CN114836666B - High-entropy alloy composite coating for improving surface hardness and wear resistance of metal substrate and processing method - Google Patents
High-entropy alloy composite coating for improving surface hardness and wear resistance of metal substrate and processing method Download PDFInfo
- Publication number
- CN114836666B CN114836666B CN202210319022.9A CN202210319022A CN114836666B CN 114836666 B CN114836666 B CN 114836666B CN 202210319022 A CN202210319022 A CN 202210319022A CN 114836666 B CN114836666 B CN 114836666B
- Authority
- CN
- China
- Prior art keywords
- diamond
- entropy alloy
- metal substrate
- coating
- composite coating
- 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.)
- Active
Links
- 238000000576 coating method Methods 0.000 title claims abstract description 113
- 239000011248 coating agent Substances 0.000 title claims abstract description 112
- 229910045601 alloy Inorganic materials 0.000 title claims abstract description 87
- 239000000956 alloy Substances 0.000 title claims abstract description 87
- 239000002131 composite material Substances 0.000 title claims abstract description 59
- 239000000758 substrate Substances 0.000 title claims abstract description 55
- 229910052751 metal Inorganic materials 0.000 title claims abstract description 50
- 239000002184 metal Substances 0.000 title claims abstract description 50
- 238000003672 processing method Methods 0.000 title claims abstract description 12
- 229910003460 diamond Inorganic materials 0.000 claims abstract description 143
- 239000010432 diamond Substances 0.000 claims abstract description 143
- 238000004372 laser cladding Methods 0.000 claims abstract description 30
- 239000000843 powder Substances 0.000 claims abstract description 26
- 238000000227 grinding Methods 0.000 claims abstract description 23
- 239000002245 particle Substances 0.000 claims abstract description 20
- 238000000034 method Methods 0.000 claims abstract description 9
- 239000010936 titanium Substances 0.000 claims description 13
- 229910001069 Ti alloy Inorganic materials 0.000 claims description 11
- 229910052782 aluminium Inorganic materials 0.000 claims description 10
- 239000011230 binding agent Substances 0.000 claims description 10
- 229910052804 chromium Inorganic materials 0.000 claims description 10
- 229910052759 nickel Inorganic materials 0.000 claims description 10
- 229910052719 titanium Inorganic materials 0.000 claims description 10
- 239000011261 inert gas Substances 0.000 claims description 9
- 239000011863 silicon-based powder Substances 0.000 claims description 9
- 239000000203 mixture Substances 0.000 claims description 7
- 229910000838 Al alloy Inorganic materials 0.000 claims description 6
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 claims description 6
- SWXVUIWOUIDPGS-UHFFFAOYSA-N diacetone alcohol Chemical group CC(=O)CC(C)(C)O SWXVUIWOUIDPGS-UHFFFAOYSA-N 0.000 claims description 6
- 229910052786 argon Inorganic materials 0.000 claims description 3
- 229920002301 cellulose acetate Polymers 0.000 claims description 3
- 238000011049 filling Methods 0.000 claims description 3
- 239000010935 stainless steel Substances 0.000 claims description 3
- 229910001220 stainless steel Inorganic materials 0.000 claims description 3
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 abstract description 5
- 229910052799 carbon Inorganic materials 0.000 abstract description 5
- 230000007547 defect Effects 0.000 abstract description 5
- 229910052710 silicon Inorganic materials 0.000 abstract description 5
- 239000010703 silicon Substances 0.000 abstract description 3
- 229910021332 silicide Inorganic materials 0.000 abstract description 2
- FVBUAEGBCNSCDD-UHFFFAOYSA-N silicide(4-) Chemical compound [Si-4] FVBUAEGBCNSCDD-UHFFFAOYSA-N 0.000 abstract description 2
- 230000007704 transition Effects 0.000 abstract description 2
- 238000010998 test method Methods 0.000 description 32
- 239000010410 layer Substances 0.000 description 26
- 230000000052 comparative effect Effects 0.000 description 18
- 239000000463 material Substances 0.000 description 9
- 238000005253 cladding Methods 0.000 description 8
- 239000010963 304 stainless steel Substances 0.000 description 5
- 229910000589 SAE 304 stainless steel Inorganic materials 0.000 description 5
- 238000007373 indentation Methods 0.000 description 5
- 238000012360 testing method Methods 0.000 description 5
- 238000011068 loading method Methods 0.000 description 3
- 238000005728 strengthening Methods 0.000 description 3
- CSCPPACGZOOCGX-UHFFFAOYSA-N Acetone Chemical compound CC(C)=O CSCPPACGZOOCGX-UHFFFAOYSA-N 0.000 description 2
- HFWDAXXYIWVODI-UHFFFAOYSA-N acetic acid;propan-2-one Chemical compound CC(C)=O.CC(C)=O.CC(O)=O HFWDAXXYIWVODI-UHFFFAOYSA-N 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 2
