WO2012115191A1 - Magnesium alloy and manufacturing method for same - Google Patents
Magnesium alloy and manufacturing method for same Download PDFInfo
- Publication number
- WO2012115191A1 WO2012115191A1 PCT/JP2012/054419 JP2012054419W WO2012115191A1 WO 2012115191 A1 WO2012115191 A1 WO 2012115191A1 JP 2012054419 W JP2012054419 W JP 2012054419W WO 2012115191 A1 WO2012115191 A1 WO 2012115191A1
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- Prior art keywords
- magnesium alloy
- plate
- region
- plane
- rolling
- Prior art date
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- 229910000861 Mg alloy Inorganic materials 0.000 title claims abstract description 127
- 238000004519 manufacturing process Methods 0.000 title claims abstract description 24
- 239000000463 material Substances 0.000 claims abstract description 122
- 239000000956 alloy Substances 0.000 claims abstract description 94
- 238000005096 rolling process Methods 0.000 claims abstract description 76
- 239000013078 crystal Substances 0.000 claims abstract description 43
- 238000000034 method Methods 0.000 claims description 22
- 239000000654 additive Substances 0.000 claims description 11
- 230000000996 additive effect Effects 0.000 claims description 11
- 238000005266 casting Methods 0.000 claims description 11
- 238000002441 X-ray diffraction Methods 0.000 claims description 7
- 238000002360 preparation method Methods 0.000 claims description 4
- 230000007797 corrosion Effects 0.000 abstract description 30
- 238000005260 corrosion Methods 0.000 abstract description 30
- 229910045601 alloy Inorganic materials 0.000 abstract description 26
- 239000011777 magnesium Substances 0.000 abstract description 8
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 abstract description 3
- 230000006866 deterioration Effects 0.000 abstract description 3
- 229910052749 magnesium Inorganic materials 0.000 abstract description 3
- 239000004033 plastic Substances 0.000 description 42
- 238000012545 processing Methods 0.000 description 31
- 238000010438 heat treatment Methods 0.000 description 23
- 239000000203 mixture Substances 0.000 description 10
- 238000011282 treatment Methods 0.000 description 9
- 238000009749 continuous casting Methods 0.000 description 8
- 238000012360 testing method Methods 0.000 description 8
- 238000012937 correction Methods 0.000 description 7
- 239000000243 solution Substances 0.000 description 7
- 238000005498 polishing Methods 0.000 description 6
- 239000002994 raw material Substances 0.000 description 6
- 230000007547 defect Effects 0.000 description 5
- 238000005452 bending Methods 0.000 description 4
- 238000001816 cooling Methods 0.000 description 4
- 238000005520 cutting process Methods 0.000 description 4
- 239000012535 impurity Substances 0.000 description 4
- 239000002244 precipitate Substances 0.000 description 4
- 229910052761 rare earth metal Inorganic materials 0.000 description 4
- 229910052727 yttrium Inorganic materials 0.000 description 4
- 229910052684 Cerium Inorganic materials 0.000 description 3
- 229910003023 Mg-Al Inorganic materials 0.000 description 3
- 238000004512 die casting Methods 0.000 description 3
- 238000003825 pressing Methods 0.000 description 3
- 238000005204 segregation Methods 0.000 description 3
- 238000004381 surface treatment Methods 0.000 description 3
- 229910052725 zinc Inorganic materials 0.000 description 3
- 229910018137 Al-Zn Inorganic materials 0.000 description 2
- 229910018573 Al—Zn Inorganic materials 0.000 description 2
- 206010013786 Dry skin Diseases 0.000 description 2
- 239000011248 coating agent Substances 0.000 description 2
- 239000011247 coating layer Substances 0.000 description 2
- 238000000576 coating method Methods 0.000 description 2
- 239000000470 constituent Substances 0.000 description 2
- 238000005336 cracking Methods 0.000 description 2
- 239000010410 layer Substances 0.000 description 2
- 239000000314 lubricant Substances 0.000 description 2
- 238000005259 measurement Methods 0.000 description 2
- 239000002245 particle Substances 0.000 description 2
- 229910052710 silicon Inorganic materials 0.000 description 2
- 229910052718 tin Inorganic materials 0.000 description 2
- 229910000674 AJ alloy Inorganic materials 0.000 description 1
- 229910018131 Al-Mn Inorganic materials 0.000 description 1
- 229910021364 Al-Si alloy Inorganic materials 0.000 description 1
- 229910018461 Al—Mn Inorganic materials 0.000 description 1
- 229910000549 Am alloy Inorganic materials 0.000 description 1
- 229910000882 Ca alloy Inorganic materials 0.000 description 1
- 229910001278 Sr alloy Inorganic materials 0.000 description 1
- 239000003082 abrasive agent Substances 0.000 description 1
- 230000002411 adverse Effects 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- 238000007743 anodising Methods 0.000 description 1
- 229910052790 beryllium Inorganic materials 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 238000005422 blasting Methods 0.000 description 1
- 229910052791 calcium Inorganic materials 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 229910052802 copper Inorganic materials 0.000 description 1
- 239000002989 correction material Substances 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 229910003460 diamond Inorganic materials 0.000 description 1
- 239000010432 diamond Substances 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005530 etching Methods 0.000 description 1
- 229910052737 gold Inorganic materials 0.000 description 1
- 238000000227 grinding Methods 0.000 description 1
- 238000005098 hot rolling Methods 0.000 description 1
- 230000010354 integration Effects 0.000 description 1
- 229910052744 lithium Inorganic materials 0.000 description 1
- 229910052748 manganese Inorganic materials 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 229910052759 nickel Inorganic materials 0.000 description 1
- 230000003287 optical effect Effects 0.000 description 1
- 230000008520 organization Effects 0.000 description 1
- 230000000149 penetrating effect Effects 0.000 description 1
- 239000000843 powder Substances 0.000 description 1
- 238000001556 precipitation Methods 0.000 description 1
- 230000002250 progressing effect Effects 0.000 description 1
- 150000003839 salts Chemical class 0.000 description 1
- 229910052709 silver Inorganic materials 0.000 description 1
- 239000006104 solid solution Substances 0.000 description 1
- 239000007921 spray Substances 0.000 description 1
- 239000007858 starting material Substances 0.000 description 1
- 238000005482 strain hardening Methods 0.000 description 1
- 229910052712 strontium Inorganic materials 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 230000003746 surface roughness Effects 0.000 description 1
- 238000010998 test method Methods 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
- 230000004580 weight loss Effects 0.000 description 1
- 238000004804 winding Methods 0.000 description 1
- 239000008207 working material Substances 0.000 description 1
- 229910052726 zirconium Inorganic materials 0.000 description 1
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
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D11/00—Continuous casting of metals, i.e. casting in indefinite lengths
- B22D11/001—Continuous casting of metals, i.e. casting in indefinite lengths of specific alloys
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D11/00—Continuous casting of metals, i.e. casting in indefinite lengths
- B22D11/06—Continuous casting of metals, i.e. casting in indefinite lengths into moulds with travelling walls, e.g. with rolls, plates, belts, caterpillars
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D11/00—Continuous casting of metals, i.e. casting in indefinite lengths
- B22D11/06—Continuous casting of metals, i.e. casting in indefinite lengths into moulds with travelling walls, e.g. with rolls, plates, belts, caterpillars
- B22D11/0622—Continuous casting of metals, i.e. casting in indefinite lengths into moulds with travelling walls, e.g. with rolls, plates, belts, caterpillars formed by two casting wheels
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D21/00—Casting non-ferrous metals or metallic compounds so far as their metallurgical properties are of importance for the casting procedure; Selection of compositions therefor
- B22D21/02—Casting exceedingly oxidisable non-ferrous metals, e.g. in inert atmosphere
- B22D21/04—Casting aluminium or magnesium
-
- 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
-
- 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 various members such as parts of transportation equipment such as automobiles, railway vehicles, airplanes, bicycle parts, casings of electronic / electric equipment, and other structural members, and magnesium alloy materials suitable for constituent materials of the members, And a manufacturing method thereof.
- it relates to a magnesium alloy material that is thick and excellent in corrosion resistance and rough skin resistance.
