CN114457272A - A kind of high entropy alloy and its laser cladding repair method of tungsten-based powder alloy die-casting mold - Google Patents
A kind of high entropy alloy and its laser cladding repair method of tungsten-based powder alloy die-casting mold Download PDFInfo
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C30/00—Alloys containing less than 50% by weight of each constituent
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22C—FOUNDRY MOULDING
- B22C3/00—Selection of compositions for coating the surfaces of moulds, cores, or patterns
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D17/00—Pressure die casting or injection die casting, i.e. casting in which the metal is forced into a mould under high pressure
- B22D17/20—Accessories: Details
- B22D17/22—Dies; Die plates; Die supports; Cooling equipment for dies; Accessories for loosening and ejecting castings from dies
- B22D17/2209—Selection of die materials
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F9/00—Making metallic powder or suspensions thereof
- B22F9/02—Making metallic powder or suspensions thereof using physical processes
- B22F9/04—Making metallic powder or suspensions thereof using physical processes starting from solid material, e.g. by crushing, grinding or milling
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- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C24/00—Coating starting from inorganic powder
- C23C24/08—Coating starting from inorganic powder by application of heat or pressure and heat
- C23C24/10—Coating starting from inorganic powder by application of heat or pressure and heat with intermediate formation of a liquid phase in the layer
- C23C24/103—Coating with metallic material, i.e. metals or metal alloys, optionally comprising hard particles, e.g. oxides, carbides or nitrides
- C23C24/106—Coating with metal alloys or metal elements only
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F9/00—Making metallic powder or suspensions thereof
- B22F9/02—Making metallic powder or suspensions thereof using physical processes
- B22F9/04—Making metallic powder or suspensions thereof using physical processes starting from solid material, e.g. by crushing, grinding or milling
- B22F2009/043—Making metallic powder or suspensions thereof using physical processes starting from solid material, e.g. by crushing, grinding or milling by ball milling
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Other Surface Treatments For Metallic Materials (AREA)
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Abstract
Description
技术领域technical field
本发明涉及一种高熵合金及其激光熔覆修复钨基粉末合金压铸模具方法,应用高能密度的激光束加热熔化高熵合金粉末并快速凝固与基体发生冶金结合在表面形成修复层,对钨基粉末合金压铸模具局部损伤表面进行修复,使模具的尺寸和功能得以恢复与重新利用并提升模具的性能,属于材料科学与工程领域。The invention relates to a high-entropy alloy and a method for repairing a tungsten-based powder alloy die-casting mold by laser cladding. A high-energy-density laser beam is used to heat and melt the high-entropy alloy powder, and the high-entropy alloy powder is rapidly solidified and metallurgically combined with a matrix to form a repair layer on the surface. The locally damaged surface of the base powder alloy die-casting mold is repaired, so that the size and function of the mold can be restored and reused, and the performance of the mold can be improved, which belongs to the field of material science and engineering.
背景技术Background technique
2004年,叶均蔚和Cantor B等研究人员率先突破传统研究的框架,提出了新的合金设计理念,即多主元高熵合金。它是由五种或五种以上元素组成,原子比为1:1或者近似1:1,每种元素的成分介于5%到35%之间。这种合金不易形成脆性金属间化合物,反而形成具有简单晶体结构的体心立方相、面心立方相、纳米结构甚至非晶结构。高熵合金热力学上具有高熵效应,结构上具有晶格畸变效应,动力学上具有迟滞扩散效应,性能上具有鸡尾酒效应,因而高熵合金具有高硬度、优异的耐磨性以及良好的耐蚀性、高温抗氧化性能、热稳定性等多种优点。高熵合金涂层的制备技术有热喷涂法、溅射法和激光熔覆等方法,热喷涂法和溅射法所制备的高熵合金薄膜厚度较小,一般为微米级,在实际应用中限制较多;激光熔覆高熵合金涂层的厚度可以达到毫米级,极大地发挥了高熵合金的力学性能优势。高熵合金的应用,尤其是其作为表面涂层时的应用,一直受到工程技术人员的关注。In 2004, researchers such as Ye Junwei and Cantor B took the lead in breaking through the traditional research framework and proposed a new alloy design concept, that is, multi-principal element high-entropy alloys. It is composed of five or more elements in an atomic ratio of 1:1 or approximately 1:1, with each element having a composition between 5% and 35%. This alloy is not prone to form brittle intermetallic compounds, but instead forms body-centered cubic, face-centered cubic, nanostructures, and even amorphous structures with simple crystal structures. High-entropy alloys have high-entropy effect in thermodynamics, lattice distortion effect in structure, hysteresis diffusion effect in kinetics, and cocktail effect in performance. Therefore, high-entropy alloys have high hardness, excellent wear resistance and good corrosion resistance. properties, high temperature oxidation resistance, thermal stability and other advantages. The preparation techniques of high-entropy alloy coatings include thermal spraying, sputtering and laser cladding. There are many restrictions; the thickness of the laser cladding high-entropy alloy coating can reach the millimeter level, which greatly exerts the advantages of the mechanical properties of the high-entropy alloy. The application of high-entropy alloys, especially as surface coatings, has always been the focus of engineers and technicians.
