CN101804553B - Magnesium alloy plastic products and process for preparation of the same - Google Patents
Magnesium alloy plastic products and process for preparation of the same Download PDFInfo
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- CN101804553B CN101804553B CN2010101193253A CN201010119325A CN101804553B CN 101804553 B CN101804553 B CN 101804553B CN 2010101193253 A CN2010101193253 A CN 2010101193253A CN 201010119325 A CN201010119325 A CN 201010119325A CN 101804553 B CN101804553 B CN 101804553B
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- 229910000861 Mg alloy Inorganic materials 0.000 title claims abstract description 132
- 238000000034 method Methods 0.000 title claims description 117
- 230000008569 process Effects 0.000 title claims description 62
- 238000004512 die casting Methods 0.000 claims abstract description 78
- 238000004519 manufacturing process Methods 0.000 claims abstract description 63
- 238000005242 forging Methods 0.000 claims abstract description 35
- 238000005266 casting Methods 0.000 claims description 93
- 238000003490 calendering Methods 0.000 claims description 23
- 238000004080 punching Methods 0.000 claims description 18
- 229910052782 aluminium Inorganic materials 0.000 claims description 12
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 12
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 claims description 10
- 239000011777 magnesium Substances 0.000 claims description 10
- 229910052749 magnesium Inorganic materials 0.000 claims description 10
- 229910052761 rare earth metal Inorganic materials 0.000 claims description 9
- 229910052748 manganese Inorganic materials 0.000 claims description 8
- 239000011572 manganese Substances 0.000 claims description 8
- 150000002910 rare earth metals Chemical class 0.000 claims description 8
- OYPRJOBELJOOCE-UHFFFAOYSA-N Calcium Chemical compound [Ca] OYPRJOBELJOOCE-UHFFFAOYSA-N 0.000 claims description 7
- 229910052791 calcium Inorganic materials 0.000 claims description 7
- 239000011575 calcium Substances 0.000 claims description 7
- 229910052712 strontium Inorganic materials 0.000 claims description 7
- CIOAGBVUUVVLOB-UHFFFAOYSA-N strontium atom Chemical compound [Sr] CIOAGBVUUVVLOB-UHFFFAOYSA-N 0.000 claims description 7
- 239000004411 aluminium Substances 0.000 claims description 6
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 claims description 5
- 229910052710 silicon Inorganic materials 0.000 claims description 5
- 239000010703 silicon Substances 0.000 claims description 5
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 claims description 4
- BQCADISMDOOEFD-UHFFFAOYSA-N Silver Chemical compound [Ag] BQCADISMDOOEFD-UHFFFAOYSA-N 0.000 claims description 4
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 claims description 4
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 claims description 4
- 239000012535 impurity Substances 0.000 claims description 4
- 229910052709 silver Inorganic materials 0.000 claims description 4
- 239000004332 silver Substances 0.000 claims description 4
- 229910052725 zinc Inorganic materials 0.000 claims description 4
- 239000011701 zinc Substances 0.000 claims description 4
- 229910052726 zirconium Inorganic materials 0.000 claims description 4
- 238000012545 processing Methods 0.000 abstract description 11
- 239000000463 material Substances 0.000 description 48
- 230000000052 comparative effect Effects 0.000 description 26
- 229910045601 alloy Inorganic materials 0.000 description 21
- 239000000956 alloy Substances 0.000 description 21
- 238000001125 extrusion Methods 0.000 description 18
- 239000007789 gas Substances 0.000 description 17
- 238000009749 continuous casting Methods 0.000 description 13
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 10
- 238000005260 corrosion Methods 0.000 description 9
- 230000007797 corrosion Effects 0.000 description 9
- 238000012360 testing method Methods 0.000 description 8
- 150000001875 compounds Chemical class 0.000 description 7
- 238000003754 machining Methods 0.000 description 7
- 238000007598 dipping method Methods 0.000 description 6
- 238000005516 engineering process Methods 0.000 description 6
- 238000010438 heat treatment Methods 0.000 description 6
- 229910052751 metal Inorganic materials 0.000 description 6
- 239000002184 metal Substances 0.000 description 6
- 230000003245 working effect Effects 0.000 description 6
- 229910052786 argon Inorganic materials 0.000 description 5
- 238000001816 cooling Methods 0.000 description 5
- 239000003085 diluting agent Substances 0.000 description 5
- 238000000465 moulding Methods 0.000 description 5
- 241001163841 Albugo ipomoeae-panduratae Species 0.000 description 4
- CURLTUGMZLYLDI-UHFFFAOYSA-N Carbon dioxide Chemical compound O=C=O CURLTUGMZLYLDI-UHFFFAOYSA-N 0.000 description 4
- 238000013461 design Methods 0.000 description 4
- 238000002844 melting Methods 0.000 description 4
- 230000008018 melting Effects 0.000 description 4
- 238000009497 press forging Methods 0.000 description 4
- 229910000636 Ce alloy Inorganic materials 0.000 description 3
- 239000003795 chemical substances by application Substances 0.000 description 3
- 230000002950 deficient Effects 0.000 description 3
- 238000012423 maintenance Methods 0.000 description 3
- 230000014759 maintenance of location Effects 0.000 description 3
- 239000007769 metal material Substances 0.000 description 3
- 239000000203 mixture Substances 0.000 description 3
- 229910052684 Cerium Inorganic materials 0.000 description 2
- 230000003064 anti-oxidating effect Effects 0.000 description 2
- 230000008901 benefit Effects 0.000 description 2
- 230000033228 biological regulation Effects 0.000 description 2
- 230000005540 biological transmission Effects 0.000 description 2
- 238000009835 boiling Methods 0.000 description 2
- 229910002092 carbon dioxide Inorganic materials 0.000 description 2
- 239000001569 carbon dioxide Substances 0.000 description 2
- 230000008859 change Effects 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000011156 evaluation Methods 0.000 description 2
- 230000002349 favourable effect Effects 0.000 description 2
- 230000004907 flux Effects 0.000 description 2
- 239000003921 oil Substances 0.000 description 2
- 230000003647 oxidation Effects 0.000 description 2
- 238000007254 oxidation reaction Methods 0.000 description 2
- 239000002994 raw material Substances 0.000 description 2
- 239000011347 resin Substances 0.000 description 2
- 229920005989 resin Polymers 0.000 description 2
- 229910000838 Al alloy Inorganic materials 0.000 description 1
- 229910001208 Crucible steel Inorganic materials 0.000 description 1
- 208000035126 Facies Diseases 0.000 description 1
- 229910002551 Fe-Mn Inorganic materials 0.000 description 1
- GANNOFFDYMSBSZ-UHFFFAOYSA-N [AlH3].[Mg] Chemical compound [AlH3].[Mg] GANNOFFDYMSBSZ-UHFFFAOYSA-N 0.000 description 1
- 238000007664 blowing Methods 0.000 description 1
- 239000012267 brine Substances 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- GWXLDORMOJMVQZ-UHFFFAOYSA-N cerium Chemical compound [Ce] GWXLDORMOJMVQZ-UHFFFAOYSA-N 0.000 description 1
- 238000002485 combustion reaction Methods 0.000 description 1
