CN102618759B - Low-shrinkage magnesium alloy - Google Patents
Low-shrinkage magnesium alloy Download PDFInfo
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- CN102618759B CN102618759B CN201210107724.7A CN201210107724A CN102618759B CN 102618759 B CN102618759 B CN 102618759B CN 201210107724 A CN201210107724 A CN 201210107724A CN 102618759 B CN102618759 B CN 102618759B
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- 229910000861 Mg alloy Inorganic materials 0.000 title claims abstract description 117
- 239000011777 magnesium Substances 0.000 claims abstract description 33
- 229910045601 alloy Inorganic materials 0.000 claims abstract description 32
- 239000000956 alloy Substances 0.000 claims abstract description 32
- REDXJYDRNCIFBQ-UHFFFAOYSA-N aluminium(3+) Chemical class [Al+3] REDXJYDRNCIFBQ-UHFFFAOYSA-N 0.000 claims abstract description 32
- 229910052748 manganese Inorganic materials 0.000 claims abstract description 28
- 229910052744 lithium Inorganic materials 0.000 claims abstract description 25
- 229910052758 niobium Inorganic materials 0.000 claims abstract description 25
- 229910052761 rare earth metal Inorganic materials 0.000 claims abstract description 15
- 150000002910 rare earth metals Chemical class 0.000 claims abstract description 14
- 229910052749 magnesium Inorganic materials 0.000 claims abstract description 6
- 229910052782 aluminium Inorganic materials 0.000 claims abstract description 5
- 229910052688 Gadolinium Inorganic materials 0.000 claims description 19
- 229910052684 Cerium Inorganic materials 0.000 claims description 5
- 229910052692 Dysprosium Inorganic materials 0.000 claims description 5
- 229910052691 Erbium Inorganic materials 0.000 claims description 5
- 229910052689 Holmium Inorganic materials 0.000 claims description 5
- 229910052779 Neodymium Inorganic materials 0.000 claims description 5
- 229910052771 Terbium Inorganic materials 0.000 claims description 5
- 229910052746 lanthanum Inorganic materials 0.000 claims description 5
- 229910052727 yttrium Inorganic materials 0.000 claims description 5
- 229910017073 AlLi Inorganic materials 0.000 claims description 4
- 229940039694 Alli Drugs 0.000 claims description 4
- AHLBNYSZXLDEJQ-FWEHEUNISA-N Orlistat Chemical compound CCCCCCCCCCC[C@H](OC(=O)[C@H](CC(C)C)NC=O)C[C@@H]1OC(=O)[C@H]1CCCCCC AHLBNYSZXLDEJQ-FWEHEUNISA-N 0.000 claims description 4
- 238000003723 Smelting Methods 0.000 claims description 4
- 229960001243 orlistat Drugs 0.000 claims description 4
- 238000005266 casting Methods 0.000 abstract description 9
- 238000004512 die casting Methods 0.000 abstract description 5
- 239000000203 mixture Substances 0.000 abstract description 4
- 239000004411 aluminium Substances 0.000 abstract description 3
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminum Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 abstract description 3
- FYYHWMGAXLPEAU-UHFFFAOYSA-N magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 abstract description 3
- 239000010955 niobium Substances 0.000 abstract 3
- 239000011572 manganese Substances 0.000 abstract 2
- 238000002425 crystallisation Methods 0.000 abstract 1
- 230000005712 crystallization Effects 0.000 abstract 1
- WHXSMMKQMYFTQS-UHFFFAOYSA-N lithium Chemical compound [Li] WHXSMMKQMYFTQS-UHFFFAOYSA-N 0.000 abstract 1
- PWHULOQIROXLJO-UHFFFAOYSA-N manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 abstract 1
- GUCVJGMIXFAOAE-UHFFFAOYSA-N niobium Chemical compound [Nb] GUCVJGMIXFAOAE-UHFFFAOYSA-N 0.000 abstract 1
- 238000007711 solidification Methods 0.000 abstract 1
- 238000000034 method Methods 0.000 description 30
- 229910000838 Al alloy Inorganic materials 0.000 description 12
- 239000012535 impurity Substances 0.000 description 9
- XKRFYHLGVUSROY-UHFFFAOYSA-N argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 8
- 239000003795 chemical substances by application Substances 0.000 description 8
- 238000002844 melting Methods 0.000 description 6
- 238000007670 refining Methods 0.000 description 6
- 230000000052 comparative effect Effects 0.000 description 5
