WO2010150651A1 - マグネシウム合金板 - Google Patents
マグネシウム合金板 Download PDFInfo
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- WO2010150651A1 WO2010150651A1 PCT/JP2010/059710 JP2010059710W WO2010150651A1 WO 2010150651 A1 WO2010150651 A1 WO 2010150651A1 JP 2010059710 W JP2010059710 W JP 2010059710W WO 2010150651 A1 WO2010150651 A1 WO 2010150651A1
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- Prior art keywords
- magnesium alloy
- plate
- alloy plate
- crystallized
- less
- Prior art date
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- 229910000861 Mg alloy Inorganic materials 0.000 title claims abstract description 99
- 238000004519 manufacturing process Methods 0.000 claims abstract description 19
- 239000002245 particle Substances 0.000 claims abstract description 18
- 229910052748 manganese Inorganic materials 0.000 claims abstract description 16
- 229910045601 alloy Inorganic materials 0.000 claims description 59
- 239000000956 alloy Substances 0.000 claims description 59
- 238000005096 rolling process Methods 0.000 claims description 35
- 238000005266 casting Methods 0.000 claims description 26
- 239000000126 substance Substances 0.000 claims description 20
- 238000000034 method Methods 0.000 claims description 14
- 238000009749 continuous casting Methods 0.000 claims description 9
- 229910052684 Cerium Inorganic materials 0.000 claims description 6
- 229910052727 yttrium Inorganic materials 0.000 claims description 6
- 229910052791 calcium Inorganic materials 0.000 claims description 3
- 229910052802 copper Inorganic materials 0.000 claims description 3
- 229910052761 rare earth metal Inorganic materials 0.000 claims description 3
- 229910052710 silicon Inorganic materials 0.000 claims description 3
- 229910052709 silver Inorganic materials 0.000 claims description 3
- 229910052712 strontium Inorganic materials 0.000 claims description 3
- 229910052726 zirconium Inorganic materials 0.000 claims description 3
- 229910052725 zinc Inorganic materials 0.000 claims description 2
- 239000000463 material Substances 0.000 description 35
- 238000012360 testing method Methods 0.000 description 26
- 239000000047 product Substances 0.000 description 19
- 239000013078 crystal Substances 0.000 description 15
- 238000010438 heat treatment Methods 0.000 description 14
- 239000000203 mixture Substances 0.000 description 13
- 238000012545 processing Methods 0.000 description 12
- 229910018131 Al-Mn Inorganic materials 0.000 description 8
- 229910018461 Al—Mn Inorganic materials 0.000 description 8
- 238000001816 cooling Methods 0.000 description 7
- 238000009864 tensile test Methods 0.000 description 7
- 230000007797 corrosion Effects 0.000 description 5
- 238000005260 corrosion Methods 0.000 description 5
- 238000005336 cracking Methods 0.000 description 5
- 238000009863 impact test Methods 0.000 description 5
- 239000000654 additive Substances 0.000 description 4
- 230000000996 additive effect Effects 0.000 description 4
- 229910052751 metal Inorganic materials 0.000 description 4
- 239000002184 metal Substances 0.000 description 4
- 238000005498 polishing Methods 0.000 description 4
- 239000011247 coating layer Substances 0.000 description 3
- 238000002425 crystallisation Methods 0.000 description 3
- 230000008025 crystallization Effects 0.000 description 3
- 230000007547 defect Effects 0.000 description 3
- 230000008520 organization Effects 0.000 description 3
- 229910018137 Al-Zn Inorganic materials 0.000 description 2
- 229910018573 Al—Zn Inorganic materials 0.000 description 2
- 230000008014 freezing Effects 0.000 description 2
- 238000007710 freezing Methods 0.000 description 2
- 238000011835 investigation Methods 0.000 description 2
- 239000011777 magnesium Substances 0.000 description 2
- 238000007712 rapid solidification Methods 0.000 description 2
- 239000002994 raw material Substances 0.000 description 2
- 238000005204 segregation Methods 0.000 description 2
- 239000006104 solid solution Substances 0.000 description 2
- 229910000549 Am alloy Inorganic materials 0.000 description 1
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 description 1
- 229910003023 Mg-Al Inorganic materials 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- 230000032683 aging Effects 0.000 description 1
- 238000005452 bending Methods 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 239000000919 ceramic Substances 0.000 description 1
- 239000013065 commercial product Substances 0.000 description 1
- 239000000470 constituent Substances 0.000 description 1
- 238000012937 correction Methods 0.000 description 1
- 238000005520 cutting process Methods 0.000 description 1
- 230000006866 deterioration Effects 0.000 description 1
- 238000004512 die casting Methods 0.000 description 1
- 238000002149 energy-dispersive X-ray emission spectroscopy Methods 0.000 description 1
- 238000011156 evaluation Methods 0.000 description 1
- 238000001125 extrusion Methods 0.000 description 1
- 238000005242 forging Methods 0.000 description 1
- 239000012535 impurity Substances 0.000 description 1
- 239000011261 inert gas Substances 0.000 description 1
- 239000010410 layer Substances 0.000 description 1
- 229910052749 magnesium Inorganic materials 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 239000007769 metal material Substances 0.000 description 1
- 230000003647 oxidation Effects 0.000 description 1
- 238000007254 oxidation reaction Methods 0.000 description 1
- 239000011148 porous material Substances 0.000 description 1
- 238000003825 pressing Methods 0.000 description 1
- 238000004080 punching Methods 0.000 description 1
- 238000004451 qualitative analysis Methods 0.000 description 1
- 238000012764 semi-quantitative analysis Methods 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
- 239000000243 solution Substances 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 238000005728 strengthening Methods 0.000 description 1
- 230000035882 stress Effects 0.000 description 1
- 238000010119 thixomolding Methods 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Images
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C23/00—Alloys based on magnesium
- C22C23/02—Alloys based on magnesium with aluminium as the next major constituent
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21B—ROLLING OF METAL
- B21B1/00—Metal-rolling methods or mills for making semi-finished products of solid or profiled cross-section; Sequence of operations in milling trains; Layout of rolling-mill plant, e.g. grouping of stands; Succession of passes or of sectional pass alternations
- B21B1/46—Metal-rolling methods or mills for making semi-finished products of solid or profiled cross-section; Sequence of operations in milling trains; Layout of rolling-mill plant, e.g. grouping of stands; Succession of passes or of sectional pass alternations for rolling metal immediately subsequent to continuous casting
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21B—ROLLING OF METAL
- B21B3/00—Rolling materials of special alloys so far as the composition of the alloy requires or permits special rolling methods or sequences ; Rolling of aluminium, copper, zinc or other non-ferrous metals
-
- 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
- C22F1/06—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of magnesium or alloys based thereon
Definitions
- the present invention relates to a magnesium alloy plate suitable for materials such as a housing and various parts, a magnesium alloy member using the alloy plate, and a method for manufacturing the magnesium alloy plate.
