CN115896513A - Rare earth adding method for rare earth-containing magnesium alloy - Google Patents
Rare earth adding method for rare earth-containing magnesium alloy Download PDFInfo
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- 229910052761 rare earth metal Inorganic materials 0.000 title claims abstract description 46
- 150000002910 rare earth metals Chemical class 0.000 title claims abstract description 40
- 238000000034 method Methods 0.000 title claims abstract description 22
- 229910000861 Mg alloy Inorganic materials 0.000 title claims abstract description 21
- 229910002058 ternary alloy Inorganic materials 0.000 claims abstract description 13
- 229910052727 yttrium Inorganic materials 0.000 claims abstract description 7
- 229910052779 Neodymium Inorganic materials 0.000 claims abstract description 6
- 229910052772 Samarium Inorganic materials 0.000 claims abstract description 6
- 229910052746 lanthanum Inorganic materials 0.000 claims abstract description 6
- 229910052684 Cerium Inorganic materials 0.000 claims abstract description 5
- 229910052691 Erbium Inorganic materials 0.000 claims abstract description 5
- 229910052689 Holmium Inorganic materials 0.000 claims abstract description 5
- 229910052777 Praseodymium Inorganic materials 0.000 claims abstract description 5
- 229910052692 Dysprosium Inorganic materials 0.000 claims abstract description 4
- 239000000956 alloy Substances 0.000 abstract description 33
- 229910045601 alloy Inorganic materials 0.000 abstract description 32
- 238000002844 melting Methods 0.000 abstract description 15
- 230000008018 melting Effects 0.000 abstract description 15
- 229910052751 metal Inorganic materials 0.000 abstract description 6
- 239000002184 metal Substances 0.000 abstract description 6
- 239000000463 material Substances 0.000 abstract description 5
- 238000002360 preparation method Methods 0.000 abstract description 4
- 238000004519 manufacturing process Methods 0.000 abstract description 3
- 239000011777 magnesium Substances 0.000 description 20
- 238000007670 refining Methods 0.000 description 17
- 239000000155 melt Substances 0.000 description 16
- 239000011701 zinc Substances 0.000 description 12
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 description 10
- 229910052749 magnesium Inorganic materials 0.000 description 10
- 238000003756 stirring Methods 0.000 description 10
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 description 8
- 230000000052 comparative effect Effects 0.000 description 8
- 239000007789 gas Substances 0.000 description 8
- 230000001681 protective effect Effects 0.000 description 8
- 239000003795 chemical substances by application Substances 0.000 description 5
- 229910009202 Y—Mn Inorganic materials 0.000 description 4
- 229910001093 Zr alloy Inorganic materials 0.000 description 4
- 239000007788 liquid Substances 0.000 description 4
- 239000000203 mixture Substances 0.000 description 4
- 238000005728 strengthening Methods 0.000 description 4
- 229910052725 zinc Inorganic materials 0.000 description 4
- 239000000243 solution Substances 0.000 description 3
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 229910052688 Gadolinium Inorganic materials 0.000 description 1
- 230000032683 aging Effects 0.000 description 1
- 238000005275 alloying Methods 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000004907 flux Effects 0.000 description 1
- 239000001257 hydrogen Substances 0.000 description 1
- 229910052739 hydrogen Inorganic materials 0.000 description 1
- 125000004435 hydrogen atom Chemical class [H]* 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- 238000001556 precipitation Methods 0.000 description 1
- 239000002893 slag Substances 0.000 description 1
- 239000006104 solid solution Substances 0.000 description 1
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Abstract
本发明涉及有色金属生产技术领域,尤其涉及一种含稀土镁合金的稀土添加方法。含稀土镁合金的稀土添加方法,其特征在于,稀土以稀土三元合金形式添加,所述稀土三元合金为RE1‑RE2‑RE3,所述RE1、RE2、RE3各自独立为La、Ce、Pr、Nd、Sm、Y、Sc、Gd、Dy、Ho、Er中的一种。本发明所述稀土添加方式,通过合理配比各稀土元素含量,使得稀土三元合金熔点降低至680~740℃,与镁合金熔炼温度基本一致;并取消了镁‑稀土中间合金的制备,可按需求配比直接添加,降低了材料成本。The invention relates to the technical field of nonferrous metal production, in particular to a method for adding rare earths to magnesium alloys containing rare earths. The method for adding rare earths to magnesium alloys containing rare earths is characterized in that the rare earths are added in the form of rare earth ternary alloys, the rare earth ternary alloys are RE1-RE2-RE3, and the RE1, RE2, and RE3 are each independently La, Ce, and Pr , Nd, Sm, Y, Sc, Gd, Dy, Ho, Er in one. The rare earth addition method of the present invention reduces the melting point of the rare earth ternary alloy to 680-740°C by rationally proportioning the contents of the rare earth elements, which is basically the same as the melting temperature of the magnesium alloy; and cancels the preparation of the magnesium-rare earth master alloy, which can Add directly according to the ratio of demand, reducing the cost of materials.
