CN111378858A - A kind of Mo-modified chromium carbide-nickel-chromium composite material and preparation method thereof - Google Patents
A kind of Mo-modified chromium carbide-nickel-chromium composite material and preparation method thereof Download PDFInfo
- Publication number
- CN111378858A CN111378858A CN202010312622.3A CN202010312622A CN111378858A CN 111378858 A CN111378858 A CN 111378858A CN 202010312622 A CN202010312622 A CN 202010312622A CN 111378858 A CN111378858 A CN 111378858A
- Authority
- CN
- China
- Prior art keywords
- powder
- composite material
- nickel
- mass
- modified
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
- 239000002131 composite material Substances 0.000 title claims abstract description 46
- 238000002360 preparation method Methods 0.000 title claims description 16
- 229910018487 Ni—Cr Inorganic materials 0.000 title claims description 14
- 150000001844 chromium Chemical class 0.000 title claims description 12
- 239000000843 powder Substances 0.000 claims abstract description 234
- 238000005245 sintering Methods 0.000 claims abstract description 63
- 229910052750 molybdenum Inorganic materials 0.000 claims abstract description 52
- 229910052804 chromium Inorganic materials 0.000 claims abstract description 31
- 238000000498 ball milling Methods 0.000 claims abstract description 24
- 229910001120 nichrome Inorganic materials 0.000 claims abstract description 24
- 239000011812 mixed powder Substances 0.000 claims abstract description 6
- 238000000748 compression moulding Methods 0.000 claims abstract description 3
- 239000011651 chromium Substances 0.000 claims description 151
- 239000002245 particle Substances 0.000 claims description 47
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 claims description 30
- 239000000463 material Substances 0.000 claims description 16
- 238000010438 heat treatment Methods 0.000 claims description 11
- 238000000227 grinding Methods 0.000 claims description 10
- 238000001272 pressureless sintering Methods 0.000 claims description 10
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 claims description 6
- 238000000465 moulding Methods 0.000 claims description 3
- 238000012986 modification Methods 0.000 claims 1
- 230000004048 modification Effects 0.000 claims 1
- VNNRSPGTAMTISX-UHFFFAOYSA-N chromium nickel Chemical compound [Cr].[Ni] VNNRSPGTAMTISX-UHFFFAOYSA-N 0.000 abstract description 5
- 238000000034 method Methods 0.000 abstract description 4
- 229910052799 carbon Inorganic materials 0.000 abstract description 2
- PXHVJJICTQNCMI-UHFFFAOYSA-N nickel Substances [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 72
- 239000000919 ceramic Substances 0.000 description 18
- 230000000052 comparative effect Effects 0.000 description 9
- 229910052751 metal Inorganic materials 0.000 description 9
- 239000002184 metal Substances 0.000 description 9
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 8
- 229910002804 graphite Inorganic materials 0.000 description 8
- 239000010439 graphite Substances 0.000 description 8
- 239000002994 raw material Substances 0.000 description 8
- 229910052759 nickel Inorganic materials 0.000 description 6
- 238000005303 weighing Methods 0.000 description 6
- 238000004519 manufacturing process Methods 0.000 description 4
- 238000002441 X-ray diffraction Methods 0.000 description 3
- 239000011195 cermet Substances 0.000 description 3
- UFGZSIPAQKLCGR-UHFFFAOYSA-N chromium carbide Chemical compound [Cr]#C[Cr]C#[Cr] UFGZSIPAQKLCGR-UHFFFAOYSA-N 0.000 description 3
- 238000005260 corrosion Methods 0.000 description 3
- 230000007797 corrosion Effects 0.000 description 3
- NIPNSKYNPDTRPC-UHFFFAOYSA-N N-[2-oxo-2-(2,4,6,7-tetrahydrotriazolo[4,5-c]pyridin-5-yl)ethyl]-2-[[3-(trifluoromethoxy)phenyl]methylamino]pyrimidine-5-carboxamide Chemical compound O=C(CNC(=O)C=1C=NC(=NC=1)NCC1=CC(=CC=C1)OC(F)(F)F)N1CC2=C(CC1)NN=N2 NIPNSKYNPDTRPC-UHFFFAOYSA-N 0.000 description 2
- 230000003647 oxidation Effects 0.000 description 2
- 238000007254 oxidation reaction Methods 0.000 description 2
- 229910003470 tongbaite Inorganic materials 0.000 description 2
- UONOETXJSWQNOL-UHFFFAOYSA-N tungsten carbide Chemical compound [W+]#[C-] UONOETXJSWQNOL-UHFFFAOYSA-N 0.000 description 2
- 229910000831 Steel Inorganic materials 0.000 description 1
- 239000002253 acid Substances 0.000 description 1
- 239000003513 alkali Substances 0.000 description 1
- 229910045601 alloy Inorganic materials 0.000 description 1
- 239000000956 alloy Substances 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 239000011230 binding agent Substances 0.000 description 1
- 238000005520 cutting process Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000009792 diffusion process Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000008204 material by function Substances 0.000 description 1
- 239000003208 petroleum Substances 0.000 description 1
- 239000013535 sea water Substances 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 230000009466 transformation Effects 0.000 description 1
Images
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C1/00—Making non-ferrous alloys
- C22C1/04—Making non-ferrous alloys by powder metallurgy
- C22C1/05—Mixtures of metal powder with non-metallic powder
- C22C1/051—Making hard metals based on borides, carbides, nitrides, oxides or silicides; Preparation of the powder mixture used as the starting material therefor
- C22C1/053—Making hard metals based on borides, carbides, nitrides, oxides or silicides; Preparation of the powder mixture used as the starting material therefor with in situ formation of hard compounds
- C22C1/055—Making hard metals based on borides, carbides, nitrides, oxides or silicides; Preparation of the powder mixture used as the starting material therefor with in situ formation of hard compounds using carbon
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C29/00—Alloys based on carbides, oxides, nitrides, borides, or silicides, e.g. cermets, or other metal compounds, e.g. oxynitrides, sulfides
- C22C29/02—Alloys based on carbides, oxides, nitrides, borides, or silicides, e.g. cermets, or other metal compounds, e.g. oxynitrides, sulfides based on carbides or carbonitrides
- C22C29/06—Alloys based on carbides, oxides, nitrides, borides, or silicides, e.g. cermets, or other metal compounds, e.g. oxynitrides, sulfides based on carbides or carbonitrides based on carbides, but not containing other metal compounds
-
- 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
- B22F2998/00—Supplementary information concerning processes or compositions relating to powder metallurgy
- B22F2998/10—Processes characterised by the sequence of their steps
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Powder Metallurgy (AREA)
Abstract
Description
技术领域technical field
本发明属于结构功能材料领域,涉及一种Mo改性的碳化铬-镍铬复合材料及其制备方法。The invention belongs to the field of structural functional materials, and relates to a Mo-modified chromium carbide-nickel-chromium composite material and a preparation method thereof.
