10 Samsung Display Co., Ltd. Reflective electrode and display device having the same
US11313016B2 (en) 2013-04-19 2022-04-26 General Research Institute For Nonferrous Metals Aluminum alloy materials suitable for the manufacture of automotive body panels and methods for producing the same
US11649536B2 (en) * 2017-04-06 2023-05-16 Constellium Neuf-Brisach Method for manufacturing a structure component for a motor vehicle body
US11674203B2 (en) * 2014-01-21 2023-06-13 Arconic Technologies Llc 6XXX aluminum alloys
US11692255B2 (en) 2016-10-27 2023-07-04 Novelis Inc. High strength 7XXX series aluminum alloys and methods of making the same
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US20100089503A1 (en) * 2007-03-14 2010-04-15 Kabushiki Kaisha Kobe Seiko Sho (Kobe Steel, Ltd.) Aluminum alloy forgings and process for production thereof
US8372220B2 (en) * 2007-03-14 2013-02-12 Kobe Steel, Ltd. Aluminum alloy forgings and process for production thereof
US20120152416A1 (en) * 2008-09-19 2012-06-21 Alistair Foster Process for forming aluminium alloy sheet components
US10689738B2 (en) * 2008-09-19 2020-06-23 Imperial Innovations Ltd. Process for forming aluminium alloy sheet components
US10731241B2 (en) * 2009-05-28 2020-08-04 Bluescope Steel Limited Metal-coated steel strip
US20120135261A1 (en) * 2009-05-28 2012-05-31 Bluescope Steel Limited Metal-coated steel strip
US8962163B2 (en) * 2009-12-22 2015-02-24 Showa Denko K.K. Aluminum alloy for anodization and aluminum alloy component
US20120298513A1 (en) * 2009-12-22 2012-11-29 Showa Denko K.K. Aluminum alloy for anodization and aluminum alloy component
US9359660B2 (en) * 2010-09-08 2016-06-07 Alcoa Inc. 6XXX aluminum alloys, and methods for producing the same
US20120055591A1 (en) * 2010-09-08 2012-03-08 Alcoa Inc. 6xxx aluminum alloys, and methods for producing the same
US11313016B2 (en) 2013-04-19 2022-04-26 General Research Institute For Nonferrous Metals Aluminum alloy materials suitable for the manufacture of automotive body panels and methods for producing the same
CN103343304A (zh) * 2013-06-18 2013-10-09 常州大学 一种提高6000系铝合金薄板拉伸性能的形变热处理方法
CN103305779A (zh) * 2013-06-18 2013-09-18 常州大学 一种6000系铝合金的形变热处理方法
US11674203B2 (en) * 2014-01-21 2023-06-13 Arconic Technologies Llc 6XXX aluminum alloys
US10294553B2 (en) * 2014-09-12 2019-05-21 Aleris Aluminum Duffel Bvba Method of annealing aluminium alloy sheet material
US20170306466A1 (en) * 2014-12-11 2017-10-26 Aleris Aluminum Duffel Bvba Method of continuously heat-treating 7000-series aluminium alloy sheet material
US10513767B2 (en) * 2014-12-11 2019-12-24 Aleris Aluminum Duffel Bvba Method of continuously heat-treating 7000-series aluminium alloy sheet material
US20200095664A1 (en) * 2015-12-18 2020-03-26 Novelis Inc. High-strength 6xxx aluminum alloys and methods of making the same
US11920229B2 (en) 2015-12-18 2024-03-05 Novelis Inc. High strength 6XXX aluminum alloys and methods of making the same
US12043887B2 (en) 2015-12-18 2024-07-23 Novelis Inc. High strength 6xxx aluminum alloys and methods of making the same
US11053576B2 (en) * 2016-07-14 2021-07-06 Uacj Corporation Method for producing aluminum alloy rolled material for molding having excellent bending workability and ridging resistance
US20190119800A1 (en) * 2016-07-14 2019-04-25 Uacj Corporation Method for producing aluminum alloy rolled material for molding having excellent bending workability and ridging resistance and comprising aluminum alloy
US10913107B2 (en) 2016-10-27 2021-02-09 Novelis Inc. Metal casting and rolling line
US11590565B2 (en) 2016-10-27 2023-02-28 Novelis Inc. Metal casting and rolling line
US11692255B2 (en) 2016-10-27 2023-07-04 Novelis Inc. High strength 7XXX series aluminum alloys and methods of making the same
US11806779B2 (en) 2016-10-27 2023-11-07 Novelis Inc. Systems and methods for making thick gauge aluminum alloy articles
US11821065B2 (en) 2016-10-27 2023-11-21 Novelis Inc. High strength 6XXX series aluminum alloys and methods of making the same
US11649536B2 (en) * 2017-04-06 2023-05-16 Constellium Neuf-Brisach Method for manufacturing a structure component for a motor vehicle body
US20220077420A1 (en) * 2020-09-09 2022-03-10 Samsung Display Co., Ltd. Reflective electrode and display device having the same

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WO2005056859A1 (fr) 2005-06-23
KR20060133996A (ko) 2006-12-27
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EP1702995A1 (fr) 2006-09-20

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