钨基粉末合金是一种以钨为硬质相,以镍、铜或镍、铁等为粘结相构成的复合材料,具有高导热,高强度,高密度,低热膨胀系数与优异抗蚀性、抗氧化性和抗冲击韧性等性能,是制造高精度模具和压铸模具的最佳材料之一。钨基粉末合金用于生产有色金属压铸模具,由于其超高导热性和低热膨胀系数,可以细化有色金属组织,提高有色金属压铸件的性能和尺寸精度,越来越受到行业关注。钨基粉末合金压铸模具在成型零件压铸生产过程中,融熔的有色金属液以高压、高温和高速进入模具型腔,对型腔表面产生剧烈的冲击和冲刷,导致钨基粉末合金压铸模具型腔表面产生腐蚀、磨损和裂纹;在填充过程中,金属液、杂质和熔渣对模具型腔表面也会产生复杂的化学作用,加速模具型腔表面的腐蚀、磨损和裂纹的产生;此外,在开模及脱模过程中模具与铸件间的摩擦也加剧了模具表面型腔的磨损。国内外的相关文献认为热磨损是钨基粉末合金压铸模具失效的主要原因之一。钨基粉末合金压铸模具型腔表面磨损过量将导致液态有色金属压制成型零件的尺寸超差和表面质量不合格。钨基粉末合金材料价格昂贵导致钨基粉末合金压铸模具制造成本高;同时,模具加工和制造难度大,投入生产后的模具修理和维护费用也高,因此,及时维修模具,防止模具进一步损坏,可以大大降低压铸生产的模具费用。合理的解决办法就是通过表面工程技术对模具局部损伤型腔表面进行修复,使得模具的尺寸和功能得以恢复与重新利用并提升模具表面的性能。目前,工程材料常用的表面工程技术有物理气相沉积(PVD)、化学气相沉积(CVD)、电火花沉积、堆焊、冷焊、热喷涂以及近年来开发的多种增材制造技术。用作修复层的材料多为合金或陶瓷材料。合金材料包括自熔性合金粉末如镍基、钴基和铁基合金粉末等。陶瓷材料包括碳化物、氧化物和硅化物粉末等。当前,修复钨基粉末合金压铸模具型腔工作面的磨损部位时,存在的主要问题是修复层和基体材料的化学成分和性能存在较大差异,材料相互间的兼容性和结合性较差,修复后的钨基粉末合金压铸模具在铸件生产过程中,型腔表面修复层不断受到金属液的高压、高温和高速冲刷,同时,型腔表面修复层由于吸收了融熔金属凝固过程中放出的热量,首先达到较高温度而膨胀,开模后,型腔表面修复层与空气接触激冷收缩而产生拉应力,这种交变应力反复循环,在修复层和基体材料界面结合处极易产生裂纹,随着生产次数的增加,最终导致修复层的开裂和剥落。钨基粉末合金压铸模具型腔表面修复层既是工作面又是功能面,因此,用作修复层材料必须具有与钨基粉末合金材料相近的导热性、低热膨胀系数与优异抗蚀性、抗氧化性和抗冲击韧性等性能。因此,如何提高钨基粉末合金压铸模具修复层的耐磨性和抗疲劳性及其与基体的结合强度,延长模具的使用寿命,提高模具利用率,同时还要保证表面所具有的高导热,低膨胀性能,是科研工作者不可推卸的责任和长期而艰巨的任务。Tungsten-based powder alloy is a composite material composed of tungsten as the hard phase and nickel, copper or nickel and iron as the binder phase. It has high thermal conductivity, high strength, high density, low thermal expansion coefficient and excellent corrosion resistance. , oxidation resistance and impact toughness and other properties, it is one of the best materials for manufacturing high-precision molds and die-casting molds. Tungsten-based powder alloys are used to produce non-ferrous metal die-casting molds. Due to their ultra-high thermal conductivity and low thermal expansion coefficient, they can refine non-ferrous metal structures and improve the performance and dimensional accuracy of non-ferrous metal die-casting parts. During the die-casting production of tungsten-based powder alloy die-casting molds, the molten non-ferrous metal liquid enters the mold cavity at high pressure, high temperature and high speed, causing severe impact and erosion on the surface of the cavity, resulting in tungsten-based powder alloy die-casting molds. Corrosion, wear and cracks occur on the surface of the cavity; during the filling process, molten metal, impurities and slag also have complex chemical effects on the surface of the mold cavity, accelerating the corrosion, wear and cracks on the surface of the mold cavity; in addition, The friction between the mold and the casting during the mold opening and demolding process also aggravates the wear of the mold surface cavity. Relevant literatures at home and abroad believe that thermal wear is one of the main reasons for the failure of tungsten-based powder alloy die-casting molds. Excessive wear on the cavity surface of tungsten-based powder alloy die-casting molds will lead to excessive size and unqualified surface quality of liquid non-ferrous metal pressed parts. The high price of tungsten-based powder alloy materials leads to high manufacturing costs of tungsten-based powder alloy die-casting molds; at the same time, mold processing and manufacturing are difficult, and mold repair and maintenance costs after production are also high. Therefore, timely repair of molds to prevent further damage to the mold, It can greatly reduce the mold cost of die casting production. The reasonable solution is to repair the locally damaged cavity surface of the mold through surface engineering technology, so that the size and function of the mold can be restored and reused and the performance of the mold surface can be improved. Currently, commonly used surface engineering techniques for engineering materials include physical vapor deposition (PVD), chemical vapor deposition (CVD), spark deposition, surfacing, cold