CN111745162A - Shape memory alloy reinforced magnesium matrix composite material with three-dimensional interpenetrating network structure and preparation method thereof - Google Patents
Shape memory alloy reinforced magnesium matrix composite material with three-dimensional interpenetrating network structure and preparation method thereof Download PDFInfo
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- 239000011777 magnesium Substances 0.000 title claims abstract description 62
- 229910052749 magnesium Inorganic materials 0.000 title claims abstract description 61
- 229910001285 shape-memory alloy Inorganic materials 0.000 title claims abstract description 52
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- 229910000861 Mg alloy Inorganic materials 0.000 claims abstract description 36
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- 238000005516 engineering process Methods 0.000 claims abstract description 11
- 238000010146 3D printing Methods 0.000 claims abstract description 10
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- HZEWFHLRYVTOIW-UHFFFAOYSA-N [Ti].[Ni] Chemical compound [Ti].[Ni] HZEWFHLRYVTOIW-UHFFFAOYSA-N 0.000 claims description 24
- 238000001764 infiltration Methods 0.000 claims description 11
- 230000008595 infiltration Effects 0.000 claims description 11
- 239000000843 powder Substances 0.000 claims description 11
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 claims description 10
- 229910052751 metal Inorganic materials 0.000 claims description 9
- 239000002184 metal Substances 0.000 claims description 9
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 claims description 8
- 238000013461 design Methods 0.000 claims description 8
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- 239000002245 particle Substances 0.000 claims description 7
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 5
- 238000010438 heat treatment Methods 0.000 claims description 5
- 229910052759 nickel Inorganic materials 0.000 claims description 5
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 claims description 4
- 229910000881 Cu alloy Inorganic materials 0.000 claims description 4
- CPLXHLVBOLITMK-UHFFFAOYSA-N Magnesium oxide Chemical compound [Mg]=O CPLXHLVBOLITMK-UHFFFAOYSA-N 0.000 claims description 4
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- 229910052786 argon Inorganic materials 0.000 claims description 4
- 229910002804 graphite Inorganic materials 0.000 claims description 4
- 239000010439 graphite Substances 0.000 claims description 4
- 238000011084 recovery Methods 0.000 claims description 4
- 229910000831 Steel Inorganic materials 0.000 claims description 3
- 229910045601 alloy Inorganic materials 0.000 claims description 3
- 239000000956 alloy Substances 0.000 claims description 3
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- 239000010959 steel Substances 0.000 claims description 3
- 229910001297 Zn alloy Inorganic materials 0.000 claims description 2
- WCERXPKXJMFQNQ-UHFFFAOYSA-N [Ti].[Ni].[Cu] Chemical compound [Ti].[Ni].[Cu] WCERXPKXJMFQNQ-UHFFFAOYSA-N 0.000 claims description 2
- IUYOGGFTLHZHEG-UHFFFAOYSA-N copper titanium Chemical compound [Ti].[Cu] IUYOGGFTLHZHEG-UHFFFAOYSA-N 0.000 claims description 2
- TVZPLCNGKSPOJA-UHFFFAOYSA-N copper zinc Chemical compound [Cu].[Zn] TVZPLCNGKSPOJA-UHFFFAOYSA-N 0.000 claims description 2
- -1 copper-aluminum-nickel Chemical compound 0.000 claims description 2
- 229910052593 corundum Inorganic materials 0.000 claims description 2
- 239000010431 corundum Substances 0.000 claims description 2
- 239000001307 helium Substances 0.000 claims description 2
- 229910052734 helium Inorganic materials 0.000 claims description 2
- SWQJXJOGLNCZEY-UHFFFAOYSA-N helium atom Chemical compound [He] SWQJXJOGLNCZEY-UHFFFAOYSA-N 0.000 claims description 2
- 230000008676 import Effects 0.000 claims description 2
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- 229910000838 Al alloy Inorganic materials 0.000 description 1