- 238000005336 cracking Methods 0.000 description 1
- 238000005520 cutting process Methods 0.000 description 1
- 238000010790 dilution Methods 0.000 description 1
- 239000012895 dilution Substances 0.000 description 1
- 230000008676 import Effects 0.000 description 1
- 229910052738 indium Inorganic materials 0.000 description 1
- APFVFJFRJDLVQX-UHFFFAOYSA-N indium atom Chemical compound [In] APFVFJFRJDLVQX-UHFFFAOYSA-N 0.000 description 1
- 229910052746 lanthanum Inorganic materials 0.000 description 1
- 230000035777 life prolongation Effects 0.000 description 1
- 239000010721 machine oil Substances 0.000 description 1
- 239000013521 mastic Substances 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 239000000155 melt Substances 0.000 description 1
- 238000012856 packing Methods 0.000 description 1
- 239000011148 porous material Substances 0.000 description 1
- 238000003825 pressing Methods 0.000 description 1
- 238000010791 quenching Methods 0.000 description 1
- 230000000171 quenching effect Effects 0.000 description 1
- 238000011084 recovery Methods 0.000 description 1
- 238000001953 recrystallisation Methods 0.000 description 1
- 238000011160 research Methods 0.000 description 1
- 238000005096 rolling process Methods 0.000 description 1
- 238000005204 segregation Methods 0.000 description 1
- 238000007493 shaping process Methods 0.000 description 1
- 238000004904 shortening Methods 0.000 description 1
- 238000002791 soaking Methods 0.000 description 1
- HPALAKNZSZLMCH-UHFFFAOYSA-M sodium;chloride;hydrate Chemical compound O.[Na+].[Cl-] HPALAKNZSZLMCH-UHFFFAOYSA-M 0.000 description 1
- 241000894007 species Species 0.000 description 1
- 239000007921 spray Substances 0.000 description 1
- 238000005482 strain hardening Methods 0.000 description 1
Classifications
-
- 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
-
- 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
- C22C—ALLOYS
- C22C23/00—Alloys based on magnesium
- C22C23/02—Alloys based on magnesium with aluminium as the next major constituent
Abstract
The invention provides the production of plastic processing products ensuring forgeability, preventing from fracture, blackening and burning surface, realizing formability of complex shape of die casting, high reliability and high intensity performance of forging products, and production of cheep and high-quality plastic processing products, as well as producing magnesium alloy plates cheaply according to requirements, further comprising production of magnesium alloy plastic processing products plastically processing the magnesium alloy plates produced cheaply.
Description
The application is application number the dividing an application for China's application of " magnesium alloy plastic process product and manufacture method thereof " that be CN200710306896.6 (applying date is on November 29th, 2007), denomination of invention.
Technical field
The present invention relates to a kind of magnesium alloy plastic process product, its manufacture method, magnesium alloy extrusion section bar and manufacture method thereof, in more detail, the present invention relates to (i) and in plastic working, guarantee plastic working, suppress to break or surface stain, burning, guarantee the manufacture method of plastic process product of the mechanical strength of plastic process product, (ii) by die casting casting and plastic working is compound, realize simultaneously the formability of the complicated shape of die casting casting, the high reliability of plastic working, the manufacture method of the plastic process product of the Combined Machining Technology of high strength, (iii) need the conveyer such as light-weighted automobile, mobile phone, the civilian motor information household appliances such as notebook computer machine, electric tool, the manufacture method of the magnesium alloy plastic process product of the industrial machines such as general purpose engine etc., (iv) plastic process product that is obtained by these manufacture methods, (v) be manufactured in the extruding of heat-resistant magnesium alloy extrudate and guarantee extruding property, blackening when suppressing extruding, guarantee the mechanical strength of extrudate, the method of more cheap high-quality heat-resistant magnesium alloy extrudate, the extrudate that (vi) is obtained by this manufacture method.
Background technology
In automobile industry, owing to combustion expense improves the light-weighted necessity that causes, the demand of light material is uprised, bring into use resin material or light metal material.Yet resin material is general owing to reclaim difficulty, problem is arranged aspect the environment of preserving our planet.Relative therewith, because the general easy recovery of metal material, thereby expect especially the expansion of its purposes.Magnesium alloy as light weight in the light metal material uses at inside components such as steering wheel, safety belt, air bag retainers at present.Yet, seek to electric motor car PWTN components either extend purposes such as engine components or transmission components from now on.For Interior Parts, making good magnesium alloy AM50, the AM60 of ductility by the die casting casting is alloy.On the other hand, the electric motor car PWTN for these purposes expansions of expectation has begun to be cast to make the good heat-resistant magnesium alloy of creep resistant of intensity and 150 ℃ of front and back by die casting.Be explained, as heat-resistant magnesium alloy, known in magnesium-aluminium system the various magnesium alloys (for example referring to Patent Document 1) of interpolation rare earth metal or calcium, strontium.
And recently, personal computer, phone housing, mobile phone mechanism components etc. are shaped by the stamping or plate forging of magnesium alloy.The blank that uses in stamping or plate forging and molding is generally the magnesium alloy plate of extruding continuous casting billet or further rolls the magnesium alloy sheet (for example, referring to Patent Document 2～3) that this magnesium alloy plate obtains.
The purposes of existing al member is for to use numerous forged articles such as piston, cylinder cover, oil pressure parts in the electric motor car power transmission based part of automobile.These high strength that can not deal with for magnesium alloy die casting goods, the purposes of high reliability, magnesium alloy is unable to cope with this purposes in the present situation.When comparing with aluminum dipping form casting goods, magnesium die casting product strength is low more than 10%, is difficult to replace aluminum dipping form casting goods with the magnesium die casting goods of same size, in most cases needs the local wall thickness raising or appends the countermeasure that antelabium etc. is guaranteed intensity.Yet these countermeasures are associated with the weight raising of magnesium die casting goods.Therefore, in magnesium die casting goods, demand improves the technology of the intensity at the position of not satisfying the intensity important document.