- 230000001680 brushing effect Effects 0.000 description 2
- 238000003763 carbonization Methods 0.000 description 2
- 229920002678 cellulose Polymers 0.000 description 2
- 239000001913 cellulose Substances 0.000 description 2
- 230000007423 decrease Effects 0.000 description 2
- 238000001035 drying Methods 0.000 description 2
- 229910052581 Si3N4 Inorganic materials 0.000 description 1
- 238000005299 abrasion Methods 0.000 description 1
- 229910002065 alloy metal Inorganic materials 0.000 description 1
- 125000004429 atom Chemical group 0.000 description 1
- 125000004432 carbon atom Chemical group C* 0.000 description 1
- 238000005255 carburizing Methods 0.000 description 1
- 238000004140 cleaning Methods 0.000 description 1
- 239000013078 crystal Substances 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000000835 fiber Substances 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 239000011159 matrix material Substances 0.000 description 1
- 239000000155 melt Substances 0.000 description 1
- 229910052914 metal silicate Inorganic materials 0.000 description 1
- 238000002156 mixing Methods 0.000 description 1
- 238000005498 polishing Methods 0.000 description 1
- 239000011148 porous material Substances 0.000 description 1
- -1 preferably inert Substances 0.000 description 1
- 230000001681 protective effect Effects 0.000 description 1
- 239000002994 raw material Substances 0.000 description 1
- 230000002787 reinforcement Effects 0.000 description 1
- 231100000241 scar Toxicity 0.000 description 1
- 239000002356 single layer Substances 0.000 description 1
- 239000002344 surface layer Substances 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Classifications
-
- 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
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C26/00—Alloys containing diamond or cubic or wurtzitic boron nitride, fullerenes or carbon nanotubes
-
- 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
-
- 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02P—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
- Y02P10/00—Technologies related to metal processing
- Y02P10/25—Process efficiency
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Other Surface Treatments For Metallic Materials (AREA)
Abstract
Description
技术领域technical field
本发明属于耐磨材料领域,具体涉及用于改善金属基底表面硬度及耐磨性的高熵合金复合涂层及加工方法。The invention belongs to the field of wear-resistant materials, and in particular relates to a high-entropy alloy composite coating and a processing method for improving the surface hardness and wear resistance of metal substrates.
背景技术Background technique
金刚石属于高硬度材料,常常应用于各种耐磨结构的表层强化。尤其是对于超耐磨材料的表面,金刚石强化后能够大大增强材料的磨损强度,提高设备的使用寿命。现有金刚石耐磨层工艺中一般采用二步法加工金刚石涂层,首先在部件表面加工区域激光熔融金属,形成金属激光熔池,随后将金刚石粉末加入到金属激光熔池中固化,即可获得金刚石膜层。Diamond is a high-hardness material and is often used in the surface strengthening of various wear-resistant structures. Especially for the surface of super wear-resistant materials, diamond strengthening can greatly enhance the wear strength of materials and improve the service life of equipment. In the existing diamond wear-resistant layer process, a two-step method is generally used to process the diamond coating. First, the laser melts the metal in the surface processing area of the component to form a metal laser molten pool. Then, the diamond powder is added to the metal laser molten pool to solidify, and the obtained diamond film.
但这种工艺存在很多显著的缺陷,首先受限于熔池内部金属液体粘性较大,金刚石嵌入的深度不足,很多金刚石粉末无法形成牢固的粘附面,易于脱落,导致金刚石层的使用寿命较短。However, there are many significant defects in this process. First of all, due to the high viscosity of the metal liquid inside the molten pool, the depth of diamond embedding is insufficient, and many diamond powders cannot form a firm adhesion surface, which is easy to fall off, resulting in a longer service life of the diamond layer. short.
其次,这种结构实质上金刚石层与金属层是分层结构,无论怎么样的加工工艺仅仅能制造单层较薄的耐磨区域,使得加工产品的耐磨性能后期下降严重。Secondly, this structure is essentially a layered structure between the diamond layer and the metal layer. No matter what kind of processing technology can only produce a single layer of thin wear-resistant area, the wear resistance of the processed product will decline seriously in the later stage.
第三,金刚石表层为立体网状碳原子规则排布,与所接触的金属界面中金属晶体仅仅是“接触”而非“结合”,金刚石颗粒仍然通过金属空腔包裹而固定,经过一段时间使用后一旦空腔扩大就会导致金刚石颗粒脱落,从而失去耐磨作用。Third, the surface layer of the diamond is regularly arranged in a three-dimensional network of carbon atoms, and the metal crystals in the contacted metal interface are only "contacted" rather than "bonded". The diamond particles are still wrapped and fixed by the metal cavity, and after a period of use Finally, once the cavity expands, the diamond particles will fall off, thus losing the wear resistance.