背景技术Background technique
碳化铬-镍复合材料(由陶瓷硬质相碳化铬和金属粘结相镍组成,其中陶瓷硬质相质量百分数一般控制在70wt.%-90wt.%之间)具有一系列优异的特性:1)高温硬度高,在1100℃下其维氏硬度(HV)大于2000HV;2)热膨胀系数明显高于其它金属陶瓷复合材料且与钢相近,因而特别适于制造各种精密的耐磨量具、刀具以及高温模具;3)密度低,其密度仅为碳化钨系金属陶瓷复合材料的一半左右,工业领域便于轻量化生产;4)高温抗氧化性能好,在1000℃加热2h也不发生任何变化,抛光后的试样在1100℃下保持24h表面不生成氧化皮;5)耐磨性能优异,由于含有硬质的碳化铬骨架相,碳化铬基金属陶瓷复合材料的室温硬度约为HRA88以上,与碳化钨系金属陶瓷复合材料YG8的硬度以及耐磨性能相当;6)耐腐蚀性能好,在强酸、强碱、海水、石油工业以及其它腐蚀介质中都具有优良的耐腐蚀性能。因此,碳化铬-镍复合材料在耐磨材料、耐蚀材料等领域具有广泛的应用前景。Chromium carbide-nickel composite material (composed of ceramic hard phase chromium carbide and metal binder phase nickel, wherein the mass percentage of ceramic hard phase is generally controlled between 70wt.%-90wt.%) has a series of excellent properties: 1 ) High temperature hardness, its Vickers hardness (HV) is greater than 2000HV at 1100 ℃; 2) The thermal expansion coefficient is significantly higher than other metal-ceramic composite materials and similar to steel, so it is especially suitable for the manufacture of various precision wear-resistant measuring tools, cutting tools and high temperature mold; 3) low density, its density is only about half of tungsten carbide cermet composite material, which is convenient for lightweight production in the industrial field; 4) high temperature oxidation resistance is good, and there is no change in heating at 1000 ° C for 2 hours. The polished sample is kept at 1100 °C for 24 hours without forming oxide scale on the surface; 5) Excellent wear resistance, due to the presence of hard chromium carbide skeleton phase, the room temperature hardness of chromium carbide-based cermet composites is about HRA88 or more, and The hardness and wear resistance of tungsten carbide cermet composite material YG8 are equivalent; 6) good corrosion resistance, excellent corrosion resistance in strong acid, strong alkali, seawater, petroleum industry and other corrosive media. Therefore, chromium carbide-nickel composite materials have broad application prospects in the fields of wear-resistant materials and corrosion-resistant materials.
近年来,国内外研究人员以Cr3C2粉和Ni粉制备出的Cr3C2-Ni金属陶瓷存在Cr3C2颗粒尺寸较大(约20-30μm)、抗弯强度较低等问题,较低的力学性能限制其生产应用。In recent years, the Cr 3 C 2 -Ni cermets prepared by domestic and foreign researchers from Cr 3 C 2 powder and Ni powder have problems such as large Cr 3 C 2 particle size (about 20-30μm) and low flexural strength. , the lower mechanical properties limit its production applications.
发明内容SUMMARY OF THE INVENTION
本发明的目的在于提供一种Mo改性的(Cr,Mo)3C2-(Cr,Mo)7C3-NiCr复合材料及其制备方法,制备的(Cr,Mo)3C2-(Cr,Mo)7C3-NiCr复合材料力学性能指标良好。The object of the present invention is to provide a Mo-modified (Cr, Mo) 3 C 2 -(Cr, Mo) 7 C 3 -NiCr composite material and a preparation method thereof. The prepared (Cr, Mo) 3 C 2 -( Cr,Mo) 7 C 3 -NiCr composite has good mechanical properties.
本发明采用以下技术方案予以实现:The present invention adopts following technical scheme to realize:
一种Mo改性的碳化铬-镍铬复合材料的制备方法,包括以下步骤:A preparation method of Mo-modified chromium carbide-nickel-chromium composite material, comprising the following steps:
步骤1,将Cr粉、C粉、Ni粉和Mo粉进行球磨混合,得到混合粉;其中,Cr粉质量占Cr粉、C粉和Ni粉总质量的69.3%,C粉质量占Cr粉、C粉和Ni粉总质量的10.7%,Ni粉质量占Cr粉、C粉和Ni粉总质量的20%,Mo粉质量占Cr粉、C粉和Ni粉总质量的0.5-1.5%;In step 1, Cr powder, C powder, Ni powder and Mo powder are ball-milled and mixed to obtain a mixed powder; wherein, the mass of Cr powder accounts for 69.3% of the total mass of Cr powder, C powder and Ni powder, and the mass of C powder accounts for Cr powder, The total mass of C powder and Ni powder is 10.7%, the mass of Ni powder is 20% of the total mass of Cr powder, C powder and Ni powder, and the mass of Mo powder is 0.5-1.5% of the total mass of Cr powder, C powder and Ni powder;
步骤2,将混合粉进行模压成型,得到原始坯体;Step 2, molding the mixed powder to obtain the original body;
步骤3,将原始坯体进行真空无压烧结,烧结温度为1100-1500℃,得到Mo改性的(Cr,Mo)3C2-(Cr,Mo)7C3-NiCr复合材料。In step 3, vacuum pressureless sintering is performed on the original body, and the sintering temperature is 1100-1500° C. to obtain a Mo-modified (Cr,Mo) 3 C 2 -(Cr, Mo) 7 C 3 -NiCr composite material.
优选的,步骤1中,球磨采用的球磨罐为玛瑙罐,磨球为玛瑙球,玛瑙球直径1-5mm,球磨采用的球料比分别为(5-10):1。Preferably, in step 1, the ball milling jar used in the ball milling is an agate jar, the grinding balls are agate balls, the diameter of the agate balls is 1-5 mm, and the ball-to-material ratio used in the ball milling is (5-10):1, respectively.
优选的,步骤1中,球磨时间为1-15小时。Preferably, in step 1, the ball milling time is 1-15 hours.
优选的,步骤1中,Cr粉纯度和粒度分别为:99.9%和≤20μm;C粉纯度和粒度分别为:99.9%和≤1μm;Ni粉纯度和粒度分别为:99.9%和≤5μm;Mo粉纯度和粒度分别为:99.9%和≤5μm。Preferably, in step 1, the purity and particle size of Cr powder are: 99.9% and ≤20 μm; the purity and particle size of C powder are: 99.9% and ≤1 μm; the purity and particle size of Ni powder are: 99.9% and ≤5 μm; Mo The powder purity and particle size are: 99.9% and ≤5μm, respectively.
优选的,步骤2中,模压成型采用的压强为200-500MPa。Preferably, in step 2, the pressure used for compression molding is 200-500 MPa.
优选的,步骤3中,烧结时间为1-4h。Preferably, in step 3, the sintering time is 1-4h.
优选的,烧结时升温速度为:5℃-10℃/分钟。Preferably, the heating rate during sintering is 5°C-10°C/min.
优选的,烧结时真空度为0.0001-0.1Pa。Preferably, the degree of vacuum during sintering is 0.0001-0.1 Pa.
