CN104862569B - Molybdenum-based material used for hot extrusion die and surface carburizing treatment technology - Google Patents
Molybdenum-based material used for hot extrusion die and surface carburizing treatment technology Download PDFInfo
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- CN104862569B CN104862569B CN201510250191.1A CN201510250191A CN104862569B CN 104862569 B CN104862569 B CN 104862569B CN 201510250191 A CN201510250191 A CN 201510250191A CN 104862569 B CN104862569 B CN 104862569B
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- 239000000463 material Substances 0.000 title claims abstract description 25
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 title claims abstract description 24
- 238000005255 carburizing Methods 0.000 title claims abstract description 20
- 229910052750 molybdenum Inorganic materials 0.000 title claims abstract description 17
- 239000011733 molybdenum Substances 0.000 title claims abstract description 17
- 238000001192 hot extrusion Methods 0.000 title claims description 12
- 238000005516 engineering process Methods 0.000 title description 3
- 239000000843 powder Substances 0.000 claims abstract description 12
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 claims abstract description 10
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims abstract description 6
- 239000003610 charcoal Substances 0.000 claims abstract description 6
- 239000010941 cobalt Substances 0.000 claims abstract description 6
- 229910017052 cobalt Inorganic materials 0.000 claims abstract description 6
- 239000003795 chemical substances by application Substances 0.000 claims abstract description 5
- 238000001125 extrusion Methods 0.000 claims abstract description 5
- 238000000034 method Methods 0.000 claims abstract description 5
- CDBYLPFSWZWCQE-UHFFFAOYSA-L Sodium Carbonate Chemical compound [Na+].[Na+].[O-]C([O-])=O CDBYLPFSWZWCQE-UHFFFAOYSA-L 0.000 claims abstract description 4
- VMHLLURERBWHNL-UHFFFAOYSA-M Sodium acetate Chemical compound [Na+].CC([O-])=O VMHLLURERBWHNL-UHFFFAOYSA-M 0.000 claims abstract description 4
- 239000001632 sodium acetate Substances 0.000 claims abstract description 4
- 235000017281 sodium acetate Nutrition 0.000 claims abstract description 4
- 239000011230 binding agent Substances 0.000 claims abstract description 3
- 229910052799 carbon Inorganic materials 0.000 claims abstract description 3
- MTPVUVINMAGMJL-UHFFFAOYSA-N trimethyl(1,1,2,2,2-pentafluoroethyl)silane Chemical compound C[Si](C)(C)C(F)(F)C(F)(F)F MTPVUVINMAGMJL-UHFFFAOYSA-N 0.000 claims description 4
- UONOETXJSWQNOL-UHFFFAOYSA-N tungsten carbide Chemical group [W+]#[C-] UONOETXJSWQNOL-UHFFFAOYSA-N 0.000 claims description 4
- QIJNJJZPYXGIQM-UHFFFAOYSA-N 1lambda4,2lambda4-dimolybdacyclopropa-1,2,3-triene Chemical compound [Mo]=C=[Mo] QIJNJJZPYXGIQM-UHFFFAOYSA-N 0.000 claims description 2
- 229910039444 MoC Inorganic materials 0.000 claims description 2
- 238000010000 carbonizing Methods 0.000 claims 1
- 239000013078 crystal Substances 0.000 claims 1
- 238000007872 degassing Methods 0.000 claims 1
- 230000014759 maintenance of location Effects 0.000 claims 1
- 238000004519 manufacturing process Methods 0.000 abstract description 6
- 239000002245 particle Substances 0.000 abstract description 3
- 150000001247 metal acetylides Chemical class 0.000 abstract 2
- -1 carbide Chemical compound 0.000 abstract 1
- 238000003763 carbonization Methods 0.000 abstract 1
- 229910000831 Steel Inorganic materials 0.000 description 8
- 239000010959 steel Substances 0.000 description 8
- 238000005245 sintering Methods 0.000 description 6
- 239000000203 mixture Substances 0.000 description 3
- 238000005260 corrosion Methods 0.000 description 2
- 230000007797 corrosion Effects 0.000 description 2
- 238000010438 heat treatment Methods 0.000 description 2
- 238000005498 polishing Methods 0.000 description 2
- 238000004663 powder metallurgy Methods 0.000 description 2