- the present invention relates to a magnesium alloy plate and a magnesium alloy member that are excellent in impact resistance at low temperatures.
- Magnesium alloys containing various additive elements in magnesium have been used as materials for casings of portable electronic devices such as mobile phones and notebook PCs, and for parts such as automobile parts.
- Patent Document 1 proposes a rolled plate made of an alloy equivalent to the AZ91 alloy in the ASTM standard and having excellent press workability.
- Magnesium alloy is lightweight and has excellent specific strength and specific rigidity, so it is desired to be used not only in a normal temperature environment of about 0-30 ° C but also in cold regions and freezing warehouses where the temperature is below freezing.
- a normal temperature environment of about 0-30 ° C but also in cold regions and freezing warehouses where the temperature is below freezing.
- conventionally, the mechanical properties of magnesium alloys in such a low temperature environment have not been sufficiently studied.
- the cast material of magnesium alloy is inferior in strength compared to a rolled material of magnesium alloy or a press-formed member. Further, as a result of investigations by the present inventors, the AZ31 alloy press member also has insufficient strength in a low-temperature environment and is inferior in impact resistance.
- a rolled plate made of AZ91 alloy as described in Patent Document 1 and a pressed member obtained by pressing the rolled plate have higher strength than a plate made of AZ31 alloy or a pressed member made of AZ31 alloy.
- a rolled plate made of AZ91 alloy and a member obtained by subjecting this rolled plate to plastic working such as press working have sufficient impact resistance characteristics in a low temperature environment. I got the knowledge that it may not be.
- one of the objects of the present invention is to provide a magnesium alloy member excellent in impact resistance even in a low temperature environment, and a magnesium alloy plate suitable for the material of this member.
- Another object of the present invention is to provide a method for producing the magnesium alloy sheet of the present invention.
- the inventors have prepared a magnesium alloy plate under various conditions, and subjected the plastic plate such as press working to the obtained plate to produce a magnesium alloy member.
- the magnesium alloy plate and member are subjected to a low temperature environment.
- the impact resistance (dentation resistance) and mechanical properties of the steel were investigated.
- the magnesium alloy plate which was difficult to be dented had a small amount of crystallized substances having a specific composition.
- the magnesium alloy member obtained by using a small magnesium alloy plate with a small specific composition is difficult to dent, and this member has a small and small amount of crystallized specific composition as well as the material plate. , And got the knowledge.
- the maximum diameter and the number of the crystallized substances are controlled, that is, the number of crystallized substances and coarse crystallized substances are reduced under specific conditions.
- the knowledge that it was preferable to cast and to roll the obtained cast plate was obtained.
- the present invention is based on the above findings.
- the magnesium alloy plate of the present invention is made of a magnesium alloy containing Al and Mn, and in the thickness direction of the magnesium alloy plate, the surface from the surface of the alloy plate to 30% of the thickness of the alloy plate is surfaced.
- a crystallized product containing both Al and Mn and having a maximum diameter of 0.1 ⁇ m or more and 1 ⁇ m or less with respect to this small region Is 15 or less.
- the crystallized particles have a mass ratio of Al to Mn: Al / Mn of 2 or more and 5 or less.
- the magnesium alloy plate of the present invention having the above specific structure can be produced, for example, by the following production method of the present invention.
- the manufacturing method of the magnesium alloy plate of this invention comprises the following casting processes and rolling processes.
- Casting process A process of casting a magnesium alloy containing Al and Mn into a plate shape.
- Rolling step A step of rolling the cast plate obtained by the casting step.
- the casting is performed by a twin roll continuous casting method. The casting is performed so that the roll temperature is 100 ° C. or less and the thickness of the cast plate obtained by the casting is 5 mm or less.
- the magnesium alloy member of the present invention is formed by subjecting the magnesium alloy plate of the present invention to plastic working such as press working.
- This alloy member also has the same structure as the magnesium alloy plate of the present invention, that is, 15 crystallized particles having the specific size and composition when an arbitrary small region of 50 ⁇ m 2 is taken from the surface region. It has the following organization.
- a cast plate having a fine structure with a small average crystal grain size is obtained by rapid solidification.
- Such a cast plate is excellent in plastic workability such as rolling because there are few coarse crystallized materials starting from cracks and deformation, and rolling can improve strength and elongation. it can.
- the alloy plate of the present invention obtained by the above-described production method has a large amount of coarse crystallized material in a region on the surface side that is particularly susceptible to impact because the coarse crystallized material is reduced and the crystallized material itself is small. It is reduced and has a structure in which fine crystallized substances are slightly present, preferably a structure in which crystallized substances are not substantially present, so that cracks and cracks are not easily generated even when subjected to an impact such as dropping.
- the crystallized product itself is small as described above, it is possible to suppress a decrease in the amount of solid solution Al, and it is possible to maintain high strength because Al is sufficiently dissolved, The strength can be further increased by rolling.
- the alloy plate of the present invention is not easily dented even when subjected to an impact, and is excellent in impact resistance not only at room temperature (about 20 ° C.) but also in a low temperature environment below 0 ° C.
- the alloy plate of the present invention having the above specific structure is excellent in plastic workability and can be easily subjected to press working, etc., and the obtained alloy member of the present invention is also particularly similar to the alloy plate of the present invention.
- the crystallized material is small and has a small structure. Therefore, the alloy member of the present invention also has high mechanical properties such as strength and elongation even in a low temperature environment, and is excellent in impact resistance.
- compositions containing at least Al and Mn as additive elements include those having various compositions containing at least Al and Mn as additive elements (remainder: Mg and impurities).