采用所述的制备方法得到的Mo改性的碳化铬-镍铬复合材料。The Mo-modified chromium carbide-nickel-chromium composite material obtained by the preparation method.
与现有技术相比,本发明具有以下有益的技术效果:Compared with the prior art, the present invention has the following beneficial technical effects:
本发明通过掺杂合金元素Mo制备得到的碳化铬-镍铬复合材料,不但具有Cr3C2相,同时,产生了Cr7C3相,而且与不掺杂Mo的碳化铬-镍复合材料相比陶瓷相颗粒尺寸明显减小。基于扩散热力学理论,Mo元素掺杂将促进Ni与Cr的互扩散现象,被Ni原子和Mo原子置换出的Cr原子一部分扩散入Ni中生成NiCr相,另一部分Cr原子增大了Cr与C的初始比例,发生了Cr7C3相的相变,从而产生了Cr7C3相。由于Cr7C3相力学性能比Cr3C2相更好,同时由于陶瓷相颗粒尺寸的减小,使得最终制备的(Cr,Mo)3C2-(Cr,Mo)7C3-NiCr复合材料的抗弯强度、硬度等力学性能有了明显的提高。本发明制备方法简单,为制备高性能(Cr,Mo)3C2-(Cr,Mo)7C3-NiCr复合材料提供了一种成本较低、工艺稳定且易于产业化的新技术。The chromium carbide-nickel-chromium composite material prepared by doping the alloy element Mo in the present invention not only has a Cr 3 C 2 phase, but also produces a Cr 7 C 3 phase, and is compatible with the chromium carbide-nickel composite material not doped with Mo. Compared with the ceramic phase, the particle size is significantly reduced. Based on the theory of diffusion thermodynamics, the doping of Mo element will promote the interdiffusion of Ni and Cr. Part of the Cr atoms replaced by Ni atoms and Mo atoms diffuses into Ni to form NiCr phase, and the other part of Cr atoms increases the interdiffusion of Cr and C. At the initial ratio, a phase transformation of the Cr 7 C 3 phase occurs, resulting in the Cr 7 C 3 phase. Since the mechanical properties of the Cr 7 C 3 phase are better than those of the Cr 3 C 2 phase, and the particle size of the ceramic phase is reduced, the final prepared (Cr,Mo) 3 C 2 -(Cr,Mo) 7 C 3 -NiCr The mechanical properties such as flexural strength and hardness of composite materials have been significantly improved. The preparation method of the invention is simple, and provides a new technology with low cost, stable process and easy industrialization for preparing high-performance (Cr,Mo) 3 C 2 -(Cr, Mo) 7 C 3 -NiCr composite material.
本发明中制备的Mo改性的(Cr,Mo)3C2-(Cr,Mo)7C3-NiCr复合材料,致密度较高,主要力学性能指标良好,适用于高温氧化、高温磨损等严酷工况。The Mo-modified (Cr, Mo) 3 C 2 -(Cr, Mo) 7 C 3 -NiCr composite material prepared in the present invention has high density and good main mechanical properties, and is suitable for high temperature oxidation, high temperature wear and the like. Harsh conditions.
附图说明Description of drawings
图1为实施例1-3的(Cr,Mo)3C2-(Cr,Mo)7C3-NiCr复合材料及对比例材料的XRD分析结果;(a)实施例1-3和(b)对比例。Fig. 1 is the XRD analysis results of the (Cr,Mo) 3 C 2 -(Cr, Mo) 7 C 3 -NiCr composite material of Example 1-3 and the material of the comparative example; (a) Examples 1-3 and (b) ) for the comparison.
图2为本发明复合材料组织图;(a)未添加Mo,(b)添加0.5wt.%Mo,(c)添加1.0wt.%Mo和(d)添加1.5wt.%Mo。Figure 2 is the structure diagram of the composite material of the present invention; (a) without Mo added, (b) with 0.5 wt.% Mo, (c) with 1.0 wt. % Mo and (d) with 1.5 wt. % Mo.
具体实施方式Detailed ways
下面结合具体的实施例对本发明做进一步的详细说明,所述是对本发明的解释而不是限定。The present invention will be further described in detail below in conjunction with specific embodiments, which are to explain rather than limit the present invention.
本发明所述的Mo改性的(Cr,Mo)3C2-(Cr,Mo)7C3-NiCr复合材料的制备方法,包括以下步骤:The preparation method of the Mo-modified (Cr,Mo) 3 C 2 -(Cr, Mo) 7 C 3 -NiCr composite material according to the present invention comprises the following steps:
步骤1,原材料选择Cr粉、C粉、Ni粉和Mo粉,其中,Cr粉质量占Cr粉、C粉和Ni粉总质量的69.3%,C粉质量占Cr粉、C粉和Ni粉总质量的10.7%,Ni粉质量占Cr粉、C粉和Ni粉总质量的20%,Mo粉质量占Cr粉、C粉和Ni粉总质量的0.5-1.5%。将Cr粉、C粉、Ni粉和Mo粉称重后装入玛瑙球磨罐中,磨球为玛瑙球(直径1-5mm),球料比为(5-10):1。Step 1, select Cr powder, C powder, Ni powder and Mo powder as raw materials, among which, the mass of Cr powder accounts for 69.3% of the total mass of Cr powder, C powder and Ni powder, and the mass of C powder accounts for the total mass of Cr powder, C powder and Ni powder. The mass of Ni powder accounts for 20% of the total mass of Cr powder, C powder and Ni powder, and the mass of Mo powder accounts for 0.5-1.5% of the total mass of Cr powder, C powder and Ni powder. The Cr powder, C powder, Ni powder and Mo powder were weighed and put into the agate ball mill jar. The grinding balls were agate balls (1-5mm in diameter), and the ratio of balls to material was (5-10):1.
步骤2,将玛瑙球磨罐放入行星式球磨机中开机转动,球磨时间为1-15小时,球磨完成之后随球磨罐一同冷却至室温,打开球磨罐将Cr粉、C粉Ni粉和Mo粉的混合粉填充到金属模具中,在200-500MPa下模压成型。Step 2, put the agate ball mill into the planetary ball mill and turn it on. The ball milling time is 1-15 hours. After the ball milling is completed, it will be cooled to room temperature together with the ball mill, and the ball mill will be opened. The mixed powder is filled into a metal mold and molded under 200-500MPa.
步骤3,将模压成型的坯体放入石墨模具中并一同放入真空无压烧结炉中进行烧结,烧结时真空度为0.0001-0.1Pa;烧结炉的升温速度为:5℃-10℃/分钟;烧结温度为:1100-1500℃(保温时间为1-4h),烧结完毕后随烧结炉一同冷却。Step 3, put the molded body into a graphite mold and put it into a vacuum pressureless sintering furnace for sintering, the vacuum degree during sintering is 0.0001-0.1Pa; the heating rate of the sintering furnace is: 5 ℃-10 ℃ / minutes; sintering temperature is: 1100-1500 ℃ (holding time is 1-4h), after the sintering is completed, it will be cooled together with the sintering furnace.
