CN108486431A - Selective laser melting process Al-Si-Mg line aluminium alloys composition and molded part preparation method - Google Patents
Selective laser melting process Al-Si-Mg line aluminium alloys composition and molded part preparation method Download PDFInfo
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- 229910000838 Al alloy Inorganic materials 0.000 title claims abstract description 71
- 229910018566 Al—Si—Mg Inorganic materials 0.000 title claims abstract description 27
- 239000000203 mixture Substances 0.000 title claims abstract description 19
- 238000002360 preparation method Methods 0.000 title claims abstract description 18
- 238000010309 melting process Methods 0.000 title 1
- 229910052751 metal Inorganic materials 0.000 claims abstract description 33
- 239000002184 metal Substances 0.000 claims abstract description 33
- 239000000843 powder Substances 0.000 claims abstract description 33
- 238000002844 melting Methods 0.000 claims abstract description 32
- 230000008018 melting Effects 0.000 claims abstract description 32
- 229910045601 alloy Inorganic materials 0.000 claims abstract description 31
- 239000000956 alloy Substances 0.000 claims abstract description 31
- 238000005516 engineering process Methods 0.000 claims abstract description 25
- 229910052782 aluminium Inorganic materials 0.000 claims abstract description 22
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims abstract description 21
- 238000000034 method Methods 0.000 claims abstract description 20
- 238000010438 heat treatment Methods 0.000 claims abstract description 8
- 238000000465 moulding Methods 0.000 claims description 18
- 239000000758 substrate Substances 0.000 claims description 10
- 238000003756 stirring Methods 0.000 claims description 9
- 230000008676 import Effects 0.000 claims description 5
- 239000000126 substance Substances 0.000 claims description 5
- 229910018580 Al—Zr Inorganic materials 0.000 claims description 3
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 claims description 3
- 239000000155 melt Substances 0.000 claims description 3
- 238000000889 atomisation Methods 0.000 claims description 2
- 238000007711 solidification Methods 0.000 claims description 2
- 230000008023 solidification Effects 0.000 claims description 2
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 claims 2
- 239000007788 liquid Substances 0.000 claims 1
- 229910052757 nitrogen Inorganic materials 0.000 claims 1
- 238000003723 Smelting Methods 0.000 abstract description 5
- 239000011159 matrix material Substances 0.000 abstract description 5
- 239000002245 particle Substances 0.000 abstract description 5
- 238000004519 manufacturing process Methods 0.000 abstract description 3
- 238000005728 strengthening Methods 0.000 abstract description 3
- 238000005266 casting Methods 0.000 description 8
- 230000009286 beneficial effect Effects 0.000 description 7
- 239000012071 phase Substances 0.000 description 7
- 238000011056 performance test Methods 0.000 description 6
- 238000012360 testing method Methods 0.000 description 6
- 229910019018 Mg 2 Si Inorganic materials 0.000 description 5
- 238000005275 alloying Methods 0.000 description 4
- 229910021364 Al-Si alloy Inorganic materials 0.000 description 3
- 230000032683 aging Effects 0.000 description 3
- 230000005540 biological transmission Effects 0.000 description 3
- 239000000463 material Substances 0.000 description 3
- 238000012545 processing Methods 0.000 description 3
- 238000001556 precipitation Methods 0.000 description 2
- 239000011856 silicon-based particle Substances 0.000 description 2
- 239000007787 solid Substances 0.000 description 2
- 229910007981 Si-Mg Inorganic materials 0.000 description 1
- 229910008316 Si—Mg Inorganic materials 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000018109 developmental process Effects 0.000 description 1
- 238000009792 diffusion process Methods 0.000 description 1
- 230000008034 disappearance Effects 0.000 description 1
- 238000010894 electron beam technology Methods 0.000 description 1
- 239000007791 liquid phase Substances 0.000 description 1
- 238000007578 melt-quenching technique Methods 0.000 description 1
- 238000007712 rapid solidification Methods 0.000 description 1
- 238000005204 segregation Methods 0.000 description 1
- 238000009827 uniform distribution Methods 0.000 description 1
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- B22F3/00—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
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- B22F9/00—Making metallic powder or suspensions thereof
- B22F9/02—Making metallic powder or suspensions thereof using physical processes
- B22F9/06—Making metallic powder or suspensions thereof using physical processes starting from liquid material
