CN107815575A - A kind of magnesium aluminum alloy casting ingot - Google Patents
A kind of magnesium aluminum alloy casting ingot Download PDFInfo
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- CN107815575A CN107815575A CN201711014105.2A CN201711014105A CN107815575A CN 107815575 A CN107815575 A CN 107815575A CN 201711014105 A CN201711014105 A CN 201711014105A CN 107815575 A CN107815575 A CN 107815575A
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- 238000005266 casting Methods 0.000 title claims abstract description 13
- 229910000838 Al alloy Inorganic materials 0.000 title abstract description 15
- SNAAJJQQZSMGQD-UHFFFAOYSA-N aluminum magnesium Chemical compound [Mg].[Al] SNAAJJQQZSMGQD-UHFFFAOYSA-N 0.000 title abstract description 14
- 239000000956 alloy Substances 0.000 claims abstract description 78
- 229910045601 alloy Inorganic materials 0.000 claims abstract description 75
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical group [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 claims abstract description 15
- 229910052749 magnesium Inorganic materials 0.000 claims abstract description 15
- 239000011777 magnesium Substances 0.000 claims abstract description 15
- 238000007670 refining Methods 0.000 claims abstract description 13
- 238000003723 Smelting Methods 0.000 claims abstract description 10
- 238000010438 heat treatment Methods 0.000 claims abstract description 10
- 239000002994 raw material Substances 0.000 claims abstract description 9
- 238000002360 preparation method Methods 0.000 claims abstract description 7
- 229910052725 zinc Inorganic materials 0.000 claims abstract description 6
- 230000032683 aging Effects 0.000 claims abstract description 4
- 238000005303 weighing Methods 0.000 claims abstract description 4
- 229910052802 copper Inorganic materials 0.000 claims abstract description 3
- 239000012535 impurity Substances 0.000 claims abstract description 3
- 229910052742 iron Inorganic materials 0.000 claims abstract description 3
- 229910052748 manganese Inorganic materials 0.000 claims abstract description 3
- 229910052759 nickel Inorganic materials 0.000 claims abstract description 3
- 229910000861 Mg alloy Inorganic materials 0.000 claims description 11
- 239000000463 material Substances 0.000 claims description 7
- 238000002844 melting Methods 0.000 claims description 7
- 230000008018 melting Effects 0.000 claims description 7
- 238000003756 stirring Methods 0.000 claims description 7
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 claims description 6
- 229910052782 aluminium Inorganic materials 0.000 claims description 6
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 6
- 238000005516 engineering process Methods 0.000 claims description 6
- KBMLJKBBKGNETC-UHFFFAOYSA-N magnesium manganese Chemical compound [Mg].[Mn] KBMLJKBBKGNETC-UHFFFAOYSA-N 0.000 claims description 6
- 229910000831 Steel Inorganic materials 0.000 claims description 5
- 239000000203 mixture Substances 0.000 claims description 5
- 239000010959 steel Substances 0.000 claims description 5
- 239000011701 zinc Substances 0.000 claims description 5
- 229910052751 metal Inorganic materials 0.000 claims description 3
- 239000002184 metal Substances 0.000 claims description 3
- 239000007788 liquid Substances 0.000 claims description 2
- 239000011572 manganese Substances 0.000 claims description 2
- 239000004411 aluminium Substances 0.000 claims 2
- 238000000034 method Methods 0.000 abstract description 17
- 229910052710 silicon Inorganic materials 0.000 abstract description 2
- 239000003795 chemical substances by application Substances 0.000 description 6
- 239000013078 crystal Substances 0.000 description 2
- 238000001035 drying Methods 0.000 description 2
- 239000000155 melt Substances 0.000 description 2
- 229910000851 Alloy steel Inorganic materials 0.000 description 1
- 229910003023 Mg-Al Inorganic materials 0.000 description 1
- 238000010521 absorption reaction Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000013016 damping Methods 0.000 description 1
- 230000018109 developmental process Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000010309 melting process Methods 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
Classifications
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- 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
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C1/00—Making non-ferrous alloys