- 238000005728 strengthening Methods 0.000 description 2
- 229910010293 ceramic material Inorganic materials 0.000 description 1
- 238000009472 formulation Methods 0.000 description 1
- 230000001050 lubricating effect Effects 0.000 description 1
- 238000010791 quenching Methods 0.000 description 1
- 230000000171 quenching effect Effects 0.000 description 1
- 239000002994 raw material Substances 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 238000004381 surface treatment Methods 0.000 description 1
- 238000005496 tempering Methods 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
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Abstract
本发明钼基材料采用钼粉作为高温挤压模具的基材,以Co作粘结剂,加入碳化物,各组份的质量百分比为:钼60~80%,碳化物15~32%,钴2~12%,加入碳占钼、碳化物、钴三者总质量0.01~0.1%;钼基材料表面渗碳处理工艺,采用质量百分比分别为65~80%的木炭粉,10~20%的无水碳酸钠,5~15%的乙酸钠作为渗碳剂,木炭粉的粒度在100目以下,渗碳温度在900~1100℃,保温时间8~10h,在材料表面形成一层致密的碳化钼从而保护材料。本发明的材料渗碳后,表面硬度HV最高可达900,而心部硬度HV只有530左右,大大地提高了模具的使用寿命,并可实现快速挤压,从而降低成本和提高生产效率。The molybdenum-based material of the present invention uses molybdenum powder as the base material of a high-temperature extrusion die, uses Co as a binder, and adds carbides. The mass percentages of each component are: molybdenum 60-80%, carbides 15-32%, cobalt 2-12%, adding carbon accounts for 0.01-0.1% of the total mass of molybdenum, carbide, and cobalt; the surface carburizing treatment process of molybdenum-based materials adopts charcoal powder with mass percentages of 65-80% and 10-20% Anhydrous sodium carbonate, 5-15% sodium acetate as carburizing agent, charcoal powder particle size below 100 mesh, carburizing temperature at 900-1100°C, holding time 8-10h, forming a layer of dense carbonization on the surface of the material Molybdenum thus protects the material. After carburizing the material of the present invention, the surface hardness HV can reach up to 900, while the core hardness HV is only about 530, which greatly improves the service life of the mold, and can realize rapid extrusion, thereby reducing costs and improving production efficiency.
Description
技术领域technical field
本发明涉及到钼基材料的配方和钼基材料表面渗碳处理的技术,属于粉末冶金、热挤压和表面处理领域。The invention relates to the formulation of molybdenum-based materials and the technology of surface carburizing treatment of molybdenum-based materials, and belongs to the fields of powder metallurgy, hot extrusion and surface treatment.
背景技术Background technique
目前国内外热挤压行业中通常采用热作模具钢做模具材料,我国主要用3Cr2W8V钢,英美、苏、瑞典则采用H13\4Cr5MoVSi钢或其他基本钢制造模具。热挤压模具是在高温、高压、磨损和热疲劳等恶劣条件下服役的,服役条件十分苛刻。例如:20Cr等材料,加热温度为1150~1200℃,在水压机上成型,模具的温度可以达到900~950℃,因高压成型,被挤压的零件越大,加工的深度越深(特别是反挤压成型的大工件),则条件越苛刻,高温强度要求也越高。所以热作模具材料应具有良好的综合性能,主要是:应具有高的抗塑性变形能力;在服役的温度(800~950℃)下有高的热稳定性及抗磨损性能;在动负荷下应有足够高的韧性;另外,热挤压模具寿命低、经济效益差是个共同的问题。At present, hot work die steel is usually used as die material in the hot extrusion industry at home and abroad. my country mainly uses 3Cr2W8V steel, while Britain, the United States, the Soviet Union, and Sweden use H13\4Cr5MoVSi steel or other basic steel to make dies. Hot extrusion dies are used under severe conditions such as high temperature, high pressure, wear and thermal fatigue, and the service conditions are very harsh. For example: 20Cr and other materials, the heating temperature is 1150 ~ 1200 ℃, forming on the hydraulic press, the temperature of the mold can reach 900 ~ 950 ℃, due to high pressure forming, the larger the extruded part, the deeper the processing depth (especially reverse Extruded large workpieces), the harsher the conditions, the higher the high temperature strength requirements. Therefore, the hot work mold material should have good comprehensive properties, mainly: it should have high plastic deformation resistance; it should have high thermal stability and wear resistance at service temperature (800-950 °C); it should have high thermal stability and wear resistance under dynamic load. It should have sufficiently high toughness; in addition, low service life of hot extrusion dies and poor economic benefits are common problems.