welding, thermal spraying, and a variety of additive manufacturing technologies developed in recent years. The materials used for the repair layer are mostly alloys or ceramic materials. Alloy materials include self-fluxing alloy powders such as nickel-based, cobalt-based and iron-based alloy powders and the like. Ceramic materials include carbides, oxides, and silicide powders, among others. At present, when repairing the worn parts of the tungsten-based powder alloy die-casting mold cavity working surface, the main problem is that the chemical composition and properties of the repair layer and the base material are quite different, and the compatibility and bonding between the materials are poor. During the production process of the repaired tungsten-based powder alloy die-casting mold, the surface repair layer of the cavity is continuously eroded by the high pressure, high temperature and high speed of the molten metal. The heat first reaches a higher temperature and expands. After the mold is opened, the repair layer on the surface of the cavity is contacted with air and quenched and shrinks to generate tensile stress. This alternating stress circulates repeatedly and is easily generated at the interface between the repair layer and the base material. Cracks, with increasing production times, eventually lead to cracking and spalling of the repaired layer. The surface repair layer of the tungsten-based powder alloy die-casting mold cavity is both a working surface and a functional surface. Therefore, the material used for the repair layer must have similar thermal conductivity, low thermal expansion coefficient, and excellent corrosion resistance and oxidation resistance to tungsten-based powder alloy materials. performance and impact toughness. Therefore, how to improve the wear resistance and fatigue resistance of the repair layer of the tungsten-based powder alloy die-casting mold and its bonding strength with the matrix, prolong the service life of the mold, improve the utilization rate of the mold, and at the same time ensure the high thermal conductivity of the surface, Low expansion performance is an inescapable responsibility and a long-term and arduous task for scientific researchers.
发明内容SUMMARY OF THE INVENTION
本发明的目的是提供一种高熵合金及其激光熔覆修复钨基粉末合金压铸模具方法,对钨基粉末合金压铸模具型腔工作面的磨损失效的部位应用高能密度的激光束加热熔化高熵合金粉末,使其快速凝固与基体形成冶金结合,在钨基粉末合金压铸模具型腔磨损失效的表面形成耐磨耐高温高熵合金修复涂层,恢复模具尺寸和功能。The purpose of the present invention is to provide a high-entropy alloy and a method for repairing a tungsten-based powder alloy die-casting mold by laser cladding. The entropy alloy powder is rapidly solidified to form a metallurgical bond with the matrix, and a wear-resistant and high-temperature-resistant high-entropy alloy repair coating is formed on the surface of the tungsten-based powder alloy die-casting mold cavity wear and failure to restore the size and function of the mold.
本发明所述的一种高熵合金及其激光熔覆修复钨基粉末合金压铸模具方法,其核心技术是:高熵合金成分及其相关工艺和方法来调控其显微组织和结构。The core technology of a high-entropy alloy and a method for repairing a tungsten-based powder alloy die-casting mold by laser cladding described in the present invention is: high-entropy alloy composition and related processes and methods to control its microstructure and structure.
本发明所述的高熵合金化学式为CoCrFeNiWx,0.5≤x≤1,由Co,Cr,Fe,Ni和W组成,其中Co,Cr,Fe和Ni具有相同的摩尔分数,摩尔比固定为1:1:1:1,W的取值为0.5≤x≤1;成分按照原子百分比计(at%):钴(Co)20%-22.2%,铬(Cr)20%-22.2%,铁(Fe)20%-22.2%,镍(Ni)20%-22.2%,钨(W)11.1%-20%。The chemical formula of the high-entropy alloy described in the present invention is CoCrFeNiW x , 0.5≤x≤1, and is composed of Co, Cr, Fe, Ni and W, wherein Co, Cr, Fe and Ni have the same mole fraction, and the mole ratio is fixed as 1 : 1:1:1, the value of W is 0.5≤x≤1; the composition is calculated in atomic percentage (at%): cobalt (Co) 20%-22.2%, chromium (Cr) 20%-22.2%, iron ( Fe) 20%-22.2%, nickel (Ni) 20%-22.2%, tungsten (W) 11.1%-20%.