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- 229910052769 Ytterbium Inorganic materials 0.000 description 1
- 238000010521 absorption reaction Methods 0.000 description 1
- JNDMLEXHDPKVFC-UHFFFAOYSA-N aluminum;oxygen(2-);yttrium(3+) Chemical compound [O-2].[O-2].[O-2].[Al+3].[Y+3] JNDMLEXHDPKVFC-UHFFFAOYSA-N 0.000 description 1
- 239000012300 argon atmosphere Substances 0.000 description 1
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Abstract
本发明涉及一种具有三维互穿网络结构并以3D打印的形状记忆合金增强体骨架增强的镁基复合材料及其制备方法。该复合材料由体积分数为10%~80%的形状记忆合金增强体与镁或镁合金基体组成,具有三维互穿网络结构,表现为增强体与基体分别具有独立的拓扑结构并在三维空间穿插互补结合。该复合材料的制备方法为:采用3D打印技术制备具有网络拓扑结构的形状记忆合金增强体骨架,在真空或保护气氛下利用熔融的镁或镁合金熔体浸渗该骨架,凝固冷却后得到复合材料。本发明的复合材料强度高、塑性大,结构和力学性能的可控性强,并且具有一定的形状记忆效应,即室温变形在马氏体相变温度以上能够部分或完全回复,作为新型结构功能一体化材料具有可观的应用前景。The invention relates to a magnesium-based composite material having a three-dimensional interpenetrating network structure and reinforced by a 3D-printed shape memory alloy reinforcement skeleton and a preparation method thereof. The composite material is composed of a shape memory alloy reinforcement with a volume fraction of 10% to 80% and a magnesium or magnesium alloy matrix, and has a three-dimensional interpenetrating network structure. The reinforcement and the matrix have independent topological structures and are interspersed in three-dimensional space. Complementary binding. The preparation method of the composite material is as follows: using 3D printing technology to prepare a shape memory alloy reinforced body skeleton with a network topology, infiltrating the skeleton with molten magnesium or magnesium alloy melt under vacuum or protective atmosphere, and obtaining a composite after solidification and cooling Material. The composite material of the invention has high strength, high plasticity, strong controllability of structure and mechanical properties, and has a certain shape memory effect, that is, the room temperature deformation can be partially or completely recovered above the martensitic transformation temperature, which serves as a novel structural function. Integrated materials have considerable application prospects.
Description
技术领域technical field
本发明涉及金属基复合材料领域,具体为一种具有三维互穿网络结构并以3D打印的形状记忆合金增强体骨架增强的镁基复合材料及其制备方法。The invention relates to the field of metal matrix composite materials, in particular to a magnesium matrix composite material having a three-dimensional interpenetrating network structure and reinforced by a 3D-printed shape memory alloy reinforcement skeleton and a preparation method thereof.
背景技术Background technique
在保证安全服役的前提下,实现结构材料的轻量化能够有效减轻结构件的重量,从而有利于节约能源并减少环境污染,因此具有重要的科学意义和实用价值。例如,在交通运输领域,汽车轻量化设计能够提高燃油效率,减少燃料消耗和尾气排放,因而已成为当今汽车发展的主要趋势之一。结构材料轻量化的实现主要依赖于其比强度和比刚度等力学性能的提高。镁与镁合金因具有较低的密度(纯镁的密度为1.74g/cm3)而表现出突出的比强度和比刚度,同时具有良好的阻尼减震、导热和电磁屏蔽等功能特性,因此被广泛应用于交通运输、生物医用、电子产品等诸多领域。Under the premise of ensuring safe service, realizing the lightweight of structural materials can effectively reduce the weight of structural parts, which is conducive to saving energy and reducing environmental pollution, so it has important scientific significance and practical value. For example, in the field of transportation, the lightweight design of automobiles can improve fuel efficiency, reduce fuel consumption and exhaust emissions, so it has become one of the main trends in today's automobile development. The realization of lightweight structural materials mainly depends on the improvement of mechanical properties such as specific strength and specific stiffness. Magnesium and magnesium alloys show outstanding specific strength and specific stiffness due to their low density (the density of pure magnesium is 1.74g/cm 3 ), and have good functional properties such as damping and shock absorption, thermal conductivity and electromagnetic shielding. Therefore, It is widely used in transportation, biomedical, electronic products and many other fields.
