CN105039816B - A kind of high strength and low cost heat resistance magnesium alloy and preparation method thereof - Google Patents
A kind of high strength and low cost heat resistance magnesium alloy and preparation method thereof Download PDFInfo
- Publication number
- CN105039816B CN105039816B CN201510427006.1A CN201510427006A CN105039816B CN 105039816 B CN105039816 B CN 105039816B CN 201510427006 A CN201510427006 A CN 201510427006A CN 105039816 B CN105039816 B CN 105039816B
- Authority
- CN
- China
- Prior art keywords
- alloy
- magnesium alloy
- low
- temperature
- heat
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
- 229910000861 Mg alloy Inorganic materials 0.000 title claims abstract description 65
- 238000002360 preparation method Methods 0.000 title claims abstract description 13
- 239000011777 magnesium Substances 0.000 claims abstract description 31
- 229910052718 tin Inorganic materials 0.000 claims abstract description 25
- 229910052782 aluminium Inorganic materials 0.000 claims abstract description 24
- 229910052787 antimony Inorganic materials 0.000 claims abstract description 22
- 229910052772 Samarium Inorganic materials 0.000 claims abstract description 8
- 229910052710 silicon Inorganic materials 0.000 claims abstract description 8
- 229910045601 alloy Inorganic materials 0.000 claims description 92
- 239000000956 alloy Substances 0.000 claims description 92
- 239000011135 tin Substances 0.000 claims description 26
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 claims description 17
- 229910052749 magnesium Inorganic materials 0.000 claims description 17
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 claims description 16
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 16
- WATWJIUSRGPENY-UHFFFAOYSA-N antimony atom Chemical compound [Sb] WATWJIUSRGPENY-UHFFFAOYSA-N 0.000 claims description 16
- 230000032683 aging Effects 0.000 claims description 15
- 229910019064 Mg-Si Inorganic materials 0.000 claims description 14
- 229910019406 Mg—Si Inorganic materials 0.000 claims description 14
- 239000002994 raw material Substances 0.000 claims description 13
- 238000005266 casting Methods 0.000 claims description 10
- 238000000034 method Methods 0.000 claims description 10
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims description 8
- CPLXHLVBOLITMK-UHFFFAOYSA-N magnesium oxide Inorganic materials [Mg]=O CPLXHLVBOLITMK-UHFFFAOYSA-N 0.000 claims description 6
- 239000000395 magnesium oxide Substances 0.000 claims description 6
- AXZKOIWUVFPNLO-UHFFFAOYSA-N magnesium;oxygen(2-) Chemical compound [O-2].[Mg+2] AXZKOIWUVFPNLO-UHFFFAOYSA-N 0.000 claims description 6
- 239000000843 powder Substances 0.000 claims description 6
- 238000010438 heat treatment Methods 0.000 claims description 4
- 238000002844 melting Methods 0.000 claims description 3
- 230000008018 melting Effects 0.000 claims description 3
- 239000004411 aluminium Substances 0.000 claims 1
- 238000005275 alloying Methods 0.000 abstract description 7
- 238000005728 strengthening Methods 0.000 abstract description 7
- 230000000694 effects Effects 0.000 abstract description 5
- 230000002195 synergetic effect Effects 0.000 abstract description 2
- 239000000243 solution Substances 0.000 description 13
- 229910052751 metal Inorganic materials 0.000 description 9
- 239000002184 metal Substances 0.000 description 9
- 238000001035 drying Methods 0.000 description 8
- 238000003756 stirring Methods 0.000 description 4
- 239000000203 mixture Substances 0.000 description 3
- 239000006104 solid solution Substances 0.000 description 3
- 229910018125 Al-Si Inorganic materials 0.000 description 2
- 229910018520 Al—Si Inorganic materials 0.000 description 2
- 229910019021 Mg 2 Sn Inorganic materials 0.000 description 2
- 229910020068 MgAl Inorganic materials 0.000 description 2
- 238000003723 Smelting Methods 0.000 description 2
- 230000015572 biosynthetic process Effects 0.000 description 2
- 238000009826 distribution Methods 0.000 description 2
- 229910000765 intermetallic Inorganic materials 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 239000011159 matrix material Substances 0.000 description 2
- 229910052761 rare earth metal Inorganic materials 0.000 description 2
- 230000035882 stress Effects 0.000 description 2
- 229910000838 Al alloy Inorganic materials 0.000 description 1
- 229910018140 Al-Sn Inorganic materials 0.000 description 1
- 229910018564 Al—Sn Inorganic materials 0.000 description 1
- 229910019018 Mg 2 Si Inorganic materials 0.000 description 1
- 229910003023 Mg-Al Inorganic materials 0.000 description 1
- 229910001245 Sb alloy Inorganic materials 0.000 description 1
- 229910000676 Si alloy Inorganic materials 0.000 description 1
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 1
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 description 1
- 238000010521 absorption reaction Methods 0.000 description 1
- SNAAJJQQZSMGQD-UHFFFAOYSA-N aluminum magnesium Chemical compound [Mg].[Al] SNAAJJQQZSMGQD-UHFFFAOYSA-N 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 238000005336 cracking Methods 0.000 description 1
- 238000013016 damping Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000004925 denaturation Methods 0.000 description 1
- 230000036425 denaturation Effects 0.000 description 1
- 210000001787 dendrite Anatomy 0.000 description 1
- 238000001514 detection method Methods 0.000 description 1
- 230000017525 heat dissipation Effects 0.000 description 1
- 239000012535 impurity Substances 0.000 description 1
