CN108247053A - A kind of method that 3D printing prepares complex-shaped composite material hot-work die - Google Patents
A kind of method that 3D printing prepares complex-shaped composite material hot-work die Download PDFInfo
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- 239000002131 composite material Substances 0.000 title claims abstract description 42
- 238000010146 3D printing Methods 0.000 title claims abstract description 25
- 238000000034 method Methods 0.000 title claims abstract description 15
- 239000000843 powder Substances 0.000 claims abstract description 81
- 229910000831 Steel Inorganic materials 0.000 claims abstract description 54
- 239000010959 steel Substances 0.000 claims abstract description 54
- 239000000919 ceramic Substances 0.000 claims abstract description 22
- 238000007639 printing Methods 0.000 claims abstract description 15
- 239000000463 material Substances 0.000 claims abstract description 13
- 239000000203 mixture Substances 0.000 claims abstract description 6
- 230000008676 import Effects 0.000 claims description 10
- 238000002360 preparation method Methods 0.000 abstract description 2
- 238000000498 ball milling Methods 0.000 abstract 2
- 238000005498 polishing Methods 0.000 abstract 1
- 239000010410 layer Substances 0.000 description 27
- 238000005516 engineering process Methods 0.000 description 12
- 239000002105 nanoparticle Substances 0.000 description 8
- 239000002184 metal Substances 0.000 description 6
- 238000004519 manufacturing process Methods 0.000 description 4
- 238000001465 metallisation Methods 0.000 description 4
- 238000003854 Surface Print Methods 0.000 description 3
- 239000011159 matrix material Substances 0.000 description 3
- 238000001816 cooling Methods 0.000 description 2
- 238000004512 die casting Methods 0.000 description 2
- 230000004927 fusion Effects 0.000 description 2
- 229910001338 liquidmetal Inorganic materials 0.000 description 2
- 238000002844 melting Methods 0.000 description 2
- 230000008018 melting Effects 0.000 description 2
- 239000002245 particle Substances 0.000 description 2
- 239000007787 solid Substances 0.000 description 2
- 238000005728 strengthening Methods 0.000 description 2
- 230000007704 transition Effects 0.000 description 2
- 238000009736 wetting Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000005266 casting Methods 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000000151 deposition Methods 0.000 description 1
- 230000008021 deposition Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005242 forging Methods 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 238000001192 hot extrusion Methods 0.000 description 1
- 238000007731 hot pressing Methods 0.000 description 1
- 230000003647 oxidation Effects 0.000 description 1
- 238000007254 oxidation reaction Methods 0.000 description 1
- 238000003672 processing method Methods 0.000 description 1
- 230000002787 reinforcement Effects 0.000 description 1
- 238000000110 selective laser sintering Methods 0.000 description 1
- 239000002344 surface layer Substances 0.000 description 1
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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
- B22F10/00—Additive manufacturing of workpieces or articles from metallic powder
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- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F10/00—Additive manufacturing of workpieces or articles from metallic powder
- B22F10/20—Direct sintering or melting
- B22F10/28—Powder bed fusion, e.g. selective laser melting [SLM] or electron beam melting [EBM]
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- B—PERFORMING OPERATIONS; TRANSPORTING
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- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F1/00—Metallic powder; Treatment of metallic powder, e.g. to facilitate working or to improve properties
- B22F1/17—Metallic particles coated with metal
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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
- B22F7/00—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression
- B22F7/02—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite layers
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- B—PERFORMING OPERATIONS; TRANSPORTING
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- B33Y10/00—Processes of additive manufacturing