然而,与钢铁、钛合金、铝合金等金属结构材料相比,镁与镁合金的绝对强度和刚度仍然偏低,并且耐磨性和耐热性较差,同时表现出较低的高温强度和抗高温蠕变能力,这在很大程度上限制其作为轻型结构材料的应用。通过在镁或镁合金基体中引入增强相制备镁基复合材料是解决上述问题的有效途径之一。常用的复合化方法是在镁或镁合金基体中引入随机均匀分布的增强相颗粒或纤维。然而,传统镁基复合材料的组织结构难于进行精确设计与控制,因而材料的力学性能无法进行有效调控,并且增强相与基体的结合仅仅通过相界面实现,容易产生相界面的应力集中和开裂等问题。此外,目前镁与镁合金复合材料发生塑性变形后无法回复初始形状,变形产生的损伤难以自动修复,这导致材料性能发生不可逆的下降。However, compared with steel, titanium alloy, aluminum alloy and other metal structural materials, the absolute strength and stiffness of magnesium and magnesium alloys are still low, and the wear resistance and heat resistance are poor, while showing lower high temperature strength and High temperature creep resistance, which largely limits its application as a lightweight structural material. One of the effective ways to solve the above problems is to prepare magnesium matrix composites by introducing reinforcing phase into magnesium or magnesium alloy matrix. The commonly used composite method is to introduce randomly and uniformly distributed reinforcing phase particles or fibers into the magnesium or magnesium alloy matrix. However, it is difficult to precisely design and control the structure of traditional magnesium matrix composites, so the mechanical properties of the material cannot be effectively controlled, and the combination of the enhanced phase and the matrix is only achieved through the phase interface, which is prone to stress concentration and cracking at the phase interface. question. In addition, the current magnesium and magnesium alloy composites cannot restore their original shape after plastic deformation, and the damage caused by the deformation is difficult to repair automatically, which leads to an irreversible decline in material properties.
发明内容SUMMARY OF THE INVENTION
本发明的目的在于提供一种具有三维互穿网络结构的形状记忆合金增强镁基复合材料及其制备方法,利用具有网络拓扑结构的形状记忆合金骨架增强镁与镁合金,并采用3D打印技术实现对镁基复合材料中增强体结构的精确设计和控制,从而在不明显提高材料密度的前提下,显著提高镁与镁合金的强度、刚度和耐磨性,并赋予材料一定的形状记忆功能,使其室温塑性变形在加热到形状记忆合金的马氏体相变温度以上时能够自动回复。The purpose of the present invention is to provide a shape memory alloy reinforced magnesium matrix composite material with a three-dimensional interpenetrating network structure and a preparation method thereof. The shape memory alloy skeleton with a network topology is used to strengthen magnesium and magnesium alloys, and the 3D printing technology is used to realize the The precise design and control of the reinforcement structure in the magnesium matrix composite material can significantly improve the strength, stiffness and wear resistance of magnesium and magnesium alloys without significantly increasing the material density, and endow the material with a certain shape memory function, The plastic deformation at room temperature can be automatically recovered when heated to above the martensitic transformation temperature of the shape memory alloy.
为了实现上述目的,本发明采取以下技术方案:In order to achieve the above object, the present invention adopts the following technical solutions:
一种具有三维互穿网络结构的形状记忆合金增强镁基复合材料,所述的复合材料由形状记忆合金增强体与镁或镁合金基体组成,以体积百分数计,形状记忆合金增强体含量为10%~80%,其余为镁或镁合金基体,该形状记忆合金为钛镍合金、钛铜合金、钛镍铜合金、铜铝镍合金、铜锌合金中的一种,并且不与熔融的镁或镁合金发生反应;所述的复合材料具有三维互穿网络结构,表现为增强体与基体分别具有独立的拓扑结构并在三维空间穿插互补结合。A shape memory alloy reinforced magnesium matrix composite material with a three-dimensional interpenetrating network structure, the composite material is composed of a shape memory alloy reinforcement and a magnesium or magnesium alloy matrix, and the content of the shape memory alloy reinforcement is 10% by volume. %~80%, the rest is magnesium or magnesium alloy matrix, the shape memory alloy is one of titanium-nickel alloy, titanium-copper alloy, titanium-nickel-copper alloy, copper-aluminum-nickel alloy, copper-zinc alloy, and does not mix with molten magnesium. Or magnesium alloy reacts; the composite material has a three-dimensional interpenetrating network structure, which is manifested in that the reinforcement and the matrix have independent topological structures and are interspersed and complementary in three-dimensional space.
所述的复合材料的压缩强度为250~800MPa,压缩应变量大于10%,密度范围为2.2~4.2g/cm3。The compressive strength of the composite material is 250-800 MPa, the compressive strain is greater than 10%, and the density is in the range of 2.2-4.2 g/cm 3 .