- 238000005336 cracking Methods 0.000 description 5
- 239000007789 gas Substances 0.000 description 5
- 238000007689 inspection Methods 0.000 description 5
- 229910052786 argon Inorganic materials 0.000 description 4
- 229910052751 metal Inorganic materials 0.000 description 4
- 239000002184 metal Substances 0.000 description 4
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 4
- 230000000694 effects Effects 0.000 description 3
- 238000009413 insulation Methods 0.000 description 3
- 239000004576 sand Substances 0.000 description 3
- 239000007787 solid Substances 0.000 description 3
- 229910017863 MgGd Inorganic materials 0.000 description 2
- 229910017697 MgY Inorganic materials 0.000 description 2
- 150000001875 compounds Chemical class 0.000 description 2
- 239000000356 contaminant Substances 0.000 description 2
- 238000005495 investment casting Methods 0.000 description 2
- 239000007788 liquid Substances 0.000 description 2
- 239000000243 solution Substances 0.000 description 2
- 238000003756 stirring Methods 0.000 description 2
- 238000010792 warming Methods 0.000 description 2
- 229910000967 As alloy Inorganic materials 0.000 description 1
- 229910001018 Cast iron Inorganic materials 0.000 description 1
- 229910017916 MgMn Inorganic materials 0.000 description 1
- 229910001257 Nb alloy Inorganic materials 0.000 description 1
- 229910052772 Samarium Inorganic materials 0.000 description 1
- 240000006802 Vicia sativa Species 0.000 description 1
- 238000010521 absorption reaction Methods 0.000 description 1
- 229910052790 beryllium Inorganic materials 0.000 description 1
- 229910052802 copper Inorganic materials 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 238000007499 fusion processing Methods 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- XEEYBQQBJWHFJM-UHFFFAOYSA-N iron Substances [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000000155 melt Substances 0.000 description 1
- 239000007769 metal material Substances 0.000 description 1
- 230000003647 oxidation Effects 0.000 description 1
- 238000007254 oxidation reaction Methods 0.000 description 1
- 238000010120 permanent mold casting Methods 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 239000002994 raw material Substances 0.000 description 1
- 229910052706 scandium Inorganic materials 0.000 description 1
- 239000006104 solid solution Substances 0.000 description 1
- 238000007669 thermal treatment Methods 0.000 description 1
- 229910052725 zinc Inorganic materials 0.000 description 1
Abstract
The invention discloses low-shrinkage magnesium alloy, and belongs to the field of magnesium alloy. The low-shrinkage magnesium alloy comprises the following elements in percent by weight: 1.5 to 25% of Al (aluminium), 0.13 to 2% of Mn (manganese), 0.0002 to 16% of rare earth, 0.0002 to 4% of Nb (niobium), 0.0002 to 9% of Li (lithium), and Mg (magnesium) in balancing amount. The beta-phase structure is changed by adding the rare earth element and the Nb element in the magnesium alloy, the grain refinement is achieved through adding the Li element, and through the combination of the elements, the crystallization latent heat is changed in alloy solidification, thereby obtaining the low-shrinkage magnesium alloy which has an excellent filling capacity, low shrinkage, excellent mechanical property, machinability, flowability and good die-casting performance and is suitable for casting.
Description
Technical field
The present invention relates to a kind of magnesium alloy, particularly a kind of MgAlMn is low-shrinkage magnesium alloy.
Background technology
Along with scientific and technological development, the vehicles taking automobile as representative need to, by alleviating the weight of vehicle body, further be researched and developed the product innovation that fuel availability is higher.In automobile industry, magnesium alloy, as a kind of novel lightweight metal material, is used for substituting traditional cast iron by automaker, to realize the object that alleviates tare.
