WO2016031937A1 - Tôle d'alliage d'aluminium pour formage - Google Patents
Tôle d'alliage d'aluminium pour formage Download PDFInfo
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- WO2016031937A1 WO2016031937A1 PCT/JP2015/074297 JP2015074297W WO2016031937A1 WO 2016031937 A1 WO2016031937 A1 WO 2016031937A1 JP 2015074297 W JP2015074297 W JP 2015074297W WO 2016031937 A1 WO2016031937 A1 WO 2016031937A1
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- 229910000838 Al alloy Inorganic materials 0.000 title claims abstract description 67
- 150000001875 compounds Chemical class 0.000 claims abstract description 92
- 239000012535 impurity Substances 0.000 claims abstract description 5
- 229910019064 Mg-Si Inorganic materials 0.000 claims description 12
- 229910019406 Mg—Si Inorganic materials 0.000 claims description 12
- 229910052718 tin Inorganic materials 0.000 claims description 5
- 229910052804 chromium Inorganic materials 0.000 claims description 3
- 229910052748 manganese Inorganic materials 0.000 claims description 3
- 229910052720 vanadium Inorganic materials 0.000 claims description 3
- 229910052726 zirconium Inorganic materials 0.000 claims description 3
- 229910052742 iron Inorganic materials 0.000 claims description 2
- 229910052802 copper Inorganic materials 0.000 claims 1
- 229910052725 zinc Inorganic materials 0.000 claims 1
- 229910018464 Al—Mg—Si Inorganic materials 0.000 abstract description 12
- 229910052782 aluminium Inorganic materials 0.000 abstract description 4
- 239000006104 solid solution Substances 0.000 description 42
- 238000001816 cooling Methods 0.000 description 41
- 238000000137 annealing Methods 0.000 description 38
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- 238000000034 method Methods 0.000 description 17
- 229910045601 alloy Inorganic materials 0.000 description 16
- 239000002244 precipitate Substances 0.000 description 13
- 238000005259 measurement Methods 0.000 description 12
- 238000005452 bending Methods 0.000 description 11
- 239000000243 solution Substances 0.000 description 11
- 238000005266 casting Methods 0.000 description 10
- 238000005097 cold rolling Methods 0.000 description 10
- 238000000465 moulding Methods 0.000 description 10
- 239000003973 paint Substances 0.000 description 10
- 238000010791 quenching Methods 0.000 description 10
- 230000000171 quenching effect Effects 0.000 description 10
- 238000005496 tempering Methods 0.000 description 10
- 238000000265 homogenisation Methods 0.000 description 9
- 238000005096 rolling process Methods 0.000 description 9
- 230000035882 stress Effects 0.000 description 9
- 238000003483 aging Methods 0.000 description 7
- 230000008018 melting Effects 0.000 description 7
- 230000008569 process Effects 0.000 description 7
- 238000009792 diffusion process Methods 0.000 description 6
- 230000006872 improvement Effects 0.000 description 6
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- 238000002844 melting Methods 0.000 description 6
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- 238000003303 reheating Methods 0.000 description 4
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- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 3
- 230000007797 corrosion Effects 0.000 description 3
- 238000005260 corrosion Methods 0.000 description 3
- 238000005336 cracking Methods 0.000 description 3
- 230000007423 decrease Effects 0.000 description 3
- 238000002149 energy-dispersive X-ray emission spectroscopy Methods 0.000 description 3
- 238000009957 hemming Methods 0.000 description 3
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- 238000005498 polishing Methods 0.000 description 3
- 230000001629 suppression Effects 0.000 description 3
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 3
- 229910000831 Steel Inorganic materials 0.000 description 2
- 239000000654 additive Substances 0.000 description 2
- 230000000996 additive effect Effects 0.000 description 2
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- 238000009749 continuous casting Methods 0.000 description 2
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- 238000011156 evaluation Methods 0.000 description 2
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- 239000003595 mist Substances 0.000 description 2
- 239000002245 particle Substances 0.000 description 2
- 239000002994 raw material Substances 0.000 description 2
- 238000007670 refining Methods 0.000 description 2
- 238000005204 segregation Methods 0.000 description 2
- 238000002791 soaking Methods 0.000 description 2
- 239000010959 steel Substances 0.000 description 2
- 238000005728 strengthening Methods 0.000 description 2
- 230000002123 temporal effect Effects 0.000 description 2
- 229910018134 Al-Mg Inorganic materials 0.000 description 1
- 229910018467 Al—Mg Inorganic materials 0.000 description 1
- 238000012935 Averaging Methods 0.000 description 1
- 241000052343 Dares Species 0.000 description 1
- 229910018643 Mn—Si Inorganic materials 0.000 description 1
- 229910008355 Si-Sn Inorganic materials 0.000 description 1
- 229910006453 Si—Sn Inorganic materials 0.000 description 1
- 230000008901 benefit Effects 0.000 description 1
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Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C21/00—Alloys based on aluminium
- C22C21/06—Alloys based on aluminium with magnesium as the next major constituent
- C22C21/08—Alloys based on aluminium with magnesium as the next major constituent with silicon
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C21/00—Alloys based on aluminium
- C22C21/02—Alloys based on aluminium with silicon as the next major constituent
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C21/00—Alloys based on aluminium
- C22C21/06—Alloys based on aluminium with magnesium as the next major constituent
-
- 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
-
- 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
- C22F1/043—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 silicon 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
Definitions
- the present invention relates to an Al—Mg—Si based aluminum alloy sheet for forming.