- C22C1/02—Making non-ferrous alloys by melting
- C22C1/03—Making non-ferrous alloys by melting using master alloys
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C1/00—Making non-ferrous alloys
- C22C1/06—Making non-ferrous alloys with the use of special agents for refining or deoxidising
-
- 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
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Crystallography & Structural Chemistry (AREA)
- Manufacture And Refinement Of Metals (AREA)
Abstract
本发明公开了一种镁铝合金铸锭,该镁铝合金铸锭包含如下质量百分比的原料:Al 8.5‑9.5%,Zn 0.45‑0.9%,Mn 0.17‑0.4%,Al‑Ti‑B中间合金0.18‑0.2%,Al‑Ti‑C中间合金0.19‑0.21%,杂质元素Si、Cu、Ni和Fe的总量小于0.1%,余量为镁。所述镁铝合金铸锭的制备方法包括熔炼工艺和热处理工艺,其熔炼工艺包括称料和烘料、熔炼、精炼和静置、铸造,热处理工艺包括固溶处理和时效处理。本发明所得的镁铝合金铸锭通过添加细化剂后,其对镁铝合金的晶粒大小,拉伸等力学性能都有较大的改善;热处理之后,合金铸锭的强度进一步得以提高。
The invention discloses a magnesium-aluminum alloy ingot, which contains the following raw materials in mass percentage: Al 8.5-9.5%, Zn 0.45-0.9%, Mn 0.17-0.4%, Al-Ti-B master alloy 0.18-0.2%, Al-Ti-C master alloy 0.19-0.21%, the total amount of impurity elements Si, Cu, Ni and Fe is less than 0.1%, and the balance is magnesium. The preparation method of the magnesium-aluminum alloy ingot includes a smelting process and a heat treatment process, wherein the smelting process includes weighing and baking, smelting, refining and standing, and casting, and the heat treatment process includes solution treatment and aging treatment. After adding a refiner, the magnesium-aluminum alloy ingot obtained by the present invention has greatly improved the grain size, tensile and other mechanical properties of the magnesium-aluminum alloy; after heat treatment, the strength of the alloy ingot is further improved.
Description
技术领域technical field
本发明属于合金领域,具体涉及一种镁铝合金铸锭。The invention belongs to the field of alloys, and in particular relates to a magnesium-aluminum alloy ingot.
背景技术Background technique
镁合金是最轻的金属结构材料,其比强度、比刚度均很高,比弹性模量与高强铝合金、合金钢的大致相同,同时具有良好的阻尼性能。因而利用镁合金材料可以充分发挥出该材料电磁屏蔽效果好、重量小、减震能力强、易于成型的特点,在工业领域具有巨大的应用潜力。截至目前为止,镁合金材料在航空航天科学领域和汽车制造等领域有着广泛的应用,随着材料技术的发展,镁合金材料具必定会有更加广阔的应用前景和使用价值。Magnesium alloy is the lightest metal structure material, its specific strength and specific stiffness are very high, its specific elastic modulus is roughly the same as that of high-strength aluminum alloy and alloy steel, and it has good damping performance. Therefore, the use of magnesium alloy materials can give full play to the characteristics of good electromagnetic shielding effect, small weight, strong shock absorption ability and easy forming of the material, and has great application potential in the industrial field. So far, magnesium alloy materials have been widely used in the fields of aerospace science and automobile manufacturing. With the development of material technology, magnesium alloy materials will have broader application prospects and use value.
AZ91是比较常应用的Mg-Al系合金,其合金具有高的强度和良好的铸造性能。但由于细化前AZ91的晶粒通常比较大,从而降低了整体的力学性能。本发明通过对AZ91合金的成分和工艺研究,在原有基础上对其细化剂和工艺进行了调整和试验,从而获得了一种细化剂和使用性能都较佳的改进的AZ91合金。AZ91 is a commonly used Mg-Al alloy, and its alloy has high strength and good casting performance. However, since the grains of AZ91 before refining are usually relatively large, the overall mechanical properties are reduced. The present invention adjusts and tests the refiner and the process based on the research on the composition and process of the AZ91 alloy, thereby obtaining an improved AZ91 alloy with better refiner and performance.
发明内容Contents of the invention
鉴于以上目的,本发明公开了一种镁铝合金铸锭,通过添加细化剂,使得制备的合金的晶粒得以细化,组织结构得到调整,其整体的力学性能得到改善和强化。In view of the above objectives, the present invention discloses a magnesium-aluminum alloy ingot. By adding a refiner, the crystal grains of the prepared alloy are refined, the microstructure is adjusted, and its overall mechanical properties are improved and strengthened.
为了实现上述目的,本发明采用的技术方案为:一种镁铝合金铸锭,包含如下质量百分比的原料:Al 8.5-9.5%,Zn 0.45-0.9%,Mn 0.17-0.4%,Al-Ti-B中间合金0.18-0.2%,Al-Ti-C中间合金0.19-0.21%,杂质元素Si、Cu、Ni和Fe的总量小于0.1%,余量为镁。In order to achieve the above object, the technical solution adopted by the present invention is: a magnesium-aluminum alloy ingot, comprising the following raw materials in mass percentage: Al 8.5-9.5%, Zn 0.45-0.9%, Mn 0.17-0.4%, Al-Ti- B master alloy 0.18-0.2%, Al-Ti-C master alloy 0.19-0.21%, the total amount of impurity elements Si, Cu, Ni and Fe is less than 0.1%, and the balance is magnesium.