Description
技术领域technical field
本发明涉及有色金属生产技术领域,尤其涉及一种含稀土镁合金的稀土添加方法。The invention relates to the technical field of nonferrous metal production, in particular to a method for adding rare earths to magnesium alloys containing rare earths.
背景技术Background technique
稀土元素在镁合金中具备除氢、除氧、除铁及除渣的作用,可以净化熔体。稀土活性高,可在镁合金熔体表面形成致密氧化膜层起到隔绝大气、保护熔体的作用。另外稀土作为合金化及微合金化元素加入镁合金中可以起到细晶强化、固溶强化、析出强化和时效强化的作用,提高镁合金力学性能和耐热性能。但是稀土元素本身熔点较高,与镁的熔点差异较大,难以直接添加,工业应用一般以低熔点镁基稀土中间合金形式添加,这种添加方式需先期制备中间合金,成本较高。本发明针对这一问题,为降低稀土镁合金成本提供一种新型的稀土添加方式,可大幅降低材料成本。Rare earth elements have the functions of removing hydrogen, oxygen, iron and slag in magnesium alloys, and can purify the melt. The rare earth has high activity and can form a dense oxide film on the surface of the magnesium alloy melt to isolate the atmosphere and protect the melt. In addition, adding rare earths as alloying and microalloying elements to magnesium alloys can play the role of fine grain strengthening, solid solution strengthening, precipitation strengthening and aging strengthening, and improve the mechanical properties and heat resistance of magnesium alloys. However, the melting point of rare earth elements is relatively high, which is quite different from that of magnesium, so it is difficult to add them directly. For industrial applications, they are generally added in the form of low melting point magnesium-based rare earth master alloys. This method of addition requires the preparation of master alloys in advance, and the cost is high. The invention aims at this problem, and provides a novel rare earth addition method for reducing the cost of the rare earth magnesium alloy, which can greatly reduce the material cost.
因此,如何提供一种降低稀土镁合金成本的稀土添加方式,以降低镁合金材料的制备成本,是本领域技术人员亟待解决的技术问题。Therefore, how to provide a rare earth addition method to reduce the cost of rare earth magnesium alloys, so as to reduce the production cost of magnesium alloy materials, is a technical problem to be solved urgently by those skilled in the art.
发明内容Contents of the invention
本发明的目的在于提供一种含稀土镁合金的稀土添加方法,以解决现有技术存在的缺陷。The object of the present invention is to provide a method for adding rare earths to magnesium alloys containing rare earths, so as to solve the defects in the prior art.
为了实现上述发明目的,本发明提供以下技术方案:In order to achieve the above-mentioned purpose of the invention, the present invention provides the following technical solutions:
本发明提供了一种含稀土镁合金的稀土添加方法,稀土以稀土三元合金形式添加。The invention provides a method for adding rare earth to a magnesium alloy containing rare earth. The rare earth is added in the form of a rare earth ternary alloy.