- B22F9/08—Making metallic powder or suspensions thereof using physical processes starting from liquid material by casting, e.g. through sieves or in water, by atomising or spraying
- B22F9/082—Making metallic powder or suspensions thereof using physical processes starting from liquid material by casting, e.g. through sieves or in water, by atomising or spraying atomising using a fluid
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- B33Y70/00—Materials specially adapted for additive manufacturing
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- C22C1/03—Making non-ferrous alloys by melting using master alloys
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- B22F9/06—Making metallic powder or suspensions thereof using physical processes starting from liquid material
- B22F9/08—Making metallic powder or suspensions thereof using physical processes starting from liquid material by casting, e.g. through sieves or in water, by atomising or spraying
- B22F9/082—Making metallic powder or suspensions thereof using physical processes starting from liquid material by casting, e.g. through sieves or in water, by atomising or spraying atomising using a fluid
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Abstract
本发明公开了一种选区激光熔化技术用Al‑Si‑Mg系铝合金组合物,按质量百分比由:Si 7‑15%、Mg 0.8‑3%、Mn 1.2‑2%、Zr 0.5‑1.5%,余量为铝组成。通过母合金熔炼,金属粉末制备,铝合金成型件的制备及热处理工艺步骤制得铝合金成型件。本发明通过选区激光熔化制造技术,大幅提高合金元素在铝基体中的溶解度,并通过增加铝合金中第二相强化粒子的浓度,大幅度提高铝合金的力学性能。本发明的Al‑Si‑Mg系铝合金成分,经过选区激光熔化技术制备获得铝合金的最大屈服强度σ0.2可达380MPa,抗拉强度σb可达520MPa,并且合金的塑性变形率超过8%。适用于通过选区激光熔化技术制备力学性能要求较高的复杂结构件。The invention discloses an Al-Si-Mg series aluminum alloy composition for selective laser melting technology, which comprises: Si 7-15%, Mg 0.8-3%, Mn 1.2-2%, Zr 0.5-1.5% by mass percentage , and the balance is composed of aluminum. The aluminum alloy molded parts are obtained through master alloy smelting, metal powder preparation, aluminum alloy molded parts preparation and heat treatment process steps. The invention greatly improves the solubility of alloy elements in the aluminum matrix through the selective laser melting manufacturing technology, and greatly improves the mechanical properties of the aluminum alloy by increasing the concentration of the second phase strengthening particles in the aluminum alloy. The Al-Si-Mg aluminum alloy composition of the present invention is prepared by selective laser melting technology to obtain the maximum yield strength σ 0.2 of the aluminum alloy up to 380MPa, the tensile strength σb up to 520MPa, and the plastic deformation rate of the alloy exceeds 8%. . It is suitable for preparing complex structural parts with high mechanical performance requirements through selective laser melting technology.
Description
技术领域technical field
本发明涉及新材料技术领域,特别涉及一系列具有高拉伸强度、高塑性变形率的选区激光熔化技术用Al-Si-Mg系铝合金组合物。The invention relates to the technical field of new materials, in particular to a series of Al-Si-Mg series aluminum alloy compositions with high tensile strength and high plastic deformation rate for selective laser melting technology.
背景技术Background technique
Al-Si合金作为产量及用量最大的铸造铝合金,具有耐磨耐侵蚀性好,热膨胀系数低,比强度高,导热性好等优点,这使得Al-Si合金被广泛应用于活塞、发动机组、缸套、轮毂、轴承、轴瓦、曲轴箱等汽车零部件。Al-Si-Mg合金中,Mg与Si元素在铝合金凝固过程中部分溶解在铝基体中,部分以Mg2Si相析出,由于作为初生相形成的Mg2Si尺寸比较粗大,多呈尖角状,割裂基体,降低了材料的力学性能。Al-Si-Mg合金经后期固溶加时效处理后,可使Mg2Si相在铝合金基体中弥散析出,析出相与基体之间存在一定的应变场,这些应变场成为位错运动的障碍从而起到沉淀强化的作用。但由于传统铸件在固溶处理过程中Mg在Al-Si合金中的固溶度有限,导致后期时效处理过程中Mg2Si粒子析出浓度受限,从而限制Al-Si-Mg合金力学性能的进一步提升。As the cast aluminum alloy with the largest output and consumption, Al-Si alloy has the advantages of good wear resistance and corrosion resistance, low thermal expansion coefficient, high specific strength, and good thermal conductivity, which makes Al-Si alloy widely used in pistons and engine blocks. , cylinder liners, hubs, bearings, bearing bushes, crankcases and other auto parts. In the Al-Si-Mg alloy, Mg and Si elements are partially dissolved in the aluminum matrix during the solidification process of the aluminum alloy, and some are precipitated as the Mg 2 Si phase. Since the Mg 2 Si formed as the primary phase is relatively coarse in size, it is mostly sharp-edged shape, split the matrix, and reduce the mechanical properties of the material. After the Al-Si-Mg alloy undergoes late solution and aging treatment, the Mg 2 Si phase can be dispersed and precipitated in the aluminum alloy matrix, and there is a certain strain field between the precipitated phase and the matrix, and these strain fields become obstacles to dislocation movement Thereby playing the role of precipitation strengthening. However, due to the limited solid solubility of Mg in the Al-Si alloy during the solution treatment of traditional castings, the precipitation concentration of Mg 2 Si particles in the later aging treatment process is limited, thereby limiting the further improvement of the mechanical properties of the Al-Si-Mg alloy. promote.