所述Al-Ti-B中间合金为Al-4Ti-B中间合金。The Al-Ti-B master alloy is Al-4Ti-B master alloy.
所述Al-Ti-C中间合金为Al-5Ti-0.8C中间合金。The Al-Ti-C master alloy is an Al-5Ti-0.8C master alloy.
上述镁铝合金铸锭的制备方法包括熔炼工艺和热处理工艺;其中,所述熔炼工艺在N2、CO2和SF6混合气体保护条件下进行,步骤如下:The preparation method of the above-mentioned magnesium-aluminum alloy ingot includes a smelting process and a heat treatment process; wherein, the smelting process is carried out under the protection condition of a mixed gas of N 2 , CO 2 and SF 6 , and the steps are as follows:
(1)称料和烘料:按原料质量百分比,分别称取镁锭、铝锭、锌锭、镁锰中间合金、Al-Ti-B中间合金和Al-Ti-C中间合金;并将各种原料放置在200-220℃的预热炉中预热4-6h;(1) Weighing and drying materials: according to the mass percentage of raw materials, respectively weigh magnesium ingots, aluminum ingots, zinc ingots, magnesium-manganese master alloys, Al-Ti-B master alloys and Al-Ti-C master alloys; The raw materials are preheated in a preheating furnace at 200-220°C for 4-6 hours;
(2)熔炼:将预热后的镁锭置于熔化炉中加热至690-700℃至镁锭完全熔化,然后升温至740-760℃,向熔化的镁液中加入预热过的铝锭和锌锭,搅拌至完全熔化,再将熔体温度回升至740-760℃时加入预热过的镁锰中间合金、Al-Ti-B中间合金和Al-Ti-C中间合金,搅拌至完全熔化,得到混合合金熔体;(2) Melting: Put the preheated magnesium ingot in a melting furnace and heat it to 690-700°C until the magnesium ingot is completely melted, then raise the temperature to 740-760°C, add the preheated aluminum ingot into the molten magnesium liquid and zinc ingot, stir until completely melted, then add the preheated magnesium-manganese master alloy, Al-Ti-B master alloy and Al-Ti-C master alloy when the melt temperature rises to 740-760°C, stir until completely Melted to obtain a mixed alloy melt;
(3)精炼和静置:将步骤(2)所得的混合合金熔体降温至700-720℃,撇去表面浮渣,然后搅拌混合均匀后保温10-15min,在此温度下精炼3-5min,精炼完成后再撇去表面浮渣,回升温度至740℃,静置15-20min;(3) Refining and standing: Cool the mixed alloy melt obtained in step (2) to 700-720°C, skim off the surface scum, then stir and mix evenly, keep it warm for 10-15min, and refine at this temperature for 3-5min After refining, skim off the scum on the surface, raise the temperature to 740°C, and let it stand for 15-20 minutes;
(4)铸造:静置结束后待混合合金熔体降温至680-690℃时,向预先加热好的钢制模具中进行浇注,得到合金铸锭;(4) Casting: after standing still, when the mixed alloy melt cools down to 680-690°C, pour it into a preheated steel mold to obtain an alloy ingot;
所述的热处理工艺为:Described heat treatment process is:
将熔炼得到的合金铸锭在420℃温度下进行8h的固溶处理,而后在200℃温度中进行10h的时效处理。The smelted alloy ingot was subjected to solution treatment at a temperature of 420° C. for 8 hours, and then to an aging treatment at a temperature of 200° C. for 10 hours.
所述熔炼工艺中混合气体N2、CO2和SF6的体积比为50:50:0.3。The volume ratio of the mixed gas N 2 , CO 2 and SF 6 in the smelting process is 50:50:0.3.
所述钢制模具的预热温度为280-300℃。The preheating temperature of the steel mold is 280-300°C.
添加细化剂的目的在于使之前的合金的晶粒能得到细化,由基础AZ91合金的75μm晶粒平均尺寸细化至39μm晶粒平均尺寸,且组织结构调整均匀,紧密均匀的合金结构致使合金的铸造性能和力学性能等都有所提高;而细化前的AZ91合金晶粒通常比较大,其铸造性能虽较好,但整体的力学性能如硬度、抗拉强度等都不太理想。The purpose of adding a refiner is to refine the grains of the previous alloy. The average grain size of the basic AZ91 alloy is refined from 75 μm to 39 μm, and the microstructure is adjusted uniformly. The compact and uniform alloy structure results in The castability and mechanical properties of the alloy have been improved; while the AZ91 alloy grains before refinement are usually relatively large, although its casting performance is good, but the overall mechanical properties such as hardness and tensile strength are not ideal.