- the aluminum alloy sheet referred to in the present invention is a rolled sheet such as a hot-rolled sheet or a cold-rolled sheet, and is subjected to tempering such as solution treatment and quenching process, and is baked and coated and cured. Says aluminum alloy plate before being done.
- aluminum is also referred to as aluminum or Al.
- panels such as outer panels (outer plates) and inner panels (inner plates) of panel structures such as automobile hoods, fenders, doors, roofs and trunk lids are thin and high-strength aluminum alloy plates.
- Al—Mg—Si based AA to JISJ6000 (hereinafter also simply referred to as 6000) aluminum alloy plates is being studied.
- This 6000 series aluminum alloy plate contains Si and Mg as essential components.
- the 6000 series aluminum alloy plate has a relatively small amount of alloy elements as compared with other 5000 series aluminum alloys having a large amount of alloy such as Mg. For this reason, when the scraps of these aluminum alloy plates are reused as an aluminum alloy melting material (melting raw material), the original 6000 series aluminum alloy ingot is easily obtained and the recyclability is excellent.
- an outer panel of an automobile is manufactured by combining an aluminum alloy plate with a forming process such as press forming and bending forming.
- a forming process such as press forming and bending forming.
- a large outer panel such as a hood or a door
- it is formed into a molded product shape as an outer panel by press molding such as overhanging, and then the inner panel is formed by hem (hemming) processing such as flat hem on the outer peripheral edge of the outer panel.
- hem hem
- the 6000 series aluminum alloy has an advantage of having excellent BH property, but has aging property at room temperature, and after the solution quenching treatment, it is age-hardened by holding at room temperature for several months to increase the strength. As a result, there is a problem that the formability to the panel, particularly the bending workability, is lowered.
- a 6000 series aluminum alloy plate when used for an automotive panel, it usually takes about 1 to 4 months after it is solution-quenched by an aluminum maker (after manufacture) and then molded into a panel by an automotive maker. It is left at room temperature (and left at room temperature), and during this time, it is considerably age-hardened (room temperature aging).
- Patent Document 1 proposes a method for improving formability, baking paintability, and corrosion resistance by adding Sn having a temporal change suppressing effect and Cu for improving formability.
- an object of the present invention is to form Sn-containing Al—Mg, which can exhibit high BH properties and good workability even in a car body paint baking process after long-term aging at room temperature. -To provide a Si-based aluminum alloy sheet.
- the gist of the forming aluminum alloy plate of the present invention is, in mass%, Mg: 0.2 to 2.0%, Si: 0.3 to 2.0%, and Sn: 0.00.
- Al—Mg—Si-based aluminum alloy plate containing 005 to 0.3% and the balance being Al and inevitable impurities is measured using a 500-fold SEM as the structure of the aluminum alloy plate.
- the average number density of the compound having an equivalent circle diameter of 0.3 to 20 ⁇ m is 0 / mm 2 and 5000 / mm 2 or less, and among the compounds measured by the SEM,
- the average number ratio of the compound containing 0.5 mass% or more of Sn to be identified is 0% or more and less than 50%.
- the manufacturing conditions such as intermediate annealing are devised, and the presence state of the contained Sn is controlled to precipitate Sn as a compound. It suppresses and promotes the solid solution of Sn in the matrix, and ensures the solid solution amount of Sn.
- the effect of improving heme workability and BH property is sufficiently exhibited by the trapping of Sn atomic vacancies and the suppression of aging by the release effect.
- the conventional Sn-containing Al—Mg—Si based aluminum alloy plate could not sufficiently exhibit such effects of Sn.
- the solid solution and precipitation of Sn which was only one of the selective additive elements, while always paying attention to the solid solution and precipitation of the main elements Mg and Si. This is probably due to the fact that they did not pay much attention.
- the Sn present form of the plate produced by a conventional method is crystallization or precipitation (hereinafter, also simply referred to as precipitation) as a compound. In contrast to this, it is difficult to solidify Sn itself, and since the solid solution state of Sn is a very rare form, it is difficult to know the effects exhibited by the solid solution of Sn. Inferred.
- the 6000 series aluminum alloy plate targeted by the present invention is required to have excellent properties such as formability, BH property, strength, weldability, and corrosion resistance as a plate for an automobile panel. That is, even for a plate that has been aged at room temperature for a long period of 100 days after the tempering treatment, the As proof stress is 110 MPa or less, the BH (bake hard) property is proof stress difference of 100 MPa or more, and the hem workability is described later in the examples. It is required that it is excellent in press formability and hem workability to automobile panels, etc., and BH properties are excellent, such as 2 or more on the basis.
- the composition of the aluminum alloy sheet as a premise is Mg: 0.2-2.0%, Si: 0.3-2.0%, and Sn: 0.0. 005 to 0.3% is included, and the balance is made of Al and inevitable impurities.
- % display of content of each element means the mass% altogether.