快速成型技术是集计算机辅助技术和激光及电子束加工于一体的新型加工技术。它可以针对性地解决铸造工艺中暴露出的一些缺陷,满足铸造过程中加工困难或无法加工的特殊零部件的成型加工需求。选区激光熔化技术为快速成型技术的一种,被称作未来快速成型领域的主要发展趋势,在金属成型中的应用将为制造业带来突破性的飞跃。Rapid prototyping technology is a new processing technology that integrates computer-aided technology and laser and electron beam processing. It can solve some defects exposed in the casting process in a targeted manner, and meet the forming processing requirements of special parts that are difficult or impossible to process in the casting process. Selected area laser melting technology is a kind of rapid prototyping technology, which is called the main development trend in the field of rapid prototyping in the future, and its application in metal forming will bring a breakthrough leap in the manufacturing industry.
选区激光熔化成型过程分为快速升温和急速降温两个阶段:首先激光束与金属粉体相互作用,由于金属粉末吸收激光束的能量,温度骤然上升并超过了金属的熔点形成熔池,此时,熔融金属处于液相平衡,金属原子可以自由移动,合金元素均匀分布;当激光束移开后,由于热源的消失,熔池温度以103-106K/s的速度下降。在此过程中,金属原子和合金元素的扩散移动受限,抑制了晶粒的长大和合金元素的偏析,凝固后的金属组织晶粒细小,合金元素分布均匀,能够大幅提高材料的强度和韧性。除此之外,由于熔池的快速凝固行为,使得Al-Si-Mg系铝合金中合金化原子的固溶度得到大幅提升,从而在铝合金后期的时效热处理过程中能够获得高浓度的Mg2Si粒子,可有效提高铝合金的强度。然而,现在选区激光熔化技术应用的铝合金成分仍以传统铸造合金成分为主,无法体现选区激光熔化技术的熔体急冷的工艺特性,实现Al-Si-Mg系铝合金性能的进一步提升。现阶段选区激光熔化成型铝合金的强度和塑性虽然远高于铸造铝合金(选区激光熔化成型铝合金的屈服强度约为200~320MPa,抗拉强度约为340~500MPa),但仍有较大提升空间。The selective laser melting molding process is divided into two stages: rapid heating and rapid cooling: firstly, the laser beam interacts with the metal powder, and because the metal powder absorbs the energy of the laser beam, the temperature rises suddenly and exceeds the melting point of the metal to form a molten pool. , the molten metal is in liquid phase equilibrium, the metal atoms can move freely, and the alloy elements are evenly distributed; when the laser beam is removed, the temperature of the molten pool drops at a rate of 10 3 -10 6 K/s due to the disappearance of the heat source. During this process, the diffusion and movement of metal atoms and alloying elements is limited, which inhibits the growth of grains and the segregation of alloying elements. The solidified metal structure has fine grains and uniform distribution of alloying elements, which can greatly improve the strength and toughness of the material. . In addition, due to the rapid solidification behavior of the molten pool, the solid solubility of the alloying atoms in the Al-Si-Mg aluminum alloy is greatly improved, so that a high concentration of Mg can be obtained during the later aging heat treatment of the aluminum alloy. 2 Si particles can effectively improve the strength of aluminum alloy. However, the composition of aluminum alloys currently used in selective laser melting technology is still dominated by traditional casting alloys, which cannot reflect the process characteristics of melt quenching in selective laser melting technology and further improve the performance of Al-Si-Mg aluminum alloys. At this stage, although the strength and plasticity of aluminum alloys formed by selective laser melting are much higher than those of cast aluminum alloys (the yield strength of aluminum alloys formed by selective laser melting is about 200-320MPa, and the tensile strength is about 340-500MPa), there are still relatively large Room for improvement.
