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CN114411035A - Precipitation strengthening type medium-entropy alloy suitable for laser additive manufacturing and preparation method thereof - Google Patents

Precipitation strengthening type medium-entropy alloy suitable for laser additive manufacturing and preparation method thereof Download PDF

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CN114411035A
CN114411035A CN202210067106.8A CN202210067106A CN114411035A CN 114411035 A CN114411035 A CN 114411035A CN 202210067106 A CN202210067106 A CN 202210067106A CN 114411035 A CN114411035 A CN 114411035A
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何峰
郭博静
谢浩宇
王志军
李俊杰
王锦程
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Northwestern Polytechnical University
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Abstract

本发明提供适用于激光增材制造的析出强化型中熵合金及其制备方法,所述析出强化型中熵合金为NiaCobCrcAldMe,其中,M为Ti、Ta、Nb和Mo中的一种或多种元素,a、b、c、d和e分别代表对应各元素的摩尔百分比,b=20%‑40%,c=20%‑25%,d>1%,e>0,d+e<7%,a+b+c+d+e=100%。本发明析出强化型中熵合金采用激光选区熔化成形技术或激光立体成形技术进行制备,实现了高致密、无裂纹、综合力学性能优异的新型析出强化型中熵合金的制备。The invention provides a precipitation-strengthened medium-entropy alloy suitable for laser additive manufacturing and a preparation method thereof. The precipitation-strengthened medium-entropy alloy is Ni a Co b Cr c Al d Me , wherein M is Ti, Ta, Nb and one or more elements in Mo, a, b, c, d and e represent the mole percentages of the corresponding elements respectively, b=20%-40%, c=20%-25%, d>1%, e>0, d+e<7%, a+b+c+d+e=100%. The precipitation-strengthened medium-entropy alloy of the present invention is prepared by using the laser selective melting forming technology or the laser three-dimensional forming technology, and realizes the preparation of a novel precipitation-strengthening medium-entropy alloy with high density, no cracks and excellent comprehensive mechanical properties.

Description

适用于激光增材制造的析出强化型中熵合金及其制备方法Precipitation-strengthened medium-entropy alloy suitable for laser additive manufacturing and preparation method thereof

技术领域technical field

本发明涉及金属材料激光增材制造技术领域,尤其涉及一种适用于激光增材制造的析出强化型中熵合金及其制备方法。The invention relates to the technical field of laser additive manufacturing of metal materials, in particular to a precipitation-strengthened medium-entropy alloy suitable for laser additive manufacturing and a preparation method thereof.

背景技术Background technique

高/中熵合金以全新的合金设计策略,采用几种等浓度或近等浓度的主元素作为合金元素,表现出优异的强度、延展性和断裂韧性的结合,具有广泛的结构化和功能化应用前景。FCC结构的高/中熵合金表现出良好的韧性但其强度普遍偏低,难以满足结构材料的应用需求,目前,在FCC高/中熵合金中引入析出相是实现FCC高/中熵合金强韧化的有效方法。High/medium-entropy alloys exhibit an excellent combination of strength, ductility, and fracture toughness, with a wide range of structuring and functionalization based on a brand-new alloy design strategy that employs several main elements of equal or near equal concentration as alloying elements application prospects. High/medium-entropy alloys with FCC structure show good toughness, but their strength is generally low, which is difficult to meet the application requirements of structural materials. Effective method of toughening.

高/中熵合金传统制备方法以电弧熔炼为主,存在形状尺寸单一、易出现成分偏析、缩松、缩孔等缺陷,难以成形全致密高性能结构复杂的高/中熵合金部件,极大限制了高/中熵合金的进一步应用与发展。The traditional preparation method of high/medium entropy alloys is mainly arc melting, which has defects such as single shape and size, easy component segregation, shrinkage porosity, shrinkage cavities, etc. This limits the further application and development of high/medium entropy alloys.

激光增材制造技术基于材料逐点、逐线、逐层累积的原理,通过高能激光束与金属粉末的快速作用,以极高的制造灵活性,实现了复杂结构或定制部件的近净成形。该技术具有材料利用率高、制造过程高柔性、周期短、微观组织均匀细小等优势,为制备综合性能优异,高精度全致密及形状复杂的高/中熵合金构件提供了巨大的潜力。然而,增材制造过程中高的温度梯度和大的冷却速率,通常会导致高的热残余应力,容易产生裂纹等冶金缺陷。尤其对于析出强化型高/中熵合金,打印过程中极易出现液化开裂及应变时效开裂等缺陷,影响构件的组织完整性和综合性能。因此,设计出适用于激光增材制造的析出强化型高/中熵合金是本领域亟需解决的关键问题。Laser additive manufacturing technology is based on the principle of point-by-point, line-by-line, and layer-by-layer accumulation of materials. Through the rapid interaction of high-energy laser beams and metal powders, the near-net shape of complex structures or customized parts is realized with extremely high manufacturing flexibility. This technology has the advantages of high material utilization, high flexibility in the manufacturing process, short cycle, uniform and small microstructure, etc., and provides great potential for the preparation of high/medium entropy alloy components with excellent comprehensive properties, high precision, full density and complex shapes. However, the high temperature gradient and large cooling rate during additive manufacturing usually lead to high thermal residual stress, which is prone to metallurgical defects such as cracks. Especially for precipitation-strengthened high/medium entropy alloys, defects such as liquefaction cracking and strain aging cracking are very likely to occur during the printing process, which affect the structural integrity and comprehensive performance of the components. Therefore, designing a precipitation-strengthened high/medium entropy alloy suitable for laser additive manufacturing is a key problem that needs to be solved urgently in this field.

发明内容SUMMARY OF THE INVENTION

本发明的目的在于克服传统高/中熵合金制备方法的缺点,提供适用于激光增材制造的析出强化型中熵合金及其制备方法,实现高致密、无裂纹、综合力学性能优异的新型析出强化型中熵合金的制备。The purpose of the present invention is to overcome the shortcomings of traditional high/medium-entropy alloy preparation methods, provide a precipitation-strengthened medium-entropy alloy suitable for laser additive manufacturing and a preparation method thereof, and realize a new type of precipitation with high density, no cracks and excellent comprehensive mechanical properties. Preparation of strengthened medium-entropy alloys.

本发明通过以下技术方案实现:The present invention is achieved through the following technical solutions:

适用于激光增材制造的析出强化型中熵合金,所述析出强化型中熵合金为NiaCobCrcAldMe,其中,M为Ti、Ta、Nb和Mo中的一种或多种元素,a、b、c、d和e分别代表对应各元素的摩尔百分比,b=20%-40%,c=20%-25%,d>1%,e>0,d+e<7%,a+b+c+d+e=100%。A precipitation-strengthened medium-entropy alloy suitable for laser additive manufacturing, wherein the precipitation-strengthened medium-entropy alloy is Ni a Co b Cr c Al d Me , wherein M is one of Ti, Ta, Nb and Mo or Multiple elements, a, b, c, d and e represent the mole percentage of each element respectively, b=20%-40%, c=20%-25%, d>1%, e>0, d+e <7%, a+b+c+d+e=100%.

优选的,采用激光选区熔化成形技术进行制备。Preferably, it is prepared by using laser selective melting forming technology.