- the percentage (mass%) based on mass is the same as the percentage (wt%) based on weight.
- the content of each chemical component may be expressed as “X% or less (excluding 0%)” as “over 0% and X% or less”.
- the 6000 series aluminum alloy plate targeted by the present invention is an excess Si type 6000 series aluminum alloy plate having a better BH property and a Si / Mg mass ratio of Si / Mg of 1 or more. Is preferred.
- the 6000 series aluminum alloy sheet secures formability by reducing the yield strength during press molding and bending, and is age-hardened by heating during relatively low temperature artificial aging treatment such as paint baking treatment of the panel after molding. Yield strength is improved, and it has excellent age-hardening ability (BH property) that can secure the required strength.
- the excess Si type 6000 series aluminum alloy plate is more excellent in this BH property than the 6000 series aluminum alloy plate having a mass ratio Si / Mg of less than 1.
- these other elements other than Mg and Si are impurities or elements that may be contained, and the content (allowable amount) at each element level in accordance with AA or JIS standards.
- the following elements are allowed to be contained in the range below the upper limit amount in accordance with the AA to JIS standards specified below.
- Mn 1.0% or less (excluding 0%), Cu: 1.0% or less (excluding 0%), Fe: 1.0% or less (excluding 0%) %), Cr: 0.3% or less (excluding 0%), Zr: 0.3% or less (excluding 0%), V: 0.3% or less (provided that 0%), Ti: 0.05% or less (excluding 0%), Zn: 1.0% or less (excluding 0%), and Ag: 0.2% or less (provided that
- it may further include one or more selected from the group consisting of:
- the Cu content is preferably 0.7% or less, more preferably 0.3% or less.
- Mn, Fe, Cr, Zr, and V are contained in a large amount, a relatively coarse compound is likely to be generated, and the hem workability (hem bendability) that is a subject of the present invention is likely to be deteriorated. Therefore, the Mn content is preferably 0.6% or less, more preferably 0.3% or less, and the Cr, Zr, and V contents are each preferably 0.2% or less, more preferably 0.1%. % Or less.
- Si 0.3-2.0%
- Si is a major element, and forms Mg-Si-based precipitates that contribute to strength improvement during solid solution strengthening and artificial aging treatment such as paint baking treatment, and exhibits age-hardening ability, which is necessary for automobile outer panels It is an indispensable element for obtaining a sufficient strength (yield strength).
- Si / Mg is set to 1.0 or more in mass ratio, and Si is further Mg than the excessive Si type generally called. It is preferable to make the composition of 6000 series aluminum alloy excessively contained. If the Si content is too small, the amount of Mg—Si based precipitates is insufficient, and the BH property is significantly reduced.
- Si is set in the range of 0.3 to 2.0%.
- a more preferred lower limit is 0.6%, and a more preferred upper limit is 1.4%.
- Mg 0.2-2.0%
- Mg is also a major element, forming solid solution strengthening and forming an Mg-Si-based precipitate that contributes to strength improvement during artificial aging treatment such as paint baking treatment, and exhibits age-hardening ability and the required proof strength as a panel It is an essential element for obtaining. If the Mg content is too small, the amount of Mg—Si-based precipitates is insufficient, and the BH property is significantly reduced. For this reason, the proof stress required as a panel cannot be obtained. On the other hand, when there is too much Mg content, a coarse crystallized substance and a precipitate will be formed and bending workability will fall remarkably. Therefore, the Mg content is in the range of 0.2 to 2.0%. A more preferred lower limit is 0.3%, and a more preferred upper limit is 1.0%.
- Sn 0.005 to 0.3%
- Sn is an essential element.
- the diffusion of Mg and Si at room temperature is suppressed, and the increase in strength at room temperature (room temperature aging) is suppressed over a long period of time.
- the trapped pores are released during the artificial aging treatment such as the paint baking treatment of the molded panel.
- the diffusion of Mg and Si can be promoted and the BH property can be increased. .
- the Sn content is in the range of 0.005 to 0.3%.
- a more preferred lower limit is 0.01%, and a more preferred upper limit is 0.2%.
- the Sn—Al—Mg—Si based aluminum alloy sheet of the present invention is an Al—Mg—Si based aluminum alloy sheet that does not contain Sn in terms of its solid solution in terms of structure and characteristics. It is very different compared to Similarly, even in the case of Al—Mg—Si-based aluminum alloy plates containing Sn (the same amount), if the production conditions such as intermediate annealing are different, the solid solution amount of Sn is different, Under manufacturing conditions (ordinary method), Sn is likely to precipitate as a compound, and the amount of solid solution is remarkably reduced (decreased). For this reason, even if it contains Sn (the same amount) in the same manner, it is possible to obtain a structure having an effect of suppressing room temperature aging at a high level as in the present invention and improving BH properties and hemmability. Not necessarily.
- the average number density of a compound having a circle equivalent diameter in the range of 0.3 to 20 ⁇ m when measured using a 500-fold SEM as the structure of the plate is 5000 pieces / mm 2 or less (including 0 pieces / mm 2) .