No. 2604670 communique of (patent documentation 1) Japan Patent
(patent documentation 2) TOHKEMY 2006-239748 communique
(patent documentation 3) TOHKEMY 2006-239750 communique
Summary of the invention
When being used for automobile electric motor-car PWTN parts, from its serviceability temperature environment, magnesium alloy plastic process product must be heat-resistant magnesium alloy.Yet, can not produce continuous casting section bar and the extrudate of the heat-resistant magnesium alloy that becomes the plastic working blank.In fact, if extruding heat-resistant magnesium alloy then have following problem.In heat-resistant magnesium alloy, in order to improve the creep properties under high temperature and the room temperature, although added silicon, rare earth element, calcium, strontium etc., lack plastic working but therefore become, the grain boundary portion place that generates compound produces easily breaks, and these elements are owing to be active, when therefore at high temperature carrying out extrusion process, then catch fire or blackening at the mould outlet place.And, lack similarly plastic working in the plastic working operation, produce easily breaking of grain boundaries, to catch fire easily or blackening when reaching a high temperature, the intensity that also can not get in the plastic working improves.
In addition, when in advance aluminum dipping form being cast section's material instead of magnesium die casting section material, for mechanical property, rigidity, hot strength are than aluminum dipping form casting section material low about 10%, particularly in automobile electric motor-car PWTN section material, although from its serviceability temperature environment use heat-resistant magnesium alloy, but for creep strength, although identical with aluminum dipping form casting material near the temperature range (150 ℃) of machine oil, but because rigidity, compressive strength are relatively low, for example for bolted, remaining axle force rate aluminum dipping form casting section material descends about 20%.Rigidity is for the moment physical characteristic of material, can not make it occur to change significantly, and strength characteristics is improved becomes problem more than 10%.On the other hand, magnesium forging section material is because roughly shaped material high price and can not being widely used in automobile industry etc.And general magnesium alloy is not wished work hardening under the standard forging temperature, does not wish the high strength as aluminum alloy forged material.And, in heat-resistant magnesium alloy, also do not produce roughly shaped material.
Further, the plastic deformation ability of magnesium alloy is inferior, and extrusion speed is slow, need to roll between heat, further, because the use amount of magnesium alloy plate is not suitable for a large amount of productions less, the acquisition of magnesium alloy continuous casting billet must depend on import etc., so the cost of magnesium alloy plate is very expensive.And this becomes not main cause widely of the extrusion molding of magnesium alloy or plate forging and molding.
The problem that the present invention has in view of these conventional arts and finishing; its purpose is to provide in a kind of extruding that is manufactured on the heat-resistant magnesium alloy extrudate guarantees extruding property; blackening when suppressing extruding; guarantee the mechanical strength of extrudate; the method of more cheap high-quality heat-resistant magnesium alloy extrudate; the extrudate that is obtained by this manufacture method; and; in with the plastic working of this extrudate as blank, guarantee plastic working; suppress to break or surface stain; burning; guarantee the manufacture method of the plastic process product of mechanical strength, by the plastic process product of this manufacture method acquisition.
And, the present invention also aims to provide a kind of by die casting casting and the plastic working of magnesium alloy is compound, realize simultaneously the formability of the complicated shape of die casting casting, the high reliability of plastic working, the Combined Machining Technology of high strength, the manufacture method of more cheap high-quality plastic process product, the plastic process product that is obtained by this manufacture method.
Further, the object of the present invention is to provide and a kind ofly can make at an easy rate magnesium alloy plate as required, the magnesium alloy plate of this cheapness manufacturing is carried out manufacture method and the magnesium alloy plastic process product of the magnesium alloy plastic process product that plastic working obtains.
The inventor etc. have carried out various researchs in order to reach above-mentioned each purpose, found that, temperature conditions, atmospheric condition during by when casting control, extrusion process, during plastic working, obtained desired result, and, by the Combined Machining Technology that die casting casting and the plastic working of combination magnesium alloy are made up, reach the high strength of magnesium alloy molding member, and then finished the present invention.And, the discovery below having obtained.Namely, preferably make magnesium alloy plate and magnesium alloy sheet as plastic working blanks such as extrusion molding or plate forging and moldings by the die casting casting method, perhaps for so that the even thickness of the sheet material of being made by this die casting casting or roll manufacturing in order to reach specific thickness.
That is, the manufacture method of heat-resistant magnesium alloy extrudate of the present invention is characterized in that and will comprise
(1) be selected from aluminium 1～10 quality %, zinc 0.2～5 quality % and silver among 0.2～5 quality % at least a,
(2) be selected from rare earth metal 0.2～5 quality %, calcium 0.02～5 quality %, strontium 0.02～5 quality % and silicon 0.2～5 quality % at least a,
(3) be selected from that manganese 1.5 quality % are following, zirconium 1.5 quality % with lower at least a, remainder by magnesium and inevitably the liquation of the magnesium alloy that consists of of impurity under inert atmosphere, maintain 650～700 ℃ of temperature, make columned casting billet by casting mold casting or continuous casting by this liquation, this casting billet is carried out extrusion process under the condition of 350～450 ℃ of billet temperature, 350～450 ℃ of vessel temps, 450～550 ℃ of mold temperatures.
And, the heat-resistant magnesium alloy extrudate of heat-resistant magnesium alloy extrudate of the present invention for being obtained by above-mentioned manufacture method.
The manufacture method of the heat-resistant magnesium alloy plastic process product of the first embodiment of the present invention is the manufacture method at the heat-resistant magnesium alloy plastic process product more than 150 ℃ the hot strength 180MPa take following content as feature: the extrudate that will be obtained by the manufacture method of above-mentioned heat-resistant magnesium alloy extrudate maintains 300～500 ℃, mold temperature is maintained be lower than in the situation that this extrudate keeps 10～30 ℃ of temperature, to this extrudate forge, roll, the plastic working such as extruding.
And, the manufacture method of the heat-resistant magnesium alloy plastic process product of the second embodiment of the present invention is characterised in that, the die casting casting ingot of magnesium alloy is remained under 250～550 ℃, mold temperature is maintained under the temperature of 10～50 ℃ of maintenance temperature that are lower than this die casting casting ingot, partly or wholly implement the plastic workings such as forging, calendering, punching press, extruding, so that intensity improves.
And, the manufacture method of the heat-resistant magnesium alloy plastic process product of the 3rd embodiment of the present invention is characterised in that, the magnesium alloy plate of thickness of slab 0.2mm～100mm is made in die casting casting by the magnesium alloy liquation, to this magnesium alloy plate forge, the plastic workings such as calendering, punching press, extruding.
And, it is characterized in that of the manufacture method of the heat-resistant magnesium alloy plastic process product of the 4th embodiment of the present invention, make the magnesium alloy plate of thickness of slab 0.2mm～100mm by the die casting casting of magnesium alloy liquation, under room temperature～400 ℃, this magnesium alloy plate is carried out once calendering more than (one-pass) at a direction or both direction, make the magnesium alloy plate of regulation wall thickness, to the magnesium alloy plate of this regulation wall thickness forge, the plastic workings such as calendering, punching press, extruding.