因此,尽管金刚石耐磨层在工业应用领域有了相当的技术进步,但在如何更好的提升耐磨度、发挥金刚石耐磨作用方面仍有很大的改进空间。Therefore, although the diamond wear-resistant layer has made considerable technical progress in the field of industrial applications, there is still a lot of room for improvement in how to better improve the wear resistance and exert the diamond wear-resistant effect.
发明内容Contents of the invention
用于改善金属基底表面硬度及耐磨性的高熵合金复合涂层及加工方法,提升金刚石微粒与金属基底材料之间的结合强度,有效提升金刚石层的耐磨强度。The high-entropy alloy composite coating and processing method for improving the surface hardness and wear resistance of metal substrates can improve the bonding strength between diamond particles and metal substrate materials, and effectively improve the wear resistance of the diamond layer.
本发明是通过以下技术方案来实现的:The present invention is achieved through the following technical solutions:
用于改善金属基底表面硬度及耐磨性的高熵合金复合涂层,包括高熵合金和金刚石粉末,高熵合金的表达式为FeaCobCrcNidAleTifSig,高熵合金与金刚石粉末微粒接触界面处发生由金刚石到合金界面区域的渗碳。A high-entropy alloy composite coating used to improve the surface hardness and wear resistance of metal substrates, including high-entropy alloys and diamond powder, the expression of high-entropy alloys is Fe a Co b Cr c Ni d Al e Ti f Sig , high Carburization from diamond to alloy interface occurs at the contact interface between entropy alloy and diamond powder particles.
优选的,高熵合金中原子比a-f的比例为1:0.5~1.5:1.1~2.1:0.5~1.4:0.1~1.0:0.2~1.1:0.1~0.8。在本发明的优选方式中,a-f的比例为1:1:1:1:0.5:0.5:0.2。Preferably, the atomic ratio a-f in the high-entropy alloy is 1:0.5-1.5:1.1-2.1:0.5-1.4:0.1-1.0:0.2-1.1:0.1-0.8. In a preferred mode of the present invention, the ratio of a-f is 1:1:1:1:0.5:0.5:0.2.
优选的,所述金刚石粉末占高熵合金的0.1-15wt%。Preferably, the diamond powder accounts for 0.1-15wt% of the high-entropy alloy.
更进一步的,所述金刚石粉末占高熵合金的3wt%-15wt%,更为优选的,为10wt%-12wt%。Furthermore, the diamond powder accounts for 3wt%-15wt% of the high-entropy alloy, more preferably, 10wt%-12wt%.
优选的,金刚石粉末的微粒平均粒度为50-80μm。Preferably, the average particle size of the diamond powder is 50-80 μm.
用于改善金属基底表面硬度及耐磨性的高熵合金复合涂层的加工方法,包括以下步骤:A processing method for a high-entropy alloy composite coating for improving the surface hardness and wear resistance of a metal substrate, comprising the following steps:
a.金属基底预处理:将金属基底进行打磨,去除毛刺,打磨表面,去除表面的氧化膜,后经超声清洗,烘干;a. Metal substrate pretreatment: Grinding the metal substrate, removing burrs, polishing the surface, removing the oxide film on the surface, and then ultrasonically cleaning and drying;
b.预置涂层:将纯Fe、Co、Cr、Ni、Al、Ti、Si粉末、金刚石粉末与粘结剂混匀,涂覆于金属基底表面,烘干后获得表面负载有涂层的金属基底;b. Pre-coating: Mix pure Fe, Co, Cr, Ni, Al, Ti, Si powder, diamond powder and binder, coat on the surface of the metal substrate, and obtain a coating on the surface after drying metal substrate;
c.激光熔覆:将上述表面负载有涂层的金属基底置于惰性气体中,惰性优选的,气体为氩气,充入量为0.13-0.37dm3,以激光熔覆头为能量源,采用正离焦的方式,垂直作用于涂层表面,优选的,控制激光熔覆头的离焦量为30-50mm,激光功率为1000-2000W,促使在金刚石粉末表层与高熵合金接触面发生渗碳强化,形成金刚石磨层。c. Laser cladding: place the above-mentioned metal substrate with the coating on its surface in an inert gas, preferably inert, the gas is argon, the filling amount is 0.13-0.37dm 3 , and the laser cladding head is used as the energy source. Adopt positive defocusing method, act vertically on the coating surface, preferably, control the defocusing amount of the laser cladding head to 30-50mm, and laser power to 1000-2000W, so as to promote the occurrence of Carburized and strengthened to form a diamond grinding layer.
需要说明的是,本技术方案中,金刚石碳与合金金属成分之间发生渗碳可以强化合金硬度,同时渗碳微观结构与Si元素形成SiC、金属硅酸盐的混合成分,将金刚石微粒与合金相牢固结合。It should be noted that in this technical solution, carburization between diamond carbon and alloy metal components can strengthen the hardness of the alloy, and at the same time, the carburizing microstructure and Si elements form a mixed composition of SiC and metal silicate, and the diamond particles and alloy firmly combined.