- the number density of the compound having an equivalent circle diameter of 0.3 ⁇ m or more is reduced to 5000 / mm 2 or less, the starting point of breakage in the structure of the plate at the time of molding is reduced, and hem workability is improved. Furthermore, since the amount of solid solution Mg and the amount of solid solution Si are increased and the amount of Mg—Si based precipitates generated during the BH treatment and contributing to the increase in strength is increased, the BH property is also improved. On the other hand, if the number density of the compound having an equivalent circle diameter of 0.3 ⁇ m or more exceeds 5000 / mm 2 , the starting point of breakage in the structure of the plate at the time of molding increases, and hemming workability, drawing and tensioning are increased.
- the press formability such as protrusion decreases. Furthermore, the amount of solid solution Mg and the amount of solid solution Si decrease, and the amount of Mg—Si-based precipitates that are generated during the BH treatment and contribute to increasing the strength is insufficient, and the BH property is also lowered.
- the equivalent circle diameter of the compound defined in the present invention is in the range of 0.3 to 20 ⁇ m, and the composition of the compound is not limited.
- the equivalent circle diameter of the compound defined in the present invention is the diameter of a circle having the same area as the compound that is indefinite, and as a method for measuring or defining the size of the compound accurately and with good reproducibility, It has been widely used.
- the average number density of compounds having an equivalent circle diameter in the range of 0.3 to 20 ⁇ m is preferably as small as possible from the viewpoint of reducing the starting point of fracture during heme processing and securing the solid solution amount of Sn. From the production limit of the efficient production method of the plate, it cannot be completely 0 pieces / mm 2 . Therefore, the lower limit in the present invention of the average number density of compounds having an equivalent circle diameter in the range of 0.3 to 20 ⁇ m does not include 0 pieces / mm 2. The lower limit is about 100 pieces / mm 2 .
- the compounds observed in the plate structure by SEM of 500 times are observed as white particles scattered in the structure when observed in a black and white image. It is a variety of compounds (precipitates, crystallization products) containing Sn such as Mn, Al—Fe—Mn—Si, Al—Si—Sn, and the like. In addition, Mg—Si compounds may also be found in small numbers as black particles scattered in the structure. As described above, the composition of the compound varies widely depending on the composition of the aluminum alloy plate, and it is difficult to limit the composition to a specific composition.
- Standard of Sn solid solution amount The present invention is characterized by securing the solid solution amount of Sn necessary for exhibiting the effect of Sn.
- a guideline (standard) for securing the solid solution amount of Sn 0.5 mass, which is identified by an X-ray spectrometer among compounds having a circle equivalent diameter measured by the SEM in the range of 0.3 to 20 ⁇ m. % Or more of the compounds containing Sn in an amount of less than 50% (including 0%), that is, not less than 0% but less than 50%, preferably less than 40% (including 0%), more preferably less than 30% (0 % Included).
- a compound having a Sn content of less than 0.5% is not a measurement target of a compound containing Sn as a measure of the Sn solid solution amount.
- a compound containing Sn with a very small amount of Sn having a Sn content of less than 0.5% by mass is also measured, a compound containing Sn smaller than the measurement error of the X-ray spectrometer is detected, and the size described above. There is a possibility that all the compounds in the range will be measured. In this case, it cannot be said that the solid solution amount of Sn is accurately reflected. Therefore, from the viewpoint of correlation and reproducibility, a lower limit value of 0.5% by mass or more is provided for the Sn content of the compound.
- the ratio of the number of compounds containing 0.5 mass% or more of Sn (average number) out of the total number of compounds measured by SEM having an equivalent circle diameter of 0.3 to 20 ⁇ m is less than 50%. Indicates that the amount of Sn that precipitates is small and the solid solution amount of Sn is sufficient to exhibit the effect of the added Sn. On the other hand, when the ratio of the number of compounds containing 0.5 mass% or more of Sn (average number) is 50% or more, the amount of precipitated Sn increases, and the solid solution amount of Sn contributes to the effect of the added Sn. The amount is so small that it does not show.
- the evaluation of the Sn solid solution amount by the number ratio of the Sn-containing compound is an indirect measurement method, but includes 0.5 mass% or more of Sn having an equivalent circle diameter in the range of 0.3 to 20 ⁇ m. If the compound is the object of measurement, it correlates well with the effect exhibited by solid solution Sn. That is, the effect exhibited by solid solution Sn correlates well with the ratio of the number of compounds containing Sn (average number), which is identified by the X-ray spectrometer whether or not Sn is contained by 0.5 mass% or more. To do. This point is supported by the examples described later.
- the ratio of the average number of compounds containing Sn of 0.5% by mass or more is less than 50%, and only after securing the solid solution amount of Sn, the capture of atomic vacancies at room temperature is not possible.
- the effect of suppressing the diffusion of Mg and Si and the increase in strength at room temperature (room temperature aging) are exhibited over a long period of time.
- the press formability, particularly the hem workability is improved at the time of press forming the panel after aging at room temperature onto the panel.
- the effect of releasing the trapped holes is also exhibited, and the diffusion of Mg and Si can be promoted to increase the BH property. .
- the lower limit of the ratio (average number) of compounds containing 0.5 mass% or more of Sn is theoretically 0% when the number of compounds containing Sn is 0 when all Sn is dissolved. This is the case.