- a relatively thin plate material having a thickness of 1 mm or less has been studied as a material of a plastic work material such as a press work material, focusing on the light weight of a magnesium alloy.
- a plastic work material such as a press work material
- a thickness of 1.5 mm or more Is desired.
- a material such as a thick magnesium alloy plate, a manufacturing method thereof, and a plastic work material such as a press work material produced using the plate have not been sufficiently studied.
- a thick magnesium alloy plate can be obtained by using a die casting method or a thixo mold method.
- casting materials such as die-cast materials
- internal defects such as nests are likely to exist, and the composition and structure are not uniform, such as locally high concentrations of additive element components and random orientation of crystal grains. It is easy to become. Therefore, a cast material such as a die-cast material is inferior in corrosion resistance compared to a cast material such as a rolled material. Further, a cast material such as a die-cast material is inferior in plastic workability due to the above internal defects and cannot be said to be suitable for a material for plastic working.
- one of the objects of the present invention is to provide a magnesium alloy material that is thick and excellent in corrosion resistance and skin roughness resistance, and a thick magnesium alloy material that has been subjected to plastic working.
- Another object of the present invention is to provide a method for producing a magnesium alloy material from which a magnesium alloy material that is thick and excellent in corrosion resistance and rough skin resistance can be obtained.
- magnesium alloy materials that have been subjected to plastic processing are the same by reducing defects during casting and making crystals finer. Even with this composition, mechanical properties such as strength, hardness and toughness, corrosion resistance, and plastic workability are excellent.
- a magnesium alloy material obtained by subjecting the magnesium alloy material subjected to the primary processing to plastic processing (secondary processing) such as press working is also excellent in the mechanical characteristics and corrosion resistance.
- a continuous cast material produced by a continuous casting method such as a twin roll casting method
- the continuous cast material has less segregation and coarse crystal precipitates than a die cast material, Excellent plastic workability.
- the present inventors rolled the continuous cast material under various conditions to produce a thick magnesium alloy plate having a thickness of 1.5 mm or more.
- the magnesium alloy plate produced under specific conditions is thick and excellent in corrosion resistance, and when subjected to plastic working such as press working and bending, the resulting plastic working material has small irregularities on the surface.
- the present invention is based on the above findings.
- the magnesium alloy material of the present invention is made of a magnesium alloy, has a plate-like portion having a thickness of 1.5 mm or more, and the plate-like portion satisfies the following orientation.
- the area from the surface of the plate-shaped part to 1/4 of the thickness in the thickness direction is the surface area, the remaining area is the internal area,
- the X-ray diffraction peak intensities of the (002) plane, (100) plane, (101) plane, (102) plane, (110) plane, and (103) plane in the surface region are respectively I F (002), I F (100), I F (101), I F (102), I F (110), and I F (103),
- the peak intensities of X-ray diffraction of the (002) plane, (100) plane, (101) plane, (102) plane, (110) plane, and (103) plane in the internal region are I C (002), I C (100), I C (101), I C (102), I C (110), and I C (103) Orientation degree of (002) plane in the
- the said magnesium alloy material of this invention can be manufactured with the following this invention manufacturing method, for example.
- the method for producing a magnesium alloy material according to the present invention relates to a method for producing a magnesium alloy material by rolling a material made of a magnesium alloy, and includes the following preparation step and rolling step.
- Preparation step A step of preparing a plate-like material obtained by continuously casting a molten magnesium alloy by a twin roll casting method.
- Rolling step A step of producing a plate-like magnesium alloy material having a thickness of 1.5 mm or more by subjecting the material to rolling in a plurality of passes. In this rolling process, the rolling reduction of each of the above passes is 25% or less.
- the rolling reduction (%) refers to ⁇ (thickness t b of raw material before rolling ⁇ thickness t a of raw material after rolling) / thickness t b of raw material before rolling ⁇ ⁇ 100.
- the above-mentioned production method of the present invention it is possible to satisfactorily perform multiple passes of rolling by using a continuous casting material having few or substantially no defects, crystal precipitates, segregation as a starting point such as cracks, or the like. Can do.
- the surface portion of the rolled material is sufficiently subjected to plastic working by rolling as compared with the inside. That is, the surface structure and the internal structure of the rolled material can be made different by repeatedly performing rolling with a relatively small rolling reduction.
- a magnesium alloy material (typically a rolled plate (one form of the magnesium alloy material of the present invention) composed of a structure in which the structure constituting the surface region and the structure constituting the internal region are different. )) Is obtained. More specifically, the structure constituting the surface region is such that the bottom surface of the magnesium alloy crystal is parallel to the rolling direction (the direction in which the material to be rolled proceeds) by sufficiently applying plastic working by rolling.
- the texture is mainly arranged (texture arranged so that the c-axis of the crystal is orthogonal to the rolling direction), and the structure constituting the inner region is a structure in which the bottom surface is arranged at random than the surface region. .
- the surface region The texture having a specific orientation, more specifically, a texture in which the (002) plane, which is the bottom surface of the magnesium alloy crystal, is strongly oriented. (002) It is composed of a structure with little orientation of the plane.
- a texture in which (002) planes are strongly oriented is one of indices indicating that deformation accompanying plastic processing is sufficiently applied during plastic processing such as rolling. As the processing such as rolling is sufficiently performed, the crystal grain size of the magnesium alloy tends to become finer, and this refinement increases the total area of the crystal grain boundary.
- the magnesium alloy material of the present invention having the specific structure is excellent in corrosion resistance because the ratio of the impurity element to the crystal grain boundary is relatively lowered.
- the magnesium alloy material of the present invention is thick and excellent in corrosion resistance.
- the magnesium alloy material is composed of different structures in the surface portion and the inside as described above, and thus has different properties (hardness, strength, impact resistance, toughness and other mechanical properties). , Corrosion resistance, vibration control, etc.). Utilizing such a characteristic difference, the magnesium alloy material of the present invention can be expected to be used for various members and materials of these members.
- the magnesium alloy material of the present invention has good plastic workability such as press working and bending work because the degree of orientation of the bottom surface ((002) face) of the inner region is small (the degree of integration in the texture is small). Therefore, it can be suitably used for a material for plastic working such as press working or bending. And, since the surface region is composed of a fine crystal structure, even if plastic processing such as press processing is performed, large unevenness is hardly generated on the surface of the material, and the plastic processing material having a smooth surface (the magnesium alloy of the present invention) One form of the material is obtained. Therefore, the magnesium alloy material of the present invention is excellent in rough skin resistance. The obtained plastic work material also has excellent surface properties.
- the internal region with respect to the average crystal grain size D F of the surface region is The ratio of the average crystal grain diameter D c in the region: D c / D F satisfies 1.5 ⁇ D c / DF .
- the crystal grain size of the inner region is larger than the surface region, in other words, the crystal grain size of the surface region is sufficiently smaller than the inner region, so that the crystal grain boundary becomes longer as described above. Excellent corrosion resistance.
- the surface region is composed of a fine crystal structure, so that the plastic workability is good and the skin roughness resistance is excellent, and the crystal grain size of the inner region is larger than the surface region. Excellent heat resistance.
- the internal to the Vickers hardness H F of the surface region the ratio of the Vickers hardness H c region: H c / H F may include forms that meet the H c / H F ⁇ 0.85.
- the Vickers hardness of the inner region is smaller than that of the surface region, in other words, the Vickers hardness of the surface region is sufficiently larger than that of the inner region, so that the wear resistance is excellent.
- the magnesium alloy material of the present invention can be composed of magnesium alloys (remainder Mg and impurities) containing various elements as additive elements.
- alloys with high concentrations of additive elements specifically magnesium alloys with a total content of 5.0% by mass or more, depend on the type of additive elements, but mechanical properties such as strength and hardness, corrosion resistance, and flame resistance Excellent in various properties such as heat resistance.
- Specific additive elements are selected from Al, Zn, Mn, Si, Be, Ca, Sr, Y, Cu, Ag, Sn, Li, Zr, Ce, Ni, Au, and rare earth elements (excluding Y and Ce) And at least one element.
- the impurity include Fe.
- Mg-Al alloys containing Al are excellent in corrosion resistance and mechanical properties such as strength and hardness. Therefore, as an embodiment of the magnesium alloy material of the present invention, an embodiment in which the magnesium alloy contains 5.0% by mass or more and 12% by mass or less of Al as an additive element.