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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
- B22F10/00—Additive manufacturing of workpieces or articles from metallic powder
- B22F10/60—Treatment of workpieces or articles after build-up
- B22F10/66—Treatment of workpieces or articles after build-up by mechanical means
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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
- B22F10/00—Additive manufacturing of workpieces or articles from metallic powder
- B22F10/60—Treatment of workpieces or articles after build-up
- B22F10/68—Cleaning or washing
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
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Abstract
本发明涉及一种3D打印制备形状复杂复合材料热作模具的方法,属于模具制备技术领域。首先将纳米Ni粉和纳米TiC陶瓷粉混合球磨,然后加入H3钢粉球磨得到复合材料;利用绘图软件绘制所需空间结构的立体模型,将H3钢粉倒入3D打印机中,打印出形状复杂的模具雏形在模具型腔处预留20mm的未打印余量,暂停打印设备,更换钢粉为Ni粉再将普通纯Ni粉在模具雏形模具型腔处且位于热作模具钢材料内部表面打印一层;暂停打印设备,将Ni粉更换为复合材料继续在打印好的纯Ni层表面打印,将成型的模具件进行清粉,刮研,打磨处理,对模具进行精抛处理得到形状复杂复合材料热作模具。本发明制备得到的形状复杂复合材料热作模具组织均匀,模具性能良好。
The invention relates to a method for preparing a complex-shaped composite material hot-working mold by 3D printing, and belongs to the technical field of mold preparation. First, mix nano-Ni powder and nano-TiC ceramic powder for ball milling, and then add H3 steel powder for ball milling to obtain a composite material; use drawing software to draw a three-dimensional model of the required space structure, pour H3 steel powder into a 3D printer, and print out a complex shape The mold prototype reserves 20mm unprinted margin at the mold cavity, suspends the printing equipment, replaces the steel powder with Ni powder, and then prints ordinary pure Ni powder on the mold cavity of the mold prototype and is located on the inner surface of the hot work mold steel material. layer; suspend the printing equipment, replace the Ni powder with a composite material and continue printing on the surface of the printed pure Ni layer, clean the formed mold parts, scrape and grind, and polish the mold, and perform fine polishing on the mold to obtain a composite material with complex shapes Hot work mold. The complex-shaped composite material prepared by the invention has uniform hot-working mold structure and good mold performance.
Description
技术领域technical field
本发明涉及一种3D打印制备形状复杂复合材料热作模具的方法,属于模具制备技术领域。The invention relates to a method for preparing a complex-shaped composite material hot-working mold by 3D printing, and belongs to the technical field of mold preparation.
背景技术Background technique
“现代工业,模具领先”已成为制造行业的共识,模具工业水平的高低己成为衡量国家制造业水平的重要标志之一。使热态金属或液态金属成形的模具用钢就是热作模具钢。热作模具钢包括热锻模、热挤压模具和压铸模。热作模具的工作情况是与热金属接触使炽热的固态金属发生塑性变形或者是使高温液态金属压铸成形。热作模具钢的工作条件恶劣,需要热作模具钢除了有足够的高温硬度和高温强度,还需要良好的高温耐磨性和断裂韧性。"Modern industry, mold leading" has become the consensus of the manufacturing industry, and the level of the mold industry has become one of the important symbols to measure the level of the country's manufacturing industry. The steel used for the mold that makes hot metal or liquid metal into shape is hot work mold steel. Hot work die steels include hot forging dies, hot extrusion dies and die casting dies. The working condition of the hot work mold is to contact the hot metal to plastically deform the hot solid metal or to die-cast the high-temperature liquid metal. The working conditions of hot work die steel are harsh. In addition to sufficient high temperature hardness and high temperature strength, hot work die steel also needs good high temperature wear resistance and fracture toughness.
随着科学技术日新月异的发展,2012年英国著名杂志《经济学人》制作专题并指出,全球工业正在经历第三次工业革命。而3D打印技术被作为“第三次工业革命的重要标志”,因为其是具有前沿性、先导性的新兴技术。目前,市场上3D打印快速成形技术使用的方法有很多种,比较主流的方法包括光固化立体成形SLA、分层实体制造 LOM、选择性激光烧结SLS、熔积成形FDM、激光选区熔融SLM等。With the rapid development of science and technology, the famous British magazine "The Economist" produced a special topic in 2012 and pointed out that the global industry is experiencing the third industrial revolution. And 3D printing technology is regarded as "an important symbol of the third industrial revolution" because it is a cutting-edge and leading emerging technology. At present, there are many methods used in 3D printing rapid prototyping technology on the market. The more mainstream methods include stereolithography SLA, layered solid manufacturing LOM, selective laser sintering SLS, fusion deposition modeling FDM, laser selective melting SLM, etc.