优选的,所述稀土三元合金为RE1-RE2-RE3,所述RE1、RE2、RE3各自独立为La、Ce、Pr、Nd、Sm、Y、Sc、Gd、Dy、Ho、Er中的一种。Preferably, the rare earth ternary alloy is RE1-RE2-RE3, and the RE1, RE2, RE3 are each independently one of La, Ce, Pr, Nd, Sm, Y, Sc, Gd, Dy, Ho, Er kind.
优选的,所述RE1质量百分比为40~65%。Preferably, the RE1 mass percentage is 40-65%.
优选的,所述RE2质量百分比为10~40%。Preferably, the RE2 mass percentage is 10-40%.
优选的,所述RE3质量百分比为5~30%。Preferably, the RE3 mass percentage is 5-30%.
经由上述技术方案可知,与现有技术相比,本发明具有如下的有益效果:It can be seen from the above technical solutions that, compared with the prior art, the present invention has the following beneficial effects:
1.本发明所述稀土添加方式,通过合理配比各稀土元素含量,使得稀土三元合金熔点降低至680~740℃,与镁合金熔炼温度基本一致;1. The rare earth addition method of the present invention reduces the melting point of the rare earth ternary alloy to 680-740°C by rationally proportioning the content of each rare earth element, which is basically the same as the melting temperature of the magnesium alloy;
2.本发明所述稀土添加方式,取消了镁-稀土中间合金的制备,可按需求配比直接添加,降低了材料成本。2. The rare earth addition method of the present invention cancels the preparation of the magnesium-rare earth master alloy, and can be directly added according to the required ratio, reducing the material cost.
具体实施方式Detailed ways
本发明提供了本发明提供了一种含稀土镁合金的稀土添加方法,稀土以稀土三元合金形式添加。The present invention provides a method for adding rare earths to magnesium alloys containing rare earths. The rare earths are added in the form of rare earth ternary alloys.
在本发明中,所述稀土三元合金为RE1-RE2-RE3,所述RE1、RE2、RE3各自独立为La、Ce、Pr、Nd、Sm、Y、Sc、Gd、Dy、Ho、Er中的一种,优选为La、Ce、Pr、Nd、Sm、Y、Sc、Gd、Ho、Er中的一种。In the present invention, the rare earth ternary alloy is RE1-RE2-RE3, and the RE1, RE2, RE3 are each independently La, Ce, Pr, Nd, Sm, Y, Sc, Gd, Dy, Ho, Er One of, preferably one of La, Ce, Pr, Nd, Sm, Y, Sc, Gd, Ho, Er.
在本发明中,所述RE1质量百分比为40~65%,优选为41~63%。In the present invention, the RE1 mass percentage is 40-65%, preferably 41-63%.
在本发明中,所述RE2质量百分比为10~40%,优选为12~38%。In the present invention, the RE2 mass percentage is 10-40%, preferably 12-38%.
在本发明中,所述RE3质量百分比为5~30%,优选为6~28%。In the present invention, the RE3 mass percentage is 5-30%, preferably 6-28%.
下面结合实施例对本发明提供的技术方案进行详细的说明,但是不能把它们理解为对本发明保护范围的限定。The technical solutions provided by the present invention will be described in detail below in conjunction with the examples, but they should not be interpreted as limiting the protection scope of the present invention.
本发明实施例及对比例所使用的精炼剂为RJ-6号熔剂。The refining agent used in the examples and comparative examples of the present invention is No. RJ-6 flux.