发明内容Contents of the invention
本发明目的要解决的技术问题是:克服传统铸造Al-Si-Mg系铝合金中第二相粒子含量受限的缺点,应用选区激光熔化技术实现Al-Si-Mg系铝合金中第二相粒子含量的提升,进而实现力学性能的提升。最终提供一系列具有优异力学性能的Al-Si-Mg系选区激光熔化技术专用铝合金,该合金的力学性能明显优于传统铸造和选区激光熔化成型技术获得的Al-Si-Mg系铝合金的力学性能。The technical problem to be solved by the present invention is: to overcome the shortcomings of the limited content of the second phase particles in the traditional casting Al-Si-Mg series aluminum alloy, and to realize the second phase particle content in the Al-Si-Mg series aluminum alloy by using the selective laser melting technology. The increase of the particle content leads to the improvement of the mechanical properties. Finally, a series of Al-Si-Mg series aluminum alloys for selective laser melting technology with excellent mechanical properties will be provided. The mechanical properties of this alloy are significantly better than those obtained by traditional casting and selective laser melting forming technology. mechanical properties.
为达到上述目的,本发明实现目的所采用的技术方案如下:In order to achieve the above object, the technical scheme adopted by the present invention to realize the object is as follows:
一种选区激光熔化技术用Al-Si-Mg系铝合金组合物,按质量百分比计,由成分及含量为:Si 7-15%、Mg 0.8-3%、Mn 1.2-2%、Zr 0.5-1.5%,余量为铝组成,总质量百分比为100%。An Al-Si-Mg aluminum alloy composition for selective laser melting technology, the composition and content are: Si 7-15%, Mg 0.8-3%, Mn 1.2-2%, Zr 0.5- 1.5%, the balance is composed of aluminum, and the total mass percentage is 100%.
其中,所述铝的纯度为99.99%的纯铝。Wherein, the purity of the aluminum is 99.99% pure aluminum.
所述的Si、Mg、Mn、Zr为单质或铝基中间合金。采用钟罩将Si、Mg、Mn、Zr压入纯铝中。Said Si, Mg, Mn and Zr are simple substances or aluminum-based master alloys. Si, Mg, Mn, Zr are pressed into pure aluminum with a bell jar.
为达到上述目的,本发明实现目的所采用的另一技术方案如下:In order to achieve the above object, another technical solution adopted by the present invention to realize the object is as follows:
一种选区激光熔化技术用Al-Si-Mg系铝合金成型件的制备方法,包括如下步骤:A method for preparing an Al-Si-Mg series aluminum alloy molding for selective laser melting technology, comprising the following steps:
S1:母合金熔炼:将坩埚预热至520±5℃后,将纯铝放置于坩埚中,继续升温至1100±5℃,待纯铝熔化后将Al-Zr中间合金压入纯铝中,并进行搅拌30分钟,待搅拌均匀后,将熔体温度降至750±5℃,然后加入Mg和Mn单质,并进行搅拌30分钟,获得成分均匀合金熔体;S1: Master alloy smelting: preheat the crucible to 520±5°C, place pure aluminum in the crucible, continue to heat up to 1100±5°C, press the Al-Zr master alloy into the pure aluminum after the pure aluminum is melted, And stir for 30 minutes, after stirring evenly, reduce the melt temperature to 750±5°C, then add Mg and Mn simple substances, and stir for 30 minutes to obtain an alloy melt with uniform composition;
S2:粉末制备:合金熔体熔化均匀后,打开坩埚底部阀门,合金熔体经内径为5mm的氧化铝导管流出,自由下落,液流经高压氮气雾化器冲击破碎成细小液滴,凝固后形成金属粉末;S2: Powder preparation: After the alloy melt is evenly melted, open the valve at the bottom of the crucible, the alloy melt flows out through an alumina conduit with an inner diameter of 5mm, and falls freely. form metal powder;
S3:铝合金成型件的制备:S3: Preparation of aluminum alloy forming parts:
1)利用CAD建立所需成型零部件的三维模型,并将其转换成可分切的数据格式;1) Use CAD to establish a three-dimensional model of the required molding parts and convert it into a data format that can be cut;
2)将三维模型连同支撑体分切成厚度为0.04mm的多层后导入SLM设备;2) Cut the 3D model together with the support body into multiple layers with a thickness of 0.04mm and then import it into the SLM equipment;
3)在一个可拆装的基板上铺一层0.04mm如步骤S2中所述金属粉末;3) Spread a layer of 0.04mm metal powder on a detachable substrate as described in step S2;
4)激光扫描步骤3)金属粉末层横截面的几何形状4次,扫描过程中激光光斑为:0.1mm,激光功率为:200-400W,激光扫描速率为:400-2000mm/s;4) Laser scanning step 3) The geometric shape of the cross-section of the metal powder layer is 4 times. During the scanning process, the laser spot is 0.1mm, the laser power is 200-400W, and the laser scanning rate is 400-2000mm/s;
5)基板下降一个层0.04mm的厚度,在基面上铺一层新的金属粉末;激光扫描新铺金属粉末层横截面的几何形状1-2次,扫描过程中激光光斑为:0.1mm,激光功率为:200-300W,激光扫描速率为:800-1300mm/s,扫描方向与上一层扫描方向顺时针转动60度;5) The substrate is dropped to a thickness of 0.04mm, and a new layer of metal powder is spread on the base surface; the geometric shape of the cross-section of the newly laid metal powder layer is scanned by laser 1-2 times, and the laser spot is 0.1mm during the scanning process. The laser power is: 200-300W, the laser scanning rate is: 800-1300mm/s, and the scanning direction is rotated 60 degrees clockwise with the scanning direction of the previous layer;
6)重复步骤5)多次,直至整个程序运行结束,得到所述铝合金成型件,重复次数由成型件尺寸决定;6) repeating step 5) multiple times until the end of the entire program operation to obtain the aluminum alloy molding, the number of repetitions is determined by the size of the molding;
S4:热处理:S4: heat treatment:
将步骤S3中得到的铝合金成型件置于150℃条件下热处理6-24h,即可得到选区熔化技术专用Al-Si-Mg系铝合金成型件。The aluminum alloy formed part obtained in step S3 is heat-treated at 150° C. for 6-24 hours to obtain an Al-Si-Mg series aluminum alloy formed part for selective melting technology.