- the higher the Al content the higher the above effect tends to be.
- the upper limit is preferably 12% by mass, and more preferably 11% by mass.
- the form containing Al of 8.3 mass% to 9.5 mass% is superior in strength and corrosion resistance.
- the total content of each element other than Al is 0.01% by mass or more and 10% by mass or less, preferably 0.1% by mass or more and 5% by mass or less.
- Mg-Al alloy in ASTM standard (Mg-Al-Zn alloy, Zn: 0.2 mass% to 1.5 mass%, for example, AZ31 alloy, AZ61 alloy, AZ91 alloy Etc.), AM alloys (Mg-Al-Mn alloys, Mn: 0.15% to 0.5% by mass), AS alloys (Mg-Al-Si alloys, Si: 0.01% to 20% by mass), Mg -Al-RE (rare earth element) alloy, AX alloy (Mg-Al-Ca alloy, Ca: 0.2 mass% to 6.0 mass%), AJ alloy (Mg-Al-Sr alloy, Sr: 0.2 mass) % To 7.0% by mass).
- ASTM standard Mg-Al-Zn alloy, Zn: 0.2 mass% to 1.5 mass%
- AS alloys Mg-Al-Si alloys, Si: 0.01% to 20% by mass
- Mg -Al-RE rare earth element
- AX alloy Mg-Al-Ca alloy
- the magnesium alloy with the balance being Mg and impurities is excellent in heat resistance and flame retardancy.
- the rare earth element is contained, the total content is preferably 0.1% by mass or more, and particularly when Y is contained, the content is preferably 0.5% by mass or more.
- the magnesium alloy material of the present invention is thick and excellent in corrosion resistance and rough skin resistance.
- the production method of the magnesium alloy material of the present invention can produce a magnesium alloy material that is thick and excellent in corrosion resistance and rough skin resistance.
- the magnesium alloy material of the present invention is composed of a magnesium alloy containing 50% by mass or more of Mg and typically the additive elements described above.
- the plate-like portion provided in the magnesium alloy material of the present invention has a pair of parallel surfaces, and the interval between both surfaces (distance between both surfaces) is substantially uniform, that is, a portion where the thickness is uniform.
- the magnesium alloy material of the present invention has a plate-like part in a part thereof, the cutting process such as a form in which a boss is joined to the other part, a form having a groove, a form having a hole penetrating the front and back, etc.
- a typical form of the magnesium alloy material of the present invention having the above plate-like portion includes a form (magnesium alloy plate) that is entirely plate-like.
- the shape (planar shape) of the magnesium alloy plate can take various shapes such as a rectangle and a circle.
- this magnesium alloy plate can take any form of the coil material which wound up the continuous long material, and the short material of predetermined length and shape.
- This magnesium alloy plate can take various forms depending on the manufacturing process. Typically, a rolled plate, a heat-treated plate or a straightened plate subjected to heat treatment or correction described later, a rolled plate, a heat-treated plate, a polished plate obtained by polishing or coating the straightened plate, a coated plate, or the like can be given. .
- the magnesium alloy material of the present invention is a molded body obtained by subjecting the magnesium alloy sheet to plastic processing (secondary processing) such as press working such as bending or drawing, and the plastic working is partially applied to the plastic.
- plastic processing secondary processing
- Examples include a partially processed material having a processed part (however, at least a part of the plate-shaped part is included).
- the molded body is, for example, a cross-sectional box having a top plate portion (bottom surface portion) and a side wall portion erected from the periphery of the top plate portion, a frame-like frame body, and the top plate portion being a disc.
- a covered cylindrical body having a cylindrical side wall portion may be used. At least the top plate portion corresponds to a plate-like portion.
- the form of the magnesium alloy material can be selected.
- the plate-like portion has a thickness of 1.5 mm or more.
- the thickness an arbitrary value of 1.5 mm or more can be selected according to a desired application.
- the thickness is 10 mm or less, particularly 5 mm or less because a thick rolled plate (one form of the magnesium alloy material of the present invention) can be produced with high productivity.
- the portion where the deformation due to plastic processing is small is the structure of the magnesium alloy plate that is the material of the plastic processing. And generally maintain mechanical properties.
- the magnesium alloy material of the present invention is characterized in that at least the surface region of the plate-like portion is composed of a structure having the texture of the bottom surface as described above, and the internal region is composed of a structure having a small degree of orientation of the bottom surface.
- the corrosion resistance is excellent as described above. Further, it is expected that the corrosion resistance, the surface hardness, and the rough skin resistance can be improved as the difference in the degree of orientation between the surface region and the inner region increases.
- the ratio O F / O c of the above-mentioned bottom peak ratio satisfies the O F / O c ⁇ 1.2 Is preferred.
- ⁇ Average crystal grain size> In a typical form of the magnesium alloy material of the present invention, a form in which the crystal grain size of the internal region is larger than that of the surface region can be mentioned.
- the internal region is excellent in heat resistance, and the surface region having a relatively small crystal grain size has high corrosion resistance and high hardness as described above.
- the surface region has a relatively fine structure, it has high hardness and excellent wear resistance, so it is difficult to be scratched and has excellent surface properties. Therefore, it is expected that the magnesium alloy material of the present invention can be suitably used for structural materials that require durability. It is expected that the corrosion resistance, the rough skin resistance, and the surface hardness can be increased as the difference in the average crystal grain size between the surface region and the inner region is larger.
- the ratio of the above average crystal grain size D c / D F is D c / D F ⁇ 2.0 preferable.
- the particle size is uniform and fine throughout the entire thickness direction.
- the average crystal grain size in the surface region and the internal region can be 3.5 ⁇ m or more.
- the average crystal grain size of the surface region and the inner region of the plate-like part is preferably 20 ⁇ m or less, particularly preferably 10 ⁇ m or less.
- the average crystal grain size varies depending on the rolling reduction in the rolling process and the heating temperature of the material, and tends to be smaller as the rolling reduction is higher and the heating temperature is lower.
- the magnesium alloy material of the present invention is excellent in mechanical properties such as strength, hardness and toughness as compared with a cast material such as a die-cast material because of being rolled.
- the Vickers hardness of the surface region is higher than that of the internal region. The greater the difference in Vickers hardness between the surface region and the inner region, the higher the surface hardness.
- the ratio of Vickers hardness (Hv): H c / H F is 0.7 ⁇ H c / H F is preferred.
- the absolute value of the Vickers hardness depends on rolling conditions such as the rolling reduction and the heating temperature of the material, the absolute value of Vickers hardness tends to increase as the content of the additive element increases.
- the magnesium alloy material of the present invention is a plastically processed material (molded body) or a partially processed material, the hardness tends to further increase due to work hardening.
- the corrosion resistance is excellent. Moreover, if it is set as the form which provides a coating layer by coating at least one part of the surface of this invention magnesium alloy material, designability and commercial value can be improved.
- twin roll method there are various continuous casting methods such as a twin roll method, a twin belt method, and a belt-and-wheel method
- twin roll method and the twin belt method are suitable for the production of a plate-shaped cast material.
- the thickness, width, and length of the cast material can be appropriately selected so that a desired rolled material (rolled plate) can be obtained. Since the thickness of the cast material is likely to be segregated if it is too thick, it is preferably 10 mm or less, particularly preferably 5 mm or less.
- the obtained continuous cast material is a long material, it is easy to transport to the next step if it is wound into a cylindrical shape to form a coil material. If the part immediately before winding in the cast material is wound in a state heated to about 100 ° C to 200 ° C, the content of additive elements such as AZ91 alloy is high, and even an alloy type that is prone to cracking becomes easy to bend. Even when the take-up diameter is small, it can be wound up without causing cracks.
- a sheet material obtained by cutting the obtained continuous cast material into an appropriate length can be used as a rolling material. In this case, a rolled material (rolled sheet) having a predetermined length is obtained.
- the composition of the cast material can be homogenized or the toughness can be enhanced by sufficiently dissolving an element such as Al.
- the solution treatment conditions include heating temperature: 350 ° C. or higher, particularly 380 ° C. or higher and 420 ° C. or lower, holding time: 1 hour or longer and 40 hours or shorter.