进一步的,包括:Further, including:

步骤1,中熵合金粉末制备及预处理Step 1, preparation and pretreatment of medium entropy alloy powder

按照权利要求1所述摩尔百分比,取各元素对应的金属原料,采用真空气雾化法制备中熵合金预合金球形粉末,过筛,烘干,得到中熵合金粉末;According to the molar percentage of claim 1, get the metal raw material corresponding to each element, adopt the vacuum air atomization method to prepare the medium-entropy alloy pre-alloy spherical powder, sieve, and dry to obtain the medium-entropy alloy powder;

步骤2,激光选区熔化成形NiaCobCrcAldMe析出强化型中熵合金Step 2, laser selective melting to form Ni a Co b Cr c Al d Me precipitation-strengthened medium-entropy alloy

根据待制备的中熵合金构件的几何形状建立三维实体模型并转换为STL格式的文件,导入激光选区熔化成形设备的建造软件中,进行分层处理;通入高纯氩气,使成形舱室内氧气含量低于300ppm,根据所设定的激光选区熔化成形的工艺参数及扫描策略,将中熵合金粉末逐层熔化成形,制备得到中熵合金构件。According to the geometric shape of the medium-entropy alloy component to be prepared, a 3D solid model is established and converted into a file in STL format, and imported into the construction software of the laser selective melting forming equipment for layering processing; high-purity argon gas is introduced to make the forming chamber The oxygen content is lower than 300ppm. According to the set process parameters and scanning strategy of laser selective melting and forming, the medium-entropy alloy powder is melted and formed layer by layer to prepare a medium-entropy alloy component.

进一步的,激光选区熔化成形的工艺参数如下:激光功率P为160~360W,扫描速率v为600~1000mm/s,扫描间距h为60-80μm,铺粉层厚t为30-50μm,光斑直径为80μm,体能量密度VED范围为140J/mm3<VED<240J/mm3,其中VED=P/vht。Further, the process parameters of laser selective melting and forming are as follows: the laser power P is 160-360W, the scanning rate v is 600-1000mm/s, the scanning distance h is 60-80μm, the powder layer thickness t is 30-50μm, and the spot diameter is 30-50μm. is 80 μm, and the volume energy density VED range is 140 J/mm 3 <VED<240 J/mm 3 , where VED=P/vht.

进一步的,扫描策略为67°旋转扫描、往复扫描、往复交织扫描或45°旋转分区扫描。Further, the scanning strategy is 67° rotation scanning, reciprocating scanning, reciprocating interleaving scanning or 45° rotation partition scanning.

进一步的,还包括热处理步骤:将中熵合金构件升温至600℃~800℃保温12h≤t≤480h,保温结束后水冷,得到热处理后的中熵合金。Further, it also includes a heat treatment step: heating the medium-entropy alloy component to 600°C to 800°C for 12h≤t≤480h, and water-cooling after the heat preservation to obtain a heat-treated medium-entropy alloy.

优选的,采用激光立体成形技术进行制备。Preferably, it is prepared by using a laser three-dimensional forming technology.

进一步的,包括:Further, including:

步骤1,中熵合金粉末制备及预处理Step 1, preparation and pretreatment of medium entropy alloy powder

按照权利要求1所述摩尔百分比,取各元素对应的金属原料,采用真空气雾化法制备中熵合金预合金球形粉末,过筛,烘干,得到中熵合金粉末;According to the molar percentage of claim 1, get the metal raw material corresponding to each element, adopt the vacuum air atomization method to prepare the medium-entropy alloy pre-alloy spherical powder, sieve, and dry to obtain the medium-entropy alloy powder;

步骤2激光立体成形NiaCobCrcAldMe析出强化型中熵合金Step 2 Laser three-dimensional forming Ni a Co b Cr c Al d Me precipitation strengthening type medium entropy alloy

根据待制备的中熵合金构件的几何形状建立三维实体模型并转换为STL格式传送到激光立体成形设备,设置打印工艺参数及激光扫描路径,将中熵合金粉末送至激光立体成形设备中高能激光束所形成的熔池中,通过在基材上逐点、逐线、逐层沉积原材料的方式,打印得到中熵合金构件。According to the geometric shape of the medium-entropy alloy component to be prepared, a three-dimensional solid model is established and converted into STL format and sent to the laser stereoforming equipment, the printing process parameters and laser scanning path are set, and the medium-entropy alloy powder is sent to the high-energy laser in the laser stereoforming equipment. In the molten pool formed by the beam, by depositing raw materials point by point, line by line and layer by layer on the substrate, the intermediate entropy alloy component is obtained by printing.

进一步的,打印工艺参数如下:激光功率为2KW~3.5KW,扫描速率为300~800mm/min,送粉速度为5-8g/min,Z轴抬升量为0.4-1.0mm,搭接率为50%,光斑直径为3mm,扫描路径为往复交织扫描路径。Further, the printing process parameters are as follows: the laser power is 2KW-3.5KW, the scanning rate is 300-800mm/min, the powder feeding speed is 5-8g/min, the Z-axis lift is 0.4-1.0mm, and the overlap ratio is 50 %, the spot diameter is 3mm, and the scanning path is a reciprocating interweaving scanning path.

进一步的,还包括热处理步骤:将中熵合金构件升温至600℃~800℃保温3h≤t≤480h,保温结束后水冷,得到热处理后的中熵合金。Further, it also includes a heat treatment step: heating the medium-entropy alloy component to 600°C to 800°C for 3h≤t≤480h, and cooling with water after the heat preservation to obtain a heat-treated medium-entropy alloy.

与现有技术相比,本发明具有如下的有益效果:Compared with the prior art, the present invention has the following beneficial effects:

本发明设计了适用于激光增材制造的析出强化型中熵合金,在NiaCobCrc基体中通过多主元化的形式,添加Al以及Ti、Ta、Nb或Mo元素,促进γ'相产生并显著增强γ'析出相的强化效果。规定上述Al、Ti、Ta、Nb、Mo之和小于7%,原因在于一方面克服了由于高体积分数的γ'相所导致的增材制造过程成形性差等问题,即降低了合金在激光增材制造中高的液化开裂及应变时效开裂等敏感性;另一方面能够获得具有优异强化效果的γ'析出相。本发明按照上述的配方,分别采用激光选区熔化成形技术与激光立体成形技术实现了高致密、无裂纹、综合力学性能优异的新型析出强化型中熵合金的制备。The invention designs a precipitation-strengthening medium-entropy alloy suitable for laser additive manufacturing. In the Ni a Co b Cr c matrix, in the form of multi-principalization, Al and Ti, Ta, Nb or Mo elements are added to promote γ' phase is generated and significantly enhances the strengthening effect of the γ' precipitation phase. It is stipulated that the sum of the above-mentioned Al, Ti, Ta, Nb, and Mo is less than 7%. High susceptibility to liquefaction cracking and strain aging cracking in material manufacturing; on the other hand, γ' precipitates with excellent strengthening effect can be obtained. According to the above formula, the present invention adopts the laser selective melting forming technology and the laser three-dimensional forming technology to realize the preparation of a new type of precipitation-strengthened medium-entropy alloy with high density, no cracks and excellent comprehensive mechanical properties.

进一步的,通过对激光增材制造样品进行热处理促进γ'析出相的产生,同时获得具有部分再结晶的非均匀组织,大幅度提高了本发明所设计的析出强化型中熵合金的综合力学性能,实现了激光增材制造中熵合金的进一步强韧化。Further, the generation of γ' precipitation phase is promoted by heat treatment of the laser additive manufacturing sample, and at the same time, a non-uniform structure with partial recrystallization is obtained, which greatly improves the comprehensive mechanical properties of the precipitation-strengthened medium-entropy alloy designed in the present invention. , further strengthening and toughening of entropy alloys in laser additive manufacturing.

附图说明Description of drawings

图1为本发明实施例1激光选区熔化成形Ni35Co35Cr25Ti3Al2中熵合金粉末形貌。Fig. 1 is the powder morphology of Ni 35 Co 35 Cr 25 Ti 3 Al 2 medium-entropy alloy powder formed by laser selective melting in Example 1 of the present invention.

图2为本发明实施例1激光选区熔化技术制备的Ni35Co35Cr25Ti3Al2中熵合金块体样品。FIG. 2 is a Ni 35 Co 35 Cr 25 Ti 3 Al 2 medium entropy alloy bulk sample prepared by laser selective melting technology in Example 1 of the present invention.

图3为本发明实施例1中激光选区熔化技术制备的Ni35Co35Cr25Ti3Al2中熵合金的致密度随体能量密度的变化规律。FIG. 3 is the variation law of the density of the entropy alloy in the Ni 35 Co 35 Cr 25 Ti 3 Al 2 prepared by the laser selective melting technology in Example 1 of the present invention with the bulk energy density.