At present, domestic MgAlMn is that the diecast magnesium alloy trade mark has YM202, YM203, YM204, YM205; The MgAlMn of USS ASTM B is that the diecast magnesium alloy trade mark has AM50A, AM60A, AM60B; The MgAlMn of Nippon Standard JIS H is that the diecast magnesium alloy trade mark has MDC2B, MDC4, MDC5; The MgAlMn of European standard EN is that the diecast magnesium alloy trade mark has EN-MC21210, EN-MC21220, EN-MC21230.The alloy of these trades mark, mobility, mechanical property, die casting performance are all very good, are widely used in the cast forms such as permanent mold casting, precision casting, low-pressure casting, die casting, semi-solid casting, sand mold casting.
Find that prior art at least exists following problem realizing contriver in process of the present invention: magnesium alloy is in the time of casting, molten metal, in the process that is frozen into solid, is subject to the impact of volumetric shrinkage, and internal stress is very large, easily cause cast(ing) surface cracking, the phenomenon that foundry goods die sinking ruptures even occurs.The impact that this decrepitation is serious the application of cast magnesium alloys, have influence on magnesium alloy member size and qualification rate.Above-mentioned diecast magnesium alloy linear shrinkage ratio is 1.5-2%, cannot effectively avoid the cast(ing) surface cracking phenomena causing because of volumetric shrinkage.
Summary of the invention
In order to solve above-mentioned problems of the prior art, the embodiment of the present invention provides a kind of low-shrinkage magnesium alloy.Described technical scheme is as follows:
A kind of low-shrinkage magnesium alloy, described magnesium alloy is made up of Mg, Al, Mn, rare earth (RE), Nb, Li, its weight percent consists of Al 1.5-25%, Mn 0.13-2%, rare earth 0.0002-16%, Nb 0.0002-4%, Li 0.0002-9%, and all the other are Mg.
Wherein, described rare earth is at least one in Gd, Y, Sc, Sm, Pr, Yb, Nd, La, Ce, Tb, Dy, Ho and Er.
Preferably, described rare earth is at least one in Gd or Gd and Y, Sc, Sm, Pr, Yb, Nd, La, Ce, Tb, Dy, Ho and Er.
Preferably, its weight percent consists of Al 1.6-6.5%, Mn 0.13-0.7%, Gd 0.1-2%, Nb 0.05-1%, Li 0.02-2%, and all the other are Mg.
More have choosing, its weight percent consists of Al 4.4-6.5%, Mn 0.26-0.6%, Gd 0.1-0.8%, Nb 0.05-0.6%, Li 0.02-2%, and all the other are Mg.
Most preferably, its weight percent consists of Al 6%, Mn 0.45%, Gd 0.4%, Nb 0.2%, Li 0.5%, and all the other are Mg.
The beneficial effect that the technical scheme that the embodiment of the present invention provides is brought is: in magnesium alloy provided by the invention, RE can form MgRE compound with Mg, Nb can form some resistant to elevated temperatures metallic compounds with other elements (as Al), and Li has strong crystal grain thinning and purifies aluminium alloy effect.Due to the combined action of above-mentioned element, while making alloy graining, latent heat changes, under the heat absorption of above-mentioned element, heat release combined action, it is diecast magnesium alloy that the time that aluminium alloy provided by the invention keeps liquid in mould is obviously longer than existing AM, make alloy in process of setting, feeding is abundant, built-in thermal stress is little, heat crack resistance is good, simultaneously, because magnesium alloy liquid volume and solid-state volume variation that the embodiment of the present invention provides are very little, therefore there is the feature that cavity filling ability is good, shrinking percentage is low.The characteristics such as alloy of the present invention also has good mechanical property, and machinability, mobility and die casting are good.
Embodiment
For making the object, technical solutions and advantages of the present invention clearer, below embodiment of the present invention is described further in detail.