- Sn is likely to precipitate in the conventional method, and it is difficult to re-dissolve Sn once precipitated. Therefore, if the production efficiency is ignored, the number ratio of compounds containing Sn can be reduced to 0%, but the number of compounds containing Sn (average number) coming from an efficient (industrial) production limit.
- the lower limit of the ratio is about 0.1%.
- Compound measurement Measurement by SEM, which is 500 times the number density of the compound having an equivalent circle diameter of 0.3 to 20 ⁇ m, is performed at 10 points at an arbitrary point of 1/4 part in the plate thickness direction from the surface of the test plate (samples Ten samples are collected), and the number density of each sample is averaged to obtain an average number density (pieces / mm 2 ).
- the measurement of the number ratio of the compound containing 0.5 mass% or more of Sn, which will be described later, is also performed along with this SEM, and similarly, the average number ratio (%) is obtained by averaging the number ratio of each sample. .
- an SEM of 500 times the surface parallel to the plate surface passes through an arbitrary point from the surface in a 1/4 part of the plate thickness direction.
- a sample is prepared by mechanically polishing a plate cross-section sample surface sampled 10 pieces from the above-mentioned site, cutting off about 0.25 mm from the plate surface by mechanical polishing, and further performing buffing to adjust the surface.
- the number of compounds in the equivalent circle diameter range is measured by an automatic analyzer to calculate the number density.
- the measurement site is the sample polishing surface, and the measurement area per sample is 240 ⁇ m ⁇ 180 ⁇ m.
- an X-ray spectrometer used for measuring the number ratio of compounds containing Sn is well known as an analyzer using energy dispersive X-ray spectroscopy (Energy Dispersive X-ray Spectroscopy), and is usually called EDX.
- This X-ray spectrometer is generally attached to the SEM used in the present invention and is widely used for quantitative analysis of the composition of the observed compound.
- the number of compounds identified as containing Sn out of the total number of compounds having an equivalent circle diameter of 0.3 to 20 ⁇ m measured by the SEM was measured. The sample measurement results are averaged and calculated as an average number ratio.
- the aluminum alloy sheet of the present invention is a conventional process or a known process, and the aluminum alloy ingot having the above-mentioned 6000 series component composition is subjected to homogenization heat treatment after casting, and then subjected to hot rolling and cold rolling to obtain a predetermined process. It is manufactured by being subjected to a tempering treatment such as solution hardening and quenching.
- an ordinary molten casting method such as a continuous casting method and a semi-continuous casting method (DC casting method) is appropriately selected for the molten aluminum alloy adjusted to be dissolved within the above-mentioned 6000 series component composition range.
- the average cooling rate during casting is as follows: It is preferable that the liquidus temperature to the solidus temperature be as large (fast) as possible at 30 ° C./min or more.
- homogenization heat treatment Next, the cast aluminum alloy ingot is subjected to a homogenization heat treatment prior to hot rolling.
- the purpose of this homogenization heat treatment (soaking) is to homogenize the structure, that is, eliminate segregation in crystal grains in the ingot structure.
- the conditions are not particularly limited as long as the object is achieved, and normal one-stage or one-stage processing may be performed.
- the homogenization heat treatment temperature is appropriately selected from the range of 500 ° C. or more and less than the melting point, and the homogenization time is 4 hours or more.
- this homogenization temperature is low, segregation within the crystal grains cannot be sufficiently eliminated, and this acts as a starting point of fracture, so that stretch flangeability and bending workability are deteriorated.
- the hot rolling may be started immediately, or the hot rolling may be started after cooling to an appropriate temperature.
- Hot rolling is composed of an ingot (slab) rough rolling process and a finish rolling process according to the thickness of the rolled sheet.
- a reverse or tandem rolling mill is appropriately used.
- the hot rolling start temperature is preferably 350 ° C. to the solidus temperature, more preferably 400 ° C. to the solidus temperature.
- Hot rolled sheet annealing Annealing (roughening) before cold rolling of this hot-rolled sheet is not always necessary, but it can be performed to further improve properties such as formability by refining crystal grains and optimizing the texture. good.
- Cold rolling In cold rolling, the hot-rolled sheet is rolled to produce a cold-rolled sheet (including a coil) having a desired final thickness. However, in order to further refine the crystal grains, the total cold rolling rate is desirably 60% or more regardless of the number of passes.
- the plate Before this cold rolling (after hot rolling) or in the middle of cold rolling (between passes), the plate is held at a high temperature of 480 ° C or higher and below the melting point for 0.1 to 10 seconds, and then 3 ° C / second or higher It is preferable to repeat the intermediate annealing forcibly cooling (rapid cooling) to room temperature at an average cooling rate of 2 times or more, so that Sn produced as a compound in the hot rolling step or the like is dissolved.
- Sn is likely to precipitate, and it is difficult to re-dissolve once precipitated Sn, and the ratio of the average number of compounds containing Sn is less than 50% of the number of compounds of the specific size described above.
- the holding time may be a short time including momentary such as 0.1 seconds, but if it exceeds 10 seconds, the mechanical properties of the plate are remarkably deteriorated.