The heat-resistant magnesium alloy plastic process product that heat-resistant magnesium alloy plastic process product of the present invention obtains for the manufacture method by the heat-resistant magnesium alloy plastic process product of above-mentioned the first embodiment～the 4th embodiment.
The invention effect
In the present invention, the casting property that has obtained in the continuous casting of heat-resistant magnesium alloy, to guarantee to perfect, in the extruding of extrudate, guarantee extruding property, the blackening when suppressing extruding, guarantee the mechanical strength of extrudate, more cheap high-quality heat-resistant magnesium alloy extrudate, and, with this extrudate as plastic workings such as the forging of blank, calendering, punching press, extruding in, guarantee plastic working, suppress to break or surface stain, burning, guarantee the mechanical strength of plastic process product.
And, in the present invention, by the plastic workings such as the die casting casting of magnesium alloy and forging, calendering, punching press, extruding is compound, can realize simultaneously formability, the high reliability of plastic working, the high strength of the complicated shape of die casting casting, obtain cheap, high-quality plastic process product.
And, in the present invention, because magnesium alloy plate can obtain at an easy rate, magnesium alloy plate to cheapness carries out plastic working, therefore can make at an easy rate the magnesium alloy plastic process product of industrial machines such as the civilian motor information household appliances such as conveyer, mobile phone, notebook computer machine, electric tool, general purpose engine such as needing light-weighted automobile etc., the purposes of the Mg alloy formed article that is obtained by plastic working becomes extensively.
The specific embodiment
For heat-resistant magnesium alloy plastic process product and the manufacture method thereof of heat-resistant magnesium alloy extrudate of the present invention and manufacture method thereof, first embodiment of the invention, need to use the heat-resistant magnesium alloy as the raw material magnesium alloy, the preferred use comprises
(1) be selected from aluminium 1～10 quality %, zinc 0.2～5 quality % and silver 0.2～5 quality % at least a,
(2) be selected from rare earth metal 0.2～5 quality %, calcium 0.02～5 quality %, strontium 0.02～5 quality % and silicon 0.2～5 quality % at least a,
(3) be selected from least a that manganese 1.5 quality % are following, zirconium 1.5 quality % are following, the magnesium alloy that remainder is made of magnesium and inevitable impurity.
During keeping, uses liquation when the casting at the continuous casting billet words of flux; then produce easily sneaking into of flux; and; in the situation of gas shield; when melt temperature surpasses 700 ℃; then protect effect to weaken, burn insufficient and generate easily oxide, become the reason of sneaking into foreign matter in the billet.On the other hand, if discontented 650 ℃, it is thick then to shake the Compound Phase of generation by heat, the main cause of breaking when becoming extruding or during plastic working.
In addition, the air when getting rid of casting enters, the remaining or segregation of the shrinkage cavity when solidifying, solidify break, the casting condition of sneaking into etc. of the generation of thick compound, above-mentioned foreign matter must the casting condition identical with the situation of general-purpose alloy.
Thereby, for the manufacture method of the heat-resistant magnesium alloy plastic process product of first embodiment of the invention, the liquation of magnesium alloy must be maintained to 650～700 ℃ of temperature under inert atmosphere gas, make columned casting billet by casting mold casting or continuous casting by this liquation.
For the extruding of billet, by the heating of plastic working, the temperature of the extrudate after the extruding raises than the design temperature of billet.If making the temperature of the extrudate at mould outlet place is about 500 ℃, then need by cooling etc. mold temperature to be controlled at 450～550 ℃, preferred 450～500 ℃.And for oxidation, the blackening of the extrudate that is suppressed at the mould outlet place, cooling, the anti-oxidation of the extrudate that is undertaken by carbon dioxide, argon gas are also effective.On the other hand, owing to the temperature that reduces billet for the extrudate of controlling the mould outlet place, in fact therefore extrusion process difficult then need the Temperature Setting of billet for than high 350～450 ℃, preferred 350～400 ℃ of the extrusion temperature in the general-purpose alloy.And, set vessel temp at 350～450 ℃.Be explained, billet need to be removed cast(ing) surface, cold shut by the outside cutting.Although change along with the shape of extrusion ratio or extrudate, preferred squeeze pressure is 100～250kgf/cm
2, extrusion speed is 2～10m/ minute.Crooked when further, preventing from pushing or guarantee that superficiality etc. is used for guaranteeing that the extruding condition of the quality of extrudate is necessary for the extruding condition identical with the situation of general-purpose alloy.
When the temperature of the extrudate when plastic working (blank) surpassed 500 ℃, the Jingjing interface of blank magnesium alloy melted burning or the blackening by oxidation.Therefore, the blank temperature when plastic working surpasses in 500 ℃ the situation, needs to use carbon dioxide, the anti-oxidation of argon gas, burning.Blank temperature in the time of need to making plastic working improves if consider the intensity of the plastic process product that plastic working causes for than high 300～500 ℃ of the blank temperature in the general-purpose alloy, then is preferably 300 ℃～400 ℃.And the Temperature Setting of mold is to hang down 10～30 ℃ than the temperature of this blank.Although all heat treatment is not essential, needing to hold blank is the heating condition (retention time) of soaking.Be explained, thermal fracture when preventing plastic working, cold cracking, guarantee that superficiality etc. is used for guaranteeing to be not limited only to the said temperature condition as the plastic working condition of plastic process product quality, identical with the situation of general-purpose alloy, must study the overall conditions such as casting mold design, molding condition.
Below, the mechanical performance of extrudate and the plastic process product of magnesium alloy is described.The plastic working of magnesium alloy is poor, and for example comparing with aluminium during extrusion process and during plastic working needs to keep high temperature.And magnesium alloy is replied easily, is recrystallized in the processing temperature zone.For example, the hot strength of the extrudate of general-purpose alloy (AZ31) is 250～280MPa, percentage elongation about 15%, and for hot strength, however identical with die casting section bar as cast article.And for plastic process product, hot strength is about 300MPa, percentage elongation is about 15%, and the significant intensity that does not obtain expecting improves.Although in heat-resistant magnesium alloy, generally suppressed answer, recrystallization, in order to ensure plastic working, at high temperature to process simultaneously.The heat-resistant magnesium alloy that the present invention uses has hot strength, percentage elongation above general-purpose alloy in the stage of molded shapes, by adjusting each condition of extruding and plastic working, particularly process at low temperatures as best one can, thereby can realize the significantly raising of hot strength, more than the hot strength 250MPa of extrudate, more than the hot strength 310MPa of plastic process product, the hot strength in the time of 150 ℃ is more than the 180MPa.