图4为本发明实施例1中分别采用铸造和激光选区熔化技术制备的Ni35Co35Cr25Ti3Al2中熵合金的扫描电镜图片,其中(a)为铸态,(b)为沉积态。Fig. 4 is the scanning electron microscope picture of the entropy alloy of Ni 35 Co 35 Cr 25 Ti 3 Al 2 prepared by casting and laser selective melting technology respectively in Example 1 of the present invention, wherein (a) is the as-cast state, (b) is the deposition state.

图5为本发明实施例1中铸态和激光选区熔化成形Ni35Co35Cr25Ti3Al2中熵合金的室温拉伸应力-应变曲线。FIG. 5 is the room temperature tensile stress-strain curve of the entropy alloy formed in the as-cast state and by laser selective melting of Ni 35 Co 35 Cr 25 Ti 3 Al 2 in Example 1 of the invention.

图6为本发明实施例1激光选区熔化成形Ni35Co35Cr25Ti3Al2中熵合金经600℃/12h热处理后的扫描电镜图片(a)和透射电镜选区电子衍射图(b)。6 is a scanning electron microscope image (a) and a transmission electron microscope selected area electron diffraction pattern (b) of the Ni 35 Co 35 Cr 25 Ti 3 Al 2 medium entropy alloy formed by laser selective melting in Example 1 of the present invention after heat treatment at 600° C./12h.

图7为本发明实施例1激光选区熔化成形Ni35Co35Cr25Ti3Al2中熵合金经不同热处理温度和时间后的室温拉伸应力-应变曲线。7 is a room temperature tensile stress-strain curve of the entropy alloy formed by laser selective melting and forming of Ni 35 Co 35 Cr 25 Ti 3 Al 2 in Example 1 of the present invention after different heat treatment temperatures and times.

图8为本发明实施例2激光立体成形Ni35Co35Cr25Ti3Al2中熵合金粉末形貌。FIG. 8 is the powder morphology of the entropy alloy in the laser three-dimensional forming of Ni 35 Co 35 Cr 25 Ti 3 Al 2 in Example 2 of the present invention.

图9为本发明实施例2激光立体成形Ni35Co35Cr25Ti3Al2中熵合金块体样品。FIG. 9 is a bulk sample of entropy alloy in Ni 35 Co 35 Cr 25 Ti 3 Al 2 medium-entropy alloy formed by laser three-dimensional forming in Example 2 of the present invention.

图10为本发明实施例2中采用不同激光功率制备的Ni35Co35Cr25Ti3Al2中熵合金的室温拉伸应力-应变曲线。10 is the room temperature tensile stress-strain curve of the entropy alloy of Ni 35 Co 35 Cr 25 Ti 3 Al 2 prepared by using different laser powers in Example 2 of the present invention.

图11为本发明实施例2中激光立体成形Ni35Co35Cr25Ti3Al2中熵合金的微观组织特征。FIG. 11 shows the microstructure characteristics of the entropy alloy in the laser three-dimensional forming Ni 35 Co 35 Cr 25 Ti 3 Al 2 in Example 2 of the present invention.

图12为本发明实施例2中采用最优激光立体成形工艺参数制备的Ni35Co35Cr25Ti3Al2中熵合金的室温拉伸应力-应变曲线。FIG. 12 is the room temperature tensile stress-strain curve of the entropy alloy of Ni 35 Co 35 Cr 25 Ti 3 Al 2 prepared by using the optimal laser three-dimensional forming process parameters in Example 2 of the present invention.

图13为本发明实施例2激光立体成形Ni35Co35Cr25Ti3Al2中熵合金经热处理后的扫描电镜图片。FIG. 13 is a scanning electron microscope picture of the entropy alloy of Ni 35 Co 35 Cr 25 Ti 3 Al 2 medium-entropy alloy after heat treatment in Example 2 of the present invention.

图14为本发明实施例2激光立体成形Ni35Co35Cr25Ti3Al2中熵合金经热处理后的显微硬度。14 is the microhardness of the entropy alloy after heat treatment in the laser three-dimensional forming of Ni 35 Co 35 Cr 25 Ti 3 Al 2 in Example 2 of the present invention.

图15为本发明实施例2激光立体成形Ni35Co35Cr25Ti3Al2中熵合金经700℃/3h热处理后(LSF-HT)的室温拉伸应力-应变曲线。15 is the room temperature tensile stress-strain curve of the laser three-dimensionally formed Ni 35 Co 35 Cr 25 Ti 3 Al 2 medium entropy alloy after heat treatment at 700° C./3h (LSF-HT).

具体实施方式Detailed ways

为了进一步理解本发明,下面结合实施例对本发明进行描述,这些描述只是进一步解释本发明的特征和优点,并非用于限制本发明的权利要求。In order to further understand the present invention, the present invention will be described below in conjunction with the embodiments. These descriptions are only used to further explain the features and advantages of the present invention, and are not intended to limit the claims of the present invention.

本发明所述的适用于激光增材制造的强塑性优异的析出强化型中熵合金,所述析出强化型中熵合金的合金组分为NiaCobCrcAldMe,其中a、b、c、d、e分别代表对应各元素的摩尔百分比,a为余量,b=20-40at.%,c=20-25at.%,d>1at.%,e>0,d+e<7at.%,a+b+c+d+e=100at.%,所述微量元素M包括Ti、Ta、Nb、Mo中的一种或多种成分。所选用中熵合金为真空气雾化或等离子旋转电极法制备的预合金球形粉末,纯度大于99.9%。The precipitation-strengthened medium-entropy alloy with excellent strong plasticity suitable for laser additive manufacturing according to the present invention, the alloy composition of the precipitation-strengthened medium-entropy alloy is Ni a Co b Cr c Al d Me , wherein a, b, c, d, and e represent the mole percentage of each element respectively, a is the remainder, b=20-40at.%, c=20-25at.%, d>1at.%, e>0, d+e <7 at.%, a+b+c+d+e=100 at.%, the trace element M includes one or more components of Ti, Ta, Nb, and Mo. The selected medium-entropy alloy is pre-alloyed spherical powder prepared by vacuum air atomization or plasma rotating electrode method, and the purity is more than 99.9%.

本发明提供了上述析出强化型中熵合金的激光选区熔化成形技术的制备方法,包括以下步骤:The present invention provides a preparation method of the above-mentioned precipitation-enhanced medium-entropy alloy laser selective melting forming technology, which comprises the following steps:

1、中熵合金粉末制备及预处理1. Preparation and pretreatment of medium entropy alloy powder

根据所述中熵合金名义化学成分中的各元素摩尔百分比进行配比,采用真空气雾化法制备中熵合金预合金球形粉末,将预合金球形粉末进行过筛,选用粉末粒径为15-53μm。氧含量及氮含量低于300ppm,优选的氧含量为131ppm,氮含量为53ppm。进行激光选区熔化前,将预合金球形粉末进行80℃,4h的烘干处理,去除粉末中的水分,随后将其放置于激光选区熔化设备送粉缸内。According to the molar percentage of each element in the nominal chemical composition of the medium-entropy alloy, the medium-entropy alloy pre-alloyed spherical powder is prepared by vacuum air atomization, and the pre-alloyed spherical powder is sieved, and the powder particle size is 15- 53 μm. The oxygen content and nitrogen content are less than 300 ppm, the preferred oxygen content is 131 ppm, and the nitrogen content is 53 ppm. Before laser selective melting, the pre-alloyed spherical powder was dried at 80°C for 4 h to remove the moisture in the powder, and then placed in the powder feeding cylinder of the laser selective melting equipment.