- additive elements other than Al and Mn include one or more elements selected from Zn, Si, Ca, Sr, Y, Cu, Ag, Ce, Zr, and rare earth elements (excluding Y and Ce).
- Al is preferably contained in an amount of 5% by mass to 12% by mass and Mn is preferably contained in an amount of 0.1% by mass to 2.0% by mass.
- the content of additive elements other than Al and Mn is Zn: 0.2 to 7.0 mass%, Si: 0.2 to 1.0 mass%, Ca: 0.2 to 6.0 mass%, Sr: 0.2 to 7.0 mass%, Y: 1.0 to 6.0 mass% %, Cu: 0.2 to 3.0 mass%, Ag: 0.5 to 3.0 mass%, Ce: 0.05 to 1.0 mass%, Zr: 0.1 to 1.0 mass%, RE (rare earth elements (excluding Y and Ce)): 1.0 to 3.5 % By weight.
- an alloy containing Al and Mn and one or more of these elements in the above range for example, an AZ-based alloy (Mg-Al-Zn-based alloy, Zn: 0.2 to 1.5 mass%) in the ASTM standard, Examples thereof include AM alloys (Mg—Al—Mn alloys, Mn: 0.15 to 0.5 mass%).
- the Al content the higher the Al content (hereinafter referred to as the Al content), the better the mechanical properties and the corrosion resistance, and the more preferable the Al content is 5.8 mass% to 10 mass%.
- magnesium alloys with an Al content of 5.8 to 10% by mass include, for example, AZ61 alloy, AZ80 alloy, AZ81 alloy, AZ91 alloy, and Mg-Al-Mn alloy for the Mg-Al-Zn alloy, AM60 alloy, and AM100 alloy.
- Etc. is a suitable composition.
- the AZ91 alloy having an Al content of 8.3 to 9.5% by mass is more excellent in mechanical properties such as corrosion resistance, strength, and plastic deformation resistance than other Mg-Al alloys.
- the alloy plate of the present invention has a pair of opposing one surface and the other surface, and these two surfaces are typically in a parallel relationship, and are usually in a front / back relationship in the scene of use. These one and other surfaces may be flat or curved. The distance between the one surface and the other surface is the thickness of the magnesium alloy plate. Since the alloy plate of the present invention is obtained by rolling a cast plate having a thickness of 5 mm or less as described above, the thickness of the alloy plate of the present invention is less than 5 mm. In particular, the alloy plate of the present invention is subjected to plastic working such as press working, and is used as a material for a thin and lightweight casing and various members.
- the thickness of the alloy plate is about 0.3 mm to 3 mm, In particular, the thickness is preferably 0.5 mm or more and 2.0 mm or less, and the thicker in the range, the better the strength, and the thinner, the more suitable for a thin and light housing. It is preferable to select the thickness of the finally obtained magnesium alloy plate by adjusting the casting conditions and rolling conditions according to the desired application.
- the alloy member of the present invention has various shapes obtained by subjecting the magnesium alloy plate to plastic working such as press working, for example, a bottom portion and a side wall portion standing from the bottom portion] -like material or box-like material Is representative.
- plastic working such as press working
- the thickness of the flat portion where the deformation due to plastic working such as press working is not substantially performed is substantially the same as the thickness of the magnesium alloy plate used as the material, and is almost the same.
- Examples of the alloy plate of the present invention include a rolled plate obtained by rolling a cast material, and a processed plate obtained by further subjecting the rolled plate to heat treatment, leveler processing, polishing processing, and the like.
- the alloy member of the present invention includes not only those in which the alloy plate is subjected to plastic processing such as press processing, but also those in which heat treatment or polishing processing is performed after plastic processing.
- the rolled plate, the treated plate, and the alloy member may further include an anticorrosive treatment layer or a coating layer.
- the alloy plate and the alloy member of the present invention are excellent in mechanical properties such as strength and elongation even under a low temperature environment as described above, and are not easily dented when subjected to an impact such as dropping.
- a flat portion where deformation (e.g., deformation due to drawing) or the like accompanying plastic working such as press working in the alloy plate or alloy member of the present invention is not substantially performed (The part (substantially similar to the material plate) has a tensile strength of 350 MPa or more, a 0.2% proof stress: 280 MPa or more, and an elongation of 2% or more.
- the alloy plate of the present invention has a structure in which a coarse crystallized substance is not substantially present and a minute crystallized substance is slightly present when an arbitrary small region is taken from the region on the surface side.
- a region from the surface of the alloy plate to 30% of the thickness of the alloy plate is defined as a surface region, and 50 ⁇ m 2 arbitrarily selected from the surface region.
- the maximum diameter of each crystallized product is measured, there are 15 or less fine crystallized products having a maximum diameter of 0.1 ⁇ m or more and 1 ⁇ m or less for one small region.
- a crystallized substance having a maximum diameter of 0.5 ⁇ m or less exists. If there is a coarse crystallized product exceeding 1 ⁇ m, the coarse crystallized product can become a starting point of cracking when subjected to an impact such as dropping, so that cracking and cracking are likely to occur, and the impact resistance is low. In addition, even if the maximum diameter is 1 ⁇ m or less, if there are more than 15 for 50 ⁇ m 2 , the number of cracks and the starting point of cracks will increase, leading to a decrease in strength and low impact resistance. . The smaller the number of crystallized particles having a maximum diameter of 0.1 to 1 ⁇ m, the better the impact resistance. More preferably, the number is 10 or less, and ideally 0.
- the crystallized product contains both Al and Mn. Details of the method for measuring the maximum diameter will be described later. In the present invention, the presence of an extremely fine crystallized product that is unlikely to cause cracking, that is, a crystallized product having a maximum diameter of less than 0.1 ⁇ m is allowed, but the crystallized product exists as described above. It is preferable not to.
- Examples of the alloy plate of the present invention include those having a small average crystal grain size and a fine structure of 20 ⁇ m or less. As described above, a cast plate having a fine structure can be obtained by performing continuous casting under specific conditions, and by rolling the cast plate, a rolled plate having the fine structure can be obtained.
- the alloy plate of the present invention having such a fine structure is excellent in mechanical properties such as strength and elongation, and can improve impact resistance even in a low temperature environment.