- the holding time it is preferable that the holding time be longer as the Al content is higher.
- the cooling rate is increased (preferably 50 ° C./min or more), so that coarse precipitates Precipitation can be suppressed.
- the cast material or solution treatment material is used as a raw material, and this material is subjected to multiple passes of rolling. It is preferable that at least one pass includes warm rolling or hot rolling performed by heating a raw material (a cast material, a solution treatment material, a processed material during rolling) to 150 ° C. or more and 400 ° C. or less.
- a raw material a cast material, a solution treatment material, a processed material during rolling
- the heating temperature is preferably 350 ° C. or lower, more preferably 300 ° C. or lower, and particularly preferably 150 ° C. or higher and 280 ° C. or lower. You may heat not only a raw material but a rolling roll. Examples of the heating temperature of the rolling roll include 100 ° C. to 250 ° C.
- the rolling reduction rate of each pass is 25% or less.
- the rolling reduction ratio of each pass can be selected as appropriate within a range of 25% or less, but if it is too small, the number of passes until the desired thickness is increased, resulting in a decrease in productivity. Is preferred.
- Conditions such as the heating temperature of the material, the temperature of the rolling roll, and the rolling reduction can be changed for each pass. Therefore, the rolling reduction rate of each pass may be the same or different.
- intermediate heat treatment may be performed between passes. By performing the intermediate heat treatment, it is possible to remove and reduce distortions, residual stresses, and the like introduced into the material before the heat treatment, and to easily perform rolling after the heat treatment.
- the conditions for the intermediate heat treatment include heating temperature: 150 ° C. to 350 ° C. (preferably 300 ° C. or less, more preferably 250 ° C. to 280 ° C., holding time: 0.5 hour to 3 hours).
- the frictional resistance during rolling can be reduced, and the material can be prevented from being seized and easily rolled.
- edge of the cast material before rolling may be trimmed to prevent the crack from progressing when the edge is cracked during rolling. You may trim in order to adjust suitably.
- polishing it is possible to remove and reduce the lubricant used during rolling, scratches and oxide films present on the surface of the rolled material, and the like.
- polishing it is preferable to use a grinding belt because it can be easily and continuously polished even if the material is a long material.
- the polishing is preferably wet in order to prevent the powder from scattering.
- ⁇ Correction ⁇ Correction may be performed after the rolling or after the polishing. By performing the correction, the flatness can be improved, and plastic processing such as press processing can be performed with high accuracy.
- a roll leveler device in which a plurality of rollers are arranged in a staggered manner can be suitably used. The correction may be performed, for example, in a state where the material is heated to 100 ° C. to 300 ° C., particularly 150 ° C. to 280 ° C. (warm correction).
- the magnesium alloy material of the present invention is a partially processed material having a molded body or a plastic processing portion, at least a part of the material that has undergone the rolling process described above (rolled material, abrasive material, correction material described above) and so on. It can be manufactured by a manufacturing method including a plastic processing step for performing plastic processing.
- This plastic working is preferably performed at a temperature range of 200 ° C. to 300 ° C., because the plastic workability of the material is improved.
- heat treatment can be performed after the plastic working to remove strain and residual stress introduced by the plastic working and to improve the mechanical characteristics.
- the heat treatment conditions include a heating temperature: 100 ° C. to 300 ° C. and a heating time: about 5 minutes to 60 minutes.
- the magnesium alloy material of the present invention is provided with the anticorrosion layer and the coating layer, at least a part of the material that has undergone the rolling process described above, or at least a part of the material that has undergone the plastic working process, It can manufacture by the manufacturing method which comprises the surface treatment process which performs.
- at least one kind of processing selected from hairline processing, diamond cutting processing, shot blasting processing, etching processing, and spin cutting processing may be applied to at least a part of the material.
- Test example A material composed of a magnesium alloy having the following composition was rolled under various conditions to produce a magnesium alloy plate having a thickness of 1.5 mm or more, and the orientation, crystal grain size, and Vickers hardness were examined.
- magnesium alloy of the above composition create a long cast plate (thickness 4.5mm (4.50mm to 4.51mm) x width 320mm) by twin-roll continuous casting method, and wind it up once to obtain the cast coil material. Produced.
- Each cast coil material was subjected to a solution treatment at 400 ° C. for 24 hours.
- the material obtained by rewinding the solid solution coil material that has undergone solution treatment is rolled in multiple passes under the rolling conditions shown in Table 1, and rolled material with a thickness of 2.0 mm (2.00 mm to 2.01 mm) or 1.5 mm (magnesium) Alloy plate) was prepared.
- Each pass was warm-rolled (material heating temperature: 250 ° C to 280 ° C, rolling roll temperature: 100 ° C to 250 ° C).
- the thickness of the cast material, the thickness of the processed material in the middle of rolling, and the thickness of the obtained magnesium alloy plate are all 50 mm from the center in the width direction of the plate to be measured and both edges in the width direction. It was set as the average of the thickness of a total of three points.
- the average crystal grain size ( ⁇ m) of the inner region and the surface region was measured based on “steel—microscopic test method of crystal grain size JIS G 0551 (2005)”.
- a cross section in the thickness direction is taken for each magnesium alloy plate, each cross section is observed with an optical microscope (400 times), and the surface region in each cross section (from the surface to the thickness direction) 3 areas (up to 1/4 of the thickness) and internal areas (remaining areas excluding the surface area), 3 fields of view (total number of fields of view: 6), average grain size for each field of view Asked.
- Table 2 shows the average value (D F ) of the average crystal grain size of a total of six views in the surface region and the average value (D C ) of the average crystal grain size of a total of six views in the internal region. Further, the ratio of the average crystal grain size D c in the inner region to the average crystal grain size D F in the surface region: D c / DF was also obtained. The results are shown in Table 2.
- the continuous cast material is rolled with a rolling reduction of 25% or less per pass over multiple passes, so that a magnesium alloy plate with a thickness of 1.5 mm or more (magnesium It can be seen that an alloy material) having an internal region structure (bottom peak ratio) and a surface region structure (bottom peak ratio) in the thickness direction is different. It can also be seen that this magnesium alloy plate has different mechanical properties in the internal region and in the surface region.
- the above-described embodiment can be appropriately changed 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 thickness and shape of the magnesium alloy material, the rolling reduction of each pass in the rolling process, the number of passes, and the like can be changed as appropriate.
- the magnesium alloy material of the present invention is a member of various fields in which corrosion resistance and wear resistance are particularly desired, such as automobile parts, railway vehicle parts, aircraft parts, bicycle parts, parts of various electronic and electrical devices, and the like. It can be suitably used as a constituent material, a bag, or the like.
- the manufacturing method of this invention magnesium alloy material can be utilized suitably for manufacture of the said this invention magnesium alloy material.
Abstract
Description
[配向性]
上記板状部の表面から厚さ方向に厚さの1/4までの領域を表面領域、残部の領域を内部領域とし、
上記表面領域における(002)面、(100)面、(101)面、(102)面、(110)面、及び(103)面のX線回折のピーク強度をそれぞれIF(002)、IF(100)、IF(101)、IF(102)、IF(110)、及びIF(103)とし、
上記内部領域における(002)面、(100)面、(101)面、(102)面、(110)面、及び(103)面のX線回折のピーク強度をそれぞれIC(002)、IC(100)、IC(101)、IC(102)、IC(110)、及びIC(103)とし、
上記表面領域における(002)面の配向度合い:IF(002)/{IF(100)+IF(002)+IF(101)+IF(102)+IF(110)+IF(103)}を底面ピーク比OF、
上記内部領域における(002)面の配向度合い:IC(002)/{IC(100)+IC(002)+IC(101)+IC(102)+IC(110)+IC(103)}を底面ピーク比OCとするとき、
上記内部領域の底面ピーク比Ocに対する上記表面領域の底面ピーク比OFの比率:OF/Ocが、1.05<OF/Ocを満たす。 The magnesium alloy material of the present invention is made of a magnesium alloy, has a plate-like portion having a thickness of 1.5 mm or more, and the plate-like portion satisfies the following orientation.