进一步优选的,步骤S2中所述的金属粉末的直径大小为15-60微米。Further preferably, the metal powder in step S2 has a diameter of 15-60 microns.
进一步优选的,步骤S2中所述雾化的压力为10MPa。Further preferably, the atomization pressure in step S2 is 10 MPa.
本发明的优点和有益效果是:Advantage and beneficial effect of the present invention are:
(1)依托选区激光制造技术,通过增加Al-Si-Mg系铝合金中Mg元素和Zr元素的含量,提升铝合金中第二相强化Mg2Si和Al3Zr粒子的浓度,实现Al-Si-Mg系铝合金力学性能的有效提升;(1) Relying on the selective laser manufacturing technology, by increasing the content of Mg element and Zr element in the Al-Si-Mg series aluminum alloy, the concentration of the second phase strengthening Mg 2 Si and Al 3 Zr particles in the aluminum alloy is increased to realize the Al- Effective improvement of mechanical properties of Si-Mg aluminum alloy;
(2)通过加入Mn和Zr元素,可同时增加选区激光熔化Al-Si-Mg系铝合金的成形性,使得铝合金的致密度超过99.9%,并且可有效避免Al-Si-Mg系铝合金中裂纹的产生。(2) By adding Mn and Zr elements, the formability of Al-Si-Mg aluminum alloys in selective laser melting can be increased at the same time, so that the density of the aluminum alloys exceeds 99.9%, and the Al-Si-Mg aluminum alloys can be effectively avoided. generation of cracks.
具体实施方式Detailed ways
为了使本发明的目的、技术方案及优点更加清楚明白,以下以Al90.5Si7Mg0.8Mn1.2Zr0.5、Al86Si10Mg1.5Mn1.5Zr1、Al78.5Si15Mg3Mn2Zr1.5三个合金成分为例,进行进一步的详细说明。应当理解,此处所描述的具体实施例仅仅用于解释本发明,并不用于限定本发明。In order to make the purpose, technical scheme and advantages of the present invention more clear, the following three terms will be Al 90.5 Si 7 Mg 0.8 Mn 1.2 Zr 0.5 , Al 86 Si 10 Mg 1.5 Mn 1.5 Zr 1 , Al 78.5 Si 15 Mg 3 Mn 2 Zr 1.5 An alloy composition is taken as an example for further detailed description. It should be understood that the specific embodiments described here are only used to explain the present invention, not to limit the present invention.