- 238000009776 industrial production Methods 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 239000007769 metal material Substances 0.000 description 1
- 238000005272 metallurgy Methods 0.000 description 1
- 239000002245 particle Substances 0.000 description 1
- 238000010791 quenching Methods 0.000 description 1
- 230000000171 quenching effect Effects 0.000 description 1
- KZUNJOHGWZRPMI-UHFFFAOYSA-N samarium atom Chemical compound [Sm] KZUNJOHGWZRPMI-UHFFFAOYSA-N 0.000 description 1
- 230000035945 sensitivity Effects 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
- 239000010703 silicon Substances 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 229910052725 zinc Inorganic materials 0.000 description 1
- 239000011701 zinc Substances 0.000 description 1
Landscapes
- Powder Metallurgy (AREA)
Abstract
本发明公开了一种低成本高强耐热镁合金及其制备方法,该镁合金由以下重量百分比的组分组成:6.2~9.3%Al,3.5~5.5%Sn,1.0~1.8%Sb,0.2~0.9%Si,0.1~0.4%Sm,余量为Mg。本发明提供的低成本高强耐热镁合金,利用多元微合金化改善镁合金的显微组织,进而提高其力学性能;合理选择合金化元素,控制各合金化元素的含量,发挥了各组分的协同强化作用,提高了镁合金的力学性能和耐热性能;本发明提供的耐热镁合金,显微组织均匀,具有较高的室温和高温强度,高温抗蠕变性优良;该合金在保持较高的力学性能的基础上,极大地降低了镁合金的成本,适合推广应用。The invention discloses a low-cost high-strength heat-resistant magnesium alloy and a preparation method thereof. The magnesium alloy is composed of the following components in weight percent: 6.2-9.3% Al, 3.5-5.5% Sn, 1.0-1.8% Sb, 0.2- 0.9% Si, 0.1-0.4% Sm, and the balance is Mg. The low-cost high-strength heat-resistant magnesium alloy provided by the present invention uses multi-element microalloying to improve the microstructure of the magnesium alloy, thereby improving its mechanical properties; rationally selecting alloying elements, controlling the content of each alloying element, and making full use of each component The synergistic strengthening effect of the magnesium alloy improves the mechanical properties and heat resistance of the magnesium alloy; the heat-resistant magnesium alloy provided by the invention has a uniform microstructure, high room temperature and high temperature strength, and excellent high temperature creep resistance; On the basis of maintaining high mechanical properties, the cost of the magnesium alloy is greatly reduced, and it is suitable for popularization and application.
Description
技术领域technical field
本发明属于金属材料及冶金技术领域,具体涉及一种低成本高强耐热镁合金及其制备方法。The invention belongs to the technical field of metal materials and metallurgy, and in particular relates to a low-cost, high-strength, heat-resistant magnesium alloy and a preparation method thereof.
背景技术Background technique
镁及镁合金作为现阶段工程应用中最轻的金属结构材料,具有低的密度、高的比强度和比刚度、优异的阻尼减震性能以及良好的散热性,在许多领域都具有非常优异的应用潜力,特别是在航空航天、汽车摩托车和高速轻轨列车以及3C产品方面具有难以替代的应用优势。Magnesium and magnesium alloys, as the lightest metal structural materials in engineering applications at the present stage, have low density, high specific strength and specific stiffness, excellent damping and shock absorption performance, and good heat dissipation, and have excellent performance in many fields. Application potential, especially in aerospace, automobiles and motorcycles, high-speed light rail trains and 3C products, it has irreplaceable application advantages.
目前商用镁合金分为铸造镁合金和变形镁合金两大类。MgAl系铸造镁合金由于具有室温力学性能良好、流动铸造性良好、机加工性能良好、低廉的价格和铸造工艺简单而应用最为广泛,其中AZ91和AM60/50系列应用最为广泛,但是该系列合金存在塑性较差以及高温力学性能较差的缺陷。At present, commercial magnesium alloys are divided into two categories: cast magnesium alloys and wrought magnesium alloys. MgAl series cast magnesium alloys are the most widely used due to their good mechanical properties at room temperature, good flow castability, good machinability, low price and simple casting process, among which AZ91 and AM60/50 series are the most widely used, but there are Defects of poor plasticity and poor high temperature mechanical properties.
为了适应市场的需要,扩大镁合金的应用范围和领域,科研工作者对现有的MgAl系铸造镁合金进行了大量研究。利用合金化提高镁合金的室温和高温力学性能是主要研究方向之一,所用的合金化元素主要有稀土元素和碱土元素以及铝、锌、锡、硅、锑等其他元素,相继开发了Mg-Al-Ca、Mg-Al-Si、Mg-Al-RE、Mg-Y-Nd等系列耐热镁合金,但上述合金由于种种原因在实际中得到的应用非常少。其中,Mg-Al-Ca系列(如AX51)合金受限于铸造性能且易于形成热裂纹;Mg-Al-Si系列(如AS41和AS21)合金,其组织中存在粗大汉字状的Mg2Si相,损害了其力学性能;Mg-Al-RE系列(如AE42)合金和Mg-Y-Nd系列(如WE43和WE54),由于合金中添加较多的稀土元素,造成合金成本较高而限制了其广泛应用;采用廉价元素提高镁合金的力学性能,对于镁合金在更广范围内的应用具有重要作用。In order to meet the needs of the market and expand the application range and fields of magnesium alloys, researchers have conducted a lot of research on the existing MgAl series cast magnesium alloys. Using alloying to improve the mechanical properties of magnesium alloys at room temperature and high temperature is one of the main research directions. The alloying elements used mainly include rare earth elements and alkaline earth elements, as well as other elements such as aluminum, zinc, tin, silicon, antimony, etc., and Mg- Al-Ca, Mg-Al-Si, Mg-Al-RE, Mg-Y-Nd and other series of heat-resistant magnesium alloys, but the above alloys are rarely used in practice due to various reasons. Among them, Mg-Al-Ca series (such as AX51) alloys are limited in casting performance and are prone to hot cracks; Mg-Al-Si series (such as AS41 and AS21) alloys have coarse Chinese character-shaped Mg 2 Si phases in their structures , which damages its mechanical properties; Mg-Al-RE series (such as AE42) alloys and Mg-Y-Nd series (such as WE43 and WE54), due to the addition of more rare earth elements in the alloy, the cost of the alloy is high and limited It is widely used; the use of cheap elements to improve the mechanical properties of magnesium alloys plays an important role in the application of magnesium alloys in a wider range.