- the cooling after annealing is not the forced cooling (rapid cooling) to room temperature by air cooling, mist, water cooling or the like with an average cooling rate of 3 ° C./second or more, that is, the average cooling rate is less than 3 ° C./second. Then, Sn once dissolved is reprecipitated and compounded.
- Annealing under such conditions is impossible in a batch furnace, including rapid cooling, and requires a continuous heat treatment furnace that winds the sheet through the furnace while unwinding it.
- the solid solution amount of Sn is inevitably insufficient by only one continuous annealing.
- the intermediate annealing by continuous annealing shall be repeated twice or more.
- the number of repetitions of continuous annealing is preferably about 2 because the efficiency of the manufacturing process is greatly reduced as the number of repetitions increases.
- the solution treatment and quenching treatment may be heating and cooling using a normal continuous heat treatment line, and is not particularly limited. However, since it is desirable to obtain a sufficient solid solution amount of each element and that the crystal grains of the plate structure are finer, the solution treatment temperature is 520 ° C. or higher and the melting temperature or lower. It is preferable that the heating be performed for at least 2 seconds, and the conditions are maintained for 0 to 10 seconds.
- the average cooling rate from the solution temperature to the quenching stop temperature is preferably 3 ° C./second or more.
- the quenching treatment is performed by selecting water cooling means and conditions such as air cooling such as a fan, mist, spray, and immersion, respectively.
- reheating treatment a pre-aging treatment (reheating treatment) is performed after the solution quenching treatment in order to form an aggregate (cluster) of atoms serving as nuclei of the Mg—Si-based compound generated during the BH treatment.
- the ultimate temperature (substance temperature) of the plate is preferably in the temperature range of 80 to 150 ° C., and the holding time is preferably in the range of 3 to 50 hours.
- the cooling to room temperature after the reheating treatment may be allowed to cool or may be forcibly quenched using the cooling means at the time of quenching in order to increase production efficiency.
- Embodiments of the present invention will be described. 6000 series aluminum alloy plates having different Sn solid solution amounts defined in the present invention were prepared according to the intermediate annealing conditions, and the number density of the compounds and the Sn solid solution amount based thereon were investigated. And BH property (coating bake hardenability) after holding this board at room temperature for 100 days and hem workability were also evaluated. The results are shown in Table 2.
- the specific production conditions for these aluminum alloy plates were as follows.
- Aluminum alloy ingots having respective compositions shown in Table 1 were commonly melted by DC casting.
- the average cooling rate during casting was set to 50 ° C./min from the liquidus temperature to the solidus temperature.
- the display in which the numerical value in each element is blank the content is below the detection limit and includes these elements No 0%.
- the ingot was subjected to soaking treatment at 540 ° C. for 4 hours in common with each example, and then hot rough rolling was started. And in each example, it was hot rolled to a thickness of 2.5 mm in the subsequent finish rolling to obtain a hot rolled sheet.
- Table 2 the aluminum alloy plate after hot rolling was subjected to rough annealing at 500 ° C. for 1 minute in common with each example, and then during the cold rolling pass (between passes) as shown in Table 2.
- Intermediate annealing with an annealing furnace was performed under various conditions with different numbers, temperatures, average cooling rates, and the like, and finally a cold-rolled sheet (product sheet) having a thickness of 1.0 mm was obtained.
- these cold-rolled sheets were subjected to a solution treatment in a 560 ° C. glass stone furnace in common with each example, held for 10 seconds after reaching the target temperature, and quenched by water cooling. Immediately after this quenching, a preliminary aging treatment was carried out by holding at 100 ° C. for 5 hours (after holding, slow cooling at a cooling rate of 0.6 ° C./hour).
- test plate (blank) was cut out from each plate immediately after the tempering treatment, and the structure (number density of compounds, number ratio of compounds containing Sn) of each test plate was measured. Moreover, the test plate (blank) was cut out from each plate after being left at room temperature for 100 days after the tempering treatment, and the strength (AS proof stress) and BH property of each test plate were examined. These results are shown in Table 2.
- Test plate structure As the structure of each test plate immediately after the tempering treatment, the average number density (pieces / mm 2 ) of the compound having a circle equivalent diameter in the range of 0.3 to 20 ⁇ m was measured with the SEM of 500 times by the measurement method described above. The average number ratio (%) of compounds containing 0.5% or more of Sn identified by the X-ray spectroscopic apparatus among the measured compounds was investigated.
- Test test In the tensile test, JISZ2201 No. 5 test pieces (25 mm ⁇ 50 mmGL ⁇ plate thickness) were sampled from each test plate after being left at room temperature for 100 days after the tempering treatment, and a tensile test was performed at room temperature. It was. The tensile direction of the test piece at this time was the direction perpendicular to the rolling direction. The tensile speed was 5 mm / min up to 0.2% proof stress and 20 mm / min after proof stress. The N number for the measurement of mechanical properties was 5, and each was calculated as an average value. The test piece for measuring the yield strength after the BH was subjected to the BH treatment after giving a pre-strain of 2% simulating press forming of the plate to the test piece by the tensile tester.