- the magnesium alloy plate having the above-mentioned fine structure and the alloy member of the present invention obtained by using a processed plate obtained by subjecting this rolled plate to a leveler treatment or the like also have a fine structure with an average crystal grain size of 20 ⁇ m or less. It has excellent impact resistance.
- a more preferable average crystal grain size is 0.1 ⁇ m or more and 10 ⁇ m or less.
- the roll temperature is more preferably 60 ° C. or less, and the thickness of the cast plate is more preferably 4.0 mm or less.
- This casting process (including the cooling process) is preferably performed in an inert gas atmosphere in order to prevent oxidation of the magnesium alloy.
- the rolling conditions include, for example, the heating temperature of the material: 200 to 400 ° C, the heating temperature of the rolling roll: 150 to 300 ° C, and the rolling reduction per pass: 5 to 50%. A pass is recommended. Control rolling described in Patent Document 1 may be used.
- By rolling the cast material not a cast metal structure but a rolled structure can be obtained. Also, by rolling, it is easy to obtain a microstructure with an average crystal grain size of 20 ⁇ m or less, and it reduces surface defects by reducing internal defects such as segregation and shrinkage cavities (pores) and surface defects during casting. An excellent rolled sheet can be obtained.
- the final heat treatment is performed after the final rolling to obtain a fine recrystallized structure having an average crystal grain size of 20 ⁇ m or less, the strength and corrosion resistance of the obtained rolled sheet can be further improved.
- the alloy member of the present invention is made of plastic such as press processing (including punching), deep drawing, forging, blow processing, and bending so that the rolled sheet (including those subjected to heat treatment and the like) has a desired shape. Obtained by processing.
- this plastic working is performed at a temperature of 200 to 280 ° C., it is possible to reduce that the rolled plate has a coarse recrystallized structure and to reduce deterioration of mechanical properties and corrosion resistance.
- heat treatment or anticorrosion treatment may be applied, or a coating layer may be formed.
- the magnesium alloy plate of the present invention and the magnesium alloy member of the present invention are excellent in impact resistance in a low temperature environment.
- the manufacturing method of the magnesium alloy plate of the present invention can manufacture the magnesium alloy plate of the present invention.
- FIG. 1 is a schematic explanatory view for explaining an impact test.
- the heating temperature of the raw material 200 to 400 ° C
- the heating temperature of the rolling roll 150 to 300 ° C
- the rolling reduction per pass 5 to 50% Rolling is performed a plurality of times until the thickness reaches 0.6 mm to produce a rolled sheet.
- the obtained rolled plate (magnesium alloy plate) is used as a sample (plate).
- the obtained rolled plate is subjected to a corner drawing process at a heating temperature of 250 ° C. to produce a cross-sectional [shaped box-shaped body, and this box-shaped body (magnesium alloy member) is used as a sample (housing). .
- a heat treatment (solution treatment) or an aging treatment for homogenizing the composition may be performed, an intermediate heat treatment may be performed during the rolling, or a final heat treatment may be performed after the final rolling.
- the rolled plate may be subjected to leveler processing or polishing processing, and the flatness may be improved by correction, or the surface may be smoothed by polishing.
- the composition of particles present in the section is determined using, for example, qualitative analysis represented by EDX and semi-quantitative analysis, and particles containing Al and Mn are crystallized.
- the maximum value of the length across each straight line in each particle is the maximum diameter of the particle, the maximum diameter is 0.1 ⁇ m or more and 1 ⁇ m or less.
- the number of crystallized substances having a size of 1 is defined as the number of crystallized substances in the small region, and the average of the five small regions is defined as the number of crystallized materials in this sample / 50 ⁇ m 2 .
- the bottom surface portion which is a flat portion that is not accompanied by squeezing deformation in the sample, is cut in the plate thickness direction, and the cross section is observed in the same manner as the sample (plate), and the number of crystallized substances / 50 ⁇ m.
- the area of the small region is set to 200 ⁇ m 2 , and the maximum diameter of the crystallized material existing in this 200 ⁇ m 2 , and the crystal distillate to measure the number / 200 ⁇ m 2 of.
- fills each said area although a shape will not be ask
- test piece for the tensile test and the test piece for the impact test described later are manufactured by cutting out from the bottom surface portion, which is a flat portion that is not accompanied by drawing deformation in the sample.
- ⁇ Shock test (low temperature) ⁇ A 30 mm ⁇ 30 mm plate piece is cut out from each sample, and the cut plate piece is used as a test piece.
- the depth of the circular hole 21 was set such that a cylindrical rod 10 described later can be sufficiently inserted.
- the circular hole 21 was arranged so as to be coaxial with the central axis.
- the cylindrical bar 10 is freely dropped from the above arrangement point (height 200 mm) toward the test piece 1, and then the dent amount of the test piece 1 is measured.
- the dent amount (mm) was a straight line connecting both opposing sides of the test piece 1, and the distance from this straight line to the most recessed part was measured using a point micrometer.
- This impact test was performed in a low temperature environment of ⁇ 30 ° C. The results are shown in Table 1. If the dent amount is 0.5 mm or less, ⁇ , and more than 0.5 mm are indicated as ⁇ , and if the dent amount cannot be measured due to cracking, it is indicated as ⁇ crack '', and if a crack (crack) occurs, ⁇ crack '' It shows.
- magnesium alloy plates and magnesium alloy members with a maximum diameter of 0.1 ⁇ m or more and 15 ⁇ m or less of Al-Mn crystallized materials are the same for any 50 ⁇ m 2 selected from the surface region.
- the amount of dents is small even in a low temperature environment such as -30 ° C., and the impact resistance is excellent.
- the reason for this is considered to be due to excellent mechanical properties such as tensile strength and elongation even in a low temperature environment.
- the sample Nos. 1-1 and 1-2 having excellent impact resistance have only a crystallized substance having a maximum diameter of 0.5 ⁇ m or less.
- Test Example 2 Using a magnesium alloy ingot shown in Table 2 (all commercially available) to produce a magnesium alloy plate and magnesium alloy member (housing) under various conditions, the structure observation of the obtained magnesium alloy plate and magnesium alloy member, An impact test (low temperature) was conducted in the same manner as in Test Example 1. The results are shown in Table 2.