Manufacture craft, the heat treating method of the magnesium alloy that the embodiment of the present invention provides are described as follows:
1, the magnesium alloy that the embodiment of the present invention provides can be made by following three kinds of melting technologies:
Technique one: the magnesium alloy composition and the content alloyage that provide according to the embodiment of the present invention; in resistance furnace, add magnesium ingot, aluminium ingot, MgMn master alloy, AlNb master alloy or NbAl master alloy; heat up to resistance furnace used, in the time that the above-mentioned metal adding melts soon, adopt argon shield or magnesium alloy covering agent protection.While being warmed up to 720 DEG C-780 DEG C, add MgRE master alloy (as MgGd, MgY, MgNd etc.) or AlRE master alloy, AlLi master alloy or MgLi master alloy, and stir, leave standstill insulation 30 minutes at 720 DEG C-780 DEG C, obtain aluminium alloy.Water a fritter sample with gained aluminium alloy, detect its Melting Quality, as: carry out gas content inspection according to gas content inspection method, if second-rate, need carry out refining treatment; If up-to-standard, described aluminium alloy temperature adjustment to 700 DEG C-740 DEG C is skimmed, then pour into a mould, obtain the foundry goods of alloy of the present invention.
In this technique, resistance furnace also can replace with other smelting furnaces; Magnesium alloy covering agent and master alloy product are market sale product; Refining treatment method adopts the ordinary method of the industry.
Technique two: the magnesium alloy composition and the content alloyage that provide according to the embodiment of the present invention, in vacuum oven, add aluminium ingot, Mn or Mn agent, AlNb master alloy or NbAl master alloy, be warming up to 820 DEG C, insulation 2-8 hour, then cool to 720 DEG C-780 DEG C, add magnesium ingot, RE, AlLi master alloy or MgLi master alloy.After added melting of metal, 720 DEG C-780 DEG C insulations 30 minutes, obtain aluminium alloy, adopt argon shield or magnesium alloy covering agent protection to prevent aluminium alloy oxidation.Water a fritter sample with gained aluminium alloy, detect its Melting Quality, as: the inspection of gas content, if second-rate, need carry out refining treatment; If up-to-standard, described aluminium alloy temperature adjustment to 700 DEG C-740 DEG C is skimmed, then pour into a mould, obtain the foundry goods of alloy of the present invention.
In this technique, vacuum oven can substitute with other smelting furnaces such as main frequency furnaces; Magnesium alloy covering agent, rare earth, Mn agent, master alloy are sell goods on market; Refining treatment method adopts the ordinary method of the industry.
Technique three: the magnesium alloy composition and the content alloyage that provide according to the embodiment of the present invention; in smelting furnace, adding standard brand MgAlMn is diecast magnesium alloy, AlNb master alloy or NbAl master alloy, and above-mentioned metal adopts argon shield or magnesium alloy covering agent protection while fusing soon.While being warmed up to 720 DEG C-780 DEG C, add MgRE master alloy (as MgGd, MgY, MgNd etc.) or AlRE master alloy, AlLi master alloy or MgLi master alloy, and stir, leave standstill insulation 30 minutes at 720 DEG C-780 DEG C, obtain aluminium alloy.Water a fritter sample with gained aluminium alloy, detect its Melting Quality, as: carry out gas content inspection according to gas content inspection method, if second-rate, need carry out refining treatment; If up-to-standard, described aluminium alloy temperature adjustment to 700 DEG C-740 DEG C is skimmed, then pour into a mould, obtain the foundry goods of alloy of the present invention.
In this technique, magnesium alloy covering agent and master alloy are sell goods on market; Refining treatment method adopts the ordinary method of the industry.
Thermal treatment and the treatment process thereof of the magnesium alloy that 2, the embodiment of the present invention provides:
Die casting in the magnesium alloy that the embodiment of the present invention provides can not heat-treated, and the cast member of other form can be heat-treated, and generally adopts T4 solution treatment.T4 solid solution treatment process is: cast member is warming up in chamber type electric resistance furnace to 390 DEG C, argon shield, is incubated 16 hours, cast member come out of the stove after shrend, 50 DEG C of water temperatures.