热作模具钢,由于高温强度低,每次热挤压后都要进行外部水冷以降低模具温度,模具要经受严重的冷热疲劳考验,在挤压成型时与炽热的工件接触,造成模具与工件之间的强烈摩擦,产生化学作用,使模具表面产生热腐蚀。这就使热作模具钢制造的热挤压模具产生塌陷、形变、拉沟、炸裂、表面腐蚀等现象,造成模具失效。硬质合金和陶瓷材料,硬度可达HV1000左右,但因硬度大,韧性差,在高温、高压的作用下,易产生裂纹而报废。Hot work die steel, due to its low strength at high temperature, needs to be cooled externally after each hot extrusion to reduce the temperature of the die. The strong friction between workpieces produces chemical action, which causes thermal corrosion on the surface of the mold. This causes the hot extrusion die made of hot work die steel to collapse, deform, pull grooves, burst, surface corrosion and other phenomena, resulting in die failure. Cemented carbide and ceramic materials have a hardness of about HV1000, but due to their high hardness and poor toughness, they are prone to cracks and are scrapped under the action of high temperature and high pressure.
发明内容Contents of the invention
本发明目的是提供一种用于热挤压模具的钼基材料与表面渗碳处理工艺。The purpose of the invention is to provide a molybdenum-based material and a surface carburizing treatment process for a hot extrusion die.
本发明采用钼粉作为高温挤压模具的基材,Co作粘结剂,加入碳化物(碳化钨或碳化钛),其各组份的质量百分比依据所需的硬度、强度、韧性和耐磨性等性能指标确定,其中钼60~80%,碳化物15~32%,钴2~12%;另外,为了除气和净化晶界,需要加入钼、碳化物、钴三者总质量0.01~0.1%的碳。The present invention uses molybdenum powder as the base material of the high temperature extrusion die, Co as the binder, adding carbide (tungsten carbide or titanium carbide), and the mass percentage of each component depends on the required hardness, strength, toughness and wear resistance The performance indicators such as molybdenum are determined, including 60-80% of molybdenum, 15-32% of carbide, and 2-12% of cobalt; in addition, in order to degas and purify the grain boundary, it is necessary to add 0.01-0.01% of the total mass of molybdenum, carbide and cobalt. 0.1% carbon.
高温高压下作业的热挤压模具钢,其服役时的工作温度往往超过回火温度。尽管采用多种手段作强韧化处理(强韧化处理+表面强化处理),以图改善服役条件,最大限度的发挥材料的潜力,但仍远远满足不了使用性能的要求,本发明采用表面渗碳技术很好的解决了此类问题。The working temperature of hot extrusion die steel operating under high temperature and high pressure often exceeds the tempering temperature when it is in service. Although multiple means are used for strengthening and toughening treatment (toughening treatment + surface strengthening treatment), in order to improve service conditions and maximize the potential of the material, it is still far from meeting the requirements of performance. The present invention uses surface Carburizing technology solves such problems very well.