实施例1:Example 1:
一、铝合金组合物的成分及含量:1. Composition and content of aluminum alloy composition:
Al90.5Si7Mg0.8Mn1.2Zr0.5 Al 90.5 Si 7 Mg 0.8 Mn 1.2 Zr 0.5
二、铝合金成型件的制备步骤:2. Preparation steps of aluminum alloy forming parts:
(1)母合金熔炼:(1) Master alloy smelting:
将坩埚预热至520±5℃后,将纯铝放置于坩埚中,继续升温至1100±5℃,待纯铝熔化后将Al-Zr中间合金压入纯铝中,并进行搅拌30分钟,待搅拌均匀后,将熔体温度降至750±5℃,然后加入Mg和Mn单质,并进行搅拌30分钟,获得成分均匀合金熔体;After preheating the crucible to 520±5°C, place the pure aluminum in the crucible, continue to heat up to 1100±5°C, press the Al-Zr master alloy into the pure aluminum after the pure aluminum is melted, and stir for 30 minutes, After stirring evenly, reduce the melt temperature to 750±5°C, then add Mg and Mn simple substances, and stir for 30 minutes to obtain a uniform alloy melt;
(2)粉末制备:(2) Powder preparation:
合金熔体熔化均匀后,打开坩埚底部阀门,合金熔体经内径为5mm的氧化铝导管流出,自由下落,液流经高压氮气雾化器冲击破碎成细小液滴,凝固后形成金属粉末;雾化压力为10MPa,最终筛选15-60微米的粉末备用;After the alloy melt is evenly melted, open the valve at the bottom of the crucible, and the alloy melt flows out through an alumina conduit with an inner diameter of 5 mm, and falls freely. The melting pressure is 10MPa, and the powder of 15-60 microns is finally screened for standby;
(3)铝合金成型件的制备:(3) Preparation of aluminum alloy forming parts:
1)利用CAD建立所需成型零部件的三维模型,并将其转换成可分切的数据格式;1) Use CAD to establish a three-dimensional model of the required molding parts and convert it into a data format that can be cut;
2)将三维模型连同支撑体分切成厚度为0.04mm的多层后导入SLM设备;2) Cut the 3D model together with the support body into multiple layers with a thickness of 0.04mm and then import it into the SLM equipment;
3)在一个可拆装的基板上铺一层0.04mm如步骤(2)中所述金属粉末;3) Lay a layer of 0.04mm metal powder as described in step (2) on a detachable substrate;
4)激光扫描步骤3)金属粉末层横截面的几何形状4次,扫描过程中激光光斑为:0.1mm,激光功率为:200W,激光扫描速率为:1100mm/s;4) Laser scanning step 3) The geometric shape of the cross section of the metal powder layer is 4 times. During the scanning process, the laser spot is 0.1mm, the laser power is 200W, and the laser scanning rate is 1100mm/s;
5)基板下降一个层0.04mm的厚度,在基面上铺一层新的金属粉末;激光扫描新铺金属粉末层横截面的几何形状1次,扫描过程中激光光斑为:0.1mm,激光功率为:200W,激光扫描速率为:1100mm/s,扫描方向与上一层扫描方向顺时针转动60度;5) The substrate is lowered by a layer with a thickness of 0.04mm, and a new layer of metal powder is spread on the base surface; the geometric shape of the cross-section of the newly laid metal powder layer is scanned by laser once, and the laser spot is 0.1mm during the scanning process. It is: 200W, the laser scanning rate is: 1100mm/s, and the scanning direction is rotated 60 degrees clockwise with the scanning direction of the previous layer;
6)重复步骤5)多次,直至整个程序运行结束,得到所述铝合金成型件,重复次数由成型件尺寸决定;6) repeating step 5) multiple times until the end of the entire program operation to obtain the aluminum alloy molding, the number of repetitions is determined by the size of the molding;
(4)热处理:(4) Heat treatment:
将步骤(3)中得到的铝合金成型件置于150℃条件下热处理6h,即可得到选区熔化技术专用Al-Si-Mg系铝合金。The aluminum alloy formed part obtained in step (3) is heat-treated at 150° C. for 6 hours to obtain an Al-Si-Mg aluminum alloy for selective melting technology.
三、本实施例的力学性能测试和有益效果Three, the mechanical performance test and beneficial effect of the present embodiment
1、力学性能测试:1. Mechanical performance test:
利用X射线衍射仪(XRD)和透射电子显微镜(TEM)对制得铝合金样品进行结构检测;利用金相显微镜(OM)扫描电子显微镜(SEM)观察铝合金样品的微观组织;应用万能力学试验机测试铝合金样品的强度。Use X-ray diffractometer (XRD) and transmission electron microscope (TEM) to detect the structure of aluminum alloy samples; use metallographic microscope (OM) scanning electron microscope (SEM) to observe the microstructure of aluminum alloy samples; apply universal mechanical test Machine testing the strength of aluminum alloy samples.
2、有益效果:2. Beneficial effects:
通过此实施例获得成型件的致密度为99.95%,其力学性能指标如下:最大抗拉强度σb为380MPa,屈服强度σ0.2为300MPa,塑性变形率为22%。该实施例的塑性变形率大于现有铸造和选区激光熔化Al-Si-Mg系铝合金的塑性变形率。The compactness of the formed part obtained through this embodiment is 99.95%, and its mechanical performance index is as follows: the maximum tensile strength σ b is 380 MPa, the yield strength σ 0.2 is 300 MPa, and the plastic deformation rate is 22%. The plastic deformation rate of this embodiment is greater than that of the existing casting and selective laser melting Al-Si-Mg aluminum alloys.