优选的,在a中,所述金属基底为钛合金金属基底、铝合金金属基底或不锈钢金属基底中的一种,优选的,所述钛合金基底为TC4钛合金基底,所述不锈钢基底为304不锈钢基底。Preferably, in a, the metal substrate is one of a titanium alloy metal substrate, an aluminum alloy metal substrate or a stainless steel metal substrate, preferably, the titanium alloy substrate is a TC4 titanium alloy substrate, and the stainless steel substrate is 304 Stainless steel base.
优选的,在b中,所述纯Fe、Co、Cr、Ni、Al、Ti、Si粉末的平均粒度为35-50μm,所述金刚石粉末的平均粒度为50-80μm,所述粘结剂质量所述纯Fe、Co、Cr、Ni、Al、Ti、Si粉末和金刚石粉末所形成的混合物质量的20~35wt%,所述的粘结剂为乙酸纤维素的二丙酮醇溶液,浓度为4.2-4.3g/100mL。Preferably, in b, the average particle size of the pure Fe, Co, Cr, Ni, Al, Ti, Si powder is 35-50 μm, the average particle size of the diamond powder is 50-80 μm, the quality of the binder The mass of the mixture formed by the pure Fe, Co, Cr, Ni, Al, Ti, Si powder and diamond powder is 20 to 35 wt%, and the binder is diacetone alcohol solution of cellulose acetate with a concentration of 4.2 -4.3g/100mL.
优选的,在c中,所述金刚石磨层的厚度为0.1~1.5mm,所述的激光熔覆的扫描速度为8-12mm/s;所述惰性气体的输送压力控制为0.05-0.15MPa。Preferably, in c, the thickness of the diamond grinding layer is 0.1-1.5mm, the scanning speed of the laser cladding is 8-12mm/s; the delivery pressure of the inert gas is controlled to be 0.05-0.15MPa.
有益效果:Beneficial effect:
1、金刚石主要成分为碳单质,本技术方案中加入硅单质,金刚石表层碳与硅之间形成SiC高硬度结构,Si与其他合金之间形成硬质金属硅化物,依靠Si的过渡元素特性在原子层面将金刚石表层原子与合金接触面牢固结合,提升金刚石微粒的固定强度;1. The main component of diamond is simple carbon. In this technical solution, simple silicon is added. A SiC high-hardness structure is formed between carbon and silicon on the surface of the diamond, and a hard metal silicide is formed between Si and other alloys. Relying on the transition element characteristics of Si in At the atomic level, the atoms on the surface of the diamond are firmly combined with the contact surface of the alloy to improve the fixation strength of the diamond particles;
2、金刚石粉末与金属粉末共混加工,通过调控激光强度,避免金刚石被碳化的同时,促进与金刚石接触的金属表面发生碳化,提升接触面处金属的硬度,提升金刚石颗粒的牢固性;2. Diamond powder and metal powder are blended and processed. By adjusting the laser intensity, the carbonization of the diamond is avoided, and the carbonization of the metal surface in contact with the diamond is promoted, the hardness of the metal at the contact surface is improved, and the firmness of the diamond particles is improved;
3、Fe、Co、Cr、Ni、Al、Ti、Si成分的硬质合金与金刚石的硬度相配合,既保证金刚石的牢固性,又能确保合金本身有足够的硬度和任性,保证金刚石的安装强度和整体合金的结构强度,以金刚石作为强化相,将涂层的硬度较金属基底有了极大提高,显著改善耐磨性;3. The cemented carbide composed of Fe, Co, Cr, Ni, Al, Ti, Si is compatible with the hardness of diamond, which not only ensures the firmness of diamond, but also ensures that the alloy itself has sufficient hardness and willfulness to ensure the installation of diamond Strength and structural strength of the overall alloy, with diamond as the strengthening phase, the hardness of the coating is greatly improved compared with the metal substrate, and the wear resistance is significantly improved;
4、激光熔覆制备的金刚石增强的高熵合金复合涂层的表面连续、光滑,表面缺陷较少,涂层与金属基底间结合较好,且涂层内部无气孔和缩松等缺陷,组织致密性好;4. The surface of the diamond-enhanced high-entropy alloy composite coating prepared by laser cladding is continuous and smooth, with few surface defects, good bonding between the coating and the metal substrate, and no defects such as pores and shrinkage porosity inside the coating. Good compactness;
5、加工方法简单,可控性好,制得的金刚石增强的高熵合金复合涂层的显微硬度和耐磨性能都得到了显著提高,有利于复合涂层适应更加复杂和恶劣的工作环境,具有很好的应用前景。5. The processing method is simple and the controllability is good. The microhardness and wear resistance of the prepared diamond-enhanced high-entropy alloy composite coating have been significantly improved, which is beneficial for the composite coating to adapt to more complex and harsh working environments. , has a good application prospect.