实施例1Example 1
制备Mg-6Zn-3La-Sm-Y-Mn合金,其中按质量百分比Zn含量为5.0%~6.0%,按质量百分比La含量为2.8%~3.5%,按质量百分比Sm含量为0.5%~1.2%,按质量百分比Y含量为0.5%~1.2%,按质量百分比Mn含量为0.3%~1.0%,余量为Mg。Prepare a Mg-6Zn-3La-Sm-Y-Mn alloy, wherein the Zn content is 5.0% to 6.0% by mass percentage, the La content is 2.8% to 3.5% by mass percentage, and the Sm content is 0.5% to 1.2% by mass percentage , the Y content is 0.5%-1.2% by mass percentage, the Mn content is 0.3%-1.0% by mass percentage, and the balance is Mg.
以La60Sm20Y20三元合金方式添加稀土制备Mg-6Zn-3La-Sm-Y-Mn合金Preparation of Mg-6Zn-3La-Sm-Y-Mn Alloy by Adding Rare Earth in La 60 Sm 20 Y 20 Ternary Alloy
(1)按所述各元素质量百分比配置,其中Mg以纯镁锭方式加入,Zn以纯锌锭方式加入,La、Sm、Y以La60Sm20Y20方式加入,Mn以Mg-20Mn中间合金方式加入。(1) According to the mass percentage of each element, Mg is added in the form of pure magnesium ingot, Zn is added in the form of pure zinc ingot, La, Sm, and Y are added in the form of La 60 Sm 20 Y 20 , and Mn is added in the form of Mg-20Mn master alloy join in.
(2)坩埚预热至200℃,加入配置好的纯镁锭、纯锌锭及Mg-20Mn中间合金,升温至400℃时通入保护气,保护气组成为CO2+SF6。(2) Preheat the crucible to 200°C, add the configured pure magnesium ingots, pure zinc ingots and Mg-20Mn master alloy, and pass in protective gas when the temperature rises to 400°C, the composition of the protective gas is CO 2 +SF 6 .
(3)熔化后升温至700℃加入配置好的La60Sm20Y20合金,熔化后充分搅拌熔体8min。(3) After melting, raise the temperature to 700°C and add the prepared La 60 Sm 20 Y 20 alloy, and fully stir the melt for 8 minutes after melting.
(4)升温至720℃分批次加入占熔体质量百分比1.5%的精炼剂并对熔体持续搅拌进行精炼处理,精炼时间13min。(4) Raise the temperature to 720° C. and add 1.5% of the refining agent accounting for the mass percentage of the melt in batches, and continuously stir the melt for refining treatment, and the refining time is 13 minutes.
(5)精炼结束后捞除表面浮渣,720℃保温,静置40min。(5) After refining, remove the scum on the surface, keep it warm at 720°C, and let it stand for 40 minutes.
(6)将合金液浇注入金属模具成型。(6) The alloy liquid is poured into a metal mold for forming.
对比例1Comparative example 1
制备Mg-6Zn-3La-Sm-Y-Mn合金,其中按质量百分比Zn含量为5.0%~6.0%,按质量百分比La含量为2.8%~3.5%,按质量百分比Sm含量为0.5%~1.2%,按质量百分比Y含量为0.5%~1.2%,按质量百分比Mn含量为0.3%~1.0%,余量为Mg。Prepare a Mg-6Zn-3La-Sm-Y-Mn alloy, wherein the Zn content is 5.0% to 6.0% by mass percentage, the La content is 2.8% to 3.5% by mass percentage, and the Sm content is 0.5% to 1.2% by mass percentage , the Y content is 0.5%-1.2% by mass percentage, the Mn content is 0.3%-1.0% by mass percentage, and the balance is Mg.
常规Mg-30La、Mg-30Sm、Mg-30Y中间合金方式添加稀土制备Mg-6Zn-3La-Sm-Y-Mn合金。Mg-6Zn-3La-Sm-Y-Mn alloys are prepared by adding rare earths to conventional Mg-30La, Mg-30Sm, and Mg-30Y master alloys.