Be subject to fusion process to select the impact of some other inevitable factor in the purity of raw material and melting, castingprocesses, the diecast magnesium alloy that the embodiment of the present invention provides may contain inevitable impurity, as Zn, Fe, Cu, Be etc., as long as described impurity does not cause obvious impact to the performance of magnesium alloy, and total impurities is controlled at the weight percent < 0.5% in described magnesium alloy finished product, in the weight percent < 0.1% of single contaminant in described magnesium alloy finished product, exist trace impurity also to allow.
Embodiment 1
Prepare magnesium alloy by step described in above-mentioned technique one, foundry goods adopts die cast, and the weight percent of described magnesium alloy consists of Al 1.5%, Mn 0.13%, Sm 0.0002%, Nb 0.0002%, Li 0.0002%, and all the other are Mg.
Foundry goods is heat-treated.The performance of the Mg alloy castings that the present embodiment provides is referring to table 1.
Embodiment 2
Prepare magnesium alloy by step described in above-mentioned technique one, foundry goods adopts semi-solid casting, and the weight percent of described magnesium alloy consists of Al 25%, Mn 2%, Y 16%, Nb 4%, Li 9%, and all the other are Mg.
Foundry goods is heat-treated.The performance of the Mg alloy castings that the present embodiment provides is referring to table 1.
Embodiment 3
Prepare magnesium alloy by step described in above-mentioned technique two, foundry goods adopts Hpdc, and the weight percent of magnesium alloy consists of Al 6%, Mn 0.2%, Gd 0.2%, Nb 1%, Li 0.6%, and all the other are Mg;
The performance of the Mg alloy castings that the present embodiment provides is referring to table 1.
Embodiment 4
Prepare magnesium alloy by step described in above-mentioned technique one, foundry goods adopts low-pressure casting, and the weight percent of described magnesium alloy consists of Al 1.6%, Mn 0.13%, Ho 0.1%, Nb 0.05%, Li 0.02%, and all the other are Mg.
Foundry goods is heat-treated.The performance of the Mg alloy castings that the present embodiment provides is referring to table 1.
Embodiment 5
Prepare magnesium alloy by step described in above-mentioned technique three, described standard brand diecast magnesium alloy used in preparation process is AM60B, foundry goods adopts precision casting, and the weight percent of described magnesium alloy consists of Al 6.5%, Mn 0.7%, Gd 2%, Nb 1%, Li 2%, and all the other are Mg.
Foundry goods is heat-treated.The performance of the Mg alloy castings that the present embodiment provides is referring to table 1.
Embodiment 6
Prepare magnesium alloy by step described in above-mentioned technique one, foundry goods adopts sand mold casting, and the weight percent of described magnesium alloy consists of Al 4.4%, Mn 0.26%, Gd 0.1%, Nb 0.05%, Li 0.02%, and all the other are Mg.
Foundry goods is heat-treated.The performance of the Mg alloy castings that the present embodiment provides is referring to table 1.
Embodiment 7
Prepare magnesium alloy by step described in above-mentioned technique two, foundry goods adopts Hpdc, and the weight percent of described magnesium alloy consists of Al 6.5%, Mn 0.6%, Gd 0.8%, Nb 0.6%, Li 2%, and all the other are Mg.
The performance of the Mg alloy castings that the present embodiment provides is referring to table 1.
Embodiment 8
Prepare magnesium alloy by step described in above-mentioned technique two, foundry goods adopts Hpdc, and the weight percent of described magnesium alloy consists of Al 6.5%, Mn 0.6%, Gd 0.4%, Nd 0.4%, Nb 0.6%, Li 2%, and all the other are Mg.
The performance of the Mg alloy castings that the present embodiment provides is referring to table 1.
Embodiment 9
Prepare magnesium alloy by step described in above-mentioned technique two, foundry goods adopts Hpdc, and the weight percent of described magnesium alloy consists of Al 6.5%, Mn 0.6%, Ce 0.8%, Nb 0.6%, Li 2%, and all the other are Mg.