进一步地,本发明所述的高熵合金中的元素或采取Mo或Nb取代W,所述的高熵合金化学式为CoCrFeNiMo或CoCrFeNiNb。其成分中各元素的摩尔比固定为1:1:1:1:1,按照原子百分比计(at%):钴(Co)20%,铬(Cr)20%,铁(Fe)20%,镍(Ni)20%,钼(Mo)20%;或钴(Co)20%,铬(Cr)20%,铁(Fe)20%,镍(Ni)20%,铌(Nb)20%。本发明所述的高熵合金相关工艺包括两部分组成,一部分是高熵合金粉末的制备工艺;另一部分是耐磨耐高温高熵合金修复涂层的激光熔覆工艺。Further, the elements in the high-entropy alloy described in the present invention may be replaced by Mo or Nb, and the chemical formula of the high-entropy alloy is CoCrFeNiMo or CoCrFeNiNb. The molar ratio of each element in its composition is fixed at 1:1:1:1:1, in atomic percentage (at%): cobalt (Co) 20%, chromium (Cr) 20%, iron (Fe) 20%, Nickel (Ni) 20%, Molybdenum (Mo) 20%; or Cobalt (Co) 20%, Chromium (Cr) 20%, Iron (Fe) 20%, Nickel (Ni) 20%, Niobium (Nb) 20%. The high-entropy alloy related process of the present invention consists of two parts, one part is the preparation process of the high-entropy alloy powder; the other part is the laser cladding process of the wear-resistant high-entropy alloy repair coating.
进一步地,本发明所述的一种高熵合金及其激光熔覆修复钨基粉末合金压铸模具工艺和方法,是通过激光熔覆的方法制备出具有耐磨耐高温高熵合金修复涂层,包括以下步骤:Further, a high-entropy alloy and its laser cladding repairing process and method for a tungsten-based powder alloy die-casting mold described in the present invention are to prepare a high-entropy alloy repair coating with wear-resistance and high-temperature resistance by means of laser cladding, Include the following steps:
第一步,制备高熵合金粉末。所述高熵合金采用的金属Co,Cr,Fe,Ni,W,Mo和Nb的纯度均大于99.9%,金属粉末颗粒大小为20-50μm;按照设计的成分采用精度为0.0001g的电子天平按摩尔比例精确称取Co,Cr,Fe,Ni和W(Mo或Nb)金属粉放入球磨罐中,并采用三种直径分别为10mm,5mm和3mm的氧化锆球磨珠,三种球磨珠的重量比为5:3:5;将粉末混合均匀并进行真空球磨,球料比15:1,球磨转速为350r/min,球磨20h以上得到高熵合金粉末;The first step is to prepare high-entropy alloy powder. The purity of the metals Co, Cr, Fe, Ni, W, Mo and Nb used in the high-entropy alloy are all greater than 99.9%, and the particle size of the metal powder is 20-50 μm; according to the designed composition, an electronic balance with an accuracy of 0.0001g is used to massage The metal powders of Co, Cr, Fe, Ni and W (Mo or Nb) were accurately weighed and put into the ball mill jar, and three kinds of zirconia balls with diameters of 10mm, 5mm and 3mm were used. The weight ratio is 5:3:5; the powder is mixed uniformly and vacuum ball milled, the ball-to-material ratio is 15:1, the ball milling speed is 350r/min, and the ball milling is more than 20h to obtain high-entropy alloy powder;
第二步,对钨基粉末合金压铸模具型腔工作面的磨损部位进行机械处理,去除疲劳层与残余应力层,清除表面氧化物和各种污物;The second step is to mechanically treat the worn parts of the working surface of the tungsten-based powder alloy die-casting mold cavity to remove the fatigue layer and residual stress layer, and to remove surface oxides and various dirt;
第三步,将第一步制备的高熵合金粉末均匀涂覆在预处理的基体表面,形成厚度为0.8-1.2mm的预置层,采用光纤连续激光器加热高熵合金粉末,在钨基粉末合金压铸模具型腔表面得到高熵合金熔覆层,所述高能密度的光纤连续激光器,通过优化得到激光熔覆的工艺参数为:激光功率1600W,扫描速度4mm/s,光斑直径3.5mm,离焦量30mm,保护气体为氩气,气体流量15L/min。In the third step, the high-entropy alloy powder prepared in the first step is uniformly coated on the surface of the pretreated substrate to form a pre-layer with a thickness of 0.8-1.2mm, and the high-entropy alloy powder is heated by a fiber continuous laser. A high-entropy alloy cladding layer is obtained on the surface of the cavity of the alloy die-casting mold. The high-energy density fiber continuous laser, the process parameters of the laser cladding obtained by optimization are: laser power 1600W, scanning speed 4mm/s, spot diameter 3.5mm, separation distance The coke amount is 30mm, the protective gas is argon, and the gas flow is 15L/min.