[Orientation]
The area from the surface of the plate-shaped part to 1/4 of the thickness in the thickness direction is the surface area, the remaining area is the internal area,
The X-ray diffraction peak intensities of the (002) plane, (100) plane, (101) plane, (102) plane, (110) plane, and (103) plane in the surface region are respectively I F (002), I F (100), I F (101), I F (102), I F (110), and I F (103),
The peak intensities of X-ray diffraction of the (002) plane, (100) plane, (101) plane, (102) plane, (110) plane, and (103) plane in the internal region are I C (002), I C (100), I C (101), I C (102), I C (110), and I C (103)
Orientation degree of (002) plane in the surface region: I F (002) / { I F (100) + I F (002) + I F (101) + I F (102) + I F (110) + I F (103)} a bottom peak ratio O F,
Orientation degree of (002) plane in the internal region: I C (002) / {I C (100) + I C (002) + I C (101) + I C (102) + I C (110) + I C (103)} when the the bottom peak ratio O C,
The ratio of the bottom peak ratio O F of the surface area relative to the bottom surface peak ratio O c of the internal region: O F / O c satisfies the 1.05 <O F / O c.
準備工程:溶解したマグネシウム合金を双ロール鋳造法により連続鋳造した板状の素材を準備する工程。
圧延工程:上記素材に複数パスの圧延を施して、厚さ1.5mm以上の板状のマグネシウム合金材を製造する工程。
この圧延工程では、上記各パスの圧下率をいずれも25%以下とする。
なお、圧下率(%)とは、{(圧延前素材の厚さtb-圧延後の素材の厚さta)/圧延前素材の厚さtb}×100をいう。 The said magnesium alloy material of this invention can be manufactured with the following this invention manufacturing method, for example. The method for producing a magnesium alloy material according to the present invention relates to a method for producing a magnesium alloy material by rolling a material made of a magnesium alloy, and includes the following preparation step and rolling step.
Preparation step: A step of preparing a plate-like material obtained by continuously casting a molten magnesium alloy by a twin roll casting method.
Rolling step: A step of producing a plate-like magnesium alloy material having a thickness of 1.5 mm or more by subjecting the material to rolling in a plurality of passes.
In this rolling process, the rolling reduction of each of the above passes is 25% or less.
The rolling reduction (%) refers to {(thickness t b of raw material before rolling−thickness t a of raw material after rolling) / thickness t b of raw material before rolling} × 100.
[マグネシウム合金材]
(組成)
本発明マグネシウム合金材は、50質量%以上のMgと、代表的には上述した添加元素とを含有するマグネシウム合金により構成される。 Hereinafter, the present invention will be described in more detail.
[Magnesium alloy material]
(composition)
The magnesium alloy material of the present invention is composed of a magnesium alloy containing 50% by mass or more of Mg and typically the additive elements described above.
本発明マグネシウム合金材に具える板状部とは、平行する一対の面を具え、両面の間隔(両面の間の距離)が実質的に均一である、即ち、厚さが均一である部分を言う。本発明マグネシウム合金材は、その一部に板状部を有していれば、その他部に、ボスなどが接合された形態、溝を有する形態、表裏に貫通する孔を有する形態など、切削加工などの加工により、局所的に厚さが異なる部分を有する形態を許容する。 (Form)
The plate-like portion provided in the magnesium alloy material of the present invention has a pair of parallel surfaces, and the interval between both surfaces (distance between both surfaces) is substantially uniform, that is, a portion where the thickness is uniform. To tell. If the magnesium alloy material of the present invention has a plate-like part in a part thereof, the cutting process such as a form in which a boss is joined to the other part, a form having a groove, a form having a hole penetrating the front and back, etc. The form which has the part from which thickness differs locally by processing, such as is permitted.
本発明マグネシウム合金材は、上記板状部の厚さが1.5mm以上であることを特徴の一つとする。この厚さは、所望の用途などに応じて、1.5mm以上の任意の値を選択することができる。但し、上記板状部を厚くするには、素材となる鋳造材も厚くする必要がある。鋳造材を厚くすると、上述のように欠陥などで圧延性の低下を招く。従って、上記厚さは10mm以下、特に5mm以下であると、肉厚の圧延板(本発明マグネシウム合金材の一形態)を生産性よく製造できて好ましい。 (thickness)
One feature of the magnesium alloy material of the present invention is that the plate-like portion has a thickness of 1.5 mm or more. As the thickness, an arbitrary value of 1.5 mm or more can be selected according to a desired application. However, in order to increase the thickness of the plate-shaped portion, it is necessary to increase the thickness of the casting material. When the cast material is thickened, the rolling property is deteriorated due to defects as described above. Therefore, it is preferable that the thickness is 10 mm or less, particularly 5 mm or less because a thick rolled plate (one form of the magnesium alloy material of the present invention) can be produced with high productivity.
<配向性>
本発明マグネシウム合金材は、少なくとも上記板状部の表面領域が上述のように底面の集合組織を有する組織により構成され、内部領域は底面の配向度合いが小さい組織から構成されることを特徴の一つとする。外部雰囲気に曝される表面領域が、(002)面が強く配向した組織により構成されることで上述のように耐食性に優れる。また、表面領域と内部領域とにおいて配向度合いの差が大きいほど、耐食性や表面硬度、耐肌荒れ性を高められると期待される。但し、上記配向度合いの差が大きくなり過ぎると、プレス加工といった塑性加工を均一的に施し難くなるため、上述した底面ピーク比の比率OF/OcはOF/Oc≦1.2を満たすことが好ましい。 (Organization)
<Orientation>
The magnesium alloy material of the present invention is characterized in that at least the surface region of the plate-like portion is composed of a structure having the texture of the bottom surface as described above, and the internal region is composed of a structure having a small degree of orientation of the bottom surface. I will. Since the surface region exposed to the external atmosphere is composed of a structure in which the (002) plane is strongly oriented, the corrosion resistance is excellent as described above. Further, it is expected that the corrosion resistance, the surface hardness, and the rough skin resistance can be improved as the difference in the degree of orientation between the surface region and the inner region increases. However, when the difference between the orientation degree is too large, it becomes difficult subjected to plastic working such as press working uniform, the ratio O F / O c of the above-mentioned bottom peak ratio satisfies the O F / O c ≦ 1.2 Is preferred.
本発明マグネシウム合金材の代表的な形態では、内部領域の結晶粒径が表面領域よりも大きい形態が挙げられる。この形態は、内部領域が耐熱性に優れ、結晶粒径が相対的に小さい表面領域が上述のように高い耐食性や高い硬度を有する。特に、表面領域が相対的に微細組織であることで、高硬度になり、耐摩耗性に優れることから、キズなどがつき難く、表面性状に優れる。そのため、本発明マグネシウム合金材は、耐久性が求められる構造材などに好適に利用できると期待される。表面領域と内部領域とにおいて平均結晶粒径の差が大きいほど、耐食性や耐肌荒れ性、表面硬度を高められると期待される。但し、上記平均結晶粒径の差が大きくなると、プレス加工といった塑性加工を均一的に施し難くなるため、上述した平均結晶粒径の比率:Dc/DFはDc/DF≦2.0が好ましい。 <Average crystal grain size>
In a typical form of the magnesium alloy material of the present invention, a form in which the crystal grain size of the internal region is larger than that of the surface region can be mentioned. In this form, the internal region is excellent in heat resistance, and the surface region having a relatively small crystal grain size has high corrosion resistance and high hardness as described above. In particular, since the surface region has a relatively fine structure, it has high hardness and excellent wear resistance, so it is difficult to be scratched and has excellent surface properties. Therefore, it is expected that the magnesium alloy material of the present invention can be suitably used for structural materials that require durability. It is expected that the corrosion resistance, the rough skin resistance, and the surface hardness can be increased as the difference in the average crystal grain size between the surface region and the inner region is larger. However, when the difference in the average crystal grain size becomes large, it becomes difficult to uniformly perform plastic working such as press working. Therefore, the ratio of the above average crystal grain size: D c / D F is D c / D F ≦ 2.0 preferable.