The performance of the Mg alloy castings that the present embodiment provides is referring to table 1.
Embodiment 10
Prepare magnesium alloy by step described in above-mentioned technique two, foundry goods adopts die cast, and the weight percent of described magnesium alloy consists of Al 2%, Mn 0.2%, La 1.2%, Nb 0.8%, Li 0.1%, and all the other are Mg.
Foundry goods is heat-treated.The performance of the Mg alloy castings that the present embodiment provides is referring to table 1.
Embodiment 11
Prepare magnesium alloy by step described in above-mentioned technique one, foundry goods adopts sand mold casting, and the weight percent of described magnesium alloy consists of Al 6%, Mn 0.5%, Tb 0.6%, Nb 0.4%, Li 0.5%, and all the other are Mg.
Foundry goods is heat-treated.The performance of the Mg alloy castings that the present embodiment provides is referring to table 1.
Embodiment 12
Prepare magnesium alloy by step described in above-mentioned technique two, foundry goods adopts die cast, and the weight percent of described magnesium alloy consists of Al 10%, Mn 1%, Dy 8%, Nb 2%, Li 1.5%, and all the other are Mg.
Foundry goods is heat-treated.The performance of the Mg alloy castings that the present embodiment provides is referring to table 1.
Embodiment 13
Prepare magnesium alloy by step described in above-mentioned technique two, foundry goods adopts die cast, and the weight percent of described magnesium alloy consists of Al 3%, Mn 0.65%, Er 1%, Nb 0.7%, Li 0.8%, and all the other are Mg.
Foundry goods is heat-treated.The performance of the Mg alloy castings that the present embodiment provides is referring to table 1.
Embodiment 14
Prepare magnesium alloy by step described in above-mentioned technique two, foundry goods adopts die cast, and the weight percent of described magnesium alloy consists of Al 5%, Mn 0.5%, Sc 0.5%, Nb 0.8%, Li 0.4%, and all the other are Mg.
Foundry goods is heat-treated.The performance of the Mg alloy castings that the present embodiment provides is referring to table 1.
Embodiment 15
Prepare magnesium alloy by step described in above-mentioned technique one, foundry goods adopts Hpdc, and described magnesium alloy weight percent consists of Al6%, Mn 0.45%, Gd 0.4%, Nb 0.2%, Li 0.5%, and all the other are Mg.
The performance of the Mg alloy castings that the present embodiment provides is referring to table 1.
Comparative example 1
Prepare magnesium alloy by step described in above-mentioned technique one, foundry goods adopts Hpdc, and described magnesium alloy weight percent consists of Al6%, Mn 0.45%, Gd 0.4%, Nb 0.2%, and all the other are Mg and inevitable impurity.
The performance of the Mg alloy castings that the present embodiment provides is referring to table 1.
Comparative example 2
Prepare magnesium alloy by step described in above-mentioned technique one, foundry goods adopts Hpdc, and described magnesium alloy weight percent consists of Al6%, Mn 0.45%, Gd 0.4%, Li 0.5%, and all the other are Mg and inevitable impurity.
The performance of the Mg alloy castings that the present embodiment provides is referring to table 1.
Comparative example 3
Prepare magnesium alloy by step described in above-mentioned technique one, foundry goods adopts Hpdc, and described magnesium alloy weight percent consists of Al6%, Mn 0.45%, Gd 0.4%, and all the other are Mg and inevitable impurity.
The performance of the Mg alloy castings that the present embodiment provides is referring to table 1.
The Mg alloy castings that each embodiment provides above can contain micro-impurity, the weight percent < 0.5% of described inevitable total impurities in described magnesium alloy finished product, the weight percent < 0.1% of single contaminant in described magnesium alloy finished product.
The linear shrinkage ratio of the Mg alloy castings that various embodiments of the present invention and comparative example provide is referring to table 1.