高熵合金的新颖之处在于,这种合金是由多种元素以等比例或近似等比例混合而成。高熵合金的主要元素有37种,其中Co,Cr,Fe,Ni在高熵合金中应用的比例高达70%以上,可以构成480多种高熵合金系统。难熔元素如Mo,Nb,V和Zr等在高熵合金中也属于常见元素。高熵合金的种类繁多,高熵效应是调控其显微组织和结构的主要因素。合金元素数量和加工条件对其显微结构有显著的影响。高熵合金结构差异呈现出不同的结构性能和功能特点。本发明所述的一种高熵合金及其激光熔覆修复钨基粉末合金压铸模具工艺和方法,首先是采用机械合金化法,运用高能行星式球磨机制备得到所需的高熵合金粉末,之后采用高能密度的激光束在钨基粉末合金压铸模具磨损的表面形成高熵合金涂层。高熵合金涂层中的钨、铁、镍元素与基体材料相同,钴,铬,钼和铌元素与钨基粉末合金也具有较好的兼容性,保证了形成的高熵合金涂层与基体间的元素扩散及良好的冶金结合。高熵合金涂层中的铬元素保证了涂层良好的抗氧化性与抗腐蚀性,镍,钴,钼和铌元素保证了高熵合金涂层良好的高温性能;钨和钼的导热性极强,高熵合金涂层中添加钨元素或钼元素可以大幅提高涂层的热导率,从而提高压铸生产有色金属铸件的性能。本发明所述的高熵合金涂层具有很好的热稳定性、耐磨性、红硬性、导热性、抗氧化性和抗腐蚀性,与钨基粉末合金的线膨胀系数相近,同时二者之间材料相互之间的兼容性和结合性较好,在钨基粉末合金表面激光熔覆耐磨耐高温高熵合金涂层可以提高钨基粉末合金压铸模具的耐磨性和高温性能。经扫描电镜表征,耐磨耐高温高熵合金涂层的显微组织呈现典型的枝晶结构。由涂层的X射线衍射图谱鉴定物相可知,高熵合金涂层主要由体心立方固溶体(与体心立方结构的W类似)和少量的Fe-Ni面心立方固溶体组成,具有典型的高熵合金物相结构。由于高熵效应和激光快速凝固,高熵合金涂层具有较高的热稳定性,适用于在压铸有色金属过程中的工况条件。The novelty of high-entropy alloys is that they consist of a mixture of elements in equal or approximately equal proportions. There are 37 main elements of high-entropy alloys, of which Co, Cr, Fe, and Ni are used in high-entropy alloys in a proportion of more than 70%, which can form more than 480 high-entropy alloy systems. Refractory elements such as Mo, Nb, V, and Zr are also common elements in high-entropy alloys. There are many kinds of high-entropy alloys, and the high-entropy effect is the main factor regulating their microstructure and structure. The amount of alloying elements and processing conditions have a significant effect on its microstructure. The structural differences of high-entropy alloys present different structural properties and functional characteristics. A high-entropy alloy and its laser cladding repairing process and method for a tungsten-based powder alloy die-casting mold according to the present invention, firstly adopt a mechanical alloying method and a high-energy planetary ball mill to prepare the required high-entropy alloy powder, and then A high-energy-density laser beam is used to form a high-entropy alloy coating on the worn surface of a tungsten-based powder alloy die-casting die. The elements of tungsten, iron and nickel in the high-entropy alloy coating are the same as those of the base material, and cobalt, chromium, molybdenum and niobium elements also have good compatibility with the tungsten-based powder alloy, which ensures that the formed high-entropy alloy coating and the base material Elemental diffusion and good metallurgical bonding between them. The chromium element in the high-entropy alloy coating ensures the good oxidation resistance and corrosion resistance of the coating, and the nickel, cobalt, molybdenum and niobium elements ensure the good high-temperature performance of the high-entropy alloy coating; the thermal conductivity of tungsten and molybdenum is extremely high. The addition of tungsten or molybdenum to the strong, high-entropy alloy coating can greatly increase the thermal conductivity of the coating, thereby improving the performance of die-casting to produce non-ferrous metal castings. The high-entropy alloy coating of the present invention has good thermal stability, wear resistance, red hardness, thermal conductivity, oxidation resistance and corrosion resistance, and is similar to the linear expansion coefficient of tungsten-based powder alloy. The compatibility and bonding between the materials are good. Laser cladding the wear-resistant, high-temperature, high-entropy alloy coating on the surface of the tungsten-based powder alloy can improve the wear resistance and high-temperature performance of the tungsten-based powder alloy die-casting mold. Characterized by scanning electron microscopy, the microstructure of the wear-resistant high-entropy alloy coating exhibits a typical dendritic structure. It can be seen from the phase identification of the X-ray diffraction pattern of the coating that the high-entropy alloy coating is mainly composed of a body-centered cubic solid solution (similar to W in a body-centered cubic structure) and a small amount of Fe-Ni face-centered cubic solid solution, with a typical high Entropy alloy phase structure. Due to the high-entropy effect and rapid laser solidification, the high-entropy alloy coating has high thermal stability and is suitable for working conditions in the process of die-casting non-ferrous metals.