- Manufacturing conditions “casting ⁇ rolling” are performed by a twin roll continuous casting method, and the roll temperature and the thickness of the cast plate are as shown in Table 2.
- the rolling conditions are the same as in Test Example 1. However, in this test, the heating time and rolling speed of the material, and the cooling rate during rolling so that the total time during which the material is maintained in the temperature range of 150 ° C to 250 ° C is 45 minutes or 90 minutes. Etc. are adjusted. In Test Example 1, the total time is about 60 minutes.
- the shape “plate” indicates that the sample is a rolled plate (magnesium alloy plate), and the “housing” is the sample prepared from this rolled plate under the same conditions as in Test Example 1. Indicates a box-shaped body (magnesium alloy member).
- Condition B die-cast
- Condition C commercial board
- Condition D commercial housing
- the production condition “extrusion ⁇ rolling” is a commercially available extrudate, and this extrudate is rolled under the same conditions as described above for “casting ⁇ rolling”, and the resulting rolled plate is used as a sample (plate).
- a box-shaped body produced from this rolled plate under the same conditions as in the above-described “casting ⁇ rolling” is used as a sample (housing).
- a magnesium alloy plate or magnesium alloy member having 15 or less Al-Mn crystallized crystals having a maximum diameter of 0.1 ⁇ m or more and 1 ⁇ m or less with respect to an arbitrary 50 ⁇ m 2 selected from the surface region is It can be seen that it has excellent impact resistance even in a low temperature environment such as -30 ° C.
- the above-described embodiment can be modified as appropriate without departing from the gist of the present invention, and is not limited to the above-described configuration.
- the composition of the magnesium alloy, the plate thickness after casting and after rolling, the roll temperature during casting, and the like may be appropriately changed.
- the magnesium alloy member of the present invention is excellent in impact resistance under a low temperature environment, it can be suitably used for various cases and parts used in a low temperature environment.
- the magnesium alloy plate of the present invention can be suitably used as a constituent material for the magnesium alloy member of the present invention.
- the manufacturing method of this invention magnesium alloy plate can be utilized suitably for manufacture of this invention magnesium alloy plate.
- test piece 10 cylinder rod 20 support base 21 circle hole
Abstract
Description
鋳造工程:AlとMnとを含有するマグネシウム合金を板状に鋳造する工程。
圧延工程:上記鋳造工程により得られた鋳造板を圧延する工程。
特に、上記鋳造は、双ロール連続鋳造法により行う。また、この鋳造は、ロール温度を100℃以下とし、この鋳造により得られる鋳造板の厚さが5mm以下となるように行う。
《組成》
本発明マグネシウム合金板及び本発明マグネシウム合金部材を構成するマグネシウム合金は、添加元素に少なくともAlとMnとを含有する種々の組成のもの(残部:Mg及び不純物)が挙げられる。Al及びMn以外の添加元素としては、Zn,Si,Ca,Sr,Y,Cu,Ag,Ce,Zr及び希土類元素(Y,Ceを除く)から選択された1種以上の元素が挙げられる。特に、Alを5質量%以上12質量%以下、Mnを0.1質量%以上2.0質量%以下含有することが好ましい。Al及びMnを上記範囲で含有することで、強度や伸びといった機械的特性に優れる上に、耐食性にも優れる。但し、上記元素の含有量が多過ぎると、塑性加工性の低下などを招く。Al,Mn以外の添加元素の含有量は、Zn:0.2~7.0質量%、Si:0.2~1.0質量%、Ca:0.2~6.0質量%、Sr:0.2~7.0質量%、Y:1.0~6.0質量%、Cu:0.2~3.0質量%、Ag:0.5~3.0質量%、Ce:0.05~1.0質量%、Zr:0.1~1.0質量%、RE(希土類元素(Y,Ceを除く)):1.0~3.5質量%が挙げられる。Al及びMnに加えて、これらの元素を含有することで、機械的特性を更に高められる。Al及びMnと、これらの元素の1種以上とを上記範囲で含有する合金の組成として、例えば、ASTM規格におけるAZ系合金(Mg-Al-Zn系合金、Zn:0.2~1.5質量%)、AM系合金(Mg-Al-Mn系合金、Mn:0.15~0.5質量%)などが挙げられる。特に、Alの含有量(以下、Al量と呼ぶ)が多いほど、機械的特性や耐食性に優れて好ましく、Al量が5.8質量%以上10質量%以下がより好ましい。Al量が5.8~10質量%のマグネシウム合金として、例えば、Mg-Al-Zn系合金では、AZ61合金、AZ80合金、AZ81合金、AZ91合金、Mg-Al-Mn系合金では、AM60合金、AM100合金などが好適な組成である。とりわけAl量が8.3~9.5質量%であるAZ91合金は、他のMg-Al系合金と比較して、耐食性や強度、耐塑性変形性といった機械的特性に更に優れる。