2、基板表面处理2. Substrate surface treatment

选取不锈钢或碳钢基板,打磨待沉积面,并依次用丙酮和酒精清洗以去除表面油污,随后吹干,将基板安装在成型平台上并进行调平。在打印之前,将基板预热到100℃-200℃,优选的基板预热温度为200℃。Select a stainless steel or carbon steel substrate, grind the surface to be deposited, and wash with acetone and alcohol in sequence to remove surface oil stains, then blow dry, install the substrate on a forming platform and level it. Before printing, the substrate is preheated to 100°C-200°C, and the preferred substrate preheating temperature is 200°C.

3、激光选区熔化成形NiaCobCrcAldMe析出强化型中熵合金3. Laser selective melting forming Ni a Co b Cr c Al d Me precipitation-strengthened medium-entropy alloy

在计算机上建立三维实体模型并转换为STL格式的文件,将其导入激光选区熔化成形设备的建造软件中,进行分层处理。激光选区熔化成形的工艺参数如下:激光功率P为160~360W,扫描速率v为600~1000mm/s,扫描间距h为60-80μm,铺粉层厚t为30-50μm,光斑直径为80μm,扫描策略可选择67°旋转扫描、往复扫描、往复交织扫描以及45°旋转分区扫描路径。打印之前,通入纯度为99.99wt.%的高纯氩气,使成形舱室内氧气含量低于300ppm。根据所设定的激光选区熔化成形的工艺参数及扫描路径,将NiaCobCrcAldMe中熵合金预合金球形粉末逐层熔化成形,制备出块体样品。本发明采用激光选区熔化成形的方式制备NiaCobCrcAldMe析出强化型中熵合金,通过选用优化的激光选区熔化成形工艺参数,即高的体能量密度VED(140J/mm3<VED<240J/mm3,VED=P/vht),可以极大提高打印合金的致密度,进而提高其综合力学性能,实现高致密、无裂纹、性能优异的析出强化型中熵合金复杂结构件的一体化精密成形。The three-dimensional solid model is established on the computer and converted into a file in STL format, and then imported into the construction software of the laser selective melting forming equipment for layered processing. The process parameters of laser selective melting and forming are as follows: laser power P is 160-360W, scanning rate v is 600-1000mm/s, scanning distance h is 60-80μm, powder layer thickness t is 30-50μm, spot diameter is 80μm, Scanning strategies can select 67° rotary scan, reciprocating scan, reciprocating interleaved scan and 45° rotary partition scan path. Before printing, high-purity argon gas with a purity of 99.99 wt. % was introduced to make the oxygen content in the forming chamber less than 300 ppm. According to the set process parameters and scanning path of laser selective melting forming, Ni a Co b Cr c Al d Me medium entropy alloy pre-alloyed spherical powder is melted and formed layer by layer to prepare a bulk sample. The present invention adopts the method of laser selective melting and forming to prepare Ni a Co b Cr c Al d Me precipitation strengthening type medium entropy alloy, and selects optimized laser selective melting and forming process parameters, that is, high volume energy density VED (140 J/mm 3 ) <VED<240J/mm 3 , VED=P/vht), which can greatly improve the density of the printed alloy, thereby improving its comprehensive mechanical properties, and realizing the complex structure of precipitation-strengthened medium-entropy alloys with high density, no cracks and excellent performance. Integrated precision forming of parts.

本发明还提供了上述析出强化型中熵合金的激光立体成形技术的制备方法,包括以下步骤:The present invention also provides a method for preparing the above-mentioned precipitation-enhanced medium-entropy alloy laser three-dimensional forming technology, comprising the following steps:

1、中熵合金粉末制备及预处理1. Preparation and pretreatment of medium entropy alloy powder

根据所述中熵合金名义化学成分中的各元素摩尔百分比进行配比,采用真空气雾化法制备中熵合金预合金球形粉末,将预合金球形粉末进行过筛,选用粉末粒径为45-150μm。氧含量及氮含量低于300ppm,优选的氧含量为131ppm,氮含量为53ppm。进行激光立体成形实验前,将粉末烘干处理以避免粉末中吸附的水分对材料成形产生的影响,随后将粉末放置于激光立体成形设备送粉器内。According to the molar percentage of each element in the nominal chemical composition of the medium-entropy alloy, the medium-entropy alloy pre-alloyed spherical powder is prepared by vacuum air atomization, and the pre-alloyed spherical powder is sieved, and the powder particle size is 45- 150μm. The oxygen content and nitrogen content are less than 300 ppm, the preferred oxygen content is 131 ppm, and the nitrogen content is 53 ppm. Before the laser three-dimensional forming experiment, the powder was dried to avoid the influence of moisture adsorbed in the powder on the material forming, and then the powder was placed in the powder feeder of the laser three-dimensional forming equipment.

2、基板表面处理2. Substrate surface treatment

选取不锈钢或碳钢基板,打磨待沉积面,并依次用丙酮和酒精清洗以去除表面油污,随后吹干,将基板固定于成型平台。A stainless steel or carbon steel substrate is selected, the surface to be deposited is polished, and then washed with acetone and alcohol in turn to remove oil stains on the surface, and then air-dried to fix the substrate on the forming platform.

3、激光立体成形NiaCobCrcAldMe析出强化型中熵合金3. Laser three-dimensional forming Ni a Co b Cr c Al d Me precipitation strengthened medium entropy alloy

根据中熵合金构件的几何形状在计算机上建立三维实体模型并转换为STL格式传送到激光成形设备,设置打印工艺参数及激光扫描路径,在数控系统的控制下,中熵合金球形粉末经同轴送粉喷嘴送至高能激光束所形成的熔池中,通过在基材上逐点、逐线、逐层沉积原材料的方式,实现特定形状及尺寸的复杂构件成形。上述激光立体成形的工艺参数如下:激光功率为2KW~3.5KW,扫描速率为300~800mm/min,送粉速度为5-8g/min,Z轴抬升量为0.4-1.0mm,搭接率为50%,光斑直径为3mm,扫描策略选择往复交织扫描,即在同一沉积层,扫描路径呈S型,相邻沉积层,扫描方向旋转90°。上述激光立体成形过程采用高纯氩气作为保护气体和载粉气体,打印过程中氧气含量低于2000ppm。根据上述设定的激光立体成形的工艺参数及扫描路径,将NiaCobCrcAldMe中熵合金粉末逐层熔化成形,制备出块体样品。通过优化激光功率、扫描速度、送粉速度以及Z轴抬升量,可以提高打印合金的质量并优化微观组织,进一步提高其综合力学性能,实现全致密、无缺陷、综合性能优异的析出强化型中熵合金复杂结构件的一体化精密成形。According to the geometric shape of the medium-entropy alloy component, a three-dimensional solid model is established on the computer, converted into STL format and sent to the laser forming equipment, and the printing process parameters and laser scanning path are set. Under the control of the numerical control system, the medium-entropy alloy spherical powder is coaxially transmitted The powder feeding nozzle is sent to the molten pool formed by the high-energy laser beam. By depositing raw materials point by point, line by line and layer by layer on the substrate, the formation of complex components with specific shapes and sizes is realized. The process parameters of the above-mentioned three-dimensional laser forming are as follows: the laser power is 2KW-3.5KW, the scanning rate is 300-800mm/min, the powder feeding speed is 5-8g/min, the Z-axis lift is 0.4-1.0mm, and the lap rate is 0.4-1.0mm. 50%, the spot diameter is 3mm, and the scanning strategy selects reciprocating interleaving scanning, that is, in the same deposition layer, the scanning path is S-shaped, and the scanning direction is rotated 90° for adjacent deposition layers. The above-mentioned laser three-dimensional forming process uses high-purity argon gas as the protective gas and powder carrier gas, and the oxygen content during the printing process is less than 2000ppm. According to the above set process parameters and scanning path of laser three-dimensional forming, Ni a Co b Cr c Al d Me medium entropy alloy powder is melted and formed layer by layer to prepare a bulk sample. By optimizing the laser power, scanning speed, powder feeding speed and Z-axis lift, the quality of the printed alloy can be improved, the microstructure can be optimized, and its comprehensive mechanical properties can be further improved to achieve a fully dense, defect-free, and comprehensive performance. Integrated precision forming of complex structural parts of entropy alloys.