(1)按所述各元素质量百分比配置,其中Mg以纯镁锭方式加入,Zn以纯锌锭方式加入,La以Mg-30La中间合金方式加入,Sm以Mg-30Sm中间合金方式加入,Y以Mg-30Y中间合金方式加入,Mn以Mg-20Mn中间合金方式加入。(1) According to the mass percentage of each element, Mg is added in the form of pure magnesium ingot, Zn is added in the form of pure zinc ingot, La is added in the form of Mg-30La master alloy, Sm is added in the form of Mg-30Sm master alloy, and Y is added in the form of Mg -30Y master alloy is added, and Mn is added as Mg-20Mn master alloy.
(2)坩埚预热至200℃,加入配置好的纯镁锭、纯锌锭及Mg-20Mn中间合金,升温至400℃时通入保护气,保护气组成为CO2+SF6。(2) Preheat the crucible to 200°C, add the configured pure magnesium ingots, pure zinc ingots and Mg-20Mn master alloy, and pass in protective gas when the temperature rises to 400°C, the composition of the protective gas is CO 2 +SF 6 .
(3)熔化后升温至740℃分批次加入配置好的Mg-30La、Mg-30Sm、Mg-30Y中间合金,熔化后充分搅拌熔体4min,捞除表面浮渣。(3) After melting, raise the temperature to 740°C and add the prepared Mg-30La, Mg-30Sm, and Mg-30Y master alloys in batches. After melting, fully stir the melt for 4 minutes to remove the surface scum.
(4)降温至720℃分批次加入占熔体质量百分比1.5%的精炼剂并对熔体持续搅拌进行精炼处理,精炼时间13min。(4) Cool down to 720° C. and add 1.5% refining agent in batches based on the mass percentage of the melt, and continuously stir the melt for refining treatment, and the refining time is 13 minutes.
(5)精炼结束后捞除表面浮渣,720℃保温,静置40min。(5) After refining, remove the scum on the surface, keep it warm at 720°C, and let it stand for 40 minutes.
(6)将合金液浇注入金属模具成型。(6) The alloy liquid is poured into a metal mold for forming.
实施例1与对比例1的添加方式,添加的温度和成本对比见表1。See Table 1 for the addition method, temperature and cost comparison of Example 1 and Comparative Example 1.
表1实施例1与对比例1的添加方式添加的温度和成本Table 1 Embodiment 1 and the temperature and cost added by the addition mode of comparative example 1
注:稀土添加成本比例为添加的稀土所需成本占总材料成本的比例。Note: Rare earth addition cost ratio is the ratio of the cost of rare earth addition to the total material cost.
实施例2Example 2
制备Mg-8Gd-4Y-Nd-Zn-Zr合金,其中按质量百分比Gd含量为7.5%~8.2%,按质量百分比Y含量为3.8%~4.5%,按质量百分比Nd含量为0.5%~1.0%,按质量百分比Zn含量为0.8%~1.5%,按质量百分比Zr含量为0.3%~0.8%,余量为Mg。Prepare Mg-8Gd-4Y-Nd-Zn-Zr alloy, wherein the Gd content is 7.5%-8.2% by mass percentage, the Y content is 3.8%-4.5% by mass percentage, and the Nd content is 0.5%-1.0% by mass percentage , the Zn content is 0.8%-1.5% by mass percentage, the Zr content is 0.3%-0.8% by mass percentage, and the balance is Mg.
以Gd62Y30Nd8三元合金方式添加稀土制备Mg-8Gd-4Y-Nd-Zn-Zr合金。Mg-8Gd-4Y-Nd-Zn-Zr alloy was prepared by adding rare earth in the form of Gd 62 Y 30 Nd 8 ternary alloy.
(1)按所述各元素质量百分比配置,其中Mg以纯镁锭方式加入,Zn以纯锌锭方式加入,Gd、Y、Nd以Gd62Y30Nd8方式加入,Zr以Mg-30Zr中间合金方式加入。(1) According to the mass percentage of each element, Mg is added in the form of pure magnesium ingot, Zn is added in the form of pure zinc ingot, Gd, Y, and Nd are added in the form of Gd 62 Y 30 Nd 8 , and Zr is added in the form of Mg-30Zr master alloy join in.