In the manufacture method of the magnesium alloy plastic process product of second embodiment of the invention, although the die casting casting ingot of magnesium alloy is remained on 250～550 ℃, mold temperature is remained on lower 10～50 ℃ and partly or entirely implement plastic working intensity is improved than the maintenance temperature of this die casting casting ingot, but the result who accurately checks this condition is, by in plastic working, the temperature of die casting casting ingot being remained on 250～550 ℃, preferred 250～400 ℃, mold temperature is remained on than low 10～50 ℃ of the maintenance temperature of die casting casting ingot, preferred 10～30 ℃, observe and to carry out the plastic working of die casting casting ingot.And the needed pressure of plastic working is 4～10kgf/mm in general-purpose alloy
2Or more than.
Although the situation of the part plastic working of die casting article does not generally produce large plastic working rate, the situation of plastic working rate 50% is compared with the die casting casting ingot in the AM50 die casting section bar, and hot strength improves more than 10%, and percentage elongation improves more than 20%.
In the manufacture method of the magnesium alloy plastic process product of second embodiment of the invention, can carry out continuously die casting casting and plastic working, no longer implement heating and enforcement plastic working preferred this moment after the die casting casting on aspect the cost.
In the manufacture method of the magnesium alloy plastic process product of second embodiment of the invention, can use various magnesium alloys.Although plastic working is poor on its characteristic of heat-resistant magnesium alloy, the heat-resistant magnesium alloy as taking into account heat resistance and plastic working (percentage elongation is more than 5%) preferably uses following magnesium alloy.
Comprise (1) be selected from aluminium 1～10 quality %, zinc 0.2～5 quality % and silver 0.2～5 quality % at least a,
(2) be selected from rare earth metal 0.2～5 quality %, calcium 0.02～5 quality %, strontium 0.02～5 quality % and silicon 0.2～5 quality % at least a,
(3) be selected from least a that manganese 1.5 quality % are following, zirconium 1.5 quality % are following, the magnesium alloy that remainder is made of magnesium and inevitable impurity.
Although put down in writing the various heat-resistant magnesium alloys that comprise above-mentioned heat-resistant magnesium alloy in Japanese kokai publication hei 6-200348 communique, the present invention also can use these heat-resistant magnesium alloys.
Above-mentioned heat-resistant magnesium alloy is being carried out in the situation of plastic working, although the required pressure of plastic working is 10～20kgf/mm
2Or more than, but for other condition, can carry out plastic working with the essentially identical condition of the situation of general-purpose alloy, can access plastic working rate 50%, 150 ℃ the above plastic process product of hot strength 160MPa.And the residual axle power of above-mentioned bolted obtains 10% raising in the time of 150 ℃.
As the die casting casting method for the manufacture of the die casting casting ingot that in the manufacture method of second embodiment of the invention, uses, can use various die casting casting methods.Although the high pressure diecasting casting method has the limited problem of wall thickness, extrusion die casting casting method, low pressure (die casting) casting method, laminar flow die casting casting method etc. are the castings that is suitable for suppressing the internal flaws such as pore and obtains the wall thickness parts.As the die casting casting method for the manufacture of the die casting casting ingot that in the manufacture method of second embodiment of the invention, uses, for example can use the die casting casting method of putting down in writing in the TOHKEMY 2001-009561 communique.In the manufacture method of the magnesium alloy plastic process product of the second embodiment of the present invention, the quantity-produced system that preferably makes these die casting castings and plastic working side by side carry out and not heat again.
In the manufacture method of the magnesium alloy plastic process product of the third and fourth embodiment of the present invention, initial, cast to make the magnesium alloy plate of thickness of slab 0.2mm～100mm by the die casting of magnesium alloy liquation.
The advantage of utilizing this die casting casting to make sheet material at first is to realize the low price production of small lot sheet material.Namely, even in the considerably less situation of the needs of magnesium alloy plate or thin plate, owing to after the sheet material that utilizes die casting casting machine production necessary amount, this die casting casting machine can be turned to the production of section's material of this sheet material various shape in addition, so need not be so that the die casting casting machine is idle.And, compare with traditional continuous casting → extruding → calendering, utilize the sheet material manufacturing process of die casting casting few, also favourable on the production cost this point.Be explained, continuous casting and calendering are not suitable for small lot batch manufacture for a large amount of systems that produce same object.And, even if to forge or the plastic working of punching press etc., when wanting metal structure with sheet material and thin plate to become worked structure, can after making sheet material by the die casting casting, apply calendering in order to improve.This calendering can be carried out once above calendering at a direction or both direction to the sheet material made by die casting casting and implements under room temperature～400 ℃, make the magnesium alloy plate of stipulating wall thickness.Also can omit continuous casting → extruding in this case, by from the sheet material that utilizes any thickness that die casting casting makes, can subdue calendering quantity, so this be favourable.
And the advantage of sheet material manufacturing of utilizing die casting casting is for the diversity of the magnesium alloy that can realize the die casting casting and can carry out liquation and process.Utilize the sheet material manufacturing of die casting casting to produce to contain the high strength of rare earth metal or calcium, strontium and have stable on heating magnesium alloy plate, and, process or the liquation of the rare earth metal of indium addition 0.1～1.0 quality % is processed by liquations such as argon gas boilings, can be better than according to purposes and requirement production corrosion resistance the magnesium alloy plate of aluminium plate.
Although the thickness that utilizes die casting to cast the sheet material that can make also depends on area, is generally below the above 15mm of 0.5mm.Especially, wanting to make in the situation of thin plate, by when casting, reducing thickness etc., can be thinned to about 0.2mm, use large scale computer, vacuum pressing and casting or laminar flow die casting, extrusion die casting if comprise, then also can make the plate of 70～100mm left and right thickness, the plate thickness that can make is in extensive range.
And, because die casting is cast into quenching, therefore utilize sheet material that the die casting casting makes and from the sheet material of continuous casting extruding maybe with this sheet material further the sheet material that obtains of calendering compare, the metal structure at initial stage is trickle, although also depend on metal species, also can realize below the average crystallite granularity 50 μ m.Corrosion resistance and mechanical strength that this has at first improved this sheet material have improved plastic deformation simultaneously.And, below the grain size number average out to 50 μ m of the metal structure of the die casting casted thin plate below the thickness 1mm that in the information household appliances goods such as PC, uses, although also depend on alloy species, but be in particular about 20～30 μ m to 10 μ m, and plastic deformation raising, and make processing temperature below 300 ℃, can drop to particularly 200～300 ℃.The die casting thin plate is applied calendering add man-hour, can obtain the trickle worked structure that can not be obtained by other manufacture method.