本发明还提供了上述激光增材制造技术制备NiaCobCrcAldMe析出强化型中熵合金的热处理方法,包括以下步骤:The present invention also provides a heat treatment method for preparing the Ni a Co b Cr c Al d Me precipitation-strengthened medium-entropy alloy by the above-mentioned laser additive manufacturing technology, comprising the following steps:

在本发明中,为促进高体积分数的析出相产生,对激光增材制造NiaCobCrcAldMe型析出强化型中熵合金进行热处理。所述热处理的方式优选包括:将激光增材制造制备的NiaCobCrcAldMe析出强化型中熵合金升温至600℃~800℃保温,所选时间12h≤t≤480h(激光选区熔化成形)或者3h≤t≤480h(激光立体成形),保温结束后水冷,得到热处理后的中熵合金。通过对上述激光增材制造NiaCobCrcAldMe中熵合金进行热处理,可有效促进高体积分数的析出相的析出,同时得到不完全再结晶的组织,进一步优化激光增材制造NiaCobCrcAldMe中熵合金的综合力学性能,实现高强高韧中熵合金的制备。In the present invention, in order to promote the generation of a high volume fraction of the precipitation phase, the laser additive manufacturing Ni a Co b Cr c Al d Me type precipitation-strengthened medium-entropy alloy is heat-treated. The heat treatment method preferably includes: heating the Ni a Co b Cr c Al d Me precipitation-strengthened medium-entropy alloy prepared by laser additive manufacturing to 600 ℃ ~ 800 ℃ for heat preservation, and the selected time is 12h≤t≤480h (laser). Selective melting and forming) or 3h≤t≤480h (laser three-dimensional forming), water cooling after heat preservation to obtain a medium-entropy alloy after heat treatment. Heat treatment of the above-mentioned laser additive manufacturing Ni a Co b Cr c Al d Me medium entropy alloy can effectively promote the precipitation of a high volume fraction of the precipitation phase, and at the same time obtain an incompletely recrystallized structure, further optimizing the laser additive manufacturing. The comprehensive mechanical properties of Ni a Co b Cr c Al d Me medium-entropy alloys realize the preparation of high-strength and high-toughness medium-entropy alloys.

实施例1Example 1

一种适用于激光增材制造的析出强化型中熵合金,该中熵合金的化学式为Ni35Co35Cr25Ti3Al2;其中,各元素的比例为摩尔百分比。所选用中熵合金为气雾化预合金球形粉末,纯度大于99.9%。A precipitation-strengthening medium-entropy alloy suitable for laser additive manufacturing, the chemical formula of the medium-entropy alloy is Ni 35 Co 35 Cr 25 Ti 3 Al 2 , wherein the ratio of each element is a mole percentage. The selected medium-entropy alloy is gas atomized pre-alloyed spherical powder with a purity greater than 99.9%.

本实施例1采用激光选区熔化技术制备中熵合金成形过程如下:The present embodiment 1 adopts the laser selective melting technology to prepare the entropy alloy forming process as follows:

1、中熵合金粉末制备及预处理1. Preparation and pretreatment of medium entropy alloy powder

将根据上述中熵合金名义化学成分中的各元素摩尔比进行配比,采用真空气雾化法制备中熵合金预合金球形粉末,将预合金粉末进行过筛,选用粒粉末粒径为15-53μm,其典型形态如图1所示。氧含量为131ppm,氮含量为53ppm。进行激光选区熔化前,将粉末进行80℃,4h的烘干处理,去除粉末中的水分。随后将其放置于激光选区熔化设备送粉缸内。According to the molar ratio of each element in the above-mentioned nominal chemical composition of the medium-entropy alloy, the pre-alloyed spherical powder of the medium-entropy alloy is prepared by the vacuum air atomization method, and the pre-alloyed powder is sieved, and the particle size of the selected powder is 15- 53 μm, and its typical morphology is shown in Figure 1. The oxygen content was 131 ppm and the nitrogen content was 53 ppm. Before laser selective melting, the powder was dried at 80°C for 4 hours to remove the moisture in the powder. It is then placed in the powder feeding cylinder of the laser selective melting equipment.

2、基板表面处理2. Substrate surface treatment

选取316L不锈钢基板,打磨待沉积面,并依次用丙酮和酒精清洗以去除表面油污,随后吹干,将基板安装在成型平台上并进行调平。在打印之前,将基板预热到200℃。A 316L stainless steel substrate was selected, the surface to be deposited was polished, and then washed with acetone and alcohol in turn to remove the surface oil stains, and then blown dry, and the substrate was mounted on a forming platform and leveled. Before printing, the substrates were preheated to 200°C.

3、激光选区熔化成形Ni35Co35Cr25Ti3Al2析出强化型中熵合金3. Laser selective melting forming of Ni 35 Co 35 Cr 25 Ti 3 Al 2 precipitation-strengthened medium-entropy alloy

在计算机上建立三维实体模型并转换为STL格式的文件,将其导入选区激光熔化成形设备的建造软件中,进行分层处理。激光选区熔化成形的工艺参数如下:激光功率为160~360W,扫描速率为600~1000mm/s,扫描间距为60-80μm,铺粉层厚为30-50μm,光斑直径为80μm,扫描策略为67°旋转扫描。打印之前,通入纯度为99.99wt.%的高纯氩气,使成形舱室内氧气含量低于300ppm。A three-dimensional solid model is established on the computer and converted into a file in STL format, which is imported into the construction software of the selective laser melting forming equipment for layered processing. The process parameters of laser selective melting and forming are as follows: the laser power is 160-360W, the scanning rate is 600-1000mm/s, the scanning distance is 60-80μm, the powder layer thickness is 30-50μm, the spot diameter is 80μm, and the scanning strategy is 67 μm. °Rotate scan. Before printing, high-purity argon gas with a purity of 99.99 wt. % was introduced to make the oxygen content in the forming chamber less than 300 ppm.

通过表1所示参数,调整激光功率、扫描速率、扫描间距,固定铺粉层厚为30μm进行激光选区熔化成形实验,得到激光选区熔化成形样品如图2所示。并对样品致密度进行测试,结果如图3所示。According to the parameters shown in Table 1, adjust the laser power, scanning rate, and scanning spacing, and fix the powder layer thickness to 30 μm to carry out the laser selective melting forming experiment, and obtain the laser selective melting forming sample as shown in Figure 2. The density of the samples was tested, and the results are shown in Figure 3.

表1实验参数Table 1 Experimental parameters

Figure BDA0003480584020000081
Figure BDA0003480584020000081

Figure BDA0003480584020000091
Figure BDA0003480584020000091

通过表1所示实验确定了最优的工艺参数:激光功率为320W,扫描速度为1000mm/s,扫描间距为70μm,铺粉层厚为30μm。The optimal process parameters are determined by the experiments shown in Table 1: the laser power is 320W, the scanning speed is 1000mm/s, the scanning spacing is 70μm, and the thickness of the powder layer is 30μm.