附图说明Description of drawings
图1.对比实施例、实施例1-14中制备得到的金刚石增强的高熵合金复合涂层的显微硬度比较图;Fig. 1. compares the microhardness figure of the diamond-enhanced high-entropy alloy composite coating prepared in comparative example, embodiment 1-14;
图2.对比实施例、实施例1-14中制备得到的金刚石增强的高熵合金复合涂层的耐磨性比较图。Figure 2. Comparison of wear resistance of diamond-enhanced high-entropy alloy composite coatings prepared in Comparative Examples and Examples 1-14.
具体实施方式Detailed ways
下面的实施例将对本发明予以进一步的说明,但并不因此而限制本发明。The following examples will further illustrate the present invention, but do not limit the present invention thereby.
实施例中所制备样品硬度测试方法:Prepared sample hardness test method in the embodiment:
将金刚石增强的高熵合金复合涂层样品的横截面镶嵌后抛光,采用HX-1000显微维氏硬度计测量涂层横截面的显微硬度,所加载荷为200g,加载时间为15s;The cross-section of the diamond-enhanced high-entropy alloy composite coating sample was inlaid and polished, and the microhardness of the coating cross-section was measured with a HX-1000 micro-Vickers hardness tester. The applied load was 200g, and the loading time was 15s;
各熔覆样品表面均匀选取5个点(点与点之间保持一定距离),测试硬度值后取平均值;Select 5 points evenly on the surface of each cladding sample (keep a certain distance between points), and take the average value after testing the hardness value;
它的工作原理是通过加载一定值的负载将金刚石压头压入被检测材料的表面,加载一定的时间,卸载后残留在试样表面的近似菱形的印记,测量得到压痕的对角线的长度得到压痕面积,然后通过计算加载载荷和压痕面积的比值即可得出该材料的显微硬度;Its working principle is to press the diamond indenter into the surface of the material to be tested by loading a certain value of load, load it for a certain period of time, and then measure the approximate diamond-shaped imprint left on the surface of the sample after unloading, and measure the diagonal of the indentation. The indentation area is obtained by the length, and then the microhardness of the material can be obtained by calculating the ratio of the loading load to the indentation area;
显微硬度测试的压头采用对面夹角为136°的正四面棱锥金刚石压头,维氏硬度值计算公式如下所示:The indenter for the microhardness test uses a regular tetrahedral pyramidal diamond indenter with an included angle of 136°. The formula for calculating the Vickers hardness value is as follows:
式中:F——载荷/kgf;In the formula: F——load/kgf;
S——压痕表面积;S - indentation surface area;
α——压头相对面夹角=136°;α——the angle between the opposite faces of the indenter = 136°;
d——平均压痕对角线长度;d - average indentation diagonal length;
HV——维氏硬度值。HV - Vickers hardness value.
实施例中所制备样品耐磨性测试方法:Prepared sample abrasion resistance test method in the embodiment:
本发明高熵合金复合涂层的耐磨性是通过多功能摩擦磨损试验机测量的,试验条件为:载荷50N,转速100r/min,磨痕半径3mm,时间30min,运动模式为球盘式,对磨头材质为Si3N4;测试前后,利用分析天平称量计算磨损量。The wear resistance of the high-entropy alloy composite coating of the present invention is measured by a multi-functional friction and wear testing machine. The test conditions are: load 50N, rotating speed 100r/min, wear scar radius 3mm, time 30min, motion mode is ball-on-disk type, The material of the grinding head is Si3N4; before and after the test, use the analytical balance to weigh and calculate the amount of wear.
对比实施例:Comparative example:
为了与下述实施例1-13进行对比,对比实施例中金属基底表面为FeaCobCrcNidAleTifSig高熵合金涂层,不加入金刚石增强相,具体加工方法如下:In order to compare with the following examples 1-13, the surface of the metal substrate in the comparative example is Fe a Co b Cr c Ni d Al e Ti f Sig high entropy alloy coating, without adding diamond reinforcement phase, the specific processing method is as follows :
使用TC4钛合金基底,将基材加工成30mm×20mm×6mm的板状试样块,再对板状试样块进行打磨去除毛刺以及表面的氧化膜,用超声波丙酮清洗,随后烘干;用粘结剂将干燥的纯Fe、Co、Cr、Ni、Al、Ti、Si粉末均匀刷涂在试样表面,高熵合金中:a=1,b=1,c=1,d=1,e=0.5,f=0.5,g=0.2。刷涂厚度为0.8mm。预置成功后,在对涂层进行激光熔覆。Using a TC4 titanium alloy substrate, the base material is processed into a plate-shaped sample block of 30mm×20mm×6mm, and then the plate-shaped sample block is polished to remove burrs and oxide films on the surface, cleaned with ultrasonic acetone, and then dried; Binder Brush dry pure Fe, Co, Cr, Ni, Al, Ti, Si powder evenly on the sample surface, in high entropy alloy: a=1, b=1, c=1, d=1, e=0.5, f=0.5, g=0.2. Brushing thickness is 0.8mm. After successful presetting, laser cladding is performed on the coating.