专利CN101871068B公开了一种低成本、含锡与铝的高强度高塑性镁合金及其制造方法,合金组分及重量百分比为3~7%Al,3~6%Sn,余量为Mg和不可避免的杂质。该合金具有高的强度和优良的塑性,不需要热处理,可直接使用的优点。但该合金组织中,Sn在枝晶间成分偏析,析出的金属间化合物Mg17Al12和Mg2Sn晶粒粗大,且分布不均匀,容易导致合金在高温下工作时,力学性能和抗蠕变性变差,从而影响镁合金的使用寿命。Patent CN101871068B discloses a low-cost, high-strength and high-plastic magnesium alloy containing tin and aluminum and its manufacturing method. The alloy composition and weight percentage are 3-7% Al, 3-6% Sn, and the balance is Mg and Avoid impurities. The alloy has the advantages of high strength and excellent plasticity, no need for heat treatment, and can be used directly. However, in the alloy structure, Sn segregates between dendrites, and the precipitated intermetallic compounds Mg 17 Al 12 and Mg 2 Sn have coarse grains and uneven distribution, which easily leads to poor mechanical properties and creep resistance when the alloy works at high temperatures. The denaturation becomes worse, thereby affecting the service life of the magnesium alloy.
发明内容Contents of the invention
本发明的目的是提供一种低成本高强耐热镁合金,在控制合金成本的基础上,提高镁合金在室温和高温条件下的力学性能,并赋予合金在高温下的优良抗蠕变性,扩大镁合金的应用范围。The purpose of the present invention is to provide a low-cost high-strength heat-resistant magnesium alloy, on the basis of controlling the cost of the alloy, improve the mechanical properties of the magnesium alloy at room temperature and high temperature, and endow the alloy with excellent creep resistance at high temperature, Expand the scope of application of magnesium alloys.
本发明的第二个目的是提供上述低成本高强耐热镁合金制备方法。The second object of the present invention is to provide the above-mentioned low-cost, high-strength, heat-resistant magnesium alloy preparation method.
为了实现以上目的,本发明所采用的技术方案是:In order to achieve the above object, the technical solution adopted in the present invention is:
一种低成本高强耐热镁合金,由以下重量百分比的组分组成:6.2~9.3%Al,3.5~5.5%Sn,1.0~1.8%Sb,0.2~0.9%Si,0.1~0.4%Sm,余量为Mg。A low-cost, high-strength, heat-resistant magnesium alloy is composed of the following components in weight percent: 6.2-9.3% Al, 3.5-5.5% Sn, 1.0-1.8% Sb, 0.2-0.9% Si, 0.1-0.4% Sm, and The amount is Mg.
本发明提供的低成本高强耐热镁合金,Al是镁合金中重要的合金元素,在镁中有非常大的固溶度,具有明显的强化作用,其强化作用表面在两方面,一是通过形成Mg17Al12金属间化合物的第二相强化,二是通过Al原子在镁基体中形成固溶体的固溶强化。为避免热稳定性较差Mg17Al12相的大量生成,镁铝系合金中Al的含量一般控制在9%以下,但是过低的Al含量会损害镁合金的铸造性能特别是合金的流动性,铸造镁合金Al的含量一般不应低于6%,本发明的镁合金中的Al含量为6.2~9.3%。添加Sn元素可以提高镁合金的流动性、降低镁合金的热裂敏感性,Sn与Mg形成的Mg2Sn相具有强化作用,有助于提高合金的强韧性;原料组成中少量的钐可以净化合金液,细化合金组织,改善Mg17Al12相的形貌和分布,提高力学性能;加入适量的锑、硅合金元素,有利于在Mg-Al或Mg-Al-Sn基体的晶界处析出耐高温性能好的金属间相,这些金属间相在高温的应力条件下,阻止晶粒滑动,从而使合金表现出优良的高温抗蠕变性。In the low-cost high-strength heat-resistant magnesium alloy provided by the present invention, Al is an important alloying element in magnesium alloy, has a very large solid solubility in magnesium, and has obvious strengthening effect, and its strengthening effect surface has two aspects, one is through The second phase strengthening is the formation of Mg 17 Al 12 intermetallic compounds, and the second is solid solution strengthening through the formation of solid solutions by Al atoms in the magnesium matrix. In order to avoid a large amount of Mg 17 Al 12 phases with poor thermal stability, the content of Al in magnesium-aluminum alloys is generally controlled below 9%, but too low Al content will damage the casting performance of magnesium alloys, especially the fluidity of alloys Generally, the Al content of the cast magnesium alloy should not be lower than 6%, and the Al content in the magnesium alloy of the present invention is 6.2-9.3%. Adding Sn element can improve the fluidity of magnesium alloy and reduce the hot cracking sensitivity of magnesium alloy. The Mg 2 Sn phase formed by Sn and Mg has a strengthening effect and helps to improve the strength and toughness of the alloy; a small amount of samarium in the raw material composition can purify Alloy liquid, refine alloy structure, improve the morphology and distribution of Mg 17 Al 12 phase, improve mechanical properties; add appropriate amount of antimony and silicon alloy elements, which is beneficial to the grain boundary of Mg-Al or Mg-Al-Sn matrix The intermetallic phases with good high temperature resistance are precipitated, and these intermetallic phases prevent the grains from sliding under high temperature stress conditions, so that the alloy exhibits excellent high temperature creep resistance.