4、激光选区熔化成形样品组织表征及性能测试4. Microstructure characterization and performance test of laser selective melting forming samples

采用扫描电子显微镜(SEM)观察在最优激光选区熔化参数成形样品的显微组织,如图4(b)所示,合金成形质量较好,未观察到裂纹等缺陷,经测试得到成形件相对致密度大于99.6%。与铸态(采用真空电弧熔炼法制备)组织相比,激光选区熔化沉积所制备的Ni35Co35Cr25Ti3Al2析出强化型中熵合金微观组织更加细小均匀。实施例1选用最优工艺参数所成形的激光选区熔化Ni35Co35Cr25Ti3Al2中熵合金(SLM)的室温屈服强度为671MPa,抗拉强度为913MPa,延伸率为36%,硬度为310HV。其强度远高于铸态,拉伸塑性与铸态相当,如图5所示,其中Ni35Co35Cr25Ti3Al2中熵合金铸态(Cast)的屈服强度为342MPa,抗拉强度为648MPa,延伸率为38%。Scanning electron microscope (SEM) was used to observe the microstructure of the samples formed by the optimal laser melting parameters. As shown in Fig. 4(b), the forming quality of the alloy was good, and no defects such as cracks were observed. The density is greater than 99.6%. Compared with the as-cast microstructure (prepared by vacuum arc melting), the microstructure of Ni 35 Co 35 Cr 25 Ti 3 Al 2 precipitation-strengthened medium-entropy alloy prepared by laser selective melting deposition is more fine and uniform. Example 1 Selected laser selective melting Ni 35 Co 35 Cr 25 Ti 3 Al 2 medium entropy alloy (SLM) formed by the optimal process parameters has a room temperature yield strength of 671 MPa, a tensile strength of 913 MPa, an elongation of 36%, and a hardness of 671 MPa. is 310HV. Its strength is much higher than that of the as-cast state, and the tensile plasticity is comparable to that of the as-cast state, as shown in Figure 5, where the yield strength of the entropy alloy as-cast (Cast) in Ni 35 Co 35 Cr 25 Ti 3 Al 2 is 342MPa, and the tensile strength is 648MPa, and the elongation is 38%.

5、激光选区熔化成形Ni35Co35Cr25Ti3Al2中熵合金热处理5. Laser selective melting forming Ni 35 Co 35 Cr 25 Ti 3 Al 2 medium entropy alloy heat treatment

通过时效处理促进激光选区熔化成形Ni35Co35Cr25Ti3Al2中熵合金析出相的产生从而实现进一步的强韧化。在本发明中,所述热处理的方式包括,将采用最优激光选区熔化参数成形的Ni35Co35Cr25Ti3Al2中熵合金升温至600℃~800℃保温,所选时间为12h≤t≤480h,保温结束后水冷,得到热处理后的中熵合金。Through aging treatment, the formation of entropy alloy precipitates in Ni 35 Co 35 Cr 25 Ti 3 Al 2 by laser selective melting is promoted to achieve further strengthening and toughening. In the present invention, the heat treatment method includes heating the Ni 35 Co 35 Cr 25 Ti 3 Al 2 medium entropy alloy formed by the optimal laser selective melting parameters to 600℃~800℃ for heat preservation, and the selected time is 12h≤ t≤480h, water cooling after heat preservation to obtain a medium entropy alloy after heat treatment.

具体进行三组实验,一组实验中,在600℃热处理12h,另一组实验中,在700℃热处理12h,再一组实验中,在700℃热处理480h。Specifically, three sets of experiments were carried out. In one set of experiments, heat treatment was performed at 600 °C for 12 h, in another set of experiments, heat treatment at 700 °C for 12 h, and in another set of experiments, heat treatment at 700 °C for 480 h.

图6为激光选区熔化成形Ni35Co35Cr25Ti3Al2中熵合金经600℃/12h热处理后的扫描电镜图片(a)和透射电镜选区电子衍射图(b),从图6(a)中可以观察到沉积态组织发生了部分再结晶,图6(b)中可同时观察到FCC相和γ'析出相的衍射斑点。对激光选区熔化成形Ni35Co35Cr25Ti3Al2中熵合金热处理样品进行室温拉伸性能测试,结果如图7所示,结果表明,热处理后强度大幅度提高,沉积态经700℃/480h热处理后屈服强度可达到1098MPa,抗拉强度为1466MPa,延伸率为25%,该室温拉伸性能是迄今为止激光增材制造高/中熵合金的最高水平。Figure 6 shows the SEM image (a) and TEM image (b) of the SEM image (a) and TEM image (b) of the Ni 35 Co 35 Cr 25 Ti 3 Al 2 medium entropy alloy formed by laser selective melting and heat treatment at 600 °C for 12 h. From Figure 6 (a) ), partial recrystallization of the deposited structure can be observed, and diffraction spots of the FCC phase and the γ' precipitation phase can be observed simultaneously in Fig. 6(b). The tensile properties of the Ni 35 Co 35 Cr 25 Ti 3 Al 2 medium-entropy alloy heat-treated samples formed by laser selective melting were tested at room temperature. The results are shown in Figure 7. The results show that the strength is greatly improved after heat treatment. After 480h heat treatment, the yield strength can reach 1098MPa, the tensile strength is 1466MPa, and the elongation is 25%.

实施例2Example 2

一种适用于激光增材制造的析出强化型中熵合金,该中熵合金的化学式为Ni35Co35Cr25Ti3Al2;其中,各元素的比例为摩尔百分比。所选用中熵合金为气雾化预合金球形粉末,纯度大于99.9%。A precipitation-strengthening medium-entropy alloy suitable for laser additive manufacturing, the chemical formula of the medium-entropy alloy is Ni 35 Co 35 Cr 25 Ti 3 Al 2 , wherein the ratio of each element is a mole percentage. The selected medium-entropy alloy is gas atomized pre-alloyed spherical powder with a purity greater than 99.9%.

本实施例2采用激光立体成形技术制备中熵合金成形过程如下:The present embodiment 2 adopts the laser three-dimensional forming technology to prepare the entropy alloy forming process as follows:

1、中熵合金粉末制备及预处理1. Preparation and pretreatment of medium entropy alloy powder

将根据所述中熵合金名义化学成分中的各元素摩尔比进行配比,采用真空气雾化法制备中熵合金预合金球形粉末,将预合金球形粉末进行过筛,选用粉末粒径为45-150μm,其典型形貌如图8所示。氧含量为131ppm,氮含量为53ppm。进行激光立体成形实验前,将粉末烘干处理以避免粉末中吸附的水分对材料成形产生的影响,随后将粉末放置于激光立体成形设备送粉器内。According to the molar ratio of each element in the nominal chemical composition of the medium-entropy alloy, the medium-entropy alloy pre-alloy spherical powder is prepared by the vacuum air atomization method, and the pre-alloy spherical powder is sieved, and the powder particle size is 45. -150 μm, and its typical morphology is shown in Figure 8. The oxygen content was 131 ppm and the nitrogen content was 53 ppm. Before the laser three-dimensional forming experiment, the powder was dried to avoid the influence of moisture adsorbed in the powder on the material forming, and then the powder was placed in the powder feeder of the laser three-dimensional forming equipment.

2、基板表面处理2. Substrate surface treatment

选取316L不锈钢基板,将待沉积面打磨,并依次用丙酮和酒精清洗以去除表面油污,随后吹干,将基板固定夹在成型平台。A 316L stainless steel substrate was selected, the surface to be deposited was polished, and washed with acetone and alcohol in turn to remove the surface oil, and then dried, and the substrate was fixed and clamped on the forming platform.

3、激光立体成形Ni35Co35Cr25Ti3Al2析出强化型中熵合金3. Laser three-dimensional forming of Ni 35 Co 35 Cr 25 Ti 3 Al 2 precipitation-strengthened medium-entropy alloys

根据中熵合金构件的几何形状在计算机上建立三维实体模型并转换为STL格式传送到激光成形设备,设置打印工艺参数及激光扫描路径,在数控系统的控制下,中熵合金粉末经同轴送粉喷嘴送至高能激光束所形成的熔池中,通过在基材上逐点、逐线、逐层沉积原材料的方式,实现特定形状及尺寸的复杂构件成形。上述激光立体成形的工艺参数如下:激光功率为2KW~3.5KW,扫描速率为300~800mm/min,送粉速度为5-8g/min,Z轴抬升量为0.4-1.0mm,搭接率为50%,光斑直径为3mm,扫描策略选择往复交织扫描,即在同一沉积层,扫描路径呈S型,相邻沉积层,扫描方向旋转90°。上述激光立体成形过程采用高纯氩气作为保护气体和载粉气体,打印过程中氧气含量低于2000ppm。According to the geometric shape of the medium-entropy alloy component, a three-dimensional solid model is established on the computer, converted into STL format and sent to the laser forming equipment, and the printing process parameters and laser scanning path are set. The powder nozzle is sent to the molten pool formed by the high-energy laser beam, and the formation of complex components with specific shapes and sizes is realized by depositing raw materials point by point, line by line and layer by layer on the substrate. The process parameters of the above-mentioned three-dimensional laser forming are as follows: the laser power is 2KW-3.5KW, the scanning rate is 300-800mm/min, the powder feeding speed is 5-8g/min, the Z-axis lift is 0.4-1.0mm, and the lap rate is 0.4-1.0mm. 50%, the spot diameter is 3mm, and the scanning strategy selects reciprocating interleaving scanning, that is, in the same deposition layer, the scanning path is S-shaped, and the scanning direction is rotated 90° for adjacent deposition layers. The above-mentioned laser three-dimensional forming process uses high-purity argon gas as the protective gas and powder carrier gas, and the oxygen content during the printing process is less than 2000ppm.