Further, in the die casting casting of magnesium alloy plate, by implementing the few casting of demoulding type agent, when shortening casting cycle, can expect mould life prolongation, prima facie raising, do not use the corrosion resistance of the sheet material that releasing agent produces to improve, suppress the burning that caused by the agent of demoulding type.
In the manufacture method of the magnesium alloy plastic process product of the present invention the third and fourth embodiment, as mentioned above, the sheet material that utilizes the die casting casting to make is carried out plastic working and makes magnesium alloy plastic process product.As this plastic working, implement the shapings such as extruding, calendering, forging or punching press.These plastic workings are known, can implement according to known technology.
The present invention also comprises the magnesium alloy plastic process product that obtains by this plastic working.As the magnesium alloy plastic process product that is obtained by plastic working of the present invention, be preferably and be forged into the shaped part material.In this magnesium alloy forged forming section material, the grain size number of the metal structure of magnesium alloy can reach below the average 50 μ m that are difficult to realize by other manufacture method, below the preferred 30 μ m.
The below specifically describes the present invention based on embodiment and comparative example.
Embodiment 1 and comparative example 1～2
Melt Mg-5Al-2Ca-2MM (cerium alloy)-0.2Mn alloy, use casting mold to make under the following conditions the columned casting billet of φ 168 * 500mm.
In embodiment 1, cast continuously with certain speed, replenish liquation in constriction.In comparative example 1, little spark in keeping, liquation occurs.And, in comparative example 2, although under the condition identical with embodiment 1, cast continuously with certain speed, on the side, produced significantly liquation shrinkage (concavo-convex).
The 1st table
| Melting temperature | Mold material | Atmosphere | Casting property | |
| Embodiment 1 comparative example 1 comparative example 2 | 680℃ 750℃ 600℃ | SKD61 SKD61 SKD61 | Ar gas SF 6Diluent gas Ar gas | There is oxide to sneak into thick Al-Fe-Mn compound above good |
Embodiment 2 and comparative example 3-4
The cylindric continuous casting billet of making among the embodiment 1 is processed into the columned extruding billet of φ 150 * 400mm, and use extruder 1650T makes the bar of φ 30 under the following conditions.
In embodiment 2, in order to control mold temperature, cooling tube is set, so that the circulation of 200 ℃ oil and adjusting mold temperature manage the blank temperature at mould outlet place below 470 ℃, to the blank blowing argon gas.In comparative example 3 and 4, do not control mold temperature.
The 2nd table
| The billet temperature | Vessel temp | Mold temperature | The extruding quality | |
| Embodiment 2 comparative examples 3 comparative examples 4 | 370℃ 300℃ 470℃ | 370℃ 300℃ 450℃ | 450℃ 300℃ 550℃ | Well can not partly burn in the extrusion die exit |
In embodiment 2, extrusion speed is that 5m/ divides, and the hot strength of the extrudate of gained is 270MPa, and percentage elongation is 10% (length direction).
Embodiment 3 and comparative example 5～6
The extrudate of making among the cut-out embodiment 2 and the roughly shaped material of making φ 30 * 50 use punching press forging machine 100T, forge the cylinder of making φ 42.5 * 25 by hermetic type under the following conditions.
The 3rd table
| The evenly heating processing time | Blank temperature | Model temperature | Casting property | |
| Embodiment 3 comparative examples 5 comparative examples 6 | 1 hour 1 hour 1 hour | 320℃ 270℃ 550℃ | 300℃ 250℃ 530℃ | Well produce the blackening of breaking |
The hot strength of the forging product that obtains among the embodiment 3 is 300MPa, and percentage elongation is that 10%, 150 ℃ hot strength is 160MPa.
Embodiment 4～12
Use following magnesium alloy, by the process identical with embodiment 1～3, under condition as shown in table 4, make forging product.Be explained, all use SF in any situation
6The liquation of diluent gas when melting keeps atmosphere, and the mould during extruding carries out adjustment by cooling tube, and the place is blown into argon gas at mould outlet, and the forging temperature when forging also is blown into Ar gas simultaneously when surpassing 400 ℃.The characteristic of gained forging product is shown in the 4th table.
(1)Mg-10Al-5MM-5Ca-0.2Mn、
(2)Mg-10Al-5MM-5Sr-0.5Ca-0.2Mn、
(3)Mg-7Al-2.5MM-2.5Ca-0.5Sr-0.2Mn、
(4)Mg-1Al-0.2MM-0.02Ca-0.8Mn、
(5)Mg-5Zn-1Y-0.5Sr-0.8Zr、
(6)Mg-0.2Zn-0.2Y-0.5Sr-0.6Zr-0.02Ca、
(7)Mg-5Ag-2MM-0.6Zr、
(8)Mg-0.2Ag-2MM-0.6Zr-0.02Ca、
(9)Mg-1Zn-5.5Y-2MM-1.5Sr-0.6Zr-0.02Ca
MM is cerium alloy (Ce, La is as the rare earth metal mixture of main component)
The 4th table
| Alloy | Melting temperature | The billet temperature | Vessel temp | Mold temperature | Forging temperature | Mold temperature | Forge quality | Hot strength (room temperature) | Hot strength (150 ℃) | |
| Embodiment 4 embodiment 5 embodiment 6 embodiment 7 embodiment 8 embodiment 9 embodiment 10 embodiment 11 embodiment 12 | (1) (2) (3) (4) (5) (6) (7) (8) (9) | 650℃ 650℃ 670℃ 700℃ 650℃ 700℃ 650℃ 700℃ 700℃ | 450℃ 450℃ 400℃ 350℃ 400℃ 350℃ 400℃ 350℃ 450℃ | 450℃ 450℃ 400℃ 350℃ 400℃ 350℃ 400℃ 350℃ 400℃ | 500℃ 500℃ 450℃ 400℃ 450℃ 400℃ 500℃ 400℃ 450℃ | 500℃ 500℃ 350℃ 300℃ 400℃ 300℃ 400℃ 300℃ 450℃ | 490℃ 490℃ 330℃ 290℃ 390℃ 290℃ 370℃ 290℃ 420℃ | Good good | 330MPa 330MPa 310MPa 260MPa 300MPa 270MPa 260MPa 250MPa 300MPa | 200MPa 200MPa 180MPa 160MPa 180MPa 170MPa 180MPa 180MPa 220MPa |
Embodiment 13
Use general-purpose alloy AZ91 (Mg-9Al-0.7Zn-0.2Mn), at the die casting casting condition:
Cold-chamber diecasting machine 350T, 660 ℃ of (SF of melt temperature
6Diluent gas),
Casting pressure 600kgf/mm
2, 400kgf/mm pressurizes after filling
2,
Spouting velocity 4m/ second, 5/100 second filling time in chamber, fastening part wall thickness 15mm,
170 ℃ of lower ACG (alternating current generator) lids of making two-wheel vehicle used engine of mold temperature (fixing, variable), but, shape is shaped by die casting, the fastener hole section at fastening edge is configured as 10mm for φ 30 relative design wall thickness 5mm, pass through forging condition: the punching press that the temperature of punching press forging machine 100T, 300 ℃ of forging temperatures, upper low punch is 270 ℃ is forged, the wall thickness that makes the fastener hole section at fastening edge is 5mm, after this fastener hole is carried out machining.The defective such as forging, can not break in the machining.And, although the case hardness (Brinell hardness) of measuring is 65, become 73 after the forging processing after casting under hard sphere diameter 10mm, test load 500kg, the condition of 30 seconds retention times.