本发明提供的低成本高强耐热镁合金,合金组分为Mg-Al-Sn-Sb-Si-Sm,利用多元微合金化改善镁合金的显微组织,进而提高其力学性能;合理选择合金化元素,控制各合金化元素的含量,发挥了各组分的协同强化作用,提高了镁合金的力学性能和耐热性能。The low-cost high-strength heat-resistant magnesium alloy provided by the invention has an alloy composition of Mg-Al-Sn-Sb-Si-Sm, and uses multi-element microalloying to improve the microstructure of the magnesium alloy, thereby improving its mechanical properties; rationally selecting the alloy Alloying elements, controlling the content of each alloying element, exerted the synergistic strengthening effect of each component, and improved the mechanical properties and heat resistance of magnesium alloys.
上述低成本高强耐热镁合金的制备方法,包括以下步骤:The preparation method of the above-mentioned low-cost high-strength heat-resistant magnesium alloy comprises the following steps:
1)将原料镁、铝、锡、锑在混合气体保护下熔化,形成合金熔液A;1) Melting raw materials magnesium, aluminum, tin and antimony under the protection of mixed gas to form alloy melt A;
2)将步骤1)所得合金熔液A加热至710~730℃时,加入中间合金Mg-Sm和中间合金Mg-Si,待合金全部熔化后,升温至740~750℃,搅拌均匀,得到合金熔液B;2) When the alloy melt A obtained in step 1) is heated to 710-730°C, the intermediate alloy Mg-Sm and the intermediate alloy Mg-Si are added, and after the alloy is completely melted, the temperature is raised to 740-750°C and stirred evenly to obtain the alloy Melt B;
3)将步骤2)所得合金熔液B的温度降至680~700℃,静置,浇铸到模具中,得铸态合金;3) reducing the temperature of the alloy melt B obtained in step 2) to 680-700° C., leaving it to stand, and casting it into a mold to obtain an as-cast alloy;
4)将步骤3)所得铸态合金进行热处理,即得。4) heat-treating the as-cast alloy obtained in step 3).
所述原料镁、铝、锡、锑、中间合金Mg-Sm和中间合金Mg-Si使用前经预热处理。原料经预热处理,有助于后续熔炼铸造过程均匀稳定进行;所述预热处理的温度为170~200℃,预热时间时间不低于2h;预热条件进一步优选为,180℃预热3h。The raw materials magnesium, aluminum, tin, antimony, master alloy Mg-Sm and master alloy Mg-Si are preheated before use. The raw materials are preheated, which helps the subsequent smelting and casting process to proceed uniformly and stably; the temperature of the preheating is 170-200°C, and the preheating time is not less than 2h; the preheating condition is further preferably 180°C 3h.
步骤1)所述混合气体为CO2和SF6。Step 1) The mixed gas is CO 2 and SF 6 .
步骤3)所述模具在浇铸前经预热处理。所述模具预热处理的温度为280~320℃;进一步优选模具预热温度为300℃。Step 3) The mold is preheated before casting. The temperature of the mold preheating treatment is 280-320°C; more preferably, the mold preheating temperature is 300°C.
步骤4)所述热处理为将铸态合金依次进行固溶处理和时效处理。Step 4) The heat treatment is to perform solution treatment and aging treatment on the as-cast alloy in sequence.
所述固溶处理的温度为415~430℃,处理时间为10~14h;固溶处理条件进一步优选为,温度425℃,处理时间为11h;固溶处理后热水淬火至室温。所用热水温度为75~90℃。The temperature of the solution treatment is 415-430° C., and the treatment time is 10-14 hours; the solution treatment conditions are more preferably, the temperature is 425° C., and the treatment time is 11 hours; after the solution treatment, the hot water is quenched to room temperature. The temperature of the hot water used is 75-90°C.
所述时效处理的温度为200~250℃,处理时间为14~18h;时效处理条件进一步优选为,温度220℃,处理时间为16h;时效处理后空冷至室温。The temperature of the aging treatment is 200-250° C., and the treatment time is 14-18 hours; the aging treatment conditions are more preferably, the temperature is 220° C., and the treatment time is 16 hours; air cooling to room temperature after the aging treatment.
所述固溶处理是在氧化镁粉末覆盖下进行。The solid solution treatment is carried out under the cover of magnesium oxide powder.