本発明合金板は、対向する一対の一面及び他面を具え、これらの二面は、代表的には、平行関係にあり、通常、使用場面において表裏の関係にある。これら一面及び他面は、平面でも曲面でもよい。これら一面と他面との間の距離がマグネシウム合金板の厚さとなる。本発明合金板は、上述のように厚さ5mm以下の鋳造板に圧延を施して得られることから、本発明合金板の厚さは、5mm未満である。特に、本発明合金板は、プレス加工といった塑性加工が施されて、薄く軽量な筐体や各種の部材の素材に利用されることから、当該合金板の厚さは、0.3mm~3mm程度、特に0.5mm以上2.0mm以下が好ましく、当該範囲において厚いほど、強度に優れ、薄いほど、薄型、軽量な筐体などに適する。所望の用途に応じて鋳造条件や圧延条件を調整して、最終的に得られるマグネシウム合金板の厚さを選択するとよい。
本発明合金板や本発明合金部材は、上述のように低温環境下であっても強度や伸びといった機械的特性に優れ、落下などの衝撃を受けた際にも凹み難い。例えば、-30℃における引張試験において、本発明合金板や本発明合金部材におけるプレス加工などの塑性加工に伴う変形(例えば、絞り加工による変形など)が実質的に施されていない平坦な箇所(素材の板とほぼ同様な箇所)は、引張強さ:350MPa以上、0.2%耐力:280MPa以上、伸び2%以上を有する。
<晶出物>
本発明合金板は、その表面側の領域から任意の小領域をとって組織観察を行った場合、粗大な晶出物が実質的に存在せず、微細な晶出物が僅かに存在する組織を有する。より具体的には、上記合金板の厚さ方向において、当該合金板の表面から当該合金板の厚さの30%までの領域を表面領域とし、この表面領域から任意に選択された50μm2の小領域をとり、一つの小領域に存在する全ての晶出物の粒径を測定する。そして、各晶出物の最大径を測定したとき、一つの小領域に対して、最大径が0.1μm以上1μm以下である微細な晶出物が15個以下である。最大径が0.5μm以下の晶出物しか存在しないことがより好ましい。1μm超の粗大な晶出物が存在すると、落下などの衝撃を受けたとき、この粗大な晶出物が割れなどの起点となり得るため、割れや亀裂が生じ易く、耐衝撃性が低い。また、最大径が1μm以下の晶出物であっても、50μm2に対して15個超存在すると、割れや亀裂の起点が多くなることで、強度の低下を招き、耐衝撃性が低くなる。最大径が0.1~1μmの晶出物の粒子が少ないほど耐衝撃性に優れる傾向にあり、10個以下がより好ましく、理想的には0個が望ましい。上記晶出物は、AlとMnの双方を含むものとする。最大径の測定方法の詳細は、後述する。なお、本発明では、割れの起因になり難いと考えられる極微細な晶出物、即ち、最大径が0.1μm未満の晶出物の存在を許容するが、上述のように晶出物は存在しない方が好ましい。
本発明合金板として、平均結晶粒径が小さく、20μm以下といった微細組織を有するものが挙げられる。上述のように特定の条件の連続鋳造を行うことで微細組織を有する鋳造板が得られ、このような鋳造板に圧延を施すことで、上記微細組織を有する圧延板とすることができる。このような微細組織を有する本発明合金板は、強度や伸びといった機械的特性にも優れ、低温環境下であっても耐衝撃性を高められる。また、上記微細組織を有するマグネシウム合金板や、この圧延板にレベラー処理などの矯正処理を行った処理板により得られた本発明合金部材も、平均結晶粒径が20μm以下の微細組織を有することができ、耐衝撃性に優れる。より好ましい平均結晶粒径は、0.1μm以上10μm以下である。
《鋳造》
本発明製造方法では、双ロール連続鋳造法を利用する。この鋳造において鋳型に利用するロールの温度を100℃以下、得られる鋳造板の厚さを5mm以下とする。このように鋳造板の厚さを薄く、かつロール温度を低くすることで、急冷凝固により上述のように晶出物の生成を抑制し、晶出物が小さくかつ少ない鋳造板とすることができる。ロール温度を100℃以下とするには、水冷などの強制冷却が可能なロールを利用することが挙げられる。ロール温度が低いほど、また、鋳造板の厚さが薄いほど、冷却速度を速めて晶出物の生成を抑制することができる。そのため、ロール温度は60℃以下、鋳造板の厚さは4.0mm以下がより好ましい。この鋳造工程(冷却工程も含む)は、マグネシウム合金の酸化などを防止するために、不活性ガス雰囲気で行うことが好ましい。
圧延条件は、例えば、素材の加熱温度:200~400℃、圧延ロールの加熱温度:150~300℃、1パスあたりの圧下率:5~50%が挙げられ、所望の厚さとなるように複数パス行うとよい。特許文献1に記載される制御圧延を利用してもよい。上記鋳造材に圧延を行うことで、鋳造の金属組織ではなく圧延組織などとすることができる。また、圧延を行うことで、平均結晶粒径が20μm以下の微細組織が得られ易く、かつ鋳造時の偏析や引け巣や空隙(ポア)といった内部欠陥、表面欠陥などを低減して、表面性状に優れた圧延板が得られる。最終の圧延後に最終熱処理を施して平均結晶粒径が20μm以下の微細な再結晶組織とすると、得られた圧延板の強度や耐食性を更に高め易い。
本発明合金部材は、上記圧延板(熱処理などを施したものも含む)に、所望の形状となるようにプレス加工(打ち抜きも含む)、深絞り加工、鍛造加工、ブロー加工、曲げ加工といった塑性加工を施すことで得られる。この塑性加工は、200~280℃の温間で行うと、圧延板の組織が粗大な再結晶組織となることを低減して、機械的特性や耐食性が劣化することを低減できる。上記塑性加工後に熱処理や防食処理を施したり、塗装層を形成してもよい。
[試験例1]
表1に示すマグネシウム合金からなるインゴット(いずれも市販)を用いて種々の条件でマグネシウム合金板やマグネシウム合金部材(筐体)を作製し、得られたマグネシウム合金板やマグネシウム合金部材の組織観察、引張試験(低温)、衝撃試験(低温)を行った。作製条件は以下の通りである。
マグネシウム合金のインゴットを不活性雰囲気中で700℃に加熱して溶湯を作製し、この溶湯を用いて上記不活性雰囲気中で双ロール連続鋳造法により、厚さ4.0mm(<5mm)の鋳造板を複数作製する。この鋳造は、ロール温度が60℃(<100℃)となるようにロールを冷却しながら行う。得られた各鋳造板を素材とし、素材の加熱温度:200~400℃、圧延ロールの加熱温度:150~300℃、1パスあたりの圧下率:5~50%の条件で、素材の厚さが0.6mmになるまで複数回圧延を施し、圧延板を作製する。得られた圧延板(マグネシウム合金板)を試料(板)とする。また、得られた圧延板に、加熱温度:250℃で角絞り加工を施して、断面[状の箱状体を作製し、この箱状体(マグネシウム合金部材)を試料(筐体)とする。
市販のダイキャスト品(断面[状の箱状体、底面部分の厚さ:0.6mm)である。
(条件C:市販板)
市販のAZ31合金からなる板(厚さ:0.6mm)である。
(条件D:市販筐体)