所述的复合材料具有一定的形状记忆效应,即复合材料在室温发生塑性变形后,在加热到形状记忆合金的马氏体相变温度以上时,其变形能够自动回复,当总室温应变量不超过20%时,回复应变量占总应变量的比例大于1%。The composite material has a certain shape memory effect, that is, after the composite material undergoes plastic deformation at room temperature, its deformation can be automatically recovered when heated to above the martensitic transformation temperature of the shape memory alloy. When it exceeds 20%, the proportion of the response variable to the total response variable is greater than 1%.
所述的具有三维互穿网络结构的形状记忆合金增强镁基复合材料的制备方法,包括以下步骤:The preparation method of the shape memory alloy reinforced magnesium matrix composite material with a three-dimensional interpenetrating network structure comprises the following steps:
1)设计具有网络拓扑结构的形状记忆合金增强体骨架,建立骨架的三维模型,将模型导入到利用激光选区熔化技术成型的金属3D打印机中,通过3D打印将形状记忆合金粉体制备成具有设计结构的形状记忆合金增强体骨架;1) Design a shape memory alloy reinforced body skeleton with a network topology, establish a three-dimensional model of the skeleton, import the model into a metal 3D printer formed by laser selective melting technology, and prepare the shape memory alloy powder through 3D printing. Structural shape memory alloy reinforcement skeleton;
2)将步骤1)打印的形状记忆合金增强体骨架与镁或镁合金一同放入坩埚,将坩埚置于熔炼设备中,在真空或保护气氛下加热使镁或镁合金熔化并浸渗入形状记忆合金增强体骨架中;2) Put the shape memory alloy reinforcement skeleton printed in step 1) into a crucible together with magnesium or magnesium alloy, place the crucible in a smelting equipment, and heat the magnesium or magnesium alloy under vacuum or a protective atmosphere to melt and infiltrate the shape memory In the alloy reinforcement framework;
3)停止加热,待镁或镁合金凝固并冷却后将坩埚从熔炼设备中取出,得到具有三维互穿网络结构的形状记忆合金增强镁基复合材料。3) Stop heating, and after the magnesium or magnesium alloy is solidified and cooled, the crucible is taken out from the smelting equipment to obtain a shape memory alloy reinforced magnesium matrix composite material with a three-dimensional interpenetrating network structure.
步骤1)中,所述的形状记忆合金粉体的粒径为1~200μm,形状记忆合金增强体骨架具有三维网络拓扑结构,骨架的孔隙率为20%~90%,平均孔径为0.01~3mm,连接筋直径为0.005~2.5mm。In step 1), the particle size of the shape memory alloy powder is 1-200 μm, the shape memory alloy reinforcement skeleton has a three-dimensional network topology, the porosity of the skeleton is 20%-90%, and the average pore diameter is 0.01-3mm , the diameter of the connecting rib is 0.005 to 2.5 mm.
步骤2)中,所述的坩埚为石墨坩埚、氧化镁坩埚、刚玉坩埚、45钢坩埚、镍坩埚中的一种,所述的保护气氛为氩气、氮气、氦气中的一种,加热温度超过镁或镁合金的熔点,为650℃~1000℃,保温时间1~100min;金属熔体浸渗形状记忆合金骨架采用无压浸渗或真空浸渗,若采用真空浸渗,真空度为-0.005~-0.5MPa。In step 2), the crucible is a kind of graphite crucible, magnesia crucible, corundum crucible, 45 steel crucible, nickel crucible, and the protective atmosphere is a kind of argon, nitrogen, helium, heating The temperature exceeds the melting point of magnesium or magnesium alloy, which is 650 ℃ ~ 1000 ℃, and the holding time is 1 ~ 100min; metal melt infiltration of shape memory alloy skeleton adopts pressureless infiltration or vacuum infiltration, if vacuum infiltration is used, the vacuum degree is -0.005~-0.5MPa.