本发明提供的低成本高强耐热镁合金的制备方法,以镁、铝、锡、锑、中间合金Mg-Sm和中间合金Mg-Si为原料熔炼铸造并经热处理,所得镁合金显微组织均匀,具有较高的室温和高温强度,且高温条件下,抗蠕变性优良;所用原料廉价易得,熔炼和铸造的难度低,过程易于控制,极大地降低了成产成本,工艺简单,操作方便,适合大规模工业化生产。The preparation method of the low-cost high-strength heat-resistant magnesium alloy provided by the present invention uses magnesium, aluminum, tin, antimony, master alloy Mg-Sm and master alloy Mg-Si as raw materials for melting and casting and heat treatment, and the microstructure of the obtained magnesium alloy is uniform , has high strength at room temperature and high temperature, and has excellent creep resistance under high temperature conditions; the raw materials used are cheap and easy to obtain, the difficulty of smelting and casting is low, the process is easy to control, and the production cost is greatly reduced. The process is simple and the operation Convenient and suitable for large-scale industrial production.
由该方法制备得到的耐热镁合金,显微组织均匀,室温抗拉强度可达到285MPa,200℃的抗拉强度达到192MPa,具有较高的室温和高温强度;该合金在200℃和70MPa条件下蠕变100小时,应变量最低为0.36%,稳态蠕变速率低至1.21×10-8s-1,具有良好的高温抗蠕变性;该合金主要组分均为廉价元素,在保持较高的力学性能的基础上,极大地降低了镁合金的成本,适合推广应用。The heat-resistant magnesium alloy prepared by this method has uniform microstructure, the tensile strength at room temperature can reach 285MPa, and the tensile strength at 200°C can reach 192MPa, which has high room temperature and high temperature strength; After creeping for 100 hours, the minimum strain is 0.36%, and the steady-state creep rate is as low as 1.21×10 -8 s -1 , which has good high temperature creep resistance; the main components of the alloy are cheap elements, and the On the basis of higher mechanical properties, the cost of the magnesium alloy is greatly reduced, and it is suitable for popularization and application.
具体实施方式detailed description
下面结合具体实施例对本发明作进一步的说明。各实施例中涉及的原料镁(Mg),铝(Al),锡(Sn),锑(Sb),中间合金Mg-Sm和中间合金Mg-Si均为市售产品。The present invention will be further described below in conjunction with specific examples. The raw materials magnesium (Mg), aluminum (Al), tin (Sn), antimony (Sb), master alloy Mg-Sm and master alloy Mg-Si involved in each embodiment are all commercially available products.
实施例1Example 1
本实施例的低成本高强耐热镁合金,由以下重量百分比的组分组成:6.2%Al,4.9%Sn,1.8%Sb,0.7%Si,0.4%Sm,余量为Mg。The low-cost high-strength heat-resistant magnesium alloy of this embodiment is composed of the following components in weight percentage: 6.2% Al, 4.9% Sn, 1.8% Sb, 0.7% Si, 0.4% Sm, and the balance is Mg.
本实施例的低成本高强耐热镁合金的制备方法,包括以下步骤:The preparation method of the low-cost high-strength heat-resistant magnesium alloy of the present embodiment comprises the following steps:
1)将原料纯镁锭、纯铝锭、纯锡粒、纯锑、Mg-Sm中间合金和Mg-Si中间合金放置于干燥箱中进行干燥预热,预热温度为180℃,预热时间为3小时;将预热后的纯镁锭、纯铝锭、纯锡粒、纯锑在CO2+SF6混合气体保护下熔化,形成合金熔液A;1) Place the raw materials of pure magnesium ingot, pure aluminum ingot, pure tin grain, pure antimony, Mg-Sm master alloy and Mg-Si master alloy in a drying oven for drying and preheating. The preheating temperature is 180°C and the preheating time is 3 hours; melt the preheated pure magnesium ingots, pure aluminum ingots, pure tin grains, and pure antimony under the protection of CO 2 +SF 6 mixed gas to form alloy melt A;
2)将步骤1)所得合金熔液A加热至720℃时,加入中间合金Mg-Sm和中间合金Mg-Si,保温10min,待合金全部熔化后去除表面浮渣,继续升温至740℃后停止升温,搅拌均匀,得到合金熔液B;2) When the alloy melt A obtained in step 1) is heated to 720°C, add the master alloy Mg-Sm and master alloy Mg-Si, keep it warm for 10 minutes, remove the surface scum after the alloy is completely melted, continue to heat up to 740°C and stop Raise the temperature and stir evenly to obtain alloy melt B;
3)将步骤2)所得合金熔液B的温度降至700℃,静置5分钟,然后浇铸到经预热的金属型模具中(金属型模具的预热温度为300℃),得铸态合金;3) Reduce the temperature of the alloy melt B obtained in step 2) to 700°C, let it stand for 5 minutes, and then cast it into a preheated metal mold (the preheating temperature of the metal mold is 300°C) to obtain the cast state alloy;
4)对步骤3)所得铸态合金依次进行固溶处理和时效处理,固溶处理在氧化镁粉末覆盖下进行,处理温度为425℃,处理时间为11h,80℃热水淬火至室温;时效处理的温度为220℃,处理时间为16h,空冷至室温,即得。4) The as-cast alloy obtained in step 3) is subjected to solution treatment and aging treatment sequentially, the solution treatment is carried out under the cover of magnesium oxide powder, the treatment temperature is 425 ° C, the treatment time is 11 h, 80 ° C hot water quenching to room temperature; aging The treatment temperature is 220° C., the treatment time is 16 hours, and air-cooled to room temperature.