实施例2:Example 2:
一、铝合金组合物的成分及含量:1. Composition and content of aluminum alloy composition:
Al86Si10Mg1.5Mn1.5Zr1 Al 86 Si 10 Mg 1.5 Mn 1.5 Zr 1
二、铝合金成型件的制备步骤:2. Preparation steps of aluminum alloy forming parts:
(1)母合金熔炼(1) Master alloy smelting
同实施例1。With embodiment 1.
(2)粉末制备(2) Powder preparation
同实施例1。With embodiment 1.
(3)铝合金成型件的制备:(3) Preparation of aluminum alloy forming parts:
选择性激光熔化(SLM)制备铝合金的步骤如下:The steps of selective laser melting (SLM) to prepare aluminum alloy are as follows:
1)利用CAD建立所需成型零部件的三维模型,并将其转换成可分切的数据格式;1) Use CAD to establish a three-dimensional model of the required molding parts and convert it into a data format that can be cut;
2)将三维模型连同支撑体分切成厚度为0.04mm的多层后导入SLM设备;2) Cut the 3D model together with the support body into multiple layers with a thickness of 0.04mm and then import it into the SLM equipment;
3)在一个可拆装的基板上铺一层0.04mm如步骤(2)中所述金属粉末;3) Lay a layer of 0.04mm metal powder as described in step (2) on a detachable substrate;
4)激光扫描步骤3)金属粉末层横截面的几何形状4次,扫描过程中激光光斑为:0.1mm,激光功率为:250W,激光扫描速率为:900mm/s;4) Laser scanning step 3) The geometric shape of the cross-section of the metal powder layer is 4 times. During the scanning process, the laser spot is 0.1mm, the laser power is 250W, and the laser scanning rate is 900mm/s;
5)基板下降一个层0.04mm的厚度,在基面上铺一层新的金属粉末;激光扫描新铺金属粉末层横截面的几何形状1次,扫描过程中激光光斑为:0.1mm,激光功率为:250W,激光扫描速率为:900mm/s,扫描方向与上一层扫描方向顺时针转动60度;5) The substrate is lowered by a layer with a thickness of 0.04mm, and a new layer of metal powder is spread on the base surface; the geometric shape of the cross-section of the newly laid metal powder layer is scanned by laser once, and the laser spot is 0.1mm during the scanning process. It is: 250W, the laser scanning rate is: 900mm/s, and the scanning direction is rotated 60 degrees clockwise with the scanning direction of the previous layer;
6)重复步骤5)多次,直至整个程序运行结束,得到所述铝合金成型件,重复次数由成型件尺寸决定;6) repeating step 5) multiple times until the end of the entire program operation to obtain the aluminum alloy molding, the number of repetitions is determined by the size of the molding;
(4)热处理:(4) Heat treatment:
将上述合金置于150℃条件下进行时效处理,时间为12h。The above alloy was aged at 150° C. for 12 hours.
三、本实施例的力学性能测试和有益效果Three, the mechanical performance test and beneficial effect of the present embodiment
1、力学性能测试:1. Mechanical performance test:
利用X射线衍射仪(XRD)和透射电子显微镜(TEM)对制得铝合金样品进行结构检测;利用金相显微镜(OM)扫描电子显微镜(SEM)观察铝合金样品的微观组织;应用万能力学试验机测试铝合金样品的强度。Use X-ray diffractometer (XRD) and transmission electron microscope (TEM) to detect the structure of aluminum alloy samples; use metallographic microscope (OM) scanning electron microscope (SEM) to observe the microstructure of aluminum alloy samples; apply universal mechanical test Machine testing the strength of aluminum alloy samples.
2、有益效果:2. Beneficial effects:
通过此实施例获得成型件的致密度为99.92%,其力学性能指标如下:最大抗拉强度σb为480MPa,屈服强度σ0.2为340MPa,塑性变形率为15%。该实施例的屈服强度大于现有铸造和选区激光熔化Al-Si-Mg系铝合金的屈服强度。The compactness of the formed part obtained through this embodiment is 99.92%, and its mechanical performance index is as follows: the maximum tensile strength σ b is 480 MPa, the yield strength σ 0.2 is 340 MPa, and the plastic deformation rate is 15%. The yield strength of this embodiment is greater than that of the existing casting and selective laser melting Al-Si-Mg aluminum alloys.
实施例3:Example 3:
一、铝合金组合物的成分及含量:1. Composition and content of aluminum alloy composition:
Al78.5Si15Mg3Mn2Zr1.5 Al 78.5 Si 15 Mg 3 Mn 2 Zr 1.5
二、铝合金成型件的制备步骤:2. Preparation steps of aluminum alloy forming parts:
(1)母合金熔炼(1) Master alloy smelting
同实施例1。With embodiment 1.