本发明表面渗碳采用65~80%的木炭粉(粒度在100目以下),10~20%的无水碳酸钠,5~15%的乙酸钠作为渗碳剂,其各组份均为质量百分比,渗碳温度在900℃~1100℃之间,保温时间8h~10h,在材料表面形成一层致密的碳化钼从而保护材料。Surface carburizing of the present invention adopts 65~80% charcoal powder (particle size is below 100 orders), 10~20% anhydrous sodium carbonate, 5~15% sodium acetate as carburizing agent, and its each component is quality Percentage, the carburizing temperature is between 900°C and 1100°C, and the holding time is 8h to 10h, forming a dense layer of molybdenum carbide on the surface of the material to protect the material.
本发明的材料渗碳后,表面硬度HV最高可达900,而心部硬度HV只有530左右。表面不仅具有硬质合金的硬度,还具有钢材料的韧性。并且在高温下具有良好的抗蠕变性能、线膨胀系数低和极低的蒸气压、高的弹性模量、受温度的影响较小、优良的导电、导热性、高温强度高及低的摩擦系数、润滑性能优良等特点。大大地提高了模具的使用寿命,并可实现快速挤压,从而降低成本和提高生产效率。After the material of the present invention is carburized, the surface hardness HV can reach up to 900, while the core hardness HV is only about 530. The surface not only has the hardness of cemented carbide, but also has the toughness of steel material. And it has good creep resistance at high temperature, low linear expansion coefficient and extremely low vapor pressure, high elastic modulus, less affected by temperature, excellent electrical conductivity, thermal conductivity, high temperature strength and low friction Coefficient, excellent lubricating performance and so on. The service life of the mold is greatly improved, and rapid extrusion can be realized, thereby reducing costs and improving production efficiency.
具体实施方式detailed description
本发明利用钼基材料经粉末冶金方法直接成形热作挤压模具,满足高温高压条件下使用性能,以提高模具使用寿命、节约原材料、节省能源、降低成本和提高生产效率。以下百分比均为质量百分比。The invention utilizes the molybdenum-based material to directly shape the hot extrusion die through the powder metallurgy method, which satisfies the service performance under high temperature and high pressure conditions, so as to improve the service life of the die, save raw materials, save energy, reduce costs and improve production efficiency. The following percentages are all percentages by mass.
实施例一:Embodiment one:
取钼粉60%,碳化钨粉32%,钴粉8%,碳粉占钼粉、碳化钨粉、钴粉总质量的0.1%,在球磨机中以300转/分的速度球磨20小时使粉末混合均匀,后在200MP等静压机上利用事先制作好的模具冷压成形,放入真空烧结炉中加压烧结(烧结温度1400℃-1500℃,压力10MPa),经过磨光表面和工作带,再进行表面渗碳处理,渗碳厚度10μm,然后进行模具装配,并在挤压机上试模,根据试模情况适当进行修模,最后投入生产应用当中。Get molybdenum powder 60%, tungsten carbide powder 32%, cobalt powder 8%, carbon powder accounts for 0.1% of the total mass of molybdenum powder, tungsten carbide powder, cobalt powder, ball mills 20 hours with the speed of 300 rev/min in ball mill to make powder Mix evenly, and then use the pre-made mold to cold press on a 200MP isostatic press, put it into a vacuum sintering furnace for pressure sintering (sintering temperature 1400°C-1500°C, pressure 10MPa), after polishing the surface and working belt, Then carry out surface carburizing treatment, the carburizing thickness is 10μm, and then carry out mold assembly, and test the mold on the extruder, repair the mold appropriately according to the situation of the mold test, and finally put it into production and application.