热作模具钢的失效主要是热裂纹和热疲劳,首先是从表面开始的,每个热做模具都会出现热裂,即在模具表面逐步形成的细小的网状裂纹,经一定次数的冲击后,裂纹变粗,使得铸件表面光洁度不能满足要求,这个时候模具就报废了,是模具的一种疲劳过程。The failure of hot work die steel is mainly due to thermal cracks and thermal fatigue. First, it starts from the surface. Every hot work die will have hot cracks, that is, small network cracks gradually formed on the surface of the die. After a certain number of impacts , the cracks become thicker, so that the surface finish of the casting cannot meet the requirements. At this time, the mold is scrapped, which is a fatigue process of the mold.
如何制备高温耐磨高温模具材料是个问题。How to prepare high-temperature wear-resistant high-temperature mold materials is a problem.
随着近年来3D打印技术的发展使得模具组织均匀,得到质量优质的工件,激光选区熔融金属粉的快速成形技术,能直接成形出完整的金属零件,便于制造复杂形状的模具。With the development of 3D printing technology in recent years, the mold structure is uniform and high-quality workpieces are obtained. The rapid prototyping technology of laser selective melting metal powder can directly form complete metal parts, which is convenient for manufacturing complex-shaped molds.
发明内容Contents of the invention
针对上述现有技术存在的问题及不足,提供一种3D打印制备形状复杂复合材料热作模具的方法。本发明的复杂复合材料热作模具的模具型腔内部表面打印一层TiC颗粒增强钢基复合材料,其具有有高硬度、高强度、高模量、高的断裂韧性以及耐高温磨损以及耐高温氧化性能优良的综合机械性能,而成为最有潜质的高温耐磨高温模具材料。而由于TiC颗粒作为钢基体中作为一种强化相,基体与增强相之间良好的界面结合。是复合材料能充分发挥良好力学作用的有力保证。在纳米级的TiC粉末表层黏着一层纳米级Ni粉可以通过激光的高温作用改变两者的润湿角,提高TiC颗粒与钢基体间的润湿性同时又可以使形成的复合材料表面层更加致密。Aiming at the problems and deficiencies in the above-mentioned prior art, a method for preparing hot-working molds of composite materials with complex shapes by 3D printing is provided. A layer of TiC particle-reinforced steel-based composite material is printed on the inner surface of the mold cavity of the complex composite hot-working mold of the present invention, which has high hardness, high strength, high modulus, high fracture toughness, high temperature wear resistance and high temperature resistance Excellent oxidation performance and comprehensive mechanical properties, and become the most potential high-temperature wear-resistant high-temperature mold material. And because TiC particles act as a strengthening phase in the steel matrix, there is a good interfacial bond between the matrix and the strengthening phase. It is a powerful guarantee that the composite material can give full play to its good mechanical effect. Adhering a layer of nano-sized Ni powder on the surface of the nano-sized TiC powder can change the wetting angle of the two through the high temperature of the laser, improve the wettability between the TiC particles and the steel matrix, and at the same time make the surface layer of the composite material formed more clear. Dense.