(2)粉末制备(2) Powder preparation
同实施例1。With embodiment 1.
(3)铝合金成型件的制备:(3) Preparation of aluminum alloy forming parts:
选择性激光熔化(SLM)制备铝合金的步骤如下:The steps of selective laser melting (SLM) to prepare aluminum alloy are as follows:
1)利用CAD建立所需成型零部件的三维模型,并将其转换成可分切的数据格式;1) Use CAD to establish a three-dimensional model of the required molding parts and convert it into a data format that can be cut;
2)将三维模型连同支撑体分切成厚度为0.04mm的多层后导入SLM设备;2) Cut the 3D model together with the support body into multiple layers with a thickness of 0.04mm and then import it into the SLM equipment;
3)在一个可拆装的基板上铺一层0.04mm如步骤(2)中所述金属粉末;3) Lay a layer of 0.04mm metal powder as described in step (2) on a detachable substrate;
4)激光扫描步骤3)金属粉末层横截面的几何形状4次,扫描过程中激光光斑为:0.1mm,激光功率为:300W,激光扫描速率为:1000mm/s;4) Laser scanning step 3) The geometric shape of the cross-section of the metal powder layer is 4 times. During the scanning process, the laser spot is 0.1mm, the laser power is 300W, and the laser scanning rate is 1000mm/s;
5)基板下降一个层0.04mm的厚度,在基面上铺一层新的金属粉末;激光扫描新铺金属粉末层横截面的几何形状2次,扫描过程中激光光斑为:0.1mm,激光功率为:300W,激光扫描速率为:1000mm/s,扫描方向与上一层扫描方向顺时针转动60度;5) The substrate is lowered by a layer with a thickness of 0.04mm, and a new layer of metal powder is spread on the base surface; the geometric shape of the cross-section of the newly laid metal powder layer is scanned twice by laser, and the laser spot is 0.1mm during the scanning process. It is: 300W, the laser scanning rate is: 1000mm/s, and the scanning direction is rotated 60 degrees clockwise with the scanning direction of the previous layer;
6)重复步骤5)多次,直至整个程序运行结束,得到所述铝合金成型件,重复次数由成型件尺寸决定;6) repeating step 5) multiple times until the end of the entire program operation to obtain the aluminum alloy molding, the number of repetitions is determined by the size of the molding;
(4)热处理:(4) Heat treatment:
将上述合金置于150℃条件下进行时效处理,时间为24h。The above alloy was aged at 150° C. for 24 hours.
三、本实施例的力学性能测试和有益效果Three, the mechanical performance test and beneficial effect of the present embodiment
1、力学性能测试:1. Mechanical performance test:
利用X射线衍射仪(XRD)和透射电子显微镜(TEM)对制得铝合金样品进行结构检测;利用金相显微镜(OM)扫描电子显微镜(SEM)观察铝合金样品的微观组织;应用万能力学试验机测试铝合金样品的强度。Use X-ray diffractometer (XRD) and transmission electron microscope (TEM) to detect the structure of aluminum alloy samples; use metallographic microscope (OM) scanning electron microscope (SEM) to observe the microstructure of aluminum alloy samples; apply universal mechanical test Machine testing the strength of aluminum alloy samples.
2、有益效果:2. Beneficial effects:
通过此实施例获得成型件的致密度为99.96%,其力学性能指标如下:最大抗拉强度σb为520MPa,屈服强度σ0.2为380MPa,塑性变形率为8%。该实施例的屈服强度和抗拉强度均大于现有铸造和选区激光熔化Al-Si-Mg系铝合金的屈服强度。The density of the molded part obtained through this embodiment is 99.96%, and its mechanical performance index is as follows: the maximum tensile strength σ b is 520MPa, the yield strength σ0.2 is 380MPa, and the plastic deformation rate is 8%. Both the yield strength and the tensile strength of this embodiment are greater than the yield strength of the existing cast and selective laser melting Al-Si-Mg aluminum alloys.
以上所述,仅为本发明较佳的具体实施方式。当然,本发明还可有其它多种实施例,在不背离本发明精神及其实质的情况下,任何熟悉本技术领域的技术人员,当可根据本发明作出各种相应的等效改变和变形,都应属于本发明所附的权利要求的保护范围。The above are only preferred specific implementation modes of the present invention. Certainly, the present invention also can have other multiple embodiments, without departing from the spirit and essence of the present invention, any person familiar with the technical field can make various corresponding equivalent changes and deformations according to the present invention , should belong to the scope of protection of the appended claims of the present invention.
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