本发明的有益效果:本发明在基础AZ91合金的基础上,添加合金细化剂,并采用合理的热工艺对添加细化剂的合金进行改进,使基础AZ91合金的晶粒得到细化,组织结构调整更均匀,从而使合金的综合性能进一步强化。Beneficial effects of the present invention: on the basis of the basic AZ91 alloy, the present invention adds an alloy refiner, and adopts a reasonable thermal process to improve the alloy added with the refiner, so that the crystal grains of the basic AZ91 alloy are refined and the microstructure is improved. The structural adjustment is more uniform, so that the comprehensive performance of the alloy is further strengthened.
附图说明Description of drawings
图1为实施例1只添加细化剂Al-4Ti-B中间合金的整体镁铝合金的晶粒尺寸大小图;Fig. 1 is the grain size figure of the whole magnesium-aluminum alloy that only adds refining agent Al-4Ti-B master alloy in embodiment 1;
图2为实施例2只添加细化剂Al-5Ti-0.8C中间合金的整体镁铝合金的晶粒尺寸大小图;Fig. 2 is the grain size figure of the whole magnesium-aluminum alloy that only adds refining agent Al-5Ti-0.8C master alloy in embodiment 2;
图3为实施例3同时添加细化剂Al-4Ti-B中间合金和Al-5Ti-0.8C中间合金的整体镁铝合金的晶粒尺寸大小图。Fig. 3 is a graph of the grain size of the overall magnesium-aluminum alloy in Example 3 with the addition of refining agents Al-4Ti-B master alloy and Al-5Ti-0.8C master alloy at the same time.
具体实施方式Detailed ways
以下对本发明的具体实施方式进行详细说明。应当理解的是,此处所描述的具体实施方式仅用于说明和解释本发明,并不用于限制本发明。实施例中,各种原料都为马可波罗网产品。Specific embodiments of the present invention will be described in detail below. It should be understood that the specific embodiments described here are only used to illustrate and explain the present invention, and are not intended to limit the present invention. In the embodiment, various raw materials are Marco Polo net products.
实施例1-3的各种成分如下:The various compositions of embodiment 1-3 are as follows:
上述镁铝合金铸锭的制备方法包括熔炼工艺和热处理工艺,具体步骤参考如下:The preparation method of the above-mentioned magnesium-aluminum alloy ingot includes a melting process and a heat treatment process, and the specific steps are as follows:
所述熔炼工艺在N2、CO2和SF6混合气体保护条件下进行,步骤如下:The smelting process is carried out under the protection condition of N 2 , CO 2 and SF 6 mixed gas, and the steps are as follows:
(1)称料和烘料:按原料质量百分比,分别称取镁锭、铝锭、锌锭、镁锰中间合金、Al-4Ti-B中间合金和Al-5Ti-0.8C中间合金;并将各种原料放置在200℃的预热炉中预热4h;(1) Weighing and drying materials: according to the mass percentage of raw materials, respectively weigh magnesium ingots, aluminum ingots, zinc ingots, magnesium-manganese master alloys, Al-4Ti-B master alloys and Al-5Ti-0.8C master alloys; and Various raw materials are preheated in a preheating furnace at 200°C for 4 hours;
(2)熔炼:将预热后的镁锭置于熔化炉中加热至690℃至镁锭完全熔化,然后升温至740℃,向熔化的镁液中加入预热过的铝锭和锌锭,搅拌至完全熔化,再将熔体温度回升至740℃时加入预热过的镁锰中间合金、Al-4Ti-B中间合金和Al-5Ti-0.8C中间合金,搅拌至完全熔化,得到混合合金熔体;(2) Melting: heat the preheated magnesium ingot to 690°C in a melting furnace until the magnesium ingot is completely melted, then raise the temperature to 740°C, add preheated aluminum and zinc ingots to the molten magnesium, Stir until it is completely melted, then add the preheated magnesium-manganese master alloy, Al-4Ti-B master alloy and Al-5Ti-0.8C master alloy when the melt temperature rises to 740°C, stir until it is completely melted to obtain a mixed alloy melt;
(3)精炼和静置:将步骤(2)所得的混合合金熔体降温至710℃,撇去表面浮渣,然后搅拌混合均匀后保温15min,在此温度下精炼5min,精炼完成后再撇去表面浮渣,回升温度至740℃,静置15min;(3) Refining and standing: Cool the mixed alloy melt obtained in step (2) to 710°C, skim off the surface scum, then stir and mix evenly, keep it warm for 15 minutes, refine at this temperature for 5 minutes, and skim after refining Remove the scum on the surface, raise the temperature to 740°C, and let stand for 15 minutes;
(4)铸造:静置结束后待混合合金熔体降温至680℃时,向预先加热至300℃的钢制模具中进行浇注,得到合金铸锭;(4) Casting: after standing still, when the mixed alloy melt is cooled to 680°C, it is poured into a steel mold preheated to 300°C to obtain an alloy ingot;
所述的热处理工艺为:Described heat treatment process is:
将熔炼得到的合金铸锭在420℃温度下进行8h的固溶处理,而后在200℃温度中进行10h的时效处理。The smelted alloy ingot was subjected to solution treatment at a temperature of 420° C. for 8 hours, and then to an aging treatment at a temperature of 200° C. for 10 hours.