实施例2Example 2
本实施例的低成本高强耐热镁合金,由以下重量百分比的组分组成:7.4%Al,5.5%Sn,1.5%Sb,0.9%Si,0.2%Sm,余量为Mg。The low-cost, high-strength, heat-resistant magnesium alloy of this embodiment is composed of the following components by weight percentage: 7.4% Al, 5.5% Sn, 1.5% Sb, 0.9% Si, 0.2% Sm, and the balance is Mg.
本实施例的低成本高强耐热镁合金的制备方法,包括以下步骤:The preparation method of the low-cost high-strength heat-resistant magnesium alloy of the present embodiment comprises the following steps:
1)将原料纯镁锭、纯铝锭、纯锡粒、纯锑、Mg-Sm中间合金和Mg-Si中间合金放置于干燥箱中进行干燥预热,预热温度为170℃,预热时间为4小时;将预热后的纯镁锭、纯铝锭、纯锡粒、纯锑在CO2+SF6混合气体保护下熔化,形成合金熔液A;1) Place the raw materials of pure magnesium ingot, pure aluminum ingot, pure tin grain, pure antimony, Mg-Sm master alloy and Mg-Si master alloy in a drying oven for drying and preheating. The preheating temperature is 170°C and the preheating time is 4 hours; melt the preheated pure magnesium ingots, pure aluminum ingots, pure tin grains, and pure antimony under the protection of CO 2 +SF 6 mixed gas to form alloy melt A;
2)将步骤1)所得合金熔液A加热至730℃时,加入中间合金Mg-Sm和中间合金Mg-Si,保温10min,待合金全部熔化后去除表面浮渣,继续升温至740℃后停止升温,搅拌均匀,得到合金熔液B;2) When the alloy melt A obtained in step 1) is heated to 730°C, add the master alloy Mg-Sm and master alloy Mg-Si, keep it warm for 10 minutes, remove the surface scum after the alloy is completely melted, continue to heat up to 740°C and stop Raise the temperature and stir evenly to obtain alloy melt B;
3)将步骤2)所得合金熔液B的温度降至690℃,静置5分钟,然后浇铸到经预热的金属型模具中(金属型模具的预热温度为300℃),得铸态合金;3) Reduce the temperature of the alloy melt B obtained in step 2) to 690°C, let it stand for 5 minutes, and then cast it into a preheated metal mold (the preheating temperature of the metal mold is 300°C) to obtain the cast state alloy;
4)对步骤3)所得铸态合金依次进行固溶处理和时效处理,固溶处理在氧化镁粉末覆盖下进行,处理温度为420℃,处理时间为13h,85℃热水淬火至室温;时效处理的温度为220℃,处理时间为16h,空冷至室温,即得。4) The as-cast alloy obtained in step 3) is subjected to solution treatment and aging treatment sequentially, the solution treatment is carried out under the cover of magnesium oxide powder, the treatment temperature is 420°C, the treatment time is 13h, and the hot water is quenched at 85°C to room temperature; aging The treatment temperature is 220° C., the treatment time is 16 hours, and air-cooled to room temperature.
实施例3Example 3
本实施例的低成本高强耐热镁合金,由以下重量百分比的组分组成:8.6%Al,4.4%Sn,1.6%Sb,0.2%Si,0.3%Sm,余量为Mg。The low-cost, high-strength, heat-resistant magnesium alloy of this embodiment is composed of the following components by weight percentage: 8.6% Al, 4.4% Sn, 1.6% Sb, 0.2% Si, 0.3% Sm, and the balance is Mg.
本实施例的低成本高强耐热镁合金的制备方法,包括以下步骤:The preparation method of the low-cost high-strength heat-resistant magnesium alloy of the present embodiment comprises the following steps:
1)将原料纯镁锭、纯铝锭、纯锡粒、纯锑、Mg-Sm中间合金和Mg-Si中间合金放置于干燥箱中进行干燥预热,预热温度为200℃,预热时间为2小时;将预热后的纯镁锭、纯铝锭、纯锡粒、纯锑在CO2+SF6混合气体保护下熔化,形成合金熔液A;1) Place the raw materials of pure magnesium ingot, pure aluminum ingot, pure tin grain, pure antimony, Mg-Sm master alloy and Mg-Si master alloy in a drying oven for drying and preheating. The preheating temperature is 200°C and the preheating time is 2 hours; melt the preheated pure magnesium ingots, pure aluminum ingots, pure tin particles, and pure antimony under the protection of CO 2 +SF 6 mixed gas to form alloy melt A;
2)将步骤1)所得合金熔液A加热至720℃时,加入中间合金Mg-Sm和中间合金Mg-Si,保温10min,待合金全部熔化后去除表面浮渣,继续升温至740℃后停止升温,搅拌均匀,得到合金熔液B;2) When the alloy melt A obtained in step 1) is heated to 720°C, add the master alloy Mg-Sm and master alloy Mg-Si, keep it warm for 10 minutes, remove the surface scum after the alloy is completely melted, continue to heat up to 740°C and stop Raise the temperature and stir evenly to obtain alloy melt B;
3)将步骤2)所得合金熔液B的温度降至700℃,静置5分钟,然后浇铸到经预热的金属型模具中(金属型模具的预热温度为300℃),得铸态合金;3) Reduce the temperature of the alloy melt B obtained in step 2) to 700°C, let it stand for 5 minutes, and then cast it into a preheated metal mold (the preheating temperature of the metal mold is 300°C) to obtain the cast state alloy;
4)对步骤3)所得铸态合金依次进行固溶处理和时效处理,固溶处理在氧化镁粉末覆盖下进行,处理温度为430℃,处理时间为10h,90℃热水淬火至室温;时效处理的温度为250℃,处理时间为15h,空冷至室温,即得。4) The as-cast alloy obtained in step 3) is subjected to solution treatment and aging treatment sequentially, the solution treatment is carried out under the cover of magnesium oxide powder, the treatment temperature is 430°C, the treatment time is 10h, and the hot water is quenched at 90°C to room temperature; aging The treatment temperature is 250° C., the treatment time is 15 hours, and air-cooled to room temperature.