AZ31合金からなる板(厚さ:0.6mm)に角絞り加工が施された、断面[状の箱状体(底面部分の厚さ:0.6mm)である(市販品)。
得られた各試料について、以下のように金属組織を観察し、晶出物を調べた。試料(板)では、試料を板厚方向に切断し、その断面を透過型電子顕微鏡(20,000倍)で観察する。この観察像において、試料(板)の厚さ方向に、当該試料(板)の表面から当該試料(板)の厚さの30%(0.6mm×30%=0.18mm)までの領域を表面領域とする。この表面領域から、任意の50μm2の小領域を5箇所選択し、各小領域中に存在する全ての晶出物の大きさを測定する。晶出物の判定は、組成により行う。上記断面を鏡面研磨した後、例えば、EDXなどに代表される定性分析と半定量分析とを用いて断面に存在する粒子の組成が求められ、Al及びMnを含む粒子を晶出物とする。なお、Al及びMnを含む各晶出物の粒子についてAlの質量とMnの質量との比Al/Mnを測定したところ、試料No.1-1,1-2のいずれもAl/Mn=2~5であった。そして、上記断面における各晶出物の粒子について当該断面に平行な直線を引き、各粒子におけるこの直線を横断する長さの最大値をその粒子の最大径とし、最大径が0.1μm以上1μm以下の大きさの晶出物の数をその小領域の晶出物の数とし、5箇所の小領域の平均をこの試料の晶出物の数/50μm2とする。試料(筐体)では、試料において絞り変形を伴わない平坦な部分である底面部を板厚方向に切断して、その断面を上記試料(板)と同様に観察して、晶出物の数/50μm2を測定する。但し、上記観察像において最大径が5μm以上を超えるような粗大な晶出物が見られる場合、小領域の面積を200μm2とし、この200μm2内に存在する晶出物の最大径、及び晶出物の数/200μm2を測定する。なお、上記各小領域は、上述の各面積を満たせば、特に形状は問わないが、矩形状(代表的には正方形)などが利用し易い。測定結果を表1に示す。
各試料(厚さ:0.6mm)からJIS 13B号の板状試験片(JIS Z 2201(1998))を作製して、JIS Z 2241(1998)の金属材料引張試験方法に基づいて引張試験を行った。ここでは、試料(板)では、標点距離GL=50mmとし、試料(筐体)では、標点距離GL=15mmとし、いずれの試料も試験温度:-30℃、引張速度:5mm/minとして引張試験を行い、引張強さ(MPa)、0.2%耐力(MPa)、伸び(%)を測定した(評価数:いずれもn=1)。その結果を表1に示す。なお、試料(筐体)では、試料において絞り変形を伴わない平坦な部分である底面部から切り出して上記引張試験の試験片、及び後述する衝撃試験の試験片を作製している。
各試料から30mm×30mmの板片を切り出し、この切り出した板片を試験片とする。この試験では、図1に示すように、水平な面に直径d=20mmの円穴21を有する支持台20を用意した。円穴21の深さは後述する円柱棒10が十分に挿入可能な大きさとした。この円穴21を塞ぐように試験片1を配置し、この状態で、試験片1から高さ200mmの地点に、重量100g、先端r=5mm、セラミックス製の円柱棒10を、その中心軸と、円穴21の中心軸とが同軸となるように配置した。そして、試験片1に向けて、上記配置地点(高さ200mm)から円柱棒10を自由落下させた後、試験片1の凹み量を測定する。凹み量(mm)は、試験片1の対向する両辺を結ぶ直線をとり、この直線から最も凹んだ部分までの距離をポイントマイクロメータを用いて測定した。この衝撃試験は、-30℃の低温環境で行った。その結果を表1に示す。凹み量が0.5mm以下を○、0.5mm超を×と示し、割れが生じて凹み量を測定できなかった場合は、「割れ」と示し、クラック(亀裂)が生じた場合は、「クラック」と示す。なお、試料(筐体)において作製した上記30mm×30mmの試験片について、任意の4箇所の厚さを測定したところ、いずれの箇所も、素材の板の厚さ(厚さ0.6mm)に等しかった(試験片の厚さ:0.6mm)。
表2に示すマグネシウム合金からなるインゴット(いずれも市販)を用いて種々の条件でマグネシウム合金板やマグネシウム合金部材(筐体)を作製し、得られたマグネシウム合金板やマグネシウム合金部材の組織観察、衝撃試験(低温)を試験例1と同様に行った。その結果を表2に示す。
Claims (5)
- AlとMnとを含有するマグネシウム合金からなるマグネシウム合金板であって、
前記マグネシウム合金板の厚さ方向において、当該合金板の表面から当該合金板の厚さの30%までの領域を表面領域とし、この表面領域から任意の50μm2の小領域をとったとき、AlとMnとの双方を含む晶出物であって最大径が0.1μm以上1μm以下の粒子が15個以下であり、
前記晶出物の粒子は、Mnに対するAlの質量比:Al/Mnが2以上5以下であることを特徴とするマグネシウム合金板。 - 前記マグネシウム合金は、Alを5質量%以上12質量%以下、Mnを0.1質量%以上2.0質量%以下含有することを特徴とする請求項1に記載のマグネシウム合金板。
- 前記マグネシウム合金は、更に、Zn,Si,Ca,Sr,Y,Cu,Ag,Ce,Zr及び希土類元素(Y,Ceを除く)から選択された1種以上の元素を含むことを特徴とする請求項1又は2に記載のマグネシウム合金板。
- 請求項1~3のいずれか1項に記載のマグネシウム合金板に塑性加工を施してなることを特徴とするマグネシウム合金部材。
- AlとMnとを含有するマグネシウム合金を板状に鋳造する鋳造工程と、
前記鋳造工程により得られた鋳造板を圧延する圧延工程とを具え、
前記鋳造は、双ロール連続鋳造法により行い、ロール温度を100℃以下、前記鋳造板の厚さを5mm以下として行うことを特徴とするマグネシウム合金板の製造方法。
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BRPI1015407A BRPI1015407A2 (pt) | 2009-06-26 | 2010-06-08 | folha de liga de magnésio. |
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KR101080164B1 (ko) * | 2011-01-11 | 2011-11-07 | 한국기계연구원 | 발화저항성과 기계적 특성이 우수한 마그네슘 합금 및 그 제조방법 |
CN103866169B (zh) * | 2014-03-12 | 2016-03-09 | 苏州凯宥电子科技有限公司 | 一种室温高塑性变形镁合金及其制备方法 |
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Citations (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH06256883A (ja) * | 1993-03-04 | 1994-09-13 | Kobe Steel Ltd | 優れたクリープ強度を有するマグネシウム合金 |
JP2006144059A (ja) * | 2004-11-18 | 2006-06-08 | Mitsubishi Alum Co Ltd | プレス成形性に優れたマグネシウム合金板およびその製造方法 |
JP2006144043A (ja) * | 2004-11-17 | 2006-06-08 | Mitsubishi Alum Co Ltd | プレス成形性に優れたマグネシウム合金板の製造方法 |
JP2006144044A (ja) * | 2004-11-17 | 2006-06-08 | Mitsubishi Alum Co Ltd | 深絞り性に優れたマグネシウム合金板およびその製造方法 |