需要说明的是,激光熔覆时,可将激光熔覆头通过机器人固定在其手臂上,通过调节机器人的运动实现熔覆头的移动,完成熔覆工作。It should be noted that during laser cladding, the laser cladding head can be fixed on its arm through the robot, and the movement of the cladding head can be realized by adjusting the movement of the robot to complete the cladding work.
利用涂层显微硬度测试方法,测得上述涂层的显微硬度约为559.3HV,利用涂层的耐磨性测试方法测得上述高熵合金涂层的磨损量约为6.3mg。Using the coating microhardness test method, the microhardness of the above coating was measured to be about 559.3HV, and the wear resistance of the above high entropy alloy coating was measured to be about 6.3mg by using the coating wear resistance test method.
实施例1:Example 1:
本实施例中,a的步骤与对比实施例一致,使用TC4钛合金基底,区别在于,增加了步骤b和c,该复合涂层的具体加工方法如下:In the present embodiment, the step of a is consistent with the comparative example, using the TC4 titanium alloy substrate, the difference is that steps b and c have been added, and the specific processing method of the composite coating is as follows:
b.在平均粒度为50μm纯Fe、Co、Cr、Ni、Al、Ti、Si粉末中混入质量分数为3%的平均粒度为80μm的金刚石粉末,经球磨机均匀混合后,烘干,球磨机转速为500r/min。将制备好的涂层原料粉末用粘结剂刷涂在已经被去除氧化膜的金属基底表面,刷涂厚度为0.8mm,粘结剂用量为上述混合物质量的20~35wt%,涂层预置好之后装夹固定于工作台上。b. In the average particle size of 50 μm pure Fe, Co, Cr, Ni, Al, Ti, Si powder, the diamond powder with an average particle size of 3% is mixed with a mass fraction of 80 μm, and after being uniformly mixed by a ball mill, it is dried, and the ball mill speed is 500r/min. Brush the prepared coating raw material powder with a binder on the surface of the metal substrate that has been removed from the oxide film, the brushing thickness is 0.8mm, the amount of the binder is 20-35wt% of the mass of the above mixture, and the coating is preset After that, clamp and fix it on the workbench.
粘结剂为乙酸纤维素-二丙酮醇溶液,乙酸纤维素-二丙酮醇溶液由200mL二丙酮醇与8.5g乙酸纤维素,经90℃水浴加热10min均匀混合而制得。The binder is cellulose acetate-diacetone alcohol solution. The cellulose acetate-diacetone alcohol solution is prepared by uniformly mixing 200mL diacetone alcohol and 8.5g cellulose acetate in a water bath at 90°C for 10 minutes.
c.如图1所示,采用光纤激光器作为能量源,功率为1500W的激光垂直作用于涂层表面,离焦量为45mm,熔覆头在机器人的控制下作直线运动,扫描速度为10mm/s,惰性气体输送方向与涂层表面平行,输送速率为15L/min。c. As shown in Figure 1, a fiber laser is used as the energy source, and the laser with a power of 1500W acts vertically on the coating surface with a defocus of 45mm. The cladding head moves linearly under the control of the robot, and the scanning speed is 10mm/ s, the delivery direction of the inert gas is parallel to the coating surface, and the delivery rate is 15L/min.
得到的金刚石磨层的厚度为0.72mm,利用涂层显微硬度测试方法测得上述3%金刚石增强的FeCoCrNiAlTiSi高熵合金复合涂层的显微硬度约为653.2HV,利用涂层的耐磨性测试方法测得上述金刚石增强的高熵合金复合涂层的磨损量约为3.7mg。The thickness of the obtained diamond grinding layer is 0.72mm, and the microhardness of the above-mentioned 3% diamond-reinforced FeCoCrNiAlTiSi high-entropy alloy composite coating is measured by the coating microhardness test method to be about 653.2HV. The test method measures that the wear amount of the diamond-enhanced high-entropy alloy composite coating is about 3.7 mg.
实施例2:Example 2:
本实施例与实施例1基本相同,使用TC4钛合金基底,所不同的是本实施例中金刚石的质量分数为6%,其他实验条件相同。This example is basically the same as Example 1, using a TC4 titanium alloy substrate, except that the mass fraction of diamond in this example is 6%, and other experimental conditions are the same.