(2)坩埚预热至200℃,加入配置好的纯镁锭、纯锌锭,升温至400℃时通入保护气,保护气组成为CO2+SF6。(2) Preheat the crucible to 200°C, add the configured pure magnesium ingots and pure zinc ingots, and pass in protective gas when the temperature rises to 400°C, the composition of the protective gas is CO 2 +SF 6 .
(3)熔化后升温至720℃加入配置好的Gd62Y30Nd8合金,熔化后充分搅拌熔体8min,升温至740℃加入配置好的Mg-30Zr中间合金,熔化后充分搅拌熔体4min。(3) After melting, heat up to 720°C and add the prepared Gd 62 Y 30 Nd 8 alloy. After melting, stir the melt for 8 minutes. Raise the temperature to 740°C and add the prepared Mg-30Zr intermediate alloy. After melting, stir the melt for 4 minutes. .
(4)降温至720℃分批次加入占熔体质量百分比1.5%的精炼剂并对熔体持续搅拌进行精炼处理,精炼时间13min。(4) Cool down to 720° C. and add 1.5% refining agent in batches based on the mass percentage of the melt, and continuously stir the melt for refining treatment, and the refining time is 13 minutes.
(5)精炼结束后捞除表面浮渣,720℃保温,静置40min。(5) After refining, remove the scum on the surface, keep it warm at 720°C, and let it stand for 40 minutes.
(6)将合金液浇注入金属模具成型。(6) The alloy liquid is poured into a metal mold for molding.
对比例2Comparative example 2
制备Mg-8Gd-4Y-Nd-Zn-Zr合金,其中按质量百分比Gd含量为7.5%~8.2%,按质量百分比Y含量为3.8%~4.5%,按质量百分比Nd含量为0.5%~1.0%,按质量百分比Zn含量为0.8%~1.5%,按质量百分比Zr含量为0.3%~0.8%,余量为Mg。Prepare Mg-8Gd-4Y-Nd-Zn-Zr alloy, wherein the Gd content is 7.5%-8.2% by mass percentage, the Y content is 3.8%-4.5% by mass percentage, and the Nd content is 0.5%-1.0% by mass percentage , the Zn content is 0.8%-1.5% by mass percentage, the Zr content is 0.3%-0.8% by mass percentage, and the balance is Mg.
常规Mg-30Gd、Mg-30Y、Mg-30Nd中间合金方式添加稀土制备Mg-8Gd-4Y-Nd-Zn-Zr合金。Mg-8Gd-4Y-Nd-Zn-Zr alloys are prepared by adding rare earths to conventional Mg-30Gd, Mg-30Y, and Mg-30Nd master alloys.
(1)按所述各元素质量百分比配置,其中Mg以纯镁锭方式加入,Zn以纯锌锭方式加入,Gd以Mg-30Gd中间合金方式加入,Y以Mg-30Y中间合金方式加入,Nd以Mg-30Nd中间合金方式加入,Zr以Mg-30Zr中间合金方式加入。(1) According to the mass percentage of each element, Mg is added in the form of pure magnesium ingot, Zn is added in the form of pure zinc ingot, Gd is added in the form of Mg-30Gd master alloy, Y is added in the form of Mg-30Y master alloy, and Nd is added in the form of Mg -30Nd master alloy is added, and Zr is added as Mg-30Zr master alloy.
(2)坩埚预热至200℃,加入配置好的纯镁锭、纯锌锭,升温至400℃时通入保护气,保护气组成为CO2+SF6。(2) Preheat the crucible to 200°C, add the configured pure magnesium ingots and pure zinc ingots, and pass in protective gas when the temperature rises to 400°C, the composition of the protective gas is CO 2 +SF 6 .