与现有技术相比,本发明的有益效果是:Compared with the prior art, the beneficial effects of the present invention are:
本发明所述的一种高熵合金及其激光熔覆修复钨基粉末合金压铸模具工艺和方法,利用高能密度的激光束在钨基粉末合金磨损表面形成的耐磨、耐高温高熵合金修复涂层,与钨基粉末合金的线膨胀系数相近,二者相互之间的兼容性和结合性较好;同时具有较高的热导率,且热扩散率值随着温度的增加而增加。A high-entropy alloy and its laser cladding repair process and method for a tungsten-based powder alloy die-casting mold described in the present invention utilize a high-energy-density laser beam to repair the wear-resistant, high-temperature-resistant high-entropy alloy formed on the wear surface of the tungsten-based powder alloy The coating has a similar linear expansion coefficient with that of tungsten-based powder alloys, and the compatibility and bonding between the two are good; at the same time, it has high thermal conductivity, and the thermal diffusivity value increases with the increase of temperature.
附图说明Description of drawings
图1是钨基粉末合金表面激光熔覆高熵合金涂层结合界面的扫描电镜照片(SEM);Fig. 1 is a scanning electron microscope (SEM) photograph of the bonding interface of the laser cladding high-entropy alloy coating on the surface of the tungsten-based powder alloy;
图2是钨基粉末合金表面激光熔覆高熵合金涂层的扫描电镜照片(SEM);Fig. 2 is the scanning electron microscope (SEM) of the laser cladding high-entropy alloy coating on the surface of the tungsten-based powder alloy;
图3是钨基粉末合金表面激光熔覆高熵合金涂层X射线衍射图谱(XRD)。Figure 3 is the X-ray diffraction pattern (XRD) of the laser cladding high-entropy alloy coating on the surface of the tungsten-based powder alloy.
具体实施方式Detailed ways
下面将结合附图对本发明的技术方案进行清楚、完整地描述,显然,所描述的实施例是本发明一部分实施例,而不是全部的实施例。下面列举的实施例仅为对本发明技术方案的进一步理解和实施,并不构成对本发明权利要求的进一步限定,因此。基于本发明中的实施例,本领域普通技术人员在没有做出创造性劳动前提下所获得的所有其他实施例,都属于本发明保护的范围。The technical solutions of the present invention will be clearly and completely described below with reference to the accompanying drawings. Obviously, the described embodiments are a part of the embodiments of the present invention, but not all of the embodiments. The examples listed below are only for further understanding and implementation of the technical solutions of the present invention, and do not constitute further limitations on the claims of the present invention, therefore. Based on the embodiments of the present invention, all other embodiments obtained by those of ordinary skill in the art without creative efforts shall fall within the protection scope of the present invention.
通过以下给出的实施例对本发明方法作进一步具体阐述。The method of the present invention is further explained in detail by the examples given below.
本发明所述的一种高熵合金及其激光熔覆修复钨基粉末合金压铸模具工艺和方法,是在钨基粉末合金压铸模具型腔工作面的磨损失效的部位应用高能密度的激光束加热熔化高熵合金粉末,使其快速凝固与基体形成冶金结合,在钨基粉末合金压铸模具磨损表面形成耐磨、耐高温高熵合金修复涂层,使得模具恢复尺寸和功能。耐磨、耐高温高熵合金涂层化学式为CoCrFeNiWx,0.5≤x≤1,由Co,Cr,Fe,Ni和W组成,其中Co,Cr,Fe和Ni具有相同的摩尔分数,W的取值为0.5≤x≤1。本发明所述的高熵合金中的元素或采取Mo或Nb取代W。The high-entropy alloy and its laser cladding repairing process and method for a tungsten-based powder alloy die-casting mold according to the present invention are the application of high-energy-density laser beam heating to the wear failure of the working surface of the tungsten-based powder alloy die-casting mold cavity. The high-entropy alloy powder is melted and rapidly solidified to form a metallurgical bond with the matrix, and a wear-resistant and high-temperature-resistant high-entropy alloy repair coating is formed on the worn surface of the tungsten-based powder alloy die-casting mold, so that the mold can recover its size and function. The chemical formula of the wear-resistant and high-temperature-resistant high-entropy alloy coating is CoCrFeNiW x , 0.5≤x≤1, composed of Co, Cr, Fe, Ni and W, wherein Co, Cr, Fe and Ni have the same mole fraction, and the value of W The value is 0.5≤x≤1. The element in the high-entropy alloy described in the present invention may take Mo or Nb to replace W.