本発明マグネシウム合金材は、圧延が施されていることでダイカスト材などの鋳造材に比較して、強度や硬度、靭性などの機械的特性にも優れる。例えば、上述のように表面領域のビッカース硬度が内部領域よりも高い。表面領域と内部領域とにおいてビッカース硬度の差が大きいほど、表面硬度が相対的に高くなる。但し、上記ビッカース硬度の差が大きくなり過ぎる(表面硬度を大きくし過ぎる)と、逆にプレス加工性を損ねるため、ビッカース硬度(Hv)の比率:Hc/HFは0.7≦Hc/HFが好ましい。ビッカース硬度の絶対値は、圧下率や素材の加熱温度などの圧延条件にもよるが、添加元素の含有量が多いほど、大きくなる傾向にある。本発明マグネシウム合金材が塑性加工材(成形体)や部分加工材である場合、加工硬化により、硬度が更に高まる傾向にある。 (Mechanical properties)
The magnesium alloy material of the present invention is excellent in mechanical properties such as strength, hardness and toughness as compared with a cast material such as a die-cast material because of being rolled. For example, as described above, the Vickers hardness of the surface region is higher than that of the internal region. The greater the difference in Vickers hardness between the surface region and the inner region, the higher the surface hardness. However, if the above Vickers hardness difference is too large (surface hardness is too large), press workability is adversely affected, so the ratio of Vickers hardness (Hv): H c / H F is 0.7 ≦ H c / H F is preferred. Although the absolute value of the Vickers hardness depends on rolling conditions such as the rolling reduction and the heating temperature of the material, the absolute value of Vickers hardness tends to increase as the content of the additive element increases. When the magnesium alloy material of the present invention is a plastically processed material (molded body) or a partially processed material, the hardness tends to further increase due to work hardening.
本発明マグネシウム合金材の表面の少なくとも一部に化成処理や陽極酸化処理といった防食処理を施して防食層を具える形態とすると、耐食性により優れる。また、本発明マグネシウム合金材の表面の少なくとも一部に塗装を施して塗装層とを具える形態とすると、意匠性や商品価値を高められる。 (Other configurations)
If the anticorrosive treatment such as chemical conversion treatment or anodizing treatment is performed on at least a part of the surface of the magnesium alloy material of the present invention to provide an anticorrosion layer, the corrosion resistance is excellent. Moreover, if it is set as the form which provides a coating layer by coating at least one part of the surface of this invention magnesium alloy material, designability and commercial value can be improved.
以下、上述した本発明製造方法の各工程をより詳細に説明する。
(準備工程)
<鋳造>
本発明製造方法では、出発材に連続鋳造材を利用する。連続鋳造法は、急冷凝固が可能であるため、添加元素の含有量が多い場合でも偏析や酸化物などを低減でき、割れの起点になり得る10μm超といった粗大な晶析出物の生成を抑制できる。従って、圧延などの塑性加工性に優れる鋳造材が得られる。また、連続鋳造法では、長尺な鋳造材を連続して製造可能であり、当該連続鋳造法によって得られた長尺材を圧延の素材に利用できる。素材が長尺である場合、長尺な圧延材を製造可能である。連続鋳造法には、双ロール法、ツインベルト法、ベルトアンドホイール法といった種々の方法があるが、板状の鋳造材の製造には、双ロール法やツインベルト法、特に双ロール法が好適であり、とりわけ特許文献1に記載の鋳造方法で製造した連続鋳造材を利用することが好ましい。鋳造材の厚さ、幅、長さは所望の圧延材(圧延板)が得られるように適宜選択することができる。鋳造材の厚さは、厚過ぎると偏析が生じ易いため、10mm以下、特に5mm以下が好ましい。得られた連続鋳造材を長尺材とする場合、円筒状に巻き取ってコイル材とすると、次工程に搬送し易い。鋳造材における巻き取り直前の箇所を100℃~200℃程度に加熱した状態で巻き取ると、AZ91合金といった添加元素の含有量が高く、割れが生じ易い合金種であっても曲げ易くなり、巻き取り径が小さい場合でも、割れなどを生じることなく巻き取れる。得られた連続鋳造材を適宜な長さに切断したシート材を圧延の素材とすることもできる。この場合、所定の長さの圧延材(圧延板)が得られる。 [Production method]
Hereafter, each process of the manufacturing method of this invention mentioned above is demonstrated in detail.
(Preparation process)
<Casting>
In the production method of the present invention, a continuous casting material is used as a starting material. Since the continuous casting method can be rapidly solidified, segregation and oxides can be reduced even when the content of additive elements is large, and the formation of coarse crystal precipitates exceeding 10 μm that can be the starting point of cracking can be suppressed. . Therefore, a cast material excellent in plastic workability such as rolling can be obtained. In the continuous casting method, a long cast material can be continuously produced, and the long material obtained by the continuous casting method can be used as a rolling material. When the material is long, a long rolled material can be manufactured. There are various continuous casting methods such as a twin roll method, a twin belt method, and a belt-and-wheel method, but the twin roll method and the twin belt method, particularly the twin roll method are suitable for the production of a plate-shaped cast material. In particular, it is preferable to use a continuous cast material produced by the casting method described in Patent Document 1. The thickness, width, and length of the cast material can be appropriately selected so that a desired rolled material (rolled plate) can be obtained. Since the thickness of the cast material is likely to be segregated if it is too thick, it is preferably 10 mm or less, particularly preferably 5 mm or less. When the obtained continuous cast material is a long material, it is easy to transport to the next step if it is wound into a cylindrical shape to form a coil material. If the part immediately before winding in the cast material is wound in a state heated to about 100 ° C to 200 ° C, the content of additive elements such as AZ91 alloy is high, and even an alloy type that is prone to cracking becomes easy to bend. Even when the take-up diameter is small, it can be wound up without causing cracks. A sheet material obtained by cutting the obtained continuous cast material into an appropriate length can be used as a rolling material. In this case, a rolled material (rolled sheet) having a predetermined length is obtained.
上記鋳造材に圧延を施す前に溶体化処理を施すと、鋳造材の組成を均質化したり、Alといった元素を十分に固溶させて靭性を高めたりできる。溶体化処理の条件は、例えば、加熱温度:350℃以上、特に380℃以上420℃以下、保持時間:1時間以上40時間以下が挙げられる。Mg-Al系合金である場合、Alの含有量が多いほど保持時間を長めにすることが好ましい。また、上記保持時間経過後、上記加熱温度からの冷却工程において、水冷や衝風といった強制冷却などを利用して、冷却速度を速めると(好ましくは50℃/min以上)、粗大な析出物の析出を抑制できる。 <Solution>
When the solution treatment is performed before rolling the cast material, the composition of the cast material can be homogenized or the toughness can be enhanced by sufficiently dissolving an element such as Al. Examples of the solution treatment conditions include heating temperature: 350 ° C. or higher, particularly 380 ° C. or higher and 420 ° C. or lower, holding time: 1 hour or longer and 40 hours or shorter. In the case of an Mg—Al-based alloy, it is preferable that the holding time be longer as the Al content is higher. Further, after the holding time has elapsed, in the cooling process from the heating temperature, using forced cooling such as water cooling or blast, the cooling rate is increased (preferably 50 ° C./min or more), so that coarse precipitates Precipitation can be suppressed.
上記鋳造材や溶体化処理材を素材とし、この素材に複数パスの圧延を施す。少なくとも1パスは、素材(鋳造材や溶体化処理材、圧延途中の加工材)を150℃以上400℃以下に加熱して行う温間圧延、或いは熱間圧延を含むことが好ましい。素材を上記温度に加熱することで、1パスあたりの圧下率を高めた場合にも圧延中に割れなどが生じ難く、上記温度を高めるほど、割れなどが少なくなり、400℃以下とすることで、素材表面の焼付きなどによる劣化や、圧延ロールの熱劣化を抑制することができる。従って、上記加熱温度は、350℃以下、更に300℃以下、特に150℃以上280℃以下が好ましい。素材だけでなく圧延ロールも加熱してもよい。圧延ロールの加熱温度は、100℃~250℃が挙げられる。 <Rolling>
The cast material or solution treatment material is used as a raw material, and this material is subjected to multiple passes of rolling. It is preferable that at least one pass includes warm rolling or hot rolling performed by heating a raw material (a cast material, a solution treatment material, a processed material during rolling) to 150 ° C. or more and 400 ° C. or less. By heating the material to the above temperature, even when the rolling reduction per pass is increased, cracks and the like are less likely to occur during rolling, and the higher the temperature, the less the cracks, etc. Deterioration due to seizure of the material surface and thermal deterioration of the rolling roll can be suppressed. Therefore, the heating temperature is preferably 350 ° C. or lower, more preferably 300 ° C. or lower, and particularly preferably 150 ° C. or higher and 280 ° C. or lower. You may heat not only a raw material but a rolling roll. Examples of the heating temperature of the rolling roll include 100 ° C. to 250 ° C.