- BH property Each test plate was commonly aged at room temperature for 100 days and then subjected to an artificial age-hardening treatment at 185 ° C. for 20 minutes (after BH). Yield strength) was determined by the tensile test. And the BH property of each test plate was evaluated from the difference between these 0.2% proof stresses (increased proof stress), and the case where the increased amount of 0.2% proof stress was 100 MPa or more was regarded as acceptable.
- Hem workability Hem workability was measured for each test plate after standing at room temperature for 100 days.
- a strip-shaped test piece with a width of 30 mm was used, and after bending 90 ° with an internal bend R of 1.0 mm by a down flange, a 1.0 mm thick inner was sandwiched, and the bent portion was further bent inwardly to about 130 degrees.
- Pre-hem processing was performed, and flat hem processing was performed in which the end was closely attached to the inner by bending 180 degrees.
- the flat hem bend (edge bend) is visually observed for surface conditions such as rough skin, minute cracks, and large cracks, and visually evaluated according to the following criteria. . 0: No cracking, rough skin, 1: Mild rough skin, 2; Deep rough skin, 3: Small surface crack, 4; Continuous surface crack, 5: Break
- each of the inventive examples shown in the numbers 1 to 4 and 12 to 23 in Table 2 is within the composition range of the present invention (alloy numbers 1 to 13 in Table 1) and within the above-mentioned preferable condition range including the intermediate annealing. Manufacture. For this reason, as shown in Table 2, each of these inventive examples satisfies the average number density of the compound defined in the present invention and the average number ratio of the compound containing 0.5 mass% or more of Sn, and precipitates Sn contained. Is suppressed, and the solid solution amount of Sn is high.
- each of the above-mentioned invention examples has a BH (baked hard) even after the long-term room temperature aging for 100 days after the tempering treatment, or even when the As proof strength is 90 to 110 MPa.
- the yield strength is 190 MPa and the difference in yield strength is 100 MPa or more.
- the As yield strength is relatively low, so that it is excellent in press formability to automobile panels and the like, and is excellent in hem workability.
- Comparative Examples 5 to 11 in Table 2 using the same alloy number 1 in Table 1 as those of the invention examples are examples in which the intermediate annealing conditions deviate from the preferred range. For this reason, these comparative examples have too many compounds prescribed
- Comparative Example 5 is not subjected to intermediate annealing. Although the comparative example 6 satisfy
- the second intermediate annealing satisfies the conditions of temperature, holding time, and average cooling rate, but the temperature of the first intermediate annealing is too low at 480 ° C.
- the first intermediate annealing satisfies the conditions of temperature, holding time, and average cooling rate, but the temperature of the second intermediate annealing is too low at 480 ° C.
- the temperatures of the first and second intermediate annealings are both less than 480 ° C. and too low.
- the temperature and holding time of the first and second intermediate annealing satisfy the conditions, but the average cooling rate of the first or second time is too slow.
- Comparative Examples 24 to 29 in Table 2 are manufactured within a preferable range including intermediate annealing conditions, Alloy Nos. 14 to 19 in Table 1 are used, and inclusion of essential elements Mg, Si, and Sn Each amount is outside the scope of the present invention. For this reason, as shown in Table 2, these Comparative Examples 24 to 29 have a relatively high As yield strength after holding at room temperature for 100 days, as compared with each invention example. It is inferior in workability or BH property. In Comparative Example 27, Sn was too much, and cracking occurred during hot rolling, so that the hot rolled sheet itself could not be manufactured.
- the comparative example 24 is the alloy 14 of Table 1, and there is too little Si.
- the comparative example 25 is the alloy 15 of Table 1, and there is too much Si.
- the comparative example 26 is the alloy 16 of Table 1, and there is too little Sn.
- the comparative example 27 is the alloy 17 of Table 1, and there is too much Sn.
- the comparative example 28 is the alloy 18 of Table 1, and there is too little Mg.
- the comparative example 29 is the alloy 19 of Table 1, and there is too much Mg.
- composition and compound structure defined in the present invention and intermediate annealing conditions for the improvement of heme workability and BH property after long-term aging of a 6000 series aluminum alloy plate containing Sn The critical significance or effect of preferable manufacturing conditions such as the above is supported.
- the present invention it is possible to provide a 6000 series aluminum alloy plate having both BH properties and formability after long-term room temperature aging.
- the application of the 6000 series aluminum alloy plate can be expanded as a member for a transport device such as an automobile, a ship or a vehicle, a home appliance, a building or a structure, and particularly as a member for a transport device such as an automobile.
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Abstract
La présente invention se rapporte à une tôle d'alliage d'aluminium à base d'Al-Mg-Si pour le formage, qui contient 0,2 à 2,0 % de Mg, 0,3 à 2,0 % de Si, et de 0,005 à 0,3 % de Si (toutes les quantités étant rapportées à la masse), le reste comprenant de l'Al et des impuretés inévitables, laquelle tôle d'alliage d'aluminium pour le formage se caractérise en ce que la structure de la tôle d'alliage d'aluminium est telle que la densité moyenne en nombre des composés ayant un diamètre équivalent à un cercle dans une plage de 0,3 à 20 µm, mesuré par MEB à un grossissement de 500 fois, est supérieure à 0/mm2 mais pas supérieure à 5 000/mm2, et celle pour les composés mesurés par MEB, le rapport de comptage moyen des composés qui contiennent 0,5 % en masse ou plus de Sn, identifiés au moyen d'un spectrographe à rayons X, est supérieur ou égal à 0 % ou plus mais inférieur à 50 %. Cette tôle en alliage d'aluminium pour le formage présente des propriétés BH élevées et une bonne aptitude au façonnage.