Cr粉纯度和粒度分别为:99.9%和≤20μm;The purity and particle size of Cr powder are: 99.9% and ≤20μm;
C粉纯度和粒度分别为:99.9%和≤1μm;The purity and particle size of C powder are: 99.9% and ≤1μm;
Ni粉纯度和粒度分别为:99.9%和≤5μm;The purity and particle size of Ni powder are: 99.9% and ≤5μm;
Mo粉纯度和粒度分别为:99.9%和≤5μm。The purity and particle size of Mo powder are: 99.9% and ≤5μm, respectively.
下面对本发明的具体实施例进行说明:Specific embodiments of the present invention are described below:
实施例1:Example 1:
首先,原材料选择Cr粉(纯度和粒度分别为:99.9%和≤20μm),C粉(纯度和粒度分别为:99.9%和≤1μm),Ni粉(纯度和粒度分别为:99.9%和≤5μm)和Mo粉(纯度和粒度分别为:99.9%和≤5μm),其中Cr粉质量占Cr粉、C粉和Ni粉总质量的69.3%,C粉质量占Cr粉、C粉和Ni粉总质量的10.7%,Ni粉质量占Cr粉、C粉和Ni粉总质量的20%,Mo粉质量占Cr粉、C粉和Ni粉总质量的0.5%。称重后装入玛瑙球磨罐中,磨球为玛瑙球(直径1mm),球料比为10:1。First, the raw materials are Cr powder (purity and particle size: 99.9% and ≤20μm, respectively), C powder (purity and particle size: 99.9% and ≤1μm, respectively), Ni powder (purity and particle size: 99.9% and ≤5μm, respectively. ) and Mo powder (purity and particle size: 99.9% and ≤5μm, respectively), of which the mass of Cr powder accounts for 69.3% of the total mass of Cr powder, C powder and Ni powder, and the mass of C powder accounts for the total mass of Cr powder, C powder and Ni powder. The mass of Ni powder accounts for 20% of the total mass of Cr powder, C powder and Ni powder, and the mass of Mo powder accounts for 0.5% of the total mass of Cr powder, C powder and Ni powder. After weighing, put it into an agate ball mill jar, the grinding balls are agate balls (diameter 1mm), and the ball-to-material ratio is 10:1.
然后,将玛瑙球磨罐放入行星式球磨机中开机转动,球磨13h完成之后并随罐体一同冷却至室温,打开罐体将球磨粉充填到金属模具中,在200MPa下模压成型;Then, put the agate ball milling jar into the planetary ball mill and turn it on. After 13 hours of ball milling, the jar is cooled to room temperature together with the jar, and the jar is opened to fill the ball mill powder into the metal mold, and press-molded at 200 MPa;
最后,将模压成型坯体放入石墨模具中并一同放入真空烧结炉中进行无压烧结,烧结时真空度为10-4Pa;烧结炉的升温速度为:5℃/分钟;烧结温度为:1300℃(保温时间为1h),烧结完毕后随烧结炉一同冷却。Finally, put the molded green body into a graphite mold and put it into a vacuum sintering furnace for pressureless sintering. The vacuum degree during sintering is 10 -4 Pa; the heating rate of the sintering furnace is 5°C/min; the sintering temperature is : 1300 ℃ (holding time is 1h), after the sintering is completed, it will be cooled together with the sintering furnace.
该实施例制备的Mo改性的(Cr,Mo)3C2-(Cr,Mo)7C3-NiCr复合材料的孔隙率为1.11%,硬度为86.9HRA,抗弯强度达1210MPa,断裂韧性达14.1MPa·m1/2。其中,陶瓷相中Cr3C2与Cr7C3的体积百分比为3:5。The Mo-modified (Cr,Mo) 3 C 2 -(Cr, Mo) 7 C 3 -NiCr composite material prepared in this example has a porosity of 1.11%, a hardness of 86.9 HRA, a flexural strength of 1210 MPa, and a fracture toughness of 1210 MPa. up to 14.1MPa·m 1/2 . Wherein, the volume percentage of Cr 3 C 2 and Cr 7 C 3 in the ceramic phase is 3:5.
实施例2:Example 2:
首先,原材料选择Cr粉(纯度和粒度分别为:99.9%和≤20μm),C粉(纯度和粒度分别为:99.9%和≤1μm),Ni粉(纯度和粒度分别为:99.9%和≤5μm)和Mo粉(纯度和粒度分别为:99.9%和≤5μm),其中Cr粉质量占Cr粉、C粉和Ni粉总质量的69.3%,C粉质量占Cr粉、C粉和Ni粉总质量的10.7%,Ni粉质量占Cr粉、C粉和Ni粉总质量的20%,Mo粉质量占Cr粉、C粉和Ni粉总质量的1.0%。称重后装入玛瑙球磨罐中,磨球为玛瑙球(直径1mm),球料比为10:1。First, the raw materials are Cr powder (purity and particle size: 99.9% and ≤20μm, respectively), C powder (purity and particle size: 99.9% and ≤1μm, respectively), Ni powder (purity and particle size: 99.9% and ≤5μm, respectively. ) and Mo powder (purity and particle size: 99.9% and ≤5μm, respectively), of which the mass of Cr powder accounts for 69.3% of the total mass of Cr powder, C powder and Ni powder, and the mass of C powder accounts for the total mass of Cr powder, C powder and Ni powder. The mass of Ni powder accounts for 20% of the total mass of Cr powder, C powder and Ni powder, and the mass of Mo powder accounts for 1.0% of the total mass of Cr powder, C powder and Ni powder. After weighing, put it into an agate ball mill jar, the grinding balls are agate balls (diameter 1mm), and the ball-to-material ratio is 10:1.
然后,将玛瑙球磨罐放入行星式球磨机中开机转动,球磨13h完成之后并随罐体一同冷却至室温,打开罐体将球磨粉充填到金属模具中,在200MPa下模压成型;Then, put the agate ball milling jar into the planetary ball mill and turn it on. After 13 hours of ball milling, the jar is cooled to room temperature together with the jar, and the jar is opened to fill the ball mill powder into the metal mold, and press-molded at 200 MPa;
最后,将模压成型坯体放入石墨模具中并一同放入真空烧结炉中进行无压烧结,烧结时真空度为10-4Pa;烧结炉的升温速度为:5℃/分钟;烧结温度为:1300℃(保温时间为1h),烧结完毕后随烧结炉一同冷却。Finally, put the molded green body into a graphite mold and put it into a vacuum sintering furnace for pressureless sintering. The vacuum degree during sintering is 10 -4 Pa; the heating rate of the sintering furnace is 5°C/min; the sintering temperature is : 1300 ℃ (holding time is 1h), after the sintering is completed, it will be cooled together with the sintering furnace.
该实施例制备的Mo改性的(Cr,Mo)3C2-(Cr,Mo)7C3-NiCr复合材料的孔隙率为0.92%,硬度为88.5HRA,抗弯强度达1290MPa,断裂韧性达15.6MPa·m1/2。其中,陶瓷相中Cr3C2与Cr7C3的体积百分比为1:3。The Mo-modified (Cr,Mo) 3 C 2 -(Cr, Mo) 7 C 3 -NiCr composite prepared in this example has a porosity of 0.92%, a hardness of 88.5HRA, a flexural strength of 1290 MPa, and a fracture toughness of 1290 MPa. up to 15.6MPa·m 1/2 . Wherein, the volume percentage of Cr 3 C 2 and Cr 7 C 3 in the ceramic phase is 1:3.