一种3D打印制备形状复杂复合材料热作模具的方法,其具体步骤如下:A method for 3D printing to prepare a complex-shaped composite material hot-working mold, the specific steps of which are as follows:
步骤1、首先将纳米Ni粉和纳米TiC陶瓷粉按体积比为85~95:5~15混合球磨8~10h,再静置10~12h得到表面黏着Ni的纳米级TiC陶瓷粉;然后向面黏着Ni的纳米级TiC陶瓷粉按照体积比为5~15:85~95加入H3钢粉球磨30~90min,再静置6~8h得到复合材料;Step 1. First mix nano-Ni powder and nano-TiC ceramic powder with a volume ratio of 85-95:5-15 and ball mill for 8-10 hours, and then stand for 10-12 hours to obtain nano-scale TiC ceramic powder with Ni adhered to the surface; The nanoscale TiC ceramic powder adhered to Ni is added with H3 steel powder ball milled for 30-90 minutes according to the volume ratio of 5-15:85-95, and then left to stand for 6-8 hours to obtain a composite material;
步骤2、利用绘图软件绘制所需空间结构的立体模型,然后导入分层软件中进行分层,根据打印的热作模具钢材料确定3D打印的加工参数,生成运行轨迹代码,导入同轴送分3D打印机中,将H3钢粉倒入3D打印机中,打印出形状复杂的模具雏形在模具型腔处预留20mm的未打印余量,暂停打印设备,更换钢粉为Ni粉再将普通纯Ni粉在模具雏形模具型腔处且位于热作模具钢材料内部表面打印一层,层厚为5mm;暂停打印设备,将Ni粉更换为步骤1的复合材料继续在打印好的纯Ni层表面打印,层厚为15mm,将成型的模具件进行清粉,刮研,打磨处理,对模具进行精抛处理得到形状复杂复合材料热作模具。Step 2. Use the drawing software to draw the three-dimensional model of the required space structure, and then import it into the layering software for layering. Determine the processing parameters of 3D printing according to the printed hot work die steel material, generate the running track code, and import it into the coaxial feeding point. In the 3D printer, pour H3 steel powder into the 3D printer, print out the prototype of the mold with complex shape, reserve 20mm unprinted margin at the mold cavity, suspend the printing equipment, replace the steel powder with Ni powder, and then replace the ordinary pure Ni Print a layer of powder on the mold cavity of the mold prototype and on the inner surface of the hot work mold steel material, with a layer thickness of 5mm; suspend the printing equipment, replace the Ni powder with the composite material in step 1 and continue printing on the surface of the printed pure Ni layer , the thickness of the layer is 15mm, the formed mold parts are cleaned, scraped and polished, and the mold is finely polished to obtain a complex-shaped composite material hot-working mold.
所述步骤1纳米Ni粉为1200目,纳米TiC陶瓷为1000目,H3钢粉为600目。In the step 1, the nano-Ni powder is 1200 mesh, the nano-TiC ceramic is 1000 mesh, and the H3 steel powder is 600 mesh.
所述步骤2中H3钢粉、Ni粉均为600目。In the step 2, H3 steel powder and Ni powder are both 600 mesh.
上述3D打印为3D激光金属沉积技术。The above 3D printing is a 3D laser metal deposition technology.
本发明的有益效果是:The beneficial effects of the present invention are:
(1)本发明制备得到的形状复杂复合材料热作模具具由于纯Ni有较大的热导率91W/(m·K),同时有与H13钢相近的热膨胀率分别为(Ni:13.0×10-6K-1,H13钢:12.2×10-6K-1),较大的热导率可以加速复合材料层的冷却,减少应力集中,相近的热膨胀系数,不会使过度层与纯H13钢基层和复合材料层界面产生应力集中而产生裂纹。(1) The complex-shaped composite hot-working mold prepared by the present invention has a relatively large thermal conductivity of 91W/(m·K) due to pure Ni, and has a thermal expansion rate similar to that of H13 steel (Ni: 13.0× 10 -6 K -1 , H13 steel: 12.2×10 -6 K -1 ), the larger thermal conductivity can accelerate the cooling of the composite material layer, reduce stress concentration, and the similar thermal expansion coefficient will not make the excessive layer and pure The interface between the H13 steel base and the composite material layer produces stress concentration and cracks.
(2)由于模具的表面和中心,钢基与陶瓷增强体的加热或冷却速度不一致,导致体积而Ni与钢之间有小的润湿角和良好的冶金结合性,可通过3D打印技术使过度层与纯H13钢基层和复合材料层具有良好的结合能力,不会因为过度层的加入而降低模具的综合性能。同时激光选区熔融3D打印技术工艺操作简单,组织均匀,模具性能良好。(2) Due to the inconsistency of heating or cooling rates between the steel base and the ceramic reinforcement on the surface and center of the mold, resulting in volume and small wetting angle and good metallurgical bonding between Ni and steel, it can be made by 3D printing technology The transition layer has a good combination ability with the pure H13 steel base layer and the composite material layer, and the comprehensive performance of the mold will not be reduced due to the addition of the transition layer. At the same time, the laser selective fusion 3D printing technology has simple operation, uniform structure and good mold performance.