本发明所述的一种高熵合金及其激光熔覆修复钨基粉末合金压铸模具工艺和方法,是通过激光熔覆的方法制备出具有耐磨耐高温高熵合金修复涂层,包括以下步骤:A high-entropy alloy and its laser cladding repairing process and method for a tungsten-based powder alloy die-casting mold described in the present invention are to prepare a high-entropy alloy repair coating with wear resistance and high temperature resistance by means of laser cladding, including the following steps :
第一步,制备高熵合金粉末。所述高熵合金采用的金属Co,Cr,Fe,Ni,W,Mo和Nb的纯度均大于99.9%,金属粉末颗粒大小为20-50μm;按照设计的成分采用精度为0.0001g的电子天平按摩尔比例精确称取Co,Cr,Fe,Ni和W(Mo或Nb)金属粉放入球磨罐中,并采用三种直径分别为10mm,5mm和3mm的氧化锆球磨珠,三种球磨珠的重量比为5:3:5;将粉末混合均匀并进行真空球磨,球料比15:1,球磨转速为350r/min,球磨20h以上得到高熵合金粉末;The first step is to prepare high-entropy alloy powder. The purity of the metals Co, Cr, Fe, Ni, W, Mo and Nb used in the high-entropy alloy are all greater than 99.9%, and the particle size of the metal powder is 20-50 μm; according to the designed composition, an electronic balance with an accuracy of 0.0001g is used to massage The metal powders of Co, Cr, Fe, Ni and W (Mo or Nb) were accurately weighed and put into the ball mill jar, and three kinds of zirconia balls with diameters of 10mm, 5mm and 3mm were used. The weight ratio is 5:3:5; the powder is mixed uniformly and vacuum ball milled, the ball-to-material ratio is 15:1, the ball milling speed is 350r/min, and the ball milling is more than 20h to obtain high-entropy alloy powder;
第二步,对钨基粉末合金压铸模具型腔工作面的磨损部位进行机械处理,去除疲劳层与残余应力层,清除表面氧化物和各种污物;The second step is to mechanically treat the worn parts of the working surface of the tungsten-based powder alloy die-casting mold cavity to remove the fatigue layer and residual stress layer, and to remove surface oxides and various dirt;
第三步,将第一步制备的高熵合金粉末均匀涂覆在预处理的基体表面,形成厚度为0.8-1.2mm的预置层,采用光纤连续激光器加热高熵合金粉末,在钨基粉末合金压铸模具型腔表面得到高熵合金熔覆层,所述高能密度的光纤连续激光器,通过优化得到激光熔覆的工艺参数为:激光功率1600W,扫描速度4mm/s,光斑直径3.5mm,离焦量30mm,保护气体为氩气,气体流量15L/min。In the third step, the high-entropy alloy powder prepared in the first step is uniformly coated on the surface of the pretreated substrate to form a pre-layer with a thickness of 0.8-1.2mm, and the high-entropy alloy powder is heated by a fiber continuous laser. A high-entropy alloy cladding layer is obtained on the surface of the cavity of the alloy die-casting mold. The high-energy density fiber continuous laser, the process parameters of the laser cladding obtained by optimization are: laser power 1600W, scanning speed 4mm/s, spot diameter 3.5mm, separation distance The coke amount is 30mm, the protective gas is argon, and the gas flow is 15L/min.
本发明所述的一种高熵合金及其激光熔覆修复钨基粉末合金压铸模具工艺和方法,下述所有实施例均采用上述高熵合金涂层成分以及工艺步骤和参数得到的。本发明所述的钨基粉末合金,其成分按质量百分比计(Wt%):W:97,N:2.1,Fe:0.9。A high-entropy alloy and its laser cladding process and method for repairing a tungsten-based powder alloy die-casting mold according to the present invention, all the following examples are obtained by using the above-mentioned high-entropy alloy coating composition, process steps and parameters. The composition of the tungsten-based powder alloy of the present invention is calculated by mass percentage (Wt%): W: 97, N: 2.1, Fe: 0.9.
实施例见下表1。Examples are shown in Table 1 below.