调整激光功率、扫描速率、送粉速度、Z轴抬升量进行最优工艺探索,并打印具有不同线能量密度的块体样品,具体采用的工艺参数如表2所示。Adjust the laser power, scanning rate, powder feeding speed, and Z-axis lifting amount to explore the optimal process, and print block samples with different linear energy densities. The specific process parameters used are shown in Table 2.

表2实施例2的具体实验参数The concrete experimental parameters of table 2 embodiment 2

Figure BDA0003480584020000111
Figure BDA0003480584020000111

采用以上激光立体成形工艺参数制备了Ni35Co35Cr25Ti3Al2中熵合金块体样品,其典型宏观形貌如图9所示。对3个样品分别进行室温拉伸性能测试,结果如图10所示。通过力学性能测试结果,确定了最优的工艺参数:激光功率为2800W,扫描速度为300mm/min,送粉速度为5g/min,Z轴抬升量0.5mm,搭接率为50%。The Ni 35 Co 35 Cr 25 Ti 3 Al 2 medium entropy alloy bulk sample was prepared using the above laser stereoforming process parameters, and its typical macroscopic morphology is shown in Figure 9. The room temperature tensile properties were tested for the three samples respectively, and the results are shown in Figure 10. Through the test results of mechanical properties, the optimal process parameters are determined: the laser power is 2800W, the scanning speed is 300mm/min, the powder feeding speed is 5g/min, the Z-axis lift is 0.5mm, and the overlap ratio is 50%.

4、激光立体成形样品组织表征及性能测试4. Microstructure characterization and performance test of laser three-dimensional forming samples

采用电子背散射衍射(EBSD)和扫描电子显微镜(SEM)观察最优参数下成形样品的显微组织,如图11所示,合金成形质量较好,未观察到裂纹,孔隙,融合不良等缺陷。并且采用激光立体成形技术制备的Ni35Co35Cr25Ti3Al2中熵合金组织中存在少量的γ'纳米级析出相的产生,如图11(b)所示。采用优选的工艺参数制备的激光立体成形Ni35Co35Cr25Ti3Al2中熵合金的室温力学性能如图12所示,沿建造方向(纵向)屈服强度为723MPa,抗拉强度为1078MPa,延伸率为39%,硬度为355HV;沿扫描方向(横向)屈服强度为566MPa,抗拉强度为1011MPa,延伸率为47%,硬度为284HV。与传统铸造相比,采用激光立体成形方法所制备的Ni35Co35Cr25Ti3Al2中熵合金样品具有高的强塑性结合。Electron backscatter diffraction (EBSD) and scanning electron microscopy (SEM) were used to observe the microstructure of the formed samples under the optimal parameters. As shown in Figure 11, the alloy forming quality was good, and no defects such as cracks, pores, and poor fusion were observed. . And there is a small amount of γ' nano-scale precipitates in the entropy alloy structure of Ni 35 Co 35 Cr 25 Ti 3 Al 2 prepared by laser stereoforming technology, as shown in Figure 11(b). The room temperature mechanical properties of the laser three-dimensionally formed Ni 35 Co 35 Cr 25 Ti 3 Al 2 entropy alloy prepared with the preferred process parameters are shown in Figure 12. The yield strength along the construction direction (longitudinal direction) is 723 MPa, and the tensile strength is 1078 MPa. The elongation is 39%, the hardness is 355HV; the yield strength along the scanning direction (transverse direction) is 566MPa, the tensile strength is 1011MPa, the elongation is 47%, and the hardness is 284HV. Compared with traditional casting, the Ni 35 Co 35 Cr 25 Ti 3 Al 2 meso-entropy alloy samples prepared by laser stereoforming have high strong-plastic bonding.

5、激光立体成形Ni35Co35Cr25Ti3Al2中熵合金热处理。5. Laser three-dimensional forming Ni 35 Co 35 Cr 25 Ti 3 Al 2 entropy alloy heat treatment.

进一步通过时效处理促进激光立体成形Ni35Co35Cr25Ti3Al2中熵合金析出相的产生从而实现进一步的强韧化。在本发明中,所述热处理的方式包括,将最优工艺参数下激光立体成形的Ni35Co35Cr25Ti3Al2中熵合金升温至700℃保温,所选时间为3h,保温结束后水冷,得到热处理后的中熵合金。Further strengthening and toughening can be achieved by further promoting the generation of entropy alloy precipitates in the laser three-dimensional forming Ni 35 Co 35 Cr 25 Ti 3 Al 2 by aging treatment. In the present invention, the heat treatment method includes: heating the Ni 35 Co 35 Cr 25 Ti 3 Al 2 medium entropy alloy formed by laser three-dimensional under optimal process parameters to 700°C for heat preservation, the selected time is 3h, and after the heat preservation is completed Water-cooled to obtain a medium-entropy alloy after heat treatment.

图13显示了激光立体成形Ni35Co35Cr25Ti3Al2中熵合金经700℃/3h热处理后的高倍扫描电镜图片,可以看到,相比于原始沉积态组织,析出相的体积分数显著增加。图14显示了采用不同激光功率制备的Ni35Co35Cr25Ti3Al2中熵合金在热处理后的显微硬度变化规律。经热处理后,由于高体积分数的析出相产生,可以看到硬度明显提高,激光功率为2.8KW的样品经700℃/3h热处理后的硬度约为415HV。图15显示了激光功率为2.8KW的Ni35Co35Cr25Ti3Al2中熵合金在700℃/3h热处理后的拉伸性能,其屈服强度为808MPa,抗拉强度为1168MPa,延伸率为32%,相比于沉积态样品,由于析出相的产生,其强度有了显著的提升。Figure 13 shows the high-magnification scanning electron microscope image of the laser three-dimensionally formed Ni 35 Co 35 Cr 25 Ti 3 Al 2 medium entropy alloy after heat treatment at 700℃/3h. It can be seen that, compared with the original as-deposited structure, the volume fraction of the precipitated phase A significant increase. Figure 14 shows the microhardness variation of Ni 35 Co 35 Cr 25 Ti 3 Al 2 medium-entropy alloys prepared with different laser powers after heat treatment. After heat treatment, due to the formation of high volume fraction of precipitates, it can be seen that the hardness is significantly improved. The hardness of the sample with a laser power of 2.8KW after heat treatment at 700℃/3h is about 415HV. Figure 15 shows the tensile properties of Ni 35 Co 35 Cr 25 Ti 3 Al 2 medium entropy alloys with a laser power of 2.8KW after heat treatment at 700°C/3h, the yield strength is 808MPa, the tensile strength is 1168MPa, and the elongation is 32%, compared with the as-deposited samples, the strength is significantly improved due to the generation of precipitates.