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KR1020177005027A KR20170029633A (ko) | 2014-08-27 | 2015-08-27 | 성형용 알루미늄 합금판 |
KR1020187023408A KR20180095117A (ko) | 2014-08-27 | 2015-08-27 | 성형용 알루미늄 합금판 |
CN201580043418.3A CN106574327A (zh) | 2014-08-27 | 2015-08-27 | 成形用铝合金板 |
US15/502,838 US20170233853A1 (en) | 2014-08-27 | 2015-08-27 | Aluminum alloy sheet for forming |
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JP2014173278A JP6224550B2 (ja) | 2014-08-27 | 2014-08-27 | 成形用アルミニウム合金板 |
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JP (1) | JP6224550B2 (fr) |
KR (2) | KR20170029633A (fr) |
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US20220081741A1 (en) * | 2019-06-06 | 2022-03-17 | Arconic Technologies Llc | Aluminum alloys having silicon, magnesium, copper and zinc |
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BR112017006271B1 (pt) * | 2014-10-28 | 2021-09-21 | Novelis Inc. | Chapa de liga de alumínio, parte de corpo automotivo e método para produzir uma chapa de liga de alumínio |
GB2552399A (en) * | 2016-02-26 | 2018-01-24 | Uacj Corp | Hot forming aluminium alloy plate and production method therefor |
CN112725666A (zh) * | 2020-11-24 | 2021-04-30 | 宁波科诺精工科技有限公司 | 一种具有冷镦不开裂效果的铝合金 |
JP2022093988A (ja) * | 2020-12-14 | 2022-06-24 | 昭和電工株式会社 | アルミニウム合金鍛造品およびアルミニウム合金鍛造品の製造方法 |
CN112831700B (zh) * | 2020-12-31 | 2022-02-08 | 安徽鑫铂铝业股份有限公司 | 一种接触网用高强度耐腐蚀铝合金及其制备方法 |
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JPH09249950A (ja) * | 1996-03-15 | 1997-09-22 | Nippon Steel Corp | 成形性および塗装焼付硬化性に優れたアルミニウム合金板の製造方法 |
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US5282909A (en) * | 1992-06-26 | 1994-02-01 | Furukawa Aluminum Co., Ltd. | Aluminum alloy extrusion material with excellent chip separation property and precision of cut face on cutting |
JPH10226894A (ja) * | 1997-02-17 | 1998-08-25 | Nippon Steel Corp | 成形加工性、塗装焼付硬化性、化成性、および耐食性に優れたアルミニウム合金板の製造方法 |
TW200536946A (en) * | 2003-12-11 | 2005-11-16 | Nippon Light Metal Co | Method for producing Al-Mg-Si alloy excellent in bake-hardenability and hemmability |
JP4794862B2 (ja) * | 2004-01-07 | 2011-10-19 | 新日本製鐵株式会社 | 塗装焼付け硬化性に優れた6000系アルミニウム合金板の製造方法 |
JP5203772B2 (ja) * | 2008-03-31 | 2013-06-05 | 株式会社神戸製鋼所 | 塗装焼付け硬化性に優れ、室温時効を抑制したアルミニウム合金板およびその製造方法 |
BR112014017965B1 (pt) * | 2012-01-27 | 2022-07-12 | Uacj Corporation | Material de liga de alumínio para barbatana de trocador de calor, método de sua fabricação e trocador de calor que utiliza o mencionado material de liga de alumínio |
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2014
- 2014-08-27 JP JP2014173278A patent/JP6224550B2/ja not_active Expired - Fee Related
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2015
- 2015-08-27 WO PCT/JP2015/074297 patent/WO2016031937A1/fr active Application Filing
- 2015-08-27 CN CN201580043418.3A patent/CN106574327A/zh active Pending
- 2015-08-27 US US15/502,838 patent/US20170233853A1/en not_active Abandoned
- 2015-08-27 KR KR1020177005027A patent/KR20170029633A/ko active IP Right Grant
- 2015-08-27 KR KR1020187023408A patent/KR20180095117A/ko active Application Filing
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JPH06340940A (ja) * | 1993-06-02 | 1994-12-13 | Kobe Steel Ltd | プレス成形性、焼付硬化性に優れたアルミニウム合金板及びその製造方法 |
JPH09249950A (ja) * | 1996-03-15 | 1997-09-22 | Nippon Steel Corp | 成形性および塗装焼付硬化性に優れたアルミニウム合金板の製造方法 |
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US20220081741A1 (en) * | 2019-06-06 | 2022-03-17 | Arconic Technologies Llc | Aluminum alloys having silicon, magnesium, copper and zinc |
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JP2016047949A (ja) | 2016-04-07 |
KR20180095117A (ko) | 2018-08-24 |
JP6224550B2 (ja) | 2017-11-01 |
KR20170029633A (ko) | 2017-03-15 |
US20170233853A1 (en) | 2017-08-17 |
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