本发明所述的一种高熵合金及其激光熔覆修复钨基粉末合金压铸模具工艺和方法,按照上述工艺步骤和成分进行钨基粉末合金压铸模具修复所达到的技术指标:A high-entropy alloy and its laser cladding repairing process and method for a tungsten-based powder alloy die-casting mold according to the present invention, the technical indicators achieved by repairing a tungsten-based powder alloy die-casting mold according to the above-mentioned process steps and components:
(1)修复后形成的高熵合金涂层的硬度是钨基粉末合金基体的1.3-1.9倍;(1) The hardness of the high-entropy alloy coating formed after repair is 1.3-1.9 times that of the tungsten-based powder alloy matrix;
(2)修复后形成的高熵合金涂层在800℃保温12h后硬度是钨基粉末合金基体的1.2-1.8倍;(2) The hardness of the high-entropy alloy coating formed after the repair is 1.2-1.8 times that of the tungsten-based powder alloy matrix after being kept at 800 °C for 12 hours;
(3)修复后形成的高熵合金涂层相对耐磨性是钨基粉末合金基体的1.4-1.8倍。(3) The relative wear resistance of the high-entropy alloy coating formed after repair is 1.4-1.8 times that of the tungsten-based powder alloy matrix.
表1 涂层合金成分及其性能指标Table 1 Coating alloy composition and its performance index
尽管本发明的实施方案已公开如上,但其并不仅仅限于说明书和实施方式中所列运用。它完全可以被适用于各种适合本发明的领域。对于熟悉本领域的人员而言,可容易地实现另外的修改。因此在不背离权利要求及等同范围所限定的一般概念下,本发明并不限于特定的细节和这里示出与描述的图例。Although embodiments of the present invention have been disclosed above, they are not limited to the applications set forth in the specification and embodiments. It can be fully adapted to various fields suitable for the present invention. Additional modifications can readily be implemented by those skilled in the art. Therefore, the invention is not to be limited to the specific details and illustrations herein shown and described, without departing from the general concept defined by the appended claims and the scope of equivalents.
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Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN116145004A (en) * | 2022-12-30 | 2023-05-23 | 贵州大学 | High-density crack-free Al-containing high-entropy alloy and laser additive manufacturing method thereof |
CN116657018A (en) * | 2023-06-12 | 2023-08-29 | 济南大学 | High-entropy alloy layer and its preparation method |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN108018548A (en) * | 2017-12-06 | 2018-05-11 | 吉林大学 | One kind repairs tungsten base powder alloy die casting coating alloy and preparation method thereof |
CN111850544A (en) * | 2020-06-22 | 2020-10-30 | 昆明理工大学 | A kind of high entropy alloy coating and preparation method thereof |
CN112226766A (en) * | 2020-11-18 | 2021-01-15 | 中国兵器科学研究院宁波分院 | Preparation method of high-entropy alloy powder laser cladding layer |
CN112663049A (en) * | 2020-12-04 | 2021-04-16 | 安徽工业大学 | High-temperature-wear-resistant carbide composite high-entropy alloy and laser cladding preparation method thereof |
CN113564595A (en) * | 2021-08-27 | 2021-10-29 | 三一石油智能装备有限公司 | Disordered alloy coating reinforced valve seat, preparation method thereof and pump |
-
2022
- 2022-02-11 CN CN202210127397.5A patent/CN114457272A/en active Pending
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN108018548A (en) * | 2017-12-06 | 2018-05-11 | 吉林大学 | One kind repairs tungsten base powder alloy die casting coating alloy and preparation method thereof |
CN111850544A (en) * | 2020-06-22 | 2020-10-30 | 昆明理工大学 | A kind of high entropy alloy coating and preparation method thereof |
CN112226766A (en) * | 2020-11-18 | 2021-01-15 | 中国兵器科学研究院宁波分院 | Preparation method of high-entropy alloy powder laser cladding layer |
CN112663049A (en) * | 2020-12-04 | 2021-04-16 | 安徽工业大学 | High-temperature-wear-resistant carbide composite high-entropy alloy and laser cladding preparation method thereof |
CN113564595A (en) * | 2021-08-27 | 2021-10-29 | 三一石油智能装备有限公司 | Disordered alloy coating reinforced valve seat, preparation method thereof and pump |
Non-Patent Citations (1)
Title |
---|
ROUZBEH MAYAHI: ""A theoretical investigation on A theoretical investigation on deformation behavior and phase prediction of CoCrFeNi-based high entropy alloys"", 《MATERIALS TODAY COMMUNICATIONS》 * |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN116145004A (en) * | 2022-12-30 | 2023-05-23 | 贵州大学 | High-density crack-free Al-containing high-entropy alloy and laser additive manufacturing method thereof |
CN116145004B (en) * | 2022-12-30 | 2024-05-28 | 贵州大学 | High-density crack-free Al-containing high-entropy alloy and laser additive manufacturing method thereof |
CN116657018A (en) * | 2023-06-12 | 2023-08-29 | 济南大学 | High-entropy alloy layer and its preparation method |
CN116657018B (en) * | 2023-06-12 | 2024-11-01 | 济南大学 | High-entropy alloy layer piece and preparation method thereof |
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