本发明的设计思想是:The design idea of the present invention is:
1)形状记忆合金的熔点远高于镁或镁合金,并且不与熔融的镁或镁合金发生反应,因而可以利用镁或镁合金熔体浸渗形状记忆合金骨架的方法制备复合材料,得到的复合材料中增强体与基体之间呈现冶金结合,界面强度高,因而表现出理想的强化与刚化效果;1) The melting point of the shape memory alloy is much higher than that of magnesium or magnesium alloy, and it does not react with molten magnesium or magnesium alloy, so the composite material can be prepared by the method of infiltrating the shape memory alloy skeleton with magnesium or magnesium alloy melt, and the obtained The metallurgical bond between the reinforcement and the matrix in the composite material is high, and the interface strength is high, so it shows the ideal strengthening and stiffening effect;
2)形状记忆合金的马氏体相变温度与镁或镁合金的蠕变温度相匹配,能够赋予材料一定的形状记忆功能,材料在室温发生塑性变形后,当加热到形状记忆合金的马氏体相变温度以上时,增强体骨架的形状记忆效应能够带动镁或镁合金基体发生蠕变,因而使得材料整体的变形得以自动回复;2) The martensitic transformation temperature of the shape memory alloy matches the creep temperature of magnesium or magnesium alloy, which can give the material a certain shape memory function. After the material undergoes plastic deformation at room temperature, when heated to the martensitic temperature of the shape memory alloy Above the bulk transformation temperature, the shape memory effect of the reinforced body skeleton can drive the magnesium or magnesium alloy matrix to creep, so that the overall deformation of the material can be automatically recovered;
3)复合材料具有三维互穿网络结构,这使得增强体与基体能够不仅仅依靠界面连接,还可以通过相互穿插连通的机械互锁形成一个整体,有利于减轻界面处的应力集中,增强两相之间的应力传导与变形的协调性;3) The composite material has a three-dimensional interpenetrating network structure, which enables the reinforcement and the matrix to not only rely on the interface to connect, but also form a whole through the interpenetrating mechanical interlocking, which is beneficial to reduce the stress concentration at the interface and strengthen the two-phase The coordination between stress conduction and deformation;
4)3D打印技术能够实现形状记忆合金增强体骨架的快速成型,并且可以对骨架的三维网络拓扑结构进行精确设计与控制,从而实现对复合材料的结构与力学性能的有效调控。4) 3D printing technology can realize the rapid prototyping of shape memory alloy reinforced skeleton, and can accurately design and control the three-dimensional network topology of the skeleton, so as to realize the effective control of the structure and mechanical properties of composite materials.
与现有材料和技术相比,本发明具有以下的优点及有益效果:Compared with existing materials and technologies, the present invention has the following advantages and beneficial effects:
1)本发明的复合材料在不明显增加镁或镁合金密度的前提下,显著提高材料的强度、刚度、耐磨性和抗高温蠕变性能,并且具有良好的塑性变形能力;1) The composite material of the present invention significantly improves the strength, stiffness, wear resistance and high temperature creep resistance of the material without significantly increasing the density of magnesium or magnesium alloy, and has good plastic deformation ability;
2)本发明的复合材料的制备方法充分发挥3D打印技术的优势,增强体骨架的三维网络拓扑结构可以在很大范围内实现精确设计与控制,因此复合材料的结构和力学性能可以实现有效调控;2) The preparation method of the composite material of the present invention gives full play to the advantages of the 3D printing technology, and the three-dimensional network topology of the reinforced body skeleton can be precisely designed and controlled in a wide range, so the structure and mechanical properties of the composite material can be effectively controlled. ;
3)本发明的复合材料具有一定的形状记忆效应,即复合材料在室温发生塑性变形后,在加热到形状记忆合金的马氏体相变温度以上时,其变形能够自动回复,当总室温应变量不超过20%时,回复应变量占总应变量的比例大于1%。3) The composite material of the present invention has a certain shape memory effect, that is, after the composite material undergoes plastic deformation at room temperature, when it is heated to above the martensitic transformation temperature of the shape memory alloy, its deformation can be automatically recovered. When the variable does not exceed 20%, the proportion of the response variable to the total response variable is greater than 1%.
4)本发明的复合材料的制备方法工艺简单,周期短,效率高,可设计性与可控性强,适于推广到其他材料体系。4) The preparation method of the composite material of the present invention has the advantages of simple process, short period, high efficiency, strong designability and controllability, and is suitable for being extended to other material systems.
附图说明Description of drawings
图1为实施例1设计的具有网络拓扑结构的钛镍合金骨架的三维模型图。FIG. 1 is a three-dimensional model diagram of a titanium-nickel alloy skeleton with a network topology designed in Example 1. FIG.