实施例3:Example 3:
首先,原材料选择Cr粉(纯度和粒度分别为:99.9%和≤20μm),C粉(纯度和粒度分别为:99.9%和≤1μm),Ni粉(纯度和粒度分别为:99.9%和≤5μm)和Mo粉(纯度和粒度分别为:99.9%和≤5μm),其中Cr粉质量占Cr粉、C粉和Ni粉总质量的69.3%,C粉质量占Cr粉、C粉和Ni粉总质量的10.7%,Ni粉质量占Cr粉、C粉和Ni粉总质量的20%,Mo粉质量占Cr粉、C粉和Ni粉总质量的1.5%。称重后装入玛瑙球磨罐中,磨球为玛瑙球(直径1mm),球料比为10:1。First, the raw materials are Cr powder (purity and particle size: 99.9% and ≤20μm, respectively), C powder (purity and particle size: 99.9% and ≤1μm, respectively), Ni powder (purity and particle size: 99.9% and ≤5μm, respectively. ) and Mo powder (purity and particle size: 99.9% and ≤5μm, respectively), of which the mass of Cr powder accounts for 69.3% of the total mass of Cr powder, C powder and Ni powder, and the mass of C powder accounts for the total mass of Cr powder, C powder and Ni powder. The mass of Ni powder accounts for 20% of the total mass of Cr powder, C powder and Ni powder, and the mass of Mo powder accounts for 1.5% of the total mass of Cr powder, C powder and Ni powder. After weighing, put it into an agate ball mill jar, the grinding balls are agate balls (diameter 1mm), and the ball-to-material ratio is 10:1.
然后,将玛瑙球磨罐放入行星式球磨机中开机转动,球磨13h完成之后并随罐体一同冷却至室温,打开罐体将球磨粉充填到金属模具中,在200MPa下模压成型;Then, put the agate ball milling jar into the planetary ball mill and turn it on. After 13 hours of ball milling, the jar is cooled to room temperature together with the jar, and the jar is opened to fill the ball mill powder into the metal mold, and press-molded at 200 MPa;
最后,将模压成型坯体放入石墨模具中并一同放入真空烧结炉中进行无压烧结,烧结时真空度为10-4Pa;烧结炉的升温速度为:5℃/分钟;烧结温度为:1300℃(保温时间为1h),烧结完毕后随烧结炉一同冷却。Finally, put the molded green body into a graphite mold and put it into a vacuum sintering furnace for pressureless sintering. The vacuum degree during sintering is 10 -4 Pa; the heating rate of the sintering furnace is 5°C/min; the sintering temperature is : 1300 ℃ (holding time is 1h), after the sintering is completed, it will be cooled together with the sintering furnace.
该实施例制备的Mo改性的(Cr,Mo)3C2-(Cr,Mo)7C3-NiCr复合材料的孔隙率为0.88%,硬度为88.8HRA,抗弯强度达1300MPa,断裂韧性达15.8MPa·m1/2。其中,陶瓷相中Cr3C2与Cr7C3的体积百分比为1:4。The Mo-modified (Cr,Mo) 3 C 2 -(Cr, Mo) 7 C 3 -NiCr composite prepared in this example has a porosity of 0.88%, a hardness of 88.8 HRA, a flexural strength of 1300 MPa, and a fracture toughness of 1300 MPa. up to 15.8MPa·m 1/2 . Wherein, the volume percentage of Cr 3 C 2 and Cr 7 C 3 in the ceramic phase is 1:4.
实施例4:Example 4:
首先,原材料选择Cr粉(纯度和粒度分别为:99.9%和≤20μm),C粉(纯度和粒度分别为:99.9%和≤1μm),Ni粉(纯度和粒度分别为:99.9%和≤5μm)和Mo粉(纯度和粒度分别为:99.9%和≤5μm),其中Cr粉质量占Cr粉、C粉和Ni粉总质量的69.3%,C粉质量占Cr粉、C粉和Ni粉总质量的10.7%,Ni粉质量占Cr粉、C粉和Ni粉总质量的20%,Mo粉质量占Cr粉、C粉和Ni粉总质量的1.5%。称重后装入玛瑙球磨罐中,磨球为玛瑙球(直径1mm),球料比为5:1。First, the raw materials are Cr powder (purity and particle size: 99.9% and ≤20μm, respectively), C powder (purity and particle size: 99.9% and ≤1μm, respectively), Ni powder (purity and particle size: 99.9% and ≤5μm, respectively. ) and Mo powder (purity and particle size: 99.9% and ≤5μm, respectively), of which the mass of Cr powder accounts for 69.3% of the total mass of Cr powder, C powder and Ni powder, and the mass of C powder accounts for the total mass of Cr powder, C powder and Ni powder. The mass of Ni powder accounts for 20% of the total mass of Cr powder, C powder and Ni powder, and the mass of Mo powder accounts for 1.5% of the total mass of Cr powder, C powder and Ni powder. After weighing, put it into an agate ball mill jar, the grinding balls are agate balls (diameter 1mm), and the ball-to-material ratio is 5:1.
然后,将玛瑙球磨罐放入行星式球磨机中开机转动,球磨1h完成之后并随罐体一同冷却至室温,打开罐体将球磨粉充填到金属模具中,在200MPa下模压成型;Then, put the agate ball milling jar into the planetary ball mill and turn it on. After 1 hour of ball milling, the jar is cooled to room temperature together with the jar body, and the jar body is opened to fill the ball mill powder into the metal mold, which is molded under 200MPa;
最后,将模压成型坯体放入石墨模具中并一同放入真空烧结炉中进行无压烧结,烧结时真空度为0.1Pa;烧结炉的升温速度为:5℃/分钟;烧结温度为:1100℃(保温时间为1h),烧结完毕后随烧结炉一同冷却。Finally, put the molded body into a graphite mold and put it into a vacuum sintering furnace for pressureless sintering. The vacuum degree during sintering is 0.1Pa; the heating rate of the sintering furnace is: 5°C/min; the sintering temperature is: 1100 ℃ (holding time is 1h), after the sintering is completed, it will be cooled together with the sintering furnace.
该实施例制备的Mo改性的(Cr,Mo)3C2-(Cr,Mo)7C3-NiCr复合材料的孔隙率为3.46%,硬度为81.2HRA,抗弯强度达720MPa,断裂韧性达7.4MPa·m1/2。其中,陶瓷相中Cr3C2与Cr7C3的体积百分比为1:5。The Mo-modified (Cr,Mo) 3 C 2 -(Cr, Mo) 7 C 3 -NiCr composite prepared in this example has a porosity of 3.46%, a hardness of 81.2 HRA, a flexural strength of 720 MPa, and a fracture toughness of 720 MPa. up to 7.4MPa·m 1/2 . Wherein, the volume percentage of Cr 3 C 2 and Cr 7 C 3 in the ceramic phase is 1:5.