JP2006144062A (ja) * | 2004-11-18 | 2006-06-08 | Mitsubishi Alum Co Ltd | 微細な結晶粒を有するマグネシウム合金薄板の製造方法 |
JP2007098470A (ja) | 2005-03-28 | 2007-04-19 | Sumitomo Electric Ind Ltd | マグネシウム合金板の製造方法 |
JP2008163402A (ja) * | 2006-12-28 | 2008-07-17 | Mitsubishi Alum Co Ltd | マグネシウム合金薄板の製造方法 |
JP2008308703A (ja) * | 2007-06-12 | 2008-12-25 | Mitsubishi Alum Co Ltd | 連続鋳造圧延用マグネシウム合金およびマグネシウム合金材料の製造方法 |
WO2009001516A1 (ja) * | 2007-06-28 | 2008-12-31 | Sumitomo Electric Industries, Ltd. | マグネシウム合金板材 |
JP2009007606A (ja) * | 2007-06-27 | 2009-01-15 | Mitsubishi Alum Co Ltd | 耐食性及び表面処理性に優れるマグネシウム合金板材とその製造方法 |
JP2009120883A (ja) * | 2007-11-13 | 2009-06-04 | Mitsubishi Alum Co Ltd | マグネシウム合金箔およびその製造方法 |
Family Cites Families (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP4613965B2 (ja) * | 2008-01-24 | 2011-01-19 | 住友電気工業株式会社 | マグネシウム合金板材 |
JP5648885B2 (ja) * | 2009-07-07 | 2015-01-07 | 住友電気工業株式会社 | マグネシウム合金板、マグネシウム合金部材、及びマグネシウム合金板の製造方法 |
-
2009
- 2009-06-26 JP JP2009152849A patent/JP2011006754A/ja active Pending
-
2010
- 2010-06-08 US US13/381,009 patent/US20120100035A1/en not_active Abandoned
- 2010-06-08 WO PCT/JP2010/059710 patent/WO2010150651A1/ja active Application Filing
- 2010-06-08 EP EP10791969.8A patent/EP2447381A4/en not_active Withdrawn
- 2010-06-08 KR KR1020117029242A patent/KR20120031008A/ko active Search and Examination
- 2010-06-08 BR BRPI1015407A patent/BRPI1015407A2/pt not_active IP Right Cessation
- 2010-06-08 RU RU2012102620/02A patent/RU2012102620A/ru unknown
- 2010-06-08 CN CN201080028074.6A patent/CN102803533B/zh not_active Expired - Fee Related
- 2010-06-25 TW TW099120731A patent/TW201111521A/zh unknown
Patent Citations (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH06256883A (ja) * | 1993-03-04 | 1994-09-13 | Kobe Steel Ltd | 優れたクリープ強度を有するマグネシウム合金 |
JP2006144043A (ja) * | 2004-11-17 | 2006-06-08 | Mitsubishi Alum Co Ltd | プレス成形性に優れたマグネシウム合金板の製造方法 |
JP2006144044A (ja) * | 2004-11-17 | 2006-06-08 | Mitsubishi Alum Co Ltd | 深絞り性に優れたマグネシウム合金板およびその製造方法 |
JP2006144059A (ja) * | 2004-11-18 | 2006-06-08 | Mitsubishi Alum Co Ltd | プレス成形性に優れたマグネシウム合金板およびその製造方法 |
JP2006144062A (ja) * | 2004-11-18 | 2006-06-08 | Mitsubishi Alum Co Ltd | 微細な結晶粒を有するマグネシウム合金薄板の製造方法 |
JP2007098470A (ja) | 2005-03-28 | 2007-04-19 | Sumitomo Electric Ind Ltd | マグネシウム合金板の製造方法 |
JP2008163402A (ja) * | 2006-12-28 | 2008-07-17 | Mitsubishi Alum Co Ltd | マグネシウム合金薄板の製造方法 |
JP2008308703A (ja) * | 2007-06-12 | 2008-12-25 | Mitsubishi Alum Co Ltd | 連続鋳造圧延用マグネシウム合金およびマグネシウム合金材料の製造方法 |
JP2009007606A (ja) * | 2007-06-27 | 2009-01-15 | Mitsubishi Alum Co Ltd | 耐食性及び表面処理性に優れるマグネシウム合金板材とその製造方法 |
WO2009001516A1 (ja) * | 2007-06-28 | 2008-12-31 | Sumitomo Electric Industries, Ltd. | マグネシウム合金板材 |
JP2009120883A (ja) * | 2007-11-13 | 2009-06-04 | Mitsubishi Alum Co Ltd | マグネシウム合金箔およびその製造方法 |
Non-Patent Citations (1)
Title |
---|
See also references of EP2447381A4 * |
Also Published As
Publication number | Publication date |
---|---|
KR20120031008A (ko) | 2012-03-29 |
TW201111521A (en) | 2011-04-01 |
RU2012102620A (ru) | 2013-08-10 |
CN102803533A (zh) | 2012-11-28 |
EP2447381A4 (en) | 2016-03-09 |
CN102803533B (zh) | 2016-01-20 |
JP2011006754A (ja) | 2011-01-13 |
BRPI1015407A2 (pt) | 2016-08-09 |
EP2447381A1 (en) | 2012-05-02 |
US20120100035A1 (en) | 2012-04-26 |
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