图2为实施例1通过3D打印技术制备的钛镍合金骨架的实物图(a)和三维X射线结构图(b)。FIG. 2 is a physical image (a) and a three-dimensional X-ray structural image (b) of the titanium-nickel alloy skeleton prepared by the 3D printing technology in Example 1.
图3为实施例1制备得到的具有三维互穿网络结构的钛镍合金增强镁基复合材料的实物图(a)和三维X射线结构图(b)。3 is a physical image (a) and a three-dimensional X-ray structural image (b) of the titanium-nickel alloy reinforced magnesium matrix composite material with a three-dimensional interpenetrating network structure prepared in Example 1.
图4为实施例1制备的具有三维互穿网络结构的钛镍合金增强镁基复合材料的室温压缩应力-应变曲线及其与纯镁的比较图。4 is a room temperature compressive stress-strain curve of the titanium-nickel alloy reinforced magnesium-based composite material with a three-dimensional interpenetrating network structure prepared in Example 1 and its comparison with pure magnesium.
图5为实施例3设计的具有网络拓扑结构的钛镍合金骨架的三维模型图。FIG. 5 is a three-dimensional model diagram of a titanium-nickel alloy skeleton with a network topology designed in Example 3. FIG.
具体实施方式:Detailed ways:
在具体实施过程中,本发明具有三维互穿网络结构的形状记忆合金增强镁基复合材料及其制备方法如下:In the specific implementation process, the present invention has a shape memory alloy reinforced magnesium matrix composite material with a three-dimensional interpenetrating network structure and a preparation method thereof as follows:
该复合材料由体积分数为10%~80%(优选为20%~70%)的形状记忆合金增强体与镁或镁合金基体组成,具有三维互穿网络结构,表现为增强体与基体分别具有独立的拓扑结构并在三维空间穿插互补结合。该复合材料的制备方法为:采用3D打印技术利用形状记忆合金粉体制备具有网络拓扑结构的形状记忆合金增强体骨架,在真空或保护气氛下利用熔融的镁或镁合金熔体浸渗该骨架,凝固冷却后得到复合材料。其中,形状记忆合金粉体的粒径为1~200μm(优选为5~70μm),形状记忆合金增强体骨架的孔隙率为20%~90%(优选为30%~80%),加热浸渗的温度超过镁或镁合金的熔点,为650℃~1000℃,金属熔体浸渗形状记忆合金骨架采用无压浸渗或真空浸渗,若采用真空浸渗,真空度为-0.005~-0.5MPa(优选为-0.005~-0.1MPa)。The composite material is composed of a shape memory alloy reinforcement with a volume fraction of 10% to 80% (preferably 20% to 70%) and a magnesium or magnesium alloy matrix, and has a three-dimensional interpenetrating network structure. Independent topological structures and interspersed complementary combinations in three-dimensional space. The preparation method of the composite material is as follows: using shape memory alloy powder to prepare a shape memory alloy reinforced body skeleton with network topology by 3D printing technology, and infiltrating the skeleton with molten magnesium or magnesium alloy melt under vacuum or protective atmosphere , and the composite material is obtained after solidification and cooling. The particle size of the shape memory alloy powder is 1 to 200 μm (preferably 5 to 70 μm), the porosity of the shape memory alloy reinforcement skeleton is 20% to 90% (preferably 30% to 80%), and the thermal impregnation The temperature exceeds the melting point of magnesium or magnesium alloy, which is 650 ° C ~ 1000 ° C. Metal melt infiltration of shape memory alloy skeleton adopts pressureless infiltration or vacuum infiltration. If vacuum infiltration is used, the vacuum degree is -0.005 ~ -0.5 MPa (preferably -0.005 to -0.1MPa).
下面结合具体实施例来对本发明做进一步阐述,应理解,以下实施例仅限用于说明本发明,而不用于限制本发明的保护范围。The present invention will be further described below in conjunction with specific embodiments, it should be understood that the following embodiments are only used to illustrate the present invention, but not to limit the protection scope of the present invention.