附图说明Description of drawings
图1是本发明制备得到的形状复杂复合材料热作模具剖面图。Fig. 1 is a cross-sectional view of a hot-working mold for a complex-shaped composite material prepared by the present invention.
具体实施方式Detailed ways
下面结合附图和具体实施方式,对本发明作进一步说明。The present invention will be further described below in combination with the accompanying drawings and specific embodiments.
实施例1Example 1
该3D打印制备形状复杂复合材料热作模具的方法,该复杂复合材料热作模具长宽为760mm,高为850mm,其具体步骤如下:The 3D printing method for preparing a composite hot-working mold with complex shape, the complex composite hot-working mold has a length and width of 760mm and a height of 850mm, and the specific steps are as follows:
步骤1、首先将纳米Ni粉和纳米TiC陶瓷粉按体积比为85:15混合球磨8h,再静置12h得到表面黏着Ni的纳米级TiC陶瓷粉;然后向面黏着Ni的纳米级TiC陶瓷粉按照体积比为15:85加入H3钢粉球磨30min,再静置6h得到复合材料;其中纳米Ni粉为1200目,纳米TiC陶瓷为1000目,H3钢粉为600目;Step 1. First mix nano-Ni powder and nano-TiC ceramic powder at a volume ratio of 85:15 and ball mill for 8 hours, then let it stand for 12 hours to obtain nano-sized TiC ceramic powder with Ni attached to the surface; then nano-sized TiC ceramic powder with Ni attached to the surface According to the volume ratio of 15:85, add H3 steel powder and ball mill for 30 minutes, and then stand still for 6 hours to obtain a composite material; the nano-Ni powder is 1200 mesh, the nano-TiC ceramic is 1000 mesh, and the H3 steel powder is 600 mesh;
步骤2、利用proe绘图软件绘制所需空间结构的立体模型,然后导入magics分层软件中进行分层,根据打印的热作模具钢材料确定3D打印的加工参数,生成运行轨迹代码,导入同轴送分3D打印机中,将H3钢粉倒入3D打印机中,打印出形状复杂的模具雏形在模具型腔处预留20mm的未打印余量,暂停打印设备,更换钢粉为Ni粉再将普通纯Ni粉在模具雏形模具型腔处且位于热作模具钢材料内部表面打印一层,层厚为5mm;暂停打印设备,将Ni粉更换为步骤1的复合材料继续在打印好的纯Ni层表面打印,层厚为15mm,将成型的模具件进行清粉,刮研,打磨处理,对模具进行精抛处理得到形状复杂复合材料热作模具;其中H3钢粉、Ni粉均为600目;上述3D打印为3D激光金属沉积技术。Step 2. Use proe drawing software to draw the three-dimensional model of the required space structure, and then import it into the magics layering software for layering. Determine the processing parameters of 3D printing according to the printed hot work die steel material, generate the running track code, and import the coaxial Send to the 3D printer, pour H3 steel powder into the 3D printer, print out the mold prototype with complex shape, reserve 20mm unprinted margin at the mold cavity, suspend the printing equipment, replace the steel powder with Ni powder, and then replace the ordinary Print a layer of pure Ni powder on the cavity of the mold prototype and on the inner surface of the hot work die steel material, with a layer thickness of 5mm; suspend the printing equipment, replace the Ni powder with the composite material in step 1 and continue to print on the pure Ni layer Surface printing, the layer thickness is 15mm, the formed mold parts are cleaned, scraped and polished, and the mold is finely polished to obtain a hot-working mold with complex shapes; the H3 steel powder and Ni powder are both 600 mesh; The above 3D printing is a 3D laser metal deposition technology.