≪研磨≫
上記圧延後、研磨を施してもよい。研磨を行うことで、圧延時に使用した潤滑剤や圧延材表面に存在するキズや酸化膜などを除去、低減できる。研磨には、研削ベルトを用いると、素材が長尺材であっても、連続して容易に研磨を施せて好ましい。また、研磨は、粉末の飛散を防止するために湿式が好ましい。 <Other processing>
≪Polishing≫
You may grind | polish after the said rolling. By polishing, it is possible to remove and reduce the lubricant used during rolling, scratches and oxide films present on the surface of the rolled material, and the like. For the polishing, it is preferable to use a grinding belt because it can be easily and continuously polished even if the material is a long material. The polishing is preferably wet in order to prevent the powder from scattering.
上記圧延後や上記研磨後、矯正を施してもよい。矯正を行うことで平坦性を高められ、プレス加工などの塑性加工を精度良く行える。矯正には、複数のローラが千鳥状に配置されたロールレベラ装置を好適に利用できる。また、矯正は、例えば、素材を100℃~300℃、特に150℃~280℃に加熱した状態(温間矯正)で行ってもよい。 ≪Correction≫
Correction may be performed after the rolling or after the polishing. By performing the correction, the flatness can be improved, and plastic processing such as press processing can be performed with high accuracy. For correction, a roll leveler device in which a plurality of rollers are arranged in a staggered manner can be suitably used. The correction may be performed, for example, in a state where the material is heated to 100 ° C. to 300 ° C., particularly 150 ° C. to 280 ° C. (warm correction).
上記本発明マグネシウム合金材を成形体や塑性加工部を具える部分加工材とする場合、上述した圧延工程を経た素材(上述した圧延材、研磨材、矯正材)の少なくとも一部にプレス加工といった塑性加工を施す塑性加工工程を具える製造方法により、製造することができる。この塑性加工は、200℃~300℃の温度域で行うと、素材の塑性加工性を高められて好ましい。また、この塑性加工後に熱処理を施して、塑性加工により導入された歪みや残留応力の除去、機械的特性の向上を図ることができる。この熱処理条件は、加熱温度:100℃~300℃、加熱時間:5分~60分程度が挙げられる。 ≪Plastic processing≫
When the magnesium alloy material of the present invention is a partially processed material having a molded body or a plastic processing portion, at least a part of the material that has undergone the rolling process described above (rolled material, abrasive material, correction material described above) and so on. It can be manufactured by a manufacturing method including a plastic processing step for performing plastic processing. This plastic working is preferably performed at a temperature range of 200 ° C. to 300 ° C., because the plastic workability of the material is improved. In addition, heat treatment can be performed after the plastic working to remove strain and residual stress introduced by the plastic working and to improve the mechanical characteristics. The heat treatment conditions include a heating temperature: 100 ° C. to 300 ° C. and a heating time: about 5 minutes to 60 minutes.
上記本発明マグネシウム合金材を上記防食層や塗装層を具える形態とする場合、上述した圧延工程を経た素材の少なくとも一部、或いは上記塑性加工工程を経た素材の少なくとも一部に防食処理や塗装を施す表面処理工程を具える製造方法により、製造することができる。その他、上記素材の少なくとも一部に、ヘアライン加工、ダイヤカット加工、ショットブラスト加工、エッチング加工及びスピンカット加工から選択される少なくとも1種の加工を施してもよい。これらの表面処理を行うことで、耐食性や機械的保護機能を高めたり、意匠性や金属質感、商品価値を高めたりすることができる。 ≪Surface treatment≫
When the magnesium alloy material of the present invention is provided with the anticorrosion layer and the coating layer, at least a part of the material that has undergone the rolling process described above, or at least a part of the material that has undergone the plastic working process, It can manufacture by the manufacturing method which comprises the surface treatment process which performs. In addition, at least one kind of processing selected from hairline processing, diamond cutting processing, shot blasting processing, etching processing, and spin cutting processing may be applied to at least a part of the material. By performing these surface treatments, corrosion resistance and mechanical protection functions can be improved, and design properties, metal texture, and commercial value can be increased.
[試験例]
以下の組成のマグネシウム合金からなる素材に、種々の条件で圧延を施して厚さ1.5mm以上のマグネシウム合金板を作製し、配向性、結晶粒径、及びビッカース硬度を調べた。 Hereinafter, more specific embodiments of the present invention will be described with reference to test examples.
[Test example]
A material composed of a magnesium alloy having the following composition was rolled under various conditions to produce a magnesium alloy plate having a thickness of 1.5 mm or more, and the orientation, crystal grain size, and Vickers hardness were examined.
得られた各マグネシウム合金板についてX線回折を行い、内部領域の底面ピーク比Ocに対する表面領域の底面ピーク比OFの比率:OF/Ocを調べた。その結果を表2に示す。表面領域の底面ピーク比OFは、各マグネシウム合金板の表面に対してX線回折を行い、内部領域の底面ピーク比Ocは、各マグネシウム合金板の表面から厚さ方向に厚さの1/4までの領域(表面領域)を化学的に除去して、内部を露出させ、この露出面に対してX線回折を行った。そして、各領域の(002)面、(100)面、(101)面、(102)面、(110)面、及び(103)面のピーク強度をそれぞれ測定し、この測定結果を利用してOF/Ocを求めた。
底面ピーク比OF:IF(002)/{IF(100)+IF(002)+IF(101)+IF(102)+IF(110)+IF(103)}
底面ピーク比OC:IC(002)/{IC(100)+IC(002)+IC(101)+IC(102)+IC(110)+IC(103)} [Orientation]
For each of the obtained magnesium alloy plate subjected to X-ray diffraction, the ratio of the bottom peak ratio O F surface area relative to the bottom surface peak ratio O c of the inner region was investigated with O F / O c. The results are shown in Table 2. Bottom peak ratio O F surface area, subjected to X-ray diffraction with respect to the surface of the magnesium alloy plate, the bottom peak ratio O c of the inner region, the first surface from the thickness in the thickness direction of the magnesium alloy plate The region up to / 4 (surface region) was chemically removed to expose the interior, and X-ray diffraction was performed on this exposed surface. And measure the peak intensity of (002) plane, (100) plane, (101) plane, (102) plane, (110) plane, and (103) plane of each region, and use this measurement result. to determine the O F / O c.
Bottom peak ratio O F: I F (002) / {I F (100) + I F (002) + I F (101) + I F (102) + I F (110) + I F (103)}
Bottom peak ratio O C : I C (002) / {I C (100) + I C (002) + I C (101) + I C (102) + I C (110) + I C (103)}
得られた各マグネシウム合金板について内部領域及び表面領域の平均結晶粒径(μm)を「鋼-結晶粒度の顕微鏡試験方法 JIS G 0551(2005)」に基づいて測定した。ここでは、各マグネシウム合金板に対して厚さ方向の断面(横断面及び縦断面)をとり、各断面を光学顕微鏡で観察し(400倍)、上記各断面における表面領域(表面から厚さ方向に厚さの1/4までの領域)、及び内部領域(表面領域を除いた残部の領域)のそれぞれについて3視野ずつとり(各領域の合計視野数:6)、視野ごとに平均結晶粒径を求めた。表面領域における合計6視野の平均結晶粒径の平均値(DF)、内部領域における合計6視野の平均結晶粒径の平均値(DC)を表2に示す。また、表面領域の平均結晶粒径DFに対する内部領域の平均結晶粒径Dcの比率:Dc/DFも求めた。その結果を表2に示す。 [Average grain size]
For each of the obtained magnesium alloy plates, the average crystal grain size (μm) of the inner region and the surface region was measured based on “steel—microscopic test method of crystal grain size JIS G 0551 (2005)”. Here, a cross section in the thickness direction (cross section and longitudinal section) is taken for each magnesium alloy plate, each cross section is observed with an optical microscope (400 times), and the surface region in each cross section (from the surface to the thickness direction) 3 areas (up to 1/4 of the thickness) and internal areas (remaining areas excluding the surface area), 3 fields of view (total number of fields of view: 6), average grain size for each field of view Asked. Table 2 shows the average value (D F ) of the average crystal grain size of a total of six views in the surface region and the average value (D C ) of the average crystal grain size of a total of six views in the internal region. Further, the ratio of the average crystal grain size D c in the inner region to the average crystal grain size D F in the surface region: D c / DF was also obtained. The results are shown in Table 2.