(3)熔化后升温至740℃分批次加入配置好的Mg-30Gd、Mg-30Y、Mg-30Nd中间合金,熔化后充分搅拌熔体4min,随后加入配置好的Mg-30Zr中间合金,熔化后充分搅拌熔体4min,捞除表面浮渣。(3) After melting, heat up to 740°C and add the configured Mg-30Gd, Mg-30Y, Mg-30Nd master alloys in batches, stir the melt for 4 minutes after melting, then add the configured Mg-30Zr master alloy, and melt Finally, fully stir the melt for 4 minutes, and remove the scum on the surface.
(4)降温至720℃分批次加入占熔体质量百分比1.5%的精炼剂并对熔体持续搅拌进行精炼处理,精炼时间13min。(4) Cool down to 720° C. and add 1.5% refining agent in batches based on the mass percentage of the melt, and continuously stir the melt for refining treatment, and the refining time is 13 minutes.
(5)精炼结束后捞除表面浮渣,720℃保温,静置40min。(5) After refining, remove the scum on the surface, keep it warm at 720°C, and let it stand for 40 minutes.
(6)将合金液浇注入金属模具成型。(6) The alloy liquid is poured into a metal mold for forming.
实施例2与对比例2的添加方式,添加的温度和成本对比见表2。See Table 2 for the addition method of Example 2 and Comparative Example 2, the temperature and cost of addition.
表2实施例2与对比例2的添加方式添加的温度和成本Table 2 Embodiment 2 and the temperature and cost added by the addition mode of comparative example 2
注:稀土添加成本比例为添加的稀土所需成本占总材料成本的比例。Note: Rare earth addition cost ratio is the ratio of the cost of rare earth addition to the total material cost.
以上所述仅是本发明的优选实施方式,应当指出,对于本技术领域的普通技术人员来说,在不脱离本发明原理的前提下,还可以做出若干改进和润饰,这些改进和润饰也应视为本发明的保护范围。The above is only a preferred embodiment of the present invention, it should be pointed out that, for those of ordinary skill in the art, without departing from the principle of the present invention, some improvements and modifications can also be made, and these improvements and modifications can also be made. It should be regarded as the protection scope of the present invention.
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Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2002121637A (en) * | 2000-10-12 | 2002-04-26 | Toyota Motor Corp | Magnesium alloy excellent in heat resistance and method for producing the same |
CN103421999A (en) * | 2013-07-15 | 2013-12-04 | 中南大学 | Rare earth-contained heat-resistant magnesium alloy and preparation method thereof |
CN104630585A (en) * | 2015-02-03 | 2015-05-20 | 闻喜县瑞格镁业有限公司 | High-strength magnesium alloy for ultrathin-wall components and preparation method thereof |
-
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- 2022-12-26 CN CN202211677692.4A patent/CN115896513A/en active Pending
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2002121637A (en) * | 2000-10-12 | 2002-04-26 | Toyota Motor Corp | Magnesium alloy excellent in heat resistance and method for producing the same |
CN103421999A (en) * | 2013-07-15 | 2013-12-04 | 中南大学 | Rare earth-contained heat-resistant magnesium alloy and preparation method thereof |
CN104630585A (en) * | 2015-02-03 | 2015-05-20 | 闻喜县瑞格镁业有限公司 | High-strength magnesium alloy for ultrathin-wall components and preparation method thereof |
Non-Patent Citations (3)
Title |
---|
《稀土》编写组: "稀土 下册", 31 October 1978, 冶金工业出版社, pages: 62 * |
徐光宪: "稀土(第2版)中册", 30 April 1978, 北京冶金工业出版社, pages: 101 * |
龙晋明, 郭忠诚, 朱晓云, 杨坤: "稀土对Mg合金组织及阻燃性能的影响", 昆明理工大学学报(理工版), no. 05 * |
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