实施例5:Example 5:
首先,原材料选择Cr粉(纯度和粒度分别为:99.9%和≤20μm),C粉(纯度和粒度分别为:99.9%和≤1μm),Ni粉(纯度和粒度分别为:99.9%和≤5μm)和Mo粉(纯度和粒度分别为:99.9%和≤5μm),其中Cr粉质量占Cr粉、C粉和Ni粉总质量的69.3%,C粉质量占Cr粉、C粉和Ni粉总质量的10.7%,Ni粉质量占Cr粉、C粉和Ni粉总质量的20%,Mo粉质量占Cr粉、C粉和Ni粉总质量的1.5%。称重后装入玛瑙球磨罐中,磨球为玛瑙球(直径5mm),球料比为10:1。First, the raw materials are Cr powder (purity and particle size: 99.9% and ≤20μm, respectively), C powder (purity and particle size: 99.9% and ≤1μm, respectively), Ni powder (purity and particle size: 99.9% and ≤5μm, respectively. ) and Mo powder (purity and particle size: 99.9% and ≤5μm, respectively), of which the mass of Cr powder accounts for 69.3% of the total mass of Cr powder, C powder and Ni powder, and the mass of C powder accounts for the total mass of Cr powder, C powder and Ni powder. The mass of Ni powder accounts for 20% of the total mass of Cr powder, C powder and Ni powder, and the mass of Mo powder accounts for 1.5% of the total mass of Cr powder, C powder and Ni powder. After weighing, put it into an agate ball mill jar, the grinding ball is agate ball (diameter 5mm), and the ratio of ball to material is 10:1.
然后,将玛瑙球磨罐放入行星式球磨机中开机转动,球磨15h完成之后并随罐体一同冷却至室温,打开罐体将球磨粉充填到金属模具中,在500MPa下模压成型;Then, put the agate ball milling jar into the planetary ball mill and turn it on. After 15 hours of ball milling, the jar is cooled to room temperature together with the jar body, and the jar body is opened to fill the ball mill powder into the metal mold, which is molded under 500MPa;
最后,将模压成型坯体放入石墨模具中并一同放入真空烧结炉中进行无压烧结,烧结时真空度为10-4Pa;烧结炉的升温速度为:10℃/分钟;烧结温度为:1500℃(保温时间为4h),烧结完毕后随烧结炉一同冷却。Finally, put the molded green body into a graphite mold and put it into a vacuum sintering furnace together for pressureless sintering, and the vacuum degree during sintering is 10 -4 Pa; the heating rate of the sintering furnace is: 10°C/min; the sintering temperature is : 1500 ℃ (holding time is 4h), after the sintering is completed, it will be cooled together with the sintering furnace.
该实施例制备的Mo改性的(Cr,Mo)3C2-(Cr,Mo)7C3-NiCr复合材料的孔隙率为1.02%,硬度为86.5HRA,抗弯强度达1120MPa,断裂韧性达12.3MPa·m1/2。其中,陶瓷相中Cr3C2与Cr7C3的体积百分比为2:5。The Mo-modified (Cr,Mo) 3 C 2 -(Cr, Mo) 7 C 3 -NiCr composite material prepared in this example has a porosity of 1.02%, a hardness of 86.5 HRA, a flexural strength of 1120 MPa, and a fracture toughness of 1120 MPa. up to 12.3MPa·m 1/2 . Wherein, the volume percentage of Cr 3 C 2 and Cr 7 C 3 in the ceramic phase is 2:5.
实施例6:Example 6:
首先,原材料选择Cr粉(纯度和粒度分别为:99.9%和≤20μm),C粉(纯度和粒度分别为:99.9%和≤1μm),Ni粉(纯度和粒度分别为:99.9%和≤5μm)和Mo粉(纯度和粒度分别为:99.9%和≤5μm),其中Cr粉质量占Cr粉、C粉和Ni粉总质量的69.3%,C粉质量占Cr粉、C粉和Ni粉总质量的10.7%,Ni粉质量占Cr粉、C粉和Ni粉总质量的20%,Mo粉质量占Cr粉、C粉和Ni粉总质量的1.5%。称重后装入玛瑙球磨罐中,磨球为玛瑙球(直径3mm),球料比为8:1。First, the raw materials are Cr powder (purity and particle size: 99.9% and ≤20μm, respectively), C powder (purity and particle size: 99.9% and ≤1μm, respectively), Ni powder (purity and particle size: 99.9% and ≤5μm, respectively. ) and Mo powder (purity and particle size: 99.9% and ≤5μm, respectively), of which the mass of Cr powder accounts for 69.3% of the total mass of Cr powder, C powder and Ni powder, and the mass of C powder accounts for the total mass of Cr powder, C powder and Ni powder. The mass of Ni powder accounts for 20% of the total mass of Cr powder, C powder and Ni powder, and the mass of Mo powder accounts for 1.5% of the total mass of Cr powder, C powder and Ni powder. After weighing, put it into an agate ball mill jar, the grinding balls are agate balls (diameter 3mm), and the ball-to-material ratio is 8:1.
然后,将玛瑙球磨罐放入行星式球磨机中开机转动,球磨10h完成之后并随罐体一同冷却至室温,打开罐体将球磨粉充填到金属模具中,在300MPa下模压成型;Then, put the agate ball milling jar into the planetary ball mill and turn it on. After 10 hours of ball milling, the jar is cooled to room temperature together with the jar, and the jar is opened to fill the ball mill powder into the metal mold, which is molded under 300MPa;
最后,将模压成型坯体放入石墨模具中并一同放入真空烧结炉中进行无压烧结,烧结时真空度为10-3Pa;烧结炉的升温速度为:8℃/分钟;烧结温度为:1300℃(保温时间为2h),烧结完毕后随烧结炉一同冷却。Finally, put the molded body into a graphite mold and put it into a vacuum sintering furnace together for pressureless sintering, the vacuum degree during sintering is 10 -3 Pa; the heating rate of the sintering furnace is: 8°C/min; the sintering temperature is : 1300 ℃ (holding time is 2h), after the sintering is completed, it will be cooled together with the sintering furnace.
该实施例制备的Mo改性的(Cr,Mo)3C2-(Cr,Mo)7C3-NiCr复合材料的孔隙率为0.91%,硬度为88.2HRA,抗弯强度达1270MPa,断裂韧性达15.4MPa·m1/2。其中,陶瓷相中Cr3C2与Cr7C3的体积百分比为3:8。The Mo-modified (Cr,Mo) 3 C 2 -(Cr, Mo) 7 C 3 -NiCr composite material prepared in this example has a porosity of 0.91%, a hardness of 88.2 HRA, a flexural strength of 1270 MPa, and a fracture toughness of 1270 MPa. up to 15.4MPa·m 1/2 . Wherein, the volume percentage of Cr 3 C 2 and Cr 7 C 3 in the ceramic phase is 3:8.