The linear shrinkage ratio table of the Mg alloy castings that the each embodiment of table 1 provides
As shown in Table 1, the linear shrinkage ratio of the Mg alloy castings that the embodiment of the present invention provides is all less than 1%, is diecast magnesium alloy well below existing MgAlMn, has good hot-cracking resistance; Simultaneously referring to embodiment 15 and comparative example 1-3, the Mg alloy castings that the embodiment of the present invention provides, compared with not adding Li or Nb or Mg alloy castings that both all do not add, has better hot-cracking resistance; The linear shrinkage ratio of embodiment 7,8 and 15 is lower than other embodiment, and the scope of embodiment 7,8 and 15 each components is in Al4.4-6.5%, Mn 0.26-0.6%, Gd 0.1-0.8%, Nb 0.05-0.6%, Li 0.02-2%; By the contrast between embodiment 7-9, the known RE containing has the effect of Gd better; The linear shrinkage ratio of the Mg alloy castings that embodiment 15 provides is minimum, and the cast magnesium alloys hot-cracking resistance that embodiment 15 provides is the strongest.
The foregoing is only preferred embodiment of the present invention, in order to limit the present invention, within the spirit and principles in the present invention not all, any amendment of doing, be equal to replacement, improvement etc., within all should being included in protection scope of the present invention.
Claims (6)
1. a low-shrinkage magnesium alloy, it is characterized in that, described magnesium alloy is made up of Mg, Al, Mn, rare earth, Nb, Li, its weight percent consists of Al1.5-25%, Mn0.13-2%, rare earth 0.0002-16%, Nb0.0002-4%, Li0.0002-9%, all the other are Mg, described Nb adds in described magnesium alloy by the form of AlNb master alloy or NbAl master alloy, described Li adds in described magnesium alloy by the form of AlLi master alloy or MgLi master alloy, and the smelting temperature of the master alloy of described Nb is 720 DEG C-780 DEG C or 820 DEG C.
2. magnesium alloy according to claim 1, is characterized in that, described rare earth is at least one in Gd, Y, Sc, Sm, Pr, Yb, Nd, La, Ce, Tb, Dy, Ho and Er.
3. magnesium alloy according to claim 1 and 2, is characterized in that, described rare earth is at least one in Gd or Gd and Y, Sc, Sm, Pr, Yb, Nd, La, Ce, Tb, Dy, Ho and Er.
4. magnesium alloy according to claim 3, is characterized in that, its weight percent consists of Al1.6-6.5%, Mn0.13-0.7%, Gd0.1-2%, Nb0.05-1%, Li0.02-2%, and all the other are Mg.
5. magnesium alloy according to claim 4, is characterized in that, its weight percent consists of Al4.4-6.5%, Mn0.26-0.6%, Gd0.1-0.8%, Nb0.05-0.6%, Li0.02-2%, and all the other are Mg.
6. magnesium alloy according to claim 5, is characterized in that, its weight percent consists of Al6%, Mn0.45%, Gd0.4%, Nb0.2%, Li0.5%, and all the other are Mg.
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| CN105256208A (en) * | 2015-10-09 | 2016-01-20 | 天长市兴宇铸造有限公司 | Boron nitride nanotube modifying Mg-Al-Mn magnesium alloy material for casting automobile parts and preparation method thereof |
| CN107779708B (en) * | 2017-12-08 | 2019-08-23 | 浙江海洋大学 | A kind of high intensity super-light Mg-Li alloy and preparation method thereof |
Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1276276A (en) * | 1999-06-08 | 2000-12-13 | 三井金属矿业株式会社 | Metal die device, die-casting method and die-cast articles |
| CN102230116A (en) * | 2011-06-23 | 2011-11-02 | 江汉大学 | High-hardness cast magnesium alloy |
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| JPH08134581A (en) * | 1994-11-14 | 1996-05-28 | Mitsui Mining & Smelting Co Ltd | Production of magnesium alloy |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1276276A (en) * | 1999-06-08 | 2000-12-13 | 三井金属矿业株式会社 | Metal die device, die-casting method and die-cast articles |
| CN102230116A (en) * | 2011-06-23 | 2011-11-02 | 江汉大学 | High-hardness cast magnesium alloy |
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| JP特开平8-134581A 1996.05.28 |
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