实施例1:Example 1:
本实施例中,制备具有三维互穿网络结构的钛镍合金增强镁基复合材料。所用的原材料包括钛镍合金粉(平均粒径为15μm,钛与镍原子比例为1:1)、金属镁。具体制备工艺如下:In this example, a titanium-nickel alloy reinforced magnesium-based composite material with a three-dimensional interpenetrating network structure was prepared. The raw materials used include titanium-nickel alloy powder (average particle size is 15 μm, and the atomic ratio of titanium and nickel is 1:1) and metal magnesium. The specific preparation process is as follows:
1)利用三维可视化实体模拟软件Autodesk Inventor Professional(AIP2019)设计具有网络拓扑结构的钛镍合金增强体骨架,建立骨架的三维模型。如图1所示,该模型的网络拓扑结构基于三重周期最小面原则建立;将模型导入到利用激光选区熔化技术成型的Realizer SLM 100型金属3D打印机中,在氩气保护下,通过3D打印将钛镍合金粉体制备成具有设计结构的钛镍合金增强体骨架,其中选用Yb:YAG(三价镱离子掺杂钇铝石榴石)激光器,功率为200W,激光束斑直径为40μm,铺粉厚度为50μm,激光扫描速度为200mm/s,扫描间隙为100μm,在氩气保护下自然冷却,打印得到的钛镍合金骨架见图2,该骨架的尺寸为10×10×10mm3,孔隙率为70%,孔径约为1~2mm,连接棱直径约为1mm;1) The 3D visualization solid simulation software Autodesk Inventor Professional (AIP2019) is used to design a titanium-nickel alloy reinforced body skeleton with a network topology, and a 3D model of the skeleton is established. As shown in Figure 1, the network topology of the model was established based on the principle of triple periodic minimum surface; the model was imported into the
2)将步骤1)打印得到的钛镍合金增强体骨架放入直径10cm的高纯石墨坩埚(石墨的含碳量>99.9wt%)中,骨架上方放置25g金属镁,将坩埚置于真空电阻炉中,在氩气环境中以5℃/min的速率从室温升温至850℃,保温5min。2) Put the titanium-nickel alloy reinforcement skeleton printed in step 1) into a high-purity graphite crucible with a diameter of 10 cm (carbon content of graphite > 99.9 wt%), place 25 g of magnesium metal above the skeleton, and place the crucible in a vacuum resistor In the furnace, the temperature was raised from room temperature to 850°C at a rate of 5°C/min in an argon atmosphere, and the temperature was maintained for 5 minutes.
3)停止加热,以5℃/min的速率降温至室温,取出坩埚,并将复合材料从坩埚中取出,得到具有三维互穿网络结构的钛镍合金增强镁基复合材料。如图3所示,在实物图中,深色部分是钛镍合金增强体,浅色部分是镁基体。在三维X射线结构图中,浅色部分是钛镍合金增强体,深色部分是镁基体。该复合材料中的钛镍合金增强体的体积分数为30%,钛镍合金增强体与镁基体分别具有独立的拓扑结构并在三维空间穿插互补结合,表现为三维互穿网络结构。3) Stop heating, cool down to room temperature at a rate of 5°C/min, take out the crucible, and take out the composite material from the crucible to obtain a titanium-nickel alloy reinforced magnesium-based composite material with a three-dimensional interpenetrating network structure. As shown in Figure 3, in the physical picture, the dark part is the titanium-nickel alloy reinforcement, and the light part is the magnesium matrix. In the three-dimensional X-ray structure diagram, the light-colored part is the titanium-nickel alloy reinforcement, and the dark-colored part is the magnesium matrix. The volume fraction of the titanium-nickel alloy reinforcement in the composite material is 30%, and the titanium-nickel alloy reinforcement and the magnesium matrix respectively have independent topological structures and interpenetrate and complement each other in three-dimensional space, showing a three-dimensional interpenetrating network structure.
经测试,该复合材料的密度为3.2g/cm3,压缩强度为320MPa,压缩塑性应变超过35%,见图4。此外,该复合材料具有形状记忆效应,当室温压缩应变量为5%时,将复合材料加热到350℃并保温5h,复合材料的应变得以自动回复,回复应变量占总应变量的比例为98.5%。After testing, the density of the composite material is 3.2 g/cm 3 , the compressive strength is 320 MPa, and the compressive plastic strain exceeds 35%, as shown in FIG. 4 . In addition, the composite material has a shape memory effect. When the compressive strain amount at room temperature is 5%, the composite material is heated to 350 ° C and kept for 5 h, the strain of the composite material can be automatically recovered, and the ratio of the recovery strain amount to the total strain amount is 98.5 %.