实施例二:Embodiment two:
取钼粉80%,碳化钛粉15%,钴粉5%,碳粉占钼粉、碳化钛粉、钴粉总质量的0.05%,在球磨机中以350转/分的速度球磨24小时使粉末混合均匀,后在200MP等静压机上利用事先制作好的模具冷压成形,放入真空烧结炉中加压烧结(烧结温度1400℃-1500℃,压力10MPa),经过磨光表面和工作带,再进行表面渗碳处理,渗碳厚度8μm,然后进行模具装配,并在挤压机上试模,根据试模情况适当进行修模,最后投入生产应用当中。Get molybdenum powder 80%, titanium carbide powder 15%, cobalt powder 5%, carbon powder accounts for 0.05% of the total mass of molybdenum powder, titanium carbide powder, cobalt powder, ball mills 24 hours with the speed ball mill of 350 rpm in ball mill to make powder Mix evenly, and then use the pre-made mold to cold press on a 200MP isostatic press, put it into a vacuum sintering furnace for pressure sintering (sintering temperature 1400°C-1500°C, pressure 10MPa), after polishing the surface and working belt, Then carry out surface carburizing treatment, the carburizing thickness is 8μm, then carry out mold assembly, and test the mold on the extruder, repair the mold appropriately according to the situation of the mold test, and finally put it into production and application.
实施例三:Embodiment three:
取75%的木炭粉(粒度在100目以下),13%的无水碳酸钠,12%乙酸钠,在球磨机上以60转/分的转速球磨两小时进行混料,将渗碳剂和渗碳件放入密封箱后以6℃/min的升温速度,升温到1000℃后保温10小时。渗碳后取出渗碳件加热到1000℃保温2小时进行水淬,再进行渗碳件工作部分表面抛光处理之后进行模具装配试模,最终投入实际生产。Get 75% charcoal powder (particle size is below 100 orders), 13% anhydrous sodium carbonate, 12% sodium acetate, carry out mixing with 60 rev/min rotating speed ball mills two hours on ball mill, carburizing agent and carburizing agent After the carbon parts are placed in the sealed box, the temperature is raised to 1000 °C at a heating rate of 6 °C/min and then kept for 10 hours. After carburizing, the carburized parts are taken out and heated to 1000°C for 2 hours for water quenching, and then the surface of the working part of the carburized parts is polished, and then the mold assembly test is carried out, and finally put into actual production.
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CN109306422A (en) * | 2018-12-13 | 2019-02-05 | 株洲硬质合金集团有限公司 | A kind of preparation method of molybdenum carbide-molybdenum composite material |
CN113832429B (en) * | 2021-08-30 | 2023-10-27 | 东方电气(广州)重型机器有限公司 | Carburizing method and carburizing device for detecting austenite grain size of ferritic steel |
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DE2203186A1 (en) * | 1971-01-25 | 1972-08-24 | Mallory & Co Inc P R | Molybdenum-base alloys - for prodn of moulds and cores for pressure-casting |
US4133682A (en) * | 1978-01-03 | 1979-01-09 | Allied Chemical Corporation | Cobalt-refractory metal-boron glassy alloys |
CN1031258A (en) * | 1987-10-12 | 1989-02-22 | 冶金工业部钢铁研究总院 | Moulding stock of molybdenum based metall-ceramic used for hot rolling |
CN103627940A (en) * | 2013-11-27 | 2014-03-12 | 江西理工大学 | Powder metallurgical molybdenum base material applied to hot extrusion die and method for forming die |
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JP3056476B1 (en) * | 1999-01-14 | 2000-06-26 | 株式会社東富士製作所 | Method for producing recycled W—Co raw material powder from cemented carbide scrap and method for producing tungsten-based sintered heavy alloy using the same |
JP2012102362A (en) * | 2010-11-09 | 2012-05-31 | Sumitomo Metal Mining Co Ltd | Boride cermet-based powder for thermal spraying |
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DE2203186A1 (en) * | 1971-01-25 | 1972-08-24 | Mallory & Co Inc P R | Molybdenum-base alloys - for prodn of moulds and cores for pressure-casting |
US4133682A (en) * | 1978-01-03 | 1979-01-09 | Allied Chemical Corporation | Cobalt-refractory metal-boron glassy alloys |
CN1031258A (en) * | 1987-10-12 | 1989-02-22 | 冶金工业部钢铁研究总院 | Moulding stock of molybdenum based metall-ceramic used for hot rolling |
CN103627940A (en) * | 2013-11-27 | 2014-03-12 | 江西理工大学 | Powder metallurgical molybdenum base material applied to hot extrusion die and method for forming die |
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