本实施例制备得到的形状复杂复合材料热作模具剖面图如图1所示,从图1中可以看出传统加工方法很难实现这种金属压铸模具,难以保证Ni层和复合材料层的厚度均一。将本实施例制备得到的形状复杂复合材料热作模具表面硬度高,显微硬度达到860HV,650℃疲劳寿命是原来H13热压铸模寿命的2倍,显微硬度提高30-45%,耐磨性提高50%。Figure 1 shows the cross-sectional view of the hot-working mold for complex composite materials prepared in this example. It can be seen from Figure 1 that it is difficult to realize such a metal die-casting mold by traditional processing methods, and it is difficult to ensure the thickness of the Ni layer and the composite material layer. Uniform. The complex-shaped composite material prepared in this example has a high surface hardness and a microhardness of 860HV. The fatigue life at 650°C is twice that of the original H13 hot-pressing mold, and the microhardness is increased by 30-45%. Sexuality increased by 50%.
实施例2Example 2
该3D打印制备形状复杂复合材料热作模具的方法,该复杂复合材料热作模具为汽车B柱,其具体步骤如下:The 3D printing method for preparing a hot-working mold of a complex composite material, the hot-working mold of a complex composite material is a B-pillar of an automobile, and the specific steps are as follows:
步骤1、首先将纳米Ni粉和纳米TiC陶瓷粉按体积比为90:10混合球磨10h,再静置10h得到表面黏着Ni的纳米级TiC陶瓷粉;然后向面黏着Ni的纳米级TiC陶瓷粉按照体积比为10:90加入H3钢粉球磨90min,再静置8h得到复合材料;其中纳米Ni粉为1200目,纳米TiC陶瓷为1000目,H3钢粉为600目;Step 1. First mix nano-Ni powder and nano-TiC ceramic powder with a volume ratio of 90:10 and ball mill for 10 hours, then let it stand for 10 hours to obtain nano-sized TiC ceramic powder with Ni attached to the surface; then nano-sized TiC ceramic powder with Ni attached to the surface According to the volume ratio of 10:90, add H3 steel powder and ball mill for 90 minutes, and then stand still for 8 hours to obtain a composite material; the nano-Ni powder is 1200 mesh, the nano-TiC ceramic is 1000 mesh, and the H3 steel powder is 600 mesh;
步骤2、利用proe绘图软件绘制所需空间结构的立体模型,然后导入magics分层软件中进行分层,根据打印的热作模具钢材料确定3D打印的加工参数,生成运行轨迹代码,导入同轴送分3D打印机中,将H3钢粉倒入3D打印机中,打印出形状复杂的模具雏形在模具型腔处预留20mm的未打印余量,暂停打印设备,更换钢粉为Ni粉再将普通纯Ni粉在模具雏形模具型腔处且位于热作模具钢材料内部表面打印一层,层厚为5mm;暂停打印设备,将Ni粉更换为步骤1的复合材料继续在打印好的纯Ni层表面打印,层厚为15mm,将成型的模具件进行清粉,刮研,打磨处理,对模具进行精抛处理得到形状复杂复合材料热作模具;其中H3钢粉、Ni粉均为600目;上述3D打印为3D激光金属沉积技术。Step 2. Use proe drawing software to draw the three-dimensional model of the required space structure, and then import it into the magics layering software for layering. Determine the processing parameters of 3D printing according to the printed hot work die steel material, generate the running track code, and import the coaxial Send to the 3D printer, pour H3 steel powder into the 3D printer, print out the mold prototype with complex shape, reserve 20mm unprinted margin at the mold cavity, suspend the printing equipment, replace the steel powder with Ni powder, and then replace the ordinary Print a layer of pure Ni powder on the cavity of the mold prototype and on the inner surface of the hot work die steel material, with a layer thickness of 5mm; suspend the printing equipment, replace the Ni powder with the composite material in step 1 and continue to print on the pure Ni layer Surface printing, the layer thickness is 15mm, the formed mold parts are cleaned, scraped and polished, and the mold is finely polished to obtain a hot-working mold with complex shapes; the H3 steel powder and Ni powder are both 600 mesh; The above 3D printing is a 3D laser metal deposition technology.