实施例1制备步骤中只加入细化剂Al-4Ti-B中间合金,实施例2制备步骤中只加入细化剂Al-5Ti-0.8C中间合金,实施例3制备步骤中同时加入细化剂Al-4Ti-B中间合金和Al-5Ti-0.8C中间合金。In the preparation step of Example 1, only the refining agent Al-4Ti-B master alloy is added; in the preparation step of Example 2, only the refining agent Al-5Ti-0.8C master alloy is added; in the preparation step of Example 3, the refining agent is added at the same time Al-4Ti-B master alloy and Al-5Ti-0.8C master alloy.
对上述实施例1-3制备的镁铝合金铸锭进行检测,得到的技术参数如下:The magnesium-aluminum alloy ingot prepared in the above-mentioned examples 1-3 is detected, and the technical parameters obtained are as follows:
由表可知,本发明的镁铝合金在原有AZ91合金基础上,添加的合金细化剂和对热处理工艺的改进,使得合金的综合性能进一步强化。It can be seen from the table that, on the basis of the original AZ91 alloy, the alloy refiner added and the heat treatment process improved further strengthen the comprehensive properties of the alloy.
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Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108411175A (en) * | 2018-04-19 | 2018-08-17 | 合肥博创机械制造有限公司 | A kind of corrosion resistance magnesium alloy and preparation method thereof |
| CN109014086A (en) * | 2018-08-17 | 2018-12-18 | 清华大学 | A kind of casting method of high-magnesium aluminum alloy |
| CN109182862A (en) * | 2018-11-21 | 2019-01-11 | 蚌埠创特新材料科技有限公司 | A kind of anticorrosive magnesium-aluminium alloy |
| CN111020326A (en) * | 2019-12-05 | 2020-04-17 | 西安理工大学 | A kind of high temperature creep resistant magnesium aluminum alloy and preparation method thereof |
| CN111235447A (en) * | 2020-04-13 | 2020-06-05 | 五台云海镁业有限公司 | High-iron magnesium alloy for ruminants and preparation method thereof |
| CN114369738A (en) * | 2022-01-18 | 2022-04-19 | 重庆理工大学 | A kind of magnesium alloy with low cost and high casting performance and preparation method thereof |
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Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108411175A (en) * | 2018-04-19 | 2018-08-17 | 合肥博创机械制造有限公司 | A kind of corrosion resistance magnesium alloy and preparation method thereof |
| CN109014086A (en) * | 2018-08-17 | 2018-12-18 | 清华大学 | A kind of casting method of high-magnesium aluminum alloy |
| CN109182862A (en) * | 2018-11-21 | 2019-01-11 | 蚌埠创特新材料科技有限公司 | A kind of anticorrosive magnesium-aluminium alloy |
| CN109182862B (en) * | 2018-11-21 | 2020-04-03 | 阜阳创启工艺品有限公司 | Corrosion-resistant magnesium-aluminum alloy |
| CN111020326A (en) * | 2019-12-05 | 2020-04-17 | 西安理工大学 | A kind of high temperature creep resistant magnesium aluminum alloy and preparation method thereof |
| CN111235447A (en) * | 2020-04-13 | 2020-06-05 | 五台云海镁业有限公司 | High-iron magnesium alloy for ruminants and preparation method thereof |
| CN114369738A (en) * | 2022-01-18 | 2022-04-19 | 重庆理工大学 | A kind of magnesium alloy with low cost and high casting performance and preparation method thereof |
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