实施例4Example 4
本实施例的低成本高强耐热镁合金,由以下重量百分比的组分组成:9.3%Al,3.5%Sn,1.2%Sb,0.4%Si,0.1%Sm,余量为Mg。The low-cost high-strength heat-resistant magnesium alloy of this embodiment is composed of the following components in weight percentage: 9.3% Al, 3.5% Sn, 1.2% Sb, 0.4% Si, 0.1% Sm, and the balance is Mg.
本实施例的低成本高强耐热镁合金的制备方法,包括以下步骤:The preparation method of the low-cost high-strength heat-resistant magnesium alloy of the present embodiment comprises the following steps:
1)将原料纯镁锭、纯铝锭、纯锡粒、纯锑、Mg-Sm中间合金和Mg-Si中间合金放置于干燥箱中进行干燥预热,预热温度为180℃,预热时间为3小时;将预热后的纯镁锭、纯铝锭、纯锡粒、纯锑在CO2+SF6混合气体保护下熔化,形成合金熔液A;1) Place the raw materials of pure magnesium ingot, pure aluminum ingot, pure tin grain, pure antimony, Mg-Sm master alloy and Mg-Si master alloy in a drying oven for drying and preheating. The preheating temperature is 180°C and the preheating time is 3 hours; melt the preheated pure magnesium ingots, pure aluminum ingots, pure tin grains, and pure antimony under the protection of CO 2 +SF 6 mixed gas to form alloy melt A;
2)将步骤1)所得合金熔液A加热至720℃时,加入中间合金Mg-Sm和中间合金Mg-Si,保温10min,待合金全部熔化后去除表面浮渣,继续升温至740℃后停止升温,搅拌均匀,得到合金熔液B;2) When the alloy melt A obtained in step 1) is heated to 720°C, add the master alloy Mg-Sm and master alloy Mg-Si, keep it warm for 10 minutes, remove the surface scum after the alloy is completely melted, continue to heat up to 740°C and stop Raise the temperature and stir evenly to obtain alloy melt B;
3)将步骤2)所得合金熔液B的温度降至700℃,静置5分钟,然后浇铸到经预热的金属型模具中(金属型模具的预热温度为300℃),得铸态合金;3) Reduce the temperature of the alloy melt B obtained in step 2) to 700°C, let it stand for 5 minutes, and then cast it into a preheated metal mold (the preheating temperature of the metal mold is 300°C) to obtain the cast state alloy;
4)对步骤3)所得铸态合金依次进行固溶处理和时效处理,固溶处理在氧化镁粉末覆盖下进行,处理温度为425℃,处理时间为11h,90℃热水淬火至室温;时效处理的温度为220℃,处理时间为16h,空冷至室温,即得。4) The as-cast alloy obtained in step 3) is subjected to solution treatment and aging treatment sequentially, the solution treatment is carried out under the cover of magnesium oxide powder, the treatment temperature is 425°C, the treatment time is 11h, and the hot water is quenched at 90°C to room temperature; aging The treatment temperature is 220° C., the treatment time is 16 hours, and air-cooled to room temperature.
试验例Test case
本试验例对实施例1~4所得低成本高强耐热镁合金的抗拉强度、屈服强度、高温抗蠕变性进行检测,其中蠕变试验测试条件为,蠕变温度200℃,应力70MPa条件下100小时。试验结果列于表1中。由表1的试验结果可知,本发明所制备的低成本高强耐热镁合金在室温~200℃范围内具有高的抗拉强度、屈服强度和抗蠕变性能,适合大规模推广应用。This test example detects the tensile strength, yield strength and high temperature creep resistance of the low-cost high-strength heat-resistant magnesium alloy obtained in Examples 1-4, wherein the creep test test conditions are: creep temperature 200 ° C, stress 70 MPa conditions Under 100 hours. The test results are listed in Table 1. From the test results in Table 1, it can be seen that the low-cost high-strength heat-resistant magnesium alloy prepared by the present invention has high tensile strength, yield strength and creep resistance in the range of room temperature to 200°C, and is suitable for large-scale application.