得到的金刚石磨层的厚度为0.76mm,利用涂层显微硬度测试方法测得上述金刚石增强的高熵合金复合涂层的显微硬度约为825.1HV,利用涂层的耐磨性测试方法测得上述金刚石增强的高熵合金复合涂层的磨损量约为3.3mg。The thickness of the obtained diamond grinding layer is 0.76mm, and the microhardness of the above-mentioned diamond-enhanced high-entropy alloy composite coating is measured by the coating microhardness test method to be about 825.1HV, and the wear resistance test method of the coating is used to measure The wear amount of the above-mentioned diamond-enhanced high-entropy alloy composite coating is about 3.3 mg.
与对比实施例相比,本实施例中采用激光熔覆的方法制备得到的金刚石增强的高熵合金复合涂层的力学性能得到明显改善。Compared with the comparative example, the mechanical properties of the diamond-enhanced high-entropy alloy composite coating prepared by laser cladding in this example are significantly improved.
实施例3:Example 3:
本实施例与实施例1基本相同,使用TC4钛合金基底,所不同的是本实施例中金刚石的质量分数为9%,其他实验条件相同。This example is basically the same as Example 1, using a TC4 titanium alloy substrate, the difference is that the mass fraction of diamond in this example is 9%, and other experimental conditions are the same.
得到的金刚石磨层的厚度为0.75mm,利用涂层显微硬度测试方法测得上述金刚石增强的高熵合金复合涂层的显微硬度约为912.4HV,利用涂层的耐磨性测试方法测得上述金刚石增强的高熵合金复合涂层的磨损量约为2.9mg。The thickness of the obtained diamond grinding layer is 0.75mm, and the microhardness of the above-mentioned diamond-enhanced high-entropy alloy composite coating is measured by the coating microhardness test method to be about 912.4HV, and the wear resistance test method of the coating is used to measure The wear amount of the above-mentioned diamond-enhanced high-entropy alloy composite coating is about 2.9 mg.
与对比实施例相比,本实施例中采用激光熔覆的方法制备得到的金刚石增强的高熵合金复合涂层的力学性能得到明显改善。Compared with the comparative example, the mechanical properties of the diamond-enhanced high-entropy alloy composite coating prepared by laser cladding in this example are significantly improved.
实施例4:Example 4:
本实施例与实施例1基本相同,使用TC4钛合金基底,所不同的是本实施例中金刚石的质量分数为10%,其他实验条件相同。This example is basically the same as Example 1, using a TC4 titanium alloy substrate, the difference is that the mass fraction of diamond in this example is 10%, and other experimental conditions are the same.
得到的金刚石磨层的厚度为0.86mm,利用涂层显微硬度测试方法测得上述金刚石增强的高熵合金复合涂层的显微硬度约为1053.6HV,利用涂层的耐磨性测试方法测得上述金刚石增强的高熵合金复合涂层的磨损量约为2.2mg。The thickness of the obtained diamond grinding layer is 0.86mm, and the microhardness of the above-mentioned diamond-enhanced high-entropy alloy composite coating is measured by the coating microhardness test method to be about 1053.6HV, and the wear resistance test method of the coating is used to measure The wear amount of the above-mentioned diamond-enhanced high-entropy alloy composite coating is about 2.2 mg.
与对比实施例相比,本实施例中采用激光熔覆的方法制备得到的金刚石增强的高熵合金复合涂层的力学性能得到明显改善。Compared with the comparative example, the mechanical properties of the diamond-enhanced high-entropy alloy composite coating prepared by laser cladding in this example are significantly improved.
实施例5:Example 5:
本实施例与实施例1基本相同,使用TC4钛合金基底,所不同的是本实施例中金刚石的质量分数为11%,其他实验条件相同。This example is basically the same as Example 1, using a TC4 titanium alloy substrate, the difference is that the mass fraction of diamond in this example is 11%, and other experimental conditions are the same.
得到的金刚石磨层的厚度为0.85mm,利用涂层显微硬度测试方法测得上述金刚石增强的高熵合金复合涂层的显微硬度约为1033.5HV,利用涂层的耐磨性测试方法测得上述金刚石增强的高熵合金复合涂层的磨损量约为2.3mg。The thickness of the obtained diamond grinding layer is 0.85mm, and the microhardness of the above-mentioned diamond-enhanced high-entropy alloy composite coating is measured by the coating microhardness test method to be about 1033.5HV, and the wear resistance test method of the coating is used to measure The wear amount of the above-mentioned diamond-enhanced high-entropy alloy composite coating is about 2.3 mg.
与对比实施例相比,本实施例中采用激光熔覆的方法制备得到的金刚石增强的高熵合金复合涂层的力学性能得到明显改善。Compared with the comparative example, the mechanical properties of the diamond-enhanced high-entropy alloy composite coating prepared by laser cladding in this example are significantly improved.