将本实施例制备得到的形状复杂复合材料热作模具采用将本实施例制备得到的高温冲压模具表面硬度高,显微硬度达到830HV,高温疲劳寿命是原来H13高温冲压模具寿命的4倍,显微硬度提高30-40%,耐磨性提高40%。The complex-shaped composite hot-working die prepared in this example adopts the high-temperature stamping die prepared in this example to have a high surface hardness, the microhardness reaches 830HV, and the high-temperature fatigue life is 4 times that of the original H13 high-temperature stamping die. The microhardness is increased by 30-40%, and the wear resistance is increased by 40%.
实施例3Example 3
该3D打印制备形状复杂复合材料热作模具的方法,其具体步骤如下:The 3D printing method for preparing a complex-shaped composite material hot-working mold, the specific steps are as follows:
步骤1、首先将纳米Ni粉和纳米TiC陶瓷粉按体积比为95:5混合球磨9h,再静置11h得到表面黏着Ni的纳米级TiC陶瓷粉;然后向面黏着Ni的纳米级TiC陶瓷粉按照体积比为5:95加入H3钢粉球磨60min,再静置7h得到复合材料;其中纳米Ni粉为1200目,纳米TiC陶瓷为1000目,H3钢粉为600目;Step 1. First mix nano-Ni powder and nano-TiC ceramic powder at a volume ratio of 95:5 and ball mill for 9 hours, then let it stand for 11 hours to obtain nano-sized TiC ceramic powder with Ni attached to the surface; then nano-sized TiC ceramic powder with Ni attached to the surface According to the volume ratio of 5:95, add H3 steel powder and ball mill for 60 minutes, and then stand still for 7 hours to obtain a composite material; the nano-Ni powder is 1200 mesh, the nano-TiC ceramic is 1000 mesh, and the H3 steel powder is 600 mesh;
步骤2、利用proe绘图软件绘制所需空间结构的立体模型,然后导入magics分层软件中进行分层,根据打印的热作模具钢材料确定3D打印的加工参数,生成运行轨迹代码,导入同轴送分3D打印机中,将H3钢粉倒入3D打印机中,打印出形状复杂的模具雏形在模具型腔处预留20mm的未打印余量,暂停打印设备,更换钢粉为Ni粉再将普通纯Ni粉在模具雏形模具型腔处且位于热作模具钢材料内部表面打印一层,层厚为5mm;暂停打印设备,将Ni粉更换为步骤1的复合材料继续在打印好的纯Ni层表面打印,层厚为15mm,将成型的模具件进行清粉,刮研,打磨处理,对模具进行精抛处理得到形状复杂复合材料热作模具;其中H3钢粉、Ni粉均为600目;上述3D打印为3D激光金属沉积技术。Step 2. Use proe drawing software to draw the three-dimensional model of the required space structure, and then import it into the magics layering software for layering. Determine the processing parameters of 3D printing according to the printed hot work die steel material, generate the running track code, and import the coaxial Send to the 3D printer, pour H3 steel powder into the 3D printer, print out the mold prototype with complex shape, reserve 20mm unprinted margin at the mold cavity, suspend the printing equipment, replace the steel powder with Ni powder, and then replace the ordinary Print a layer of pure Ni powder on the cavity of the mold prototype and on the inner surface of the hot work die steel material, with a layer thickness of 5mm; suspend the printing equipment, replace the Ni powder with the composite material in step 1 and continue to print on the pure Ni layer Surface printing, the layer thickness is 15mm, the formed mold parts are cleaned, scraped and polished, and the mold is finely polished to obtain a hot-working mold with complex shapes; the H3 steel powder and Ni powder are both 600 mesh; The above 3D printing is a 3D laser metal deposition technology.
以上结合附图对本发明的具体实施方式作了详细说明,但是本发明并不限于上述实施方式,在本领域普通技术人员所具备的知识范围内,还可以在不脱离本发明宗旨的前提下作出各种变化。The specific embodiments of the present invention have been described in detail above in conjunction with the accompanying drawings, but the present invention is not limited to the above embodiments. Variations.
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