得られた各マグネシウム合金板について内部領域及び表面領域のビッカース硬度(Hv)を調べた。ビッカース硬度は、平均結晶粒径の測定と同様に、各マグネシウム合金板に対して厚さ方向の断面(横断面及び縦断面)をとり、表面領域のビッカース硬度HFは、上記各断面における表面領域に圧子を押し当てて測定し、内部領域のビッカース硬度Hcは、上記各断面における内部領域に圧子を押し当てて測定した。表面領域における上記両断面のビッカース硬度の平均値(HF)、内部領域における上記両断面のビッカース硬度の平均値(HC)を表2に示す。また、表面領域のビッカース硬度HFに対する内部領域のビッカース硬度Hcの比率:Hc/HFも求めた。その結果を表2に示す。 [Vickers hardness]
The Vickers hardness (Hv) of the internal region and the surface region was examined for each obtained magnesium alloy plate. Vickers hardness, as with the measurement of the average crystal grain size, taken in the thickness direction of the cross section (cross section and longitudinal section) for each magnesium alloy plates, Vickers hardness H F in the surface region, the surface of each section measured by pressing an indenter to the area, the Vickers hardness H c of the internal region was measured by pressing an indenter to the internal area of each cross section. Table 2 shows the average value (H F ) of the Vickers hardness of both cross sections in the surface region and the average value (H C ) of the Vickers hardness of both cross sections in the internal region. The ratio of the Vickers hardness H c of the inner region to the Vickers hardness H F of the surface area: H c / H F was also determined. The results are shown in Table 2.
得られた各マグネシウム合金板について耐食性を調べた。ここでは、JIS Z 2371(2000)に準拠して試験片を作製して(厚さは作製した板厚とした)、96時間の塩水噴霧試験を行い、試験後の腐食減量(mg/cm2)を調べた。その結果を表2に示す。 [Corrosion test]
Each magnesium alloy plate obtained was examined for corrosion resistance. Here, a test piece was prepared in accordance with JIS Z 2371 (2000) (the thickness was the thickness of the prepared plate), a 96-hour salt spray test was performed, and the corrosion weight loss after the test (mg / cm 2 ) Was investigated. The results are shown in Table 2.
Claims (5)
- マグネシウム合金からなり、板状部を有するマグネシウム合金材であって、
前記板状部の厚さが1.5mm以上であり、
前記板状部は、以下の配向性を満たすことを特徴とするマグネシウム合金材。
[配向性]
前記板状部の表面から厚さ方向に厚さの1/4までの領域を表面領域、残部を内部領域とし、
前記表面領域における(002)面、(100)面、(101)面、(102)面、(110)面、及び(103)面のX線回折のピーク強度をそれぞれIF(002)、IF(100)、IF(101)、IF(102)、IF(110)、及びIF(103)とし、
前記内部領域における(002)面、(100)面、(101)面、(102)面、(110)面、及び(103)面のX線回折のピーク強度をそれぞれIC(002)、IC(100)、IC(101)、IC(102)、IC(110)、及びIC(103)とし、
前記表面領域における(002)面の配向度合い:IF(002)/{IF(100)+IF(002)+IF(101)+IF(102)+IF(110)+IF(103)}を底面ピーク比OF、
前記内部領域における(002)面の配向度合い:IC(002)/{IC(100)+IC(002)+IC(101)+IC(102)+IC(110)+IC(103)}を底面ピーク比OCとするとき、
前記内部領域の底面ピーク比Ocに対する前記表面領域の底面ピーク比OFの比率:OF/Ocが、1.05<OF/Ocを満たす。 A magnesium alloy material made of a magnesium alloy and having a plate-like portion,
The thickness of the plate-like portion is 1.5 mm or more,
The said plate-shaped part satisfy | fills the following orientation, The magnesium alloy material characterized by the above-mentioned.
[Orientation]
The area from the surface of the plate-like part to 1/4 of the thickness in the thickness direction is the surface area, the remainder is the internal area,
The X-ray diffraction peak intensities of the (002) plane, (100) plane, (101) plane, (102) plane, (110) plane, and (103) plane in the surface region are I F (002), I F (100), I F (101), I F (102), I F (110), and I F (103),
The X-ray diffraction peak intensities of the (002) plane, (100) plane, (101) plane, (102) plane, (110) plane, and (103) plane in the internal region are respectively I C (002), I C (100), I C (101), I C (102), I C (110), and I C (103)
Orientation degree of (002) plane in the surface region: I F (002) / { I F (100) + I F (002) + I F (101) + I F (102) + I F (110) + I F (103)} a bottom peak ratio O F,
Orientation degree of (002) plane in the inner region: I C (002) / {I C (100) + I C (002) + I C (101) + I C (102) + I C (110) + I C (103)} when the the bottom peak ratio O C,
The ratio of the bottom peak ratio O F of the surface region relative to the bottom surface peak ratio O c of the internal region: O F / O c satisfies the 1.05 <O F / O c. - 前記表面領域の平均結晶粒径をDF、前記内部領域の平均結晶粒径をDcとするとき、前記表面領域の平均結晶粒径DFに対する前記内部領域の平均結晶粒径Dcの比率:Dc/DFが、1.5<Dc/DFを満たすことを特徴とする請求項1に記載のマグネシウム合金材。 The average crystal grain diameter D F of the surface region, when the average crystal grain size of the inner region and D c, the ratio of the average crystal grain size D c of the inner region to the average grain diameter D F of the surface area 2. The magnesium alloy material according to claim 1, wherein: D c / D F satisfies 1.5 <D c / D F.
- 前記表面領域のビッカース硬度(Hv)をHF、前記内部領域のビッカース硬度(Hv)をHcとするとき、前記表面領域のビッカース硬度HFに対する前記内部領域のビッカース硬度Hcの比率:Hc/HFが、Hc/HF<0.85を満たす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材。 Vickers hardness (Hv) H F of the surface region, wherein the Vickers hardness of the inner region (Hv) when the H c, the ratio of the Vickers hardness H c of the inner region with respect to the Vickers hardness H F of the surface area: H c / H F is a magnesium alloy material according to claim 1 or 2, characterized in that satisfy H c / H F <0.85.
- 前記マグネシウム合金は、添加元素にAlを5.0質量%以上12質量%以下含有することを特徴とする請求項1~3のいずれか1項に記載のマグネシウム合金材。 4. The magnesium alloy material according to claim 1, wherein the magnesium alloy contains 5.0% by mass to 12% by mass of Al as an additive element.
- マグネシウム合金からなる素材に圧延を施してマグネシウム合金材を製造するマグネシウム合金材の製造方法であって、
溶解したマグネシウム合金を双ロール鋳造法により連続鋳造した板状の素材を準備する準備工程と、
前記素材に複数パスの圧延を施して、厚さ1.5mm以上の板状のマグネシウム合金材を製造する圧延工程とを具え、
前記各パスの圧下率をいずれも25%以下とすることを特徴とするマグネシウム合金材の製造方法。 A method for producing a magnesium alloy material by rolling a material made of a magnesium alloy to produce a magnesium alloy material,
A preparation step of preparing a plate-like material continuously cast from a melted magnesium alloy by a twin roll casting method;
A rolling process for producing a plate-like magnesium alloy material having a thickness of 1.5 mm or more by rolling a plurality of passes on the material,
A method for producing a magnesium alloy material, wherein the rolling reduction of each pass is 25% or less.
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