Embodiment 14
Use general-purpose alloy AM50 (Mg-5Al-0.2Mn), at the die casting casting condition:
Cold-chamber diecasting machine 350T, 680 ℃ of (SF of melt temperature
6Diluent gas),
Casting pressure 600kgf/mm
2, 400kgf/mm pressurizes after filling
2,
Spouting velocity 4m/ second, 3/100 second filling time in chamber, fastening part wall thickness 15mm,
180 ℃ of lower four-wheel air bag for vehicle retainers of making of mold temperature (fixing, variable), but, shape is shaped by die casting, the fastener hole section at fastening edge is configured as 6mm for φ 30 relative design wall thickness 3mm, pass through forging condition: the punching press that the temperature of punching press forging machine 100T, 300 ℃ of forging temperatures, upper low punch is 270 ℃ is forged, the wall thickness that makes the fastener hole section at fastening edge is 3mm, after this fastener hole is carried out machining.The defective such as forging, can not break in the machining.And, although the case hardness (Brinell hardness) of measuring is 55, become 62 after the forging processing after casting under hard sphere diameter 10mm, test load 500kg, the condition of 30 seconds retention times.
Embodiment 15～21
Use the magnesium alloy of following composition:
(10)Mg-10Al-5MM-5Ca-0.2Mn、
(11)Mg-10Al-5MM-5Sr-0.5Ca-0.2Mn、
(12)Mg-7Al-2.5MM-2.5Ca-0.5Sr-0.2Mn、
(13)Mg-1Al-0.2MM-0.02Ca-0.8Mn、
(14)Mg-5Zn-2MM-1.5Sr-0.8Zr、
(15)Mg-0.2Zn-0.2MM-0.5Ca-0.6Zr、
(16)Mg-1Zn-5.5Y-2MM-1.5Sr-0.5Zr-0.02Ca
At the die casting casting condition:
Cold-chamber diecasting machine 250T, melt temperature are set as such as the 5th table institute temp. displaying function,
Casting pressure 600kgf/mm
2, 400kgf/mm pressurizes after filling
2,
2/100 second filling time in spouting velocity 5m/ second, chamber,
180 ℃ of lower test sheet materials of making 150mm * 150mm * 6mm of mold temperature (fixing, variable), in forging condition:
Punching press forging machine 100T, flat-die forging ground extension drawing-down,
Forging temperature, drift temperature are set in temperature shown in the 5th table according to each alloy, and it is thick to make the test film of 30mm * 30mm * 6mm become 3mm.
Be explained, all use SF in any situation
6The liquation of diluent gas when melting keeps atmosphere, and the mould during extruding uses cooling tube to carry out adjustment, also is blown into simultaneously Ar gas when forging temperature surpasses 400 ℃ during forging.The characteristic of the forging product that obtains is shown in the 5th table.
The 5th table
| Alloy | Melt temperature | Forging temperature | Punching press (temperature) | Hot strength (room temperature) | Hot strength (150 ℃) | |
| Embodiment 15 embodiment 16 embodiment 17 embodiment 18 embodiment 19 embodiment 20 embodiment 21 | (10) (11) (12) (13) (14) (15) (16) | 650℃ 650℃ 670℃ 700℃ 650℃ 700℃ 700℃ | 450℃ 450℃ 400℃ 350℃ 400℃ 300℃ 400℃ | 400℃ 400℃ 370℃ 340℃ 370℃ 290℃ 390℃ | 350MPa 350MPa 330MPa 280MPa 300MPa 260MPa 320MPa | 220MPa 220MPa 200MPa 180MPa 200MPa 180MPa 270MPa |
Embodiment 22～31 and comparative example 7～10
In embodiment 22～31 and comparative example 7～10, use the magnesium alloy of following composition (quality %).
AZ31：Mg-3％Al-0.7％Zn-0.2％Mn、
AZ61：Mg-6％Al-0.7％Zn-0.2％Mn、
AM50：Mg-5％Al-0.2％Mn、
ACM522:Mg-5%Al-2%Ca-2% cerium alloy-0.2%Mn.
Above-mentioned any raw material magnesium alloy of packing in the crucible of cast steel casting thing system also melts it, and in order to improve the corrosion resistance of alloy, in this liquation, add the cerium alloy of 0.2 quality % and make the boiling of Ar gas, and, so that dilution SF
6Flow through this molten surface.Melt temperature is maintained 650～700 ℃, at 200 ℃ of mold temperatures, spouting velocity 4.5m/ second, ejection pressure 450kfg/cm
2Condition under cast to make the sheet material of 100mm * 100m, thickness 0.2～5mm by die casting.And for a part of sheet material, making blank temperature is 350 ℃, so that rolling direction rotationally enforcement calendering of per 90 degree in each path.Its depression degree is shown in the 6th table.The average crystallite granularity of the metal structure of the kind of use alloy, the manufacture method of sheet material, the depression degree in the calendering situation, final thickness of slab, final sheet material is shown in the 6th table.
And, prepare the freely extrusion plate of continuous casting billet shown in the 7th table and calendering section bar, as a comparative example.
The 6th table
| Alloy | Manufacturing method of plate thereof | Depress | Final thickness of slab | Grain size number | |
| Embodiment 22 embodiment 23 embodiment 24 embodiment 25 embodiment 26 embodiment 27 embodiment 28 embodiment 29 embodiment 30 embodiment 31 | AZ31 AZ31 AZ31 AZ31 AZ31 AM50 AM50 AM50 ACM522 ACM522 | Casting+the calendering of casting mould mold casting+Die mold casting+Die mold casting+Die mold mold | 5→1.5mm 1.5→0.5mm 1.5→0.5mm 1→0.5mm | 5mm 1.5mm 1.5mm 0.5mm 0.5mm 0.8mm 0.8mm 0.2mm 1mm 0.8mm | 100μm 70μm 70μm 40μm 30μm 25μm 25μm 20μm 10μm 10μm |
The 7th table
| Alloy | Manufacturing method of plate thereof | Thickness of slab | |
| Comparative example 7 comparative examples 8 comparative examples 9 comparative examples 10 | AZ31 AZ31 AZ31 AZ61 | Extrusion plate calendering material calendering material calendering material | 5mm 1.5mm 0.8mm 1.5mm |
Use above-described embodiment and comparative example, respectively in the processing temperature shown in the 8th table, make bottom surface diameter 20mm, height 30mm is above, punching press inclined-plane, side 5 is spent cup-shaped test specimen by punching press (plate forgings).At this moment, end face is processed.Plastic working and corrosion resistance by following standard evaluation punching press (plate forging).These evaluation results are shown in the 8th table.