表1实施例1~4低成本高强耐热镁合金的性能检测结果Table 1 The performance detection results of low-cost high-strength heat-resistant magnesium alloys in Examples 1-4
Claims (10)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510427006.1A CN105039816B (en) | 2015-07-20 | 2015-07-20 | A kind of high strength and low cost heat resistance magnesium alloy and preparation method thereof |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510427006.1A CN105039816B (en) | 2015-07-20 | 2015-07-20 | A kind of high strength and low cost heat resistance magnesium alloy and preparation method thereof |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN105039816A CN105039816A (en) | 2015-11-11 |
| CN105039816B true CN105039816B (en) | 2017-05-31 |
Family
ID=54446780
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510427006.1A Expired - Fee Related CN105039816B (en) | 2015-07-20 | 2015-07-20 | A kind of high strength and low cost heat resistance magnesium alloy and preparation method thereof |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105039816B (en) |
Families Citing this family (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105478750A (en) * | 2015-12-22 | 2016-04-13 | 安徽省春谷3D打印智能装备产业技术研究院有限公司 | High tenacity metallic material composition for printer and preparation method of high tenacity metal |
| KR101858856B1 (en) * | 2016-12-21 | 2018-05-17 | 주식회사 포스코 | High strength magnesium alloy having excellent fire-retardant, and method for manufacturing the same |
| CN107116314B (en) * | 2017-04-27 | 2019-12-24 | 河南科技大学 | A kind of magnesium alloy brazing filler metal containing Sm and its preparation method and application |
| TWI685572B (en) * | 2018-12-04 | 2020-02-21 | 國立中興大學 | Melting of pure silicon in liquid magnesium and a fabricating method of magnesium-based thermoelectric materials |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1637160A (en) * | 2004-01-09 | 2005-07-13 | 高田株式会社 | Die casting magnesium alloy and magnesium die casting |
| CN100338250C (en) * | 2004-05-19 | 2007-09-19 | 中国科学院金属研究所 | High strength and high toughness cast magnesium alloy and preparing process thereof |
| CN101532106A (en) * | 2009-04-13 | 2009-09-16 | 河南科技大学 | Heat resisting casting rare earth magnesium alloy and preparation method thereof |
| CN101643872A (en) * | 2009-09-01 | 2010-02-10 | 吉林大学 | High-strength high-plasticity magnesium alloy and preparation method thereof |
| CN104694805A (en) * | 2015-02-27 | 2015-06-10 | 河南科技大学 | Low-cost multi-component heat-resistant magnesium alloy and preparation method of magnesium alloy |
-
2015
- 2015-07-20 CN CN201510427006.1A patent/CN105039816B/en not_active Expired - Fee Related
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1637160A (en) * | 2004-01-09 | 2005-07-13 | 高田株式会社 | Die casting magnesium alloy and magnesium die casting |
| CN100338250C (en) * | 2004-05-19 | 2007-09-19 | 中国科学院金属研究所 | High strength and high toughness cast magnesium alloy and preparing process thereof |
| CN101532106A (en) * | 2009-04-13 | 2009-09-16 | 河南科技大学 | Heat resisting casting rare earth magnesium alloy and preparation method thereof |
| CN101643872A (en) * | 2009-09-01 | 2010-02-10 | 吉林大学 | High-strength high-plasticity magnesium alloy and preparation method thereof |
| CN104694805A (en) * | 2015-02-27 | 2015-06-10 | 河南科技大学 | Low-cost multi-component heat-resistant magnesium alloy and preparation method of magnesium alloy |
Also Published As
| Publication number | Publication date |
|---|---|
| CN105039816A (en) | 2015-11-11 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN109881063B (en) | A kind of high-strength, toughness and high-modulus die-casting magnesium alloy and preparation method thereof | |
| CN104694805B (en) | Low-cost multi-component heat-resistant magnesium alloy and preparation method of magnesium alloy | |
| CN103695741B (en) | A kind of Mg-Zn-Al-Sn-Mn series magnesium alloy and preparation method thereof | |
| CN103421999B (en) | A kind of containing Heat Resistant Rare Earth-magnesium Alloy and preparation method thereof | |
| CN102978497B (en) | Casting magnesium alloy with high strength and toughness and preparation method thereof | |
| CN109881062B (en) | High-strength, high-toughness and high-modulus extrusion casting magnesium alloy and preparation method thereof | |
| CN100588733C (en) | A kind of magnesium alloy for semi-solid forming and its semi-solid blank preparation method | |
| CN101440449B (en) | Multicomponent heat resisting magnesium alloy and preparation thereof | |
| CN105018812B (en) | A kind of heat resistance magnesium alloy and preparation method thereof | |
| CN102154580B (en) | High-intensity heat-resistant magnesium alloy material and preparation process thereof | |
| CN100424210C (en) | Die-cast heat-resistant magnesium alloy | |
| CN103146973B (en) | High-temperature-resistant rare earth magnesium alloy | |
| CN105112742B (en) | A kind of Al-Si-Mg-Cu-Ti-Sc casting wrought alloy and preparation method thereof | |
| CN104674092B (en) | A kind of Mg Al Zn system heat resistance magnesium alloy containing Sm and preparation method thereof | |
| CN104233026A (en) | Heat-resistant magnesium alloy and preparation method thereof | |
| CN109957687A (en) | A kind of die-casting aluminum-silicon alloy and preparation method thereof | |
| CN105039816B (en) | A kind of high strength and low cost heat resistance magnesium alloy and preparation method thereof | |
| CN109852856B (en) | High-strength, high-toughness and high-modulus metal mold gravity casting magnesium alloy and preparation method thereof | |
| CN109930045B (en) | High strength, toughness and heat resistance Mg-Gd alloy suitable for gravity casting and preparation method thereof | |
| CN105154733B (en) | A kind of non-rare earth cast magnesium alloy and preparation method thereof | |
| CN111705249A (en) | A kind of high-strength heat-resistant rare earth magnesium alloy and preparation method thereof | |
| CN103074531B (en) | Heat resistant alloy of rare earth and magnesium and preparation method thereof | |
| CN107190189B (en) | A kind of magnesium alloy with mechanical and anti-corrosion properties and preparation method thereof | |
| CN103045922B (en) | Heat-resisting casting magnesium alloy | |
| CN103484742A (en) | High-strength damping magnesium alloy |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20170531 Termination date: 20180720 |