对比例:Comparative ratio:
首先,原材料选择Cr粉(纯度和粒度分别为:99.9%和≤20μm),C粉(纯度和粒度分别为:99.9%和≤1μm)和Ni粉(纯度和粒度分别为:99.9%和≤5μm),其中Cr粉质量占Cr粉、C粉和Ni粉总质量的69.3%,C粉质量占Cr粉、C粉和Ni粉总质量的10.7%,Ni粉质量占Cr粉、C粉和Ni粉总质量的20%,称重后装入玛瑙球磨罐中,磨球为玛瑙球(直径1mm),球料比为10:1。First, the raw materials are Cr powder (purity and particle size: 99.9% and ≤20μm, respectively), C powder (purity and particle size: 99.9% and ≤1μm, respectively) and Ni powder (purity and particle size: 99.9% and ≤5μm, respectively ), in which the mass of Cr powder accounts for 69.3% of the total mass of Cr powder, C powder and Ni powder, the mass of C powder accounts for 10.7% of the total mass of Cr powder, C powder and Ni powder, and the mass of Ni powder accounts for Cr powder, C powder and Ni powder. 20% of the total mass of the powder is weighed and put into an agate ball mill jar. The grinding balls are agate balls (diameter 1mm), and the ball-to-material ratio is 10:1.
然后,将玛瑙球磨罐放入行星式球磨机中开机转动,球磨13h完成之后并随罐体一同冷却至室温,打开罐体将球磨粉充填到金属模具中,在200MPa下模压成型;Then, put the agate ball milling jar into the planetary ball mill and turn it on. After 13 hours of ball milling, the jar is cooled to room temperature together with the jar, and the jar is opened to fill the ball mill powder into the metal mold, and press-molded at 200 MPa;
最后,将模压成型坯体放入石墨模具中并一同放入真空烧结炉中进行无压烧结,烧结时真空度为10-4Pa;烧结炉的升温速度为:5℃/分钟;烧结温度为:1300℃(保温时间为1h),烧结完毕后随烧结炉一同冷却。Finally, put the molded green body into a graphite mold and put it into a vacuum sintering furnace for pressureless sintering. The vacuum degree during sintering is 10 -4 Pa; the heating rate of the sintering furnace is 5°C/min; the sintering temperature is : 1300 ℃ (holding time is 1h), after the sintering is completed, it will be cooled together with the sintering furnace.
该对比例制备的不添加Mo的Cr3C2-Ni复合材料的孔隙率为1.44%,硬度为85.4HRA,抗弯强度达1040MPa,断裂韧性达13.2MPa·m1/2。其中,陶瓷相全部为Cr3C2,不含Cr7C3。The Cr 3 C 2 -Ni composite material without Mo added in this comparative example has a porosity of 1.44%, a hardness of 85.4 HRA, a flexural strength of 1040 MPa, and a fracture toughness of 13.2 MPa·m 1/2 . Among them, all the ceramic phases are Cr 3 C 2 and do not contain Cr 7 C 3 .
实施例1-3及对比例制备的材料的XRD图如图1所示,从XRD图谱的峰可以看出,实施例1-3添加Mo得到的材料包含(Cr,Mo)3C2、(Cr,Mo)7C3和NiCr三相,而对比例不添加Mo制备的材料只有Cr3C2和Ni两相。The XRD patterns of the materials prepared in Examples 1-3 and Comparative Examples are shown in Figure 1. It can be seen from the peaks of the XRD patterns that the materials obtained by adding Mo in Example 1-3 include (Cr, Mo) 3 C 2 , ( Cr, Mo) 7 C 3 and NiCr three phases, while the material prepared without adding Mo in the comparative example has only two phases of Cr 3 C 2 and Ni.
对比例为不添加Mo制备的Cr3C2-Ni复合材料,使用Cr粉、C粉和Ni粉烧结,在球磨时间13h,烧结温度为1300℃,保温时间1h条件下,烧结后组织如图2(a)所示,组织中不含Cr7C3,灰色部分为Cr3C2,白色部分为Ni。本发明实施例1-3在球磨混合13h、在模压成型压力200MPa和烧结温度1300℃,保温时间1h等条件不变的情况下,采用Cr粉、C粉、Ni粉和不同含量的Mo粉制备得到新型的Mo改性的(Cr,Mo)3C2-(Cr,Mo)7C3-NiCr复合材料,如图2中(b)、(c)、(d)所示,黑色部分为(Cr,Mo)3C2,灰色部分为(Cr,Mo)7C3,白色部分为NiCr。通过比较可以看出,实施例1-3添加Mo后得到的陶瓷相颗粒尺寸相比于对比例明显降低。与Cr3C2相比,新生成的Cr7C3具备更优异的硬度和强度,并且陶瓷相颗粒尺寸降低,因此(Cr,Mo)3C2-(Cr,Mo)7C3-NiCr复合材料力学性能更加优异,主要力学性能指标良好,如表1所示。The comparative example is a Cr 3 C 2 -Ni composite material prepared without adding Mo, using Cr powder, C powder and Ni powder for sintering, under the conditions of ball milling time of 13h, sintering temperature of 1300°C, and holding time of 1h, the microstructure after sintering is shown in the figure. As shown in 2(a), Cr 7 C 3 is not contained in the structure, the gray portion is Cr 3 C 2 , and the white portion is Ni. Examples 1-3 of the present invention were prepared by using Cr powder, C powder, Ni powder and Mo powder with different contents under the conditions of ball milling for 13 hours, molding pressure of 200 MPa, sintering temperature of 1300 °C, and holding time of 1 hour. A new Mo-modified (Cr,Mo) 3 C 2 -(Cr, Mo) 7 C 3 -NiCr composite material was obtained, as shown in (b), (c) and (d) in Figure 2, the black part is (Cr,Mo) 3 C 2 , the gray part is (Cr, Mo) 7 C 3 , and the white part is NiCr. It can be seen from the comparison that the particle size of the ceramic phase obtained by adding Mo in Examples 1-3 is significantly reduced compared to the comparative example. Compared with Cr 3 C 2 , the newly formed Cr 7 C 3 has more excellent hardness and strength, and the particle size of the ceramic phase is reduced, so (Cr,Mo) 3 C 2 -(Cr,Mo) 7 C 3 -NiCr The mechanical properties of the composites are more excellent, and the main mechanical properties are good, as shown in Table 1.
表1对比例与实施例力学性能对比值Table 1 Comparative Example and Example Mechanical Properties Contrast Value
与对比例相比,Mo改性的(Cr,Mo)3C2-(Cr,Mo)7C3-NiCr复合材料中陶瓷相颗粒尺寸明显降低,与Cr3C2相比,新生成的Cr7C3具备更优异的硬度和强度,因此(Cr,Mo)3C2-(Cr,Mo)7C3-NiCr复合材料力学性能均明显提高,本发明生产周期短且工艺较简单。Compared with the comparative example, the particle size of the ceramic phase in the Mo-modified (Cr,Mo) 3 C 2 -(Cr,Mo) 7 C 3 -NiCr composites was significantly reduced, and the newly formed particles were significantly smaller than those of Cr 3 C 2 . Cr 7 C 3 has more excellent hardness and strength, so the mechanical properties of the (Cr,Mo) 3 C 2 -(Cr, Mo) 7 C 3 -NiCr composite material are obviously improved, and the production cycle of the invention is short and the process is relatively simple.