实施例2:Example 2:
本实施例中,制备具有三维互穿网络结构的钛镍合金增强镁合金基复合材料。所用的原材料包括钛镍合金粉(平均粒径为15μm,钛与镍原子比例为1:1)、AZ91D镁合金。具体制备工艺如下:In this example, a titanium-nickel alloy reinforced magnesium alloy matrix composite material with a three-dimensional interpenetrating network structure was prepared. The raw materials used include titanium-nickel alloy powder (average particle size is 15 μm, and the atomic ratio of titanium and nickel is 1:1) and AZ91D magnesium alloy. The specific preparation process is as follows:
1)该步骤与实施例1中的步骤1)相同;1) this step is identical to step 1) in Example 1;
2)该步骤与实施例1中的步骤2)的不同之处在于,浸渗镍钛合金骨架所用的金属为AZ91D镁合金,浸渗温度为860℃;2) The difference between this step and step 2) in Example 1 is that the metal used for the infiltration of the nickel-titanium alloy skeleton is AZ91D magnesium alloy, and the infiltration temperature is 860°C;
3)该步骤与实施例1中的步骤3)相同。3) This step is the same as step 3) in Example 1.
经测试,该复合材料的密度为3.4g/cm3,压缩强度为400MPa,压缩塑性应变超过30%。此外,该复合材料具有形状记忆效应,当室温压缩应变量为5%时,将复合材料加热到300℃并保温5h,复合材料的应变得以自动回复,回复应变量占总应变量的比例为96.4%。After testing, the density of the composite material is 3.4 g/cm 3 , the compressive strength is 400 MPa, and the compressive plastic strain exceeds 30%. In addition, the composite material has a shape memory effect. When the compressive strain at room temperature is 5%, the composite material is heated to 300 ° C and kept for 5 h, the strain of the composite material can be automatically recovered, and the ratio of the recovery strain to the total strain is 96.4 %.
实施例3:Example 3:
本实施例中,制备具有三维互穿网络结构的钛镍合金增强镁基复合材料。所用的原材料包括钛镍合金粉(平均粒径为15μm,钛与镍原子比例为1:1)、金属镁。具体制备工艺如下:In this example, a titanium-nickel alloy reinforced magnesium-based composite material with a three-dimensional interpenetrating network structure was prepared. The raw materials used include titanium-nickel alloy powder (average particle size is 15 μm, and the atomic ratio of titanium and nickel is 1:1) and metal magnesium. The specific preparation process is as follows:
1)该步骤与实施例1中的步骤1)类似,所不同的是,3D打印的钛镍合金骨架结构不同,见图5。1) This step is similar to step 1) in Example 1, except that the skeleton structure of the 3D-printed titanium-nickel alloy is different, see Figure 5.
2)该步骤与实施例1中的步骤2)相同;2) this step is the same as step 2) in Example 1;
3)该步骤与实施例1中的步骤3)类似,所不同的是,该复合材料中的钛镍合金增强体的体积分数为64%。3) This step is similar to step 3) in Example 1, except that the volume fraction of the titanium-nickel alloy reinforcement in the composite material is 64%.
经测试,该复合材料的密度为4.1g/cm3,压缩强度为590MPa,压缩塑性应变超过25%。此外,该复合材料具有形状记忆效应,当室温压缩应变量为5%时,将复合材料加热到350℃并保温5h,复合材料的应变得以自动回复,回复应变量占总应变量的比例为99.4%。After testing, the density of the composite material is 4.1 g/cm 3 , the compressive strength is 590 MPa, and the compressive plastic strain exceeds 25%. In addition, the composite material has a shape memory effect. When the compressive strain amount at room temperature is 5%, the composite material is heated to 350 ° C and kept for 5 h, the strain of the composite material can be automatically recovered, and the ratio of the recovery strain amount to the total strain amount is 99.4 %.
实施例结果表明,本发明的复合材料具有轻质、高强度、高塑性等优异性能以及形状记忆功能,即室温变形在马氏体相变温度以上能够部分或完全回复,同时其结构和力学性能可以通过3D打印技术进行设计和有效控制,因此作为新型结构功能一体化材料具有可观的应用前景。The results of the examples show that the composite material of the present invention has excellent properties such as light weight, high strength and high plasticity, as well as a shape memory function, that is, the room temperature deformation can be partially or completely recovered above the martensitic transformation temperature, and its structure and mechanical properties. It can be designed and effectively controlled by 3D printing technology, so it has considerable application prospects as a new structure-function integrated material.
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