＜plastic working 〉
Zero: test specimen does not have the defectives such as crack,
△: although test specimen does not have the crack, have the apparent problems such as shrinkage,
*: test specimen has the crack.
＜corrosion resistance 〉
Observe the surface state of sheet material brine spray after 72 hours.
◎: white rust generation area occupation ratio (than AZ91 excellent corrosion resistance) below 10%,
Zero: white rust generation area occupation ratio is (degree of corrosion resistance AZ91) below 20% more than 10%,
△: white rust generation area occupation ratio is more than 20% below 50%,
*: white rust generation area occupation ratio surpasses 50%.
The 8th table
| Processing temperature | Plastic working | Corrosion resistance | |
| Embodiment 22 embodiment 23 embodiment 24 embodiment 25 embodiment 26 embodiment 27 embodiment 28 embodiment 29 embodiment 30 embodiment 31 comparative examples 7 comparative examples 8 comparative example 9-1 comparative example 9-2 comparative examples 10 | 350℃ 300℃ 250℃ 250℃ 250℃ 250℃ 250℃ 200℃ 250℃ 250℃ 350℃ 350℃ 300℃ 250℃ 300℃ | ○ ○ ○ △ ○ △ ○ ○ ○ ○ ○ ○ ○ △ × | △ △ △ △ △ ○ ○ ○ ◎ ◎ × × × × △ |
Claims (6)
1. the manufacture method of a magnesium alloy plastic process product, it is characterized in that, at 250～550 ℃ of lower die casting casting ingots that keep magnesium alloy, mold temperature maintained than this die casting casting ingot keep under the temperature of low 10～50 ℃ of temperature, partly or wholly implement plastic working, so that intensity improves
Magnesium alloy is for comprising
(1) be selected from least a of aluminium 1～10 quality %, zinc 0.2～5 quality % and silver 0.2～5 quality %,
(2) be selected from least a of rare earth metal 0.2～5 quality %, calcium 0.02～5 quality %, strontium 0.02～5 quality % and silicon 0.2～5 quality %, and
(3) be selected from least a that manganese 1.5 quality % are following, zirconium 1.5 quality % are following, the magnesium alloy that remainder is made of magnesium and inevitable impurity.
2. the manufacture method of magnesium alloy plastic process product as claimed in claim 1 is characterized in that, carries out continuously die casting casting and plastic working.
3. the manufacture method of magnesium alloy plastic process product as claimed in claim 2 is characterized in that, implements no longer heatedly plastic working after the die casting casting.
4. such as the manufacture method of claim 1,2 or 3 described magnesium alloy plastic process products, it is characterized in that plastic working is extruding, calendering, forging or punching press.
5. the magnesium alloy plastic process product that obtains of the manufacture method of magnesium alloy plastic process product according to claim 4.
6. use conveyer, the information household appliances of the magnesium alloy plastic process product that the manufacture method by magnesium alloy plastic process product claimed in claim 4 obtains, the parts of industry machine.
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| CN116162874A (en) * | 2023-02-17 | 2023-05-26 | 中国科学院长春应用化学研究所 | Deformable magnesium alloy and preparation method thereof |
Family Cites Families (13)
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|---|---|---|---|---|
| US1570868A (en) * | 1920-08-04 | 1926-01-26 | American Magnesium Corp | Extruding magnesium |
| JP4776751B2 (en) * | 2000-04-14 | 2011-09-21 | パナソニック株式会社 | Magnesium alloy sheet manufacturing method |
| JP2001328033A (en) * | 2000-05-19 | 2001-11-27 | Matsushita Electric Ind Co Ltd | Metal small piece and method of making it |
| JP3869255B2 (en) * | 2001-06-14 | 2007-01-17 | 富士通株式会社 | Metal molded body manufacturing method and metal molded body manufactured thereby |
| JP3861720B2 (en) * | 2002-03-12 | 2006-12-20 | Ｔｋｊ株式会社 | Forming method of magnesium alloy |
| JP2003340553A (en) * | 2002-05-28 | 2003-12-02 | Sumitomo Metal Ind Ltd | Continuous casting method for magnesium alloy sheet |
| JP4263463B2 (en) * | 2002-11-29 | 2009-05-13 | 株式会社不二越 | Magnesium alloy ingot and manufacturing method thereof |
| CN1203203C (en) * | 2003-01-08 | 2005-05-25 | 华南理工大学 | Magnesium-aluminium-zinc alloy containing rare earth and its preparing method |
| KR101127113B1 (en) * | 2004-01-09 | 2012-03-26 | 켄지 히가시 | Magnesium alloy for die cast and magnesium die cast products using the same |
| CN1603020A (en) * | 2004-11-12 | 2005-04-06 | 洛阳铜加工集团有限责任公司 | Technological process for continuous casting and rolling wrought magnesium alloy thin plate and band |
| CN100363147C (en) * | 2005-05-20 | 2008-01-23 | 东北轻合金有限责任公司 | Method for extruding shape bar from magnesium alloy |
| CN100363145C (en) * | 2005-05-20 | 2008-01-23 | 东北轻合金有限责任公司 | Method for manufacturing extruded bar from magnesium alloy |
| CN100400699C (en) * | 2006-07-10 | 2008-07-09 | 东北大学 | Method for preparing 300MPa grade and isotropous AZ31 magnesium alloy sheet |
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2007
- 2007-03-19 JP JP2007071405A patent/JP2008229650A/en active Pending
- 2007-11-23 KR KR1020070120092A patent/KR20080085662A/en not_active Application Discontinuation
- 2007-11-29 CN CN2007103068966A patent/CN101269386B/en not_active Expired - Fee Related
- 2007-11-29 CN CN201010119321A patent/CN101773948A/en active Pending
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| KR20080085662A (en) | 2008-09-24 |
| CN101773948A (en) | 2010-07-14 |
| CN101269386B (en) | 2010-04-21 |
| CN101804553A (en) | 2010-08-18 |
| CN101269386A (en) | 2008-09-24 |
| JP2008229650A (en) | 2008-10-02 |
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