同时,本发明通过添加不同含量Mo粉改善复合材料组织构成,通过调控添加Mo粉含量,控制陶瓷相Cr3C2与Cr7C3的组织占比,从而有效地降低陶瓷颗粒尺寸,提高力学性能。通过对比实施例1-3可以看出,随着Mo添加量的增加,陶瓷相中Cr7C3的占比随之增加,力学性能亦随之增加,同时陶瓷相颗粒尺寸与未添加Mo相比明显减小。At the same time, the present invention improves the microstructure of the composite material by adding Mo powder with different contents, and controls the microstructure ratio of the ceramic phase Cr 3 C 2 and Cr 7 C 3 by adjusting the content of the Mo powder added, thereby effectively reducing the size of the ceramic particles and improving the mechanical properties. performance. By comparing Examples 1-3, it can be seen that with the increase of Mo addition, the proportion of Cr 7 C 3 in the ceramic phase increases, and the mechanical properties also increase. ratio is significantly reduced.
Claims (9)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202010312622.3A CN111378858A (en) | 2020-04-20 | 2020-04-20 | A kind of Mo-modified chromium carbide-nickel-chromium composite material and preparation method thereof |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202010312622.3A CN111378858A (en) | 2020-04-20 | 2020-04-20 | A kind of Mo-modified chromium carbide-nickel-chromium composite material and preparation method thereof |
Publications (1)
Publication Number | Publication Date |
---|---|
CN111378858A true CN111378858A (en) | 2020-07-07 |
Family
ID=71222768
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN202010312622.3A Pending CN111378858A (en) | 2020-04-20 | 2020-04-20 | A kind of Mo-modified chromium carbide-nickel-chromium composite material and preparation method thereof |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN111378858A (en) |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS55148744A (en) * | 1979-05-10 | 1980-11-19 | Sumitomo Electric Ind Ltd | Hard alloy for cutting copper and copper alloy |
CN103695836A (en) * | 2013-12-10 | 2014-04-02 | 西北农林科技大学 | Crystal form control method for preparing chromium carbide coating by using chemical gas-phase reaction method |
CN105332012A (en) * | 2015-12-21 | 2016-02-17 | 马鞍山马钢表面工程技术有限公司 | Copper plate electroplating and thermal spraying composite gradient coating of crystallizer and preparation method of coating |
CN105458259A (en) * | 2015-12-08 | 2016-04-06 | 湖北工业大学 | A Laser Forming Method of Cr3C2-NiCr Composite Components |
CN110195211A (en) * | 2019-05-09 | 2019-09-03 | 西安交通大学 | A kind of preparation method of controllable polymorphic type chromium carbide modified graphite |
-
2020
- 2020-04-20 CN CN202010312622.3A patent/CN111378858A/en active Pending
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS55148744A (en) * | 1979-05-10 | 1980-11-19 | Sumitomo Electric Ind Ltd | Hard alloy for cutting copper and copper alloy |
CN103695836A (en) * | 2013-12-10 | 2014-04-02 | 西北农林科技大学 | Crystal form control method for preparing chromium carbide coating by using chemical gas-phase reaction method |
CN105458259A (en) * | 2015-12-08 | 2016-04-06 | 湖北工业大学 | A Laser Forming Method of Cr3C2-NiCr Composite Components |
CN105332012A (en) * | 2015-12-21 | 2016-02-17 | 马鞍山马钢表面工程技术有限公司 | Copper plate electroplating and thermal spraying composite gradient coating of crystallizer and preparation method of coating |
CN110195211A (en) * | 2019-05-09 | 2019-09-03 | 西安交通大学 | A kind of preparation method of controllable polymorphic type chromium carbide modified graphite |
Non-Patent Citations (1)
Title |
---|
WENYAN ZHAI,AT AL: "Effect of molybdenum addition on the microstructure and mechanical properties of Cr3C2-20wt.%Ni cermet,", 《MATERIALS AT HIGH TEMPERATURES》 * |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN100497689C (en) | High-intensity high-tenacity super fine crystal WC-10Co hard alloy preparation method | |
CN101008064A (en) | Whisker plasticizing tungsten carbide-cobalt base hard alloy material and its preparation process | |
CN102628138A (en) | Trace cobalt-containing tungsten carbide without bonding phase and preparation method thereof | |
CN107385303A (en) | A kind of high fine and close and high tenacity metal material and preparation method thereof | |
CN104532041B (en) | Preparation process of a Mo2NiB2-based cermet | |
CN102828096B (en) | Metal ceramic cutting tool material and preparation method thereof | |
CN107523710A (en) | A kind of whisker modified Ti (C, N) based composite metal ceramic preparation of resistance to high temperature oxidation | |
CN103757513A (en) | A Al2O3/Ti (C, N) nanocomposite cermet mold material and its prepn | |
CN111235453A (en) | A kind of cemented carbide with high entropy alloy layer on the surface and preparation method thereof | |
CN105734390A (en) | Method for preparing cubic boron nitride glomerocryst composite combined with high-entropy alloy | |
CN110358960A (en) | A kind of preparation method of high-strength and high ductility Ti (C, N) based ceramic metal | |
CN104789846B (en) | Vanadium carbide nitride titanium based hard alloy and its production method | |
CN114959406A (en) | Oscillatory pressure sintering ultrahigh-temperature medium-entropy ceramic reinforced refractory fine-grain medium-entropy alloy composite material | |
CN114635069A (en) | A kind of high-strength-toughness medium-entropy alloy binder phase Ti(C,N)-based cermet and preparation method thereof | |
CN106916986B (en) | A kind of low cost Mo2FeB2The preparation method of based ceramic metal | |
CN109628786B (en) | Forming preparation method of high-temperature-resistant strengthening and toughening Ti (C, N) -based metal ceramic product | |
CN109053191B (en) | Titanium carbonitride based cermet without binder phase and preparation method thereof | |
CN103949647B (en) | A kind of self-diffusion gradient function complex cutter material and its preparation method | |
CN103468994B (en) | Method for preparing molybdenum nickel chromium boron multivariant boride metal ceramic | |
CN111378858A (en) | A kind of Mo-modified chromium carbide-nickel-chromium composite material and preparation method thereof | |
CN115138849B (en) | Preparation method of binding phase-free hard alloy cutter material | |
CN103710576B (en) | The high-strength nickel niobium alloy material that a kind of scandium, tantalum strengthen | |
CN110484763A (en) | A kind of cermet based on novel binder and its preparation method and application | |
CN1286769C (en) | Preparation method of aluminium oxide base ceramic composite | |
CN112941391B (en) | NbC-containing high-density composite metal ceramic material and preparation method thereof |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PB01 | Publication | ||
PB01 | Publication | ||
SE01 | Entry into force of request for substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
WD01 | Invention patent application deemed withdrawn after publication | ||
WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20200707 |