Claims (10)

1.适用于激光增材制造的析出强化型中熵合金,其特征在于,所述析出强化型中熵合金为NiaCobCrcAldMe,其中,M为Ti、Ta、Nb和Mo中的一种或多种元素,a、b、c、d和e分别代表对应各元素的摩尔百分比,b=20%-40%,c=20%-25%,d>1%,e>0,d+e<7%,a+b+c+d+e=100%。1. A precipitation-strengthened medium-entropy alloy suitable for laser additive manufacturing, wherein the precipitation-strengthened medium-entropy alloy is Ni a Co b Cr c Al d Me , wherein M is Ti, Ta, Nb and One or more elements in Mo, a, b, c, d and e represent the mole percentage of each element respectively, b=20%-40%, c=20%-25%, d>1%, e >0, d+e<7%, a+b+c+d+e=100%. 2.权利要求1所述的适用于激光增材制造的析出强化型中熵合金的制备方法,其特征在于,采用激光选区熔化成形技术进行制备。2. The method for preparing a precipitation-strengthened medium-entropy alloy suitable for laser additive manufacturing according to claim 1, characterized in that the preparation is performed by using a laser selective melting and forming technology. 3.根据权利要求2所述的适用于激光增材制造的析出强化型中熵合金的制备方法,其特征在于,包括:3. The preparation method of a precipitation-strengthened medium-entropy alloy suitable for laser additive manufacturing according to claim 2, characterized in that, comprising: 步骤1,中熵合金粉末制备及预处理Step 1, preparation and pretreatment of medium entropy alloy powder 按照权利要求1所述摩尔百分比,取各元素对应的金属原料,采用真空气雾化法制备中熵合金预合金球形粉末,过筛,烘干,得到中熵合金粉末;According to the molar percentage of claim 1, get the metal raw material corresponding to each element, adopt the vacuum air atomization method to prepare the medium-entropy alloy pre-alloy spherical powder, sieve, and dry to obtain the medium-entropy alloy powder; 步骤2,激光选区熔化成形NiaCobCrcAldMe析出强化型中熵合金Step 2, laser selective melting to form Ni a Co b Cr c Al d Me precipitation-strengthened medium-entropy alloy 根据待制备的中熵合金构件的几何形状建立三维实体模型并转换为STL格式的文件,导入激光选区熔化成形设备的建造软件中,进行分层处理;通入高纯氩气,使成形舱室内氧气含量低于300ppm,根据所设定的激光选区熔化成形的工艺参数及扫描策略,将中熵合金粉末逐层熔化成形,制备得到中熵合金构件。According to the geometric shape of the medium-entropy alloy component to be prepared, a 3D solid model is established and converted into a file in STL format, and imported into the construction software of the laser selective melting forming equipment for layering processing; high-purity argon gas is introduced to make the forming chamber The oxygen content is lower than 300ppm. According to the set process parameters and scanning strategy of laser selective melting and forming, the medium-entropy alloy powder is melted and formed layer by layer to prepare a medium-entropy alloy component. 4.根据权利要求3所述的适用于激光增材制造的析出强化型中熵合金的制备方法,其特征在于,激光选区熔化成形的工艺参数如下:激光功率P为160~360W,扫描速率v为600~1000mm/s,扫描间距h为60-80μm,铺粉层厚t为30-50μm,光斑直径为80μm,体能量密度VED范围为140J/mm3<VED<240J/mm3,其中VED=P/vht。4. The method for preparing a precipitation-strengthened medium-entropy alloy suitable for laser additive manufacturing according to claim 3, wherein the process parameters of laser selective melting and forming are as follows: the laser power P is 160-360 W, the scanning rate v is 600~1000mm/s, the scanning distance h is 60-80μm, the thickness of the powder layer t is 30-50μm, the spot diameter is 80μm, and the volume energy density VED range is 140J/mm 3 <VED<240J/mm 3 , where VED =P/vht. 5.根据权利要求3所述的适用于激光增材制造的析出强化型中熵合金的制备方法,其特征在于,扫描策略为67°旋转扫描、往复扫描、往复交织扫描或45°旋转分区扫描。5. The preparation method of a precipitation-strengthened medium-entropy alloy suitable for laser additive manufacturing according to claim 3, wherein the scanning strategy is 67° rotation scanning, reciprocating scanning, reciprocating interweaving scanning or 45° rotation zone scanning . 6.根据权利要求3所述的适用于激光增材制造的析出强化型中熵合金的制备方法,其特征在于,还包括热处理步骤:将中熵合金构件升温至600℃~800℃保温12h≤t≤480h,保温结束后水冷,得到热处理后的中熵合金。6 . The method for preparing a precipitation-strengthened medium-entropy alloy suitable for laser additive manufacturing according to claim 3 , further comprising a heat treatment step: heating the medium-entropy alloy component to 600℃~800℃ for 12h≤ t≤480h, water cooling after the heat preservation, to obtain the medium entropy alloy after heat treatment. 7.权利要求1所述的适用于激光增材制造的析出强化型中熵合金的制备方法,其特征在于,采用激光立体成形技术进行制备。7 . The method for preparing a precipitation-strengthened medium-entropy alloy suitable for laser additive manufacturing according to claim 1 , wherein the preparation is carried out by using a laser three-dimensional forming technology. 8 . 8.根据权利要求7所述的适用于激光增材制造的析出强化型中熵合金的制备方法,其特征在于,包括:8. The preparation method of a precipitation-strengthened medium-entropy alloy suitable for laser additive manufacturing according to claim 7, characterized in that, comprising: 步骤1,中熵合金粉末制备及预处理Step 1, preparation and pretreatment of medium entropy alloy powder 按照权利要求1所述摩尔百分比,取各元素对应的金属原料,采用真空气雾化法制备中熵合金预合金球形粉末,过筛,烘干,得到中熵合金粉末;According to the molar percentage of claim 1, get the metal raw material corresponding to each element, adopt the vacuum air atomization method to prepare the medium-entropy alloy pre-alloy spherical powder, sieve, and dry to obtain the medium-entropy alloy powder; 步骤2激光立体成形NiaCobCrcAldMe析出强化型中熵合金Step 2 Laser three-dimensional forming Ni a Co b Cr c Al d Me precipitation strengthening type medium entropy alloy 根据待制备的中熵合金构件的几何形状建立三维实体模型并转换为STL格式传送到激光立体成形设备,设置打印工艺参数及激光扫描路径,将中熵合金粉末送至激光立体成形设备中高能激光束所形成的熔池中,通过在基材上逐点、逐线、逐层沉积原材料的方式,打印得到中熵合金构件。According to the geometric shape of the medium-entropy alloy component to be prepared, a three-dimensional solid model is established and converted into STL format and sent to the laser stereoforming equipment, the printing process parameters and laser scanning path are set, and the medium-entropy alloy powder is sent to the high-energy laser in the laser stereoforming equipment. In the molten pool formed by the beam, by depositing raw materials point by point, line by line and layer by layer on the substrate, the intermediate entropy alloy component is obtained by printing. 9.根据权利要求8所述的适用于激光增材制造的析出强化型中熵合金的制备方法,其特征在于,打印工艺参数如下:激光功率为2KW~3.5KW,扫描速率为300~800mm/min,送粉速度为5-8g/min,Z轴抬升量为0.4-1.0mm,搭接率为50%,光斑直径为3mm,扫描路径为往复交织扫描路径。9 . The method for preparing a precipitation-strengthened medium-entropy alloy suitable for laser additive manufacturing according to claim 8 , wherein the printing process parameters are as follows: the laser power is 2KW~3.5KW, and the scanning rate is 300~800mm/ min, the powder feeding speed is 5-8g/min, the Z-axis lift is 0.4-1.0mm, the overlap ratio is 50%, the spot diameter is 3mm, and the scanning path is a reciprocating interweaving scanning path. 10.根据权利要求8所述的适用于激光增材制造的析出强化型中熵合金的制备方法,其特征在于,还包括热处理步骤:将中熵合金构件升温至600℃~800℃保温3h≤t≤480h,保温结束后水冷,得到热处理后的中熵合金。10 . The method for preparing a precipitation-strengthened medium-entropy alloy suitable for laser additive manufacturing according to claim 8 , further comprising a heat treatment step: heating the medium-entropy alloy component to 600° C. to 800° C. for 3h≤ t≤480h, water cooling after the heat preservation, to obtain the medium entropy alloy after heat treatment.
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