实施例6:Embodiment 6:
本实施例与实施例1基本相同,使用TC4钛合金基底,所不同的是本实施例中金刚石的质量分数为12%,其他实验条件相同。This example is basically the same as Example 1, using a TC4 titanium alloy substrate, the difference is that the mass fraction of diamond in this example is 12%, and other experimental conditions are the same.
得到的金刚石磨层的厚度为0.84mm,利用涂层显微硬度测试方法测得上述金刚石增强的高熵合金复合涂层的显微硬度约为1028.4HV,利用涂层的耐磨性测试方法测得上述金刚石增强的高熵合金复合涂层的磨损量约为2.6mg。The thickness of the obtained diamond grinding layer is 0.84mm, and the microhardness of the above-mentioned diamond-enhanced high-entropy alloy composite coating is measured by the coating microhardness test method to be about 1028.4HV, and the wear resistance test method of the coating is used to measure The wear amount of the above-mentioned diamond-enhanced high-entropy alloy composite coating is about 2.6mg.
与对比实施例相比,本实施例中采用激光熔覆的方法制备得到的金刚石增强的高熵合金复合涂层的力学性能得到明显改善。Compared with the comparative example, the mechanical properties of the diamond-enhanced high-entropy alloy composite coating prepared by laser cladding in this example are significantly improved.
实施例7:Embodiment 7:
本实施例与实施例1基本相同,使用304不锈钢基底,所不同的是本实施例中金刚石的质量分数为9%,其他实验条件相同。This embodiment is basically the same as Embodiment 1, using 304 stainless steel substrate, the difference is that the mass fraction of diamond in this embodiment is 9%, and other experimental conditions are the same.
得到的金刚石磨层的厚度为0.53mm,利用涂层显微硬度测试方法测得上述金刚石增强的高熵合金复合涂层的显微硬度约为901.2HV,利用涂层的耐磨性测试方法测得上述金刚石增强的高熵合金复合涂层的磨损量约为3.8mg。The thickness of the obtained diamond grinding layer is 0.53mm, and the microhardness of the above-mentioned diamond-enhanced high-entropy alloy composite coating is measured by the coating microhardness test method to be about 901.2HV, and the wear resistance test method of the coating is used to measure The wear amount of the above-mentioned diamond-enhanced high-entropy alloy composite coating is about 3.8 mg.
与对比实施例相比,本实施例中采用激光熔覆的方法制备得到的金刚石增强的高熵合金复合涂层的力学性能得到明显改善。Compared with the comparative example, the mechanical properties of the diamond-enhanced high-entropy alloy composite coating prepared by laser cladding in this example are significantly improved.
实施例8:Embodiment 8:
本实施例与实施例1基本相同,使用304不锈钢基底,所不同的是本实施例中金刚石的质量分数为10%,其他实验条件相同。This embodiment is basically the same as Embodiment 1, using 304 stainless steel substrate, the difference is that the mass fraction of diamond in this embodiment is 10%, and other experimental conditions are the same.
得到的金刚石磨层的厚度为0.73mm,利用涂层显微硬度测试方法测得上述金刚石增强的高熵合金复合涂层的显微硬度约为1072.9HV,利用涂层的耐磨性测试方法测得上述金刚石增强的高熵合金复合涂层的磨损量约为2.5mg。The thickness of the obtained diamond grinding layer is 0.73mm, and the microhardness of the above-mentioned diamond-enhanced high-entropy alloy composite coating is measured by the coating microhardness test method to be about 1072.9HV, and the wear resistance test method of the coating is used to measure The wear amount of the above-mentioned diamond-enhanced high-entropy alloy composite coating is about 2.5 mg.
与对比实施例相比,本实施例中采用激光熔覆的方法制备得到的金刚石增强的高熵合金复合涂层的力学性能得到明显改善。Compared with the comparative example, the mechanical properties of the diamond-enhanced high-entropy alloy composite coating prepared by laser cladding in this example are significantly improved.
实施例9:Embodiment 9:
本实施例与实施例1基本相同,使用304不锈钢基底,所不同的是本实施例中金刚石的质量分数为11%,其他实验条件相同。This embodiment is basically the same as Embodiment 1, using 304 stainless steel substrate, the difference is that the mass fraction of diamond in this embodiment is 11%, and other experimental conditions are the same.
得到的金刚石磨层的厚度为0.64mm,利用涂层显微硬度测试方法测得上述金刚石增强的高熵合金复合涂层的显微硬度约为1042.1HV,利用涂层的耐磨性测试方法测得上述金刚石增强的高熵合金复合涂层的磨损量约为2.7mg。The thickness of the obtained diamond grinding layer is 0.64mm, and the microhardness of the above-mentioned diamond-enhanced high-entropy alloy composite coating is measured by the coating microhardness test method to be about 1042.1HV, and the wear resistance test method of the coating is used to measure The wear amount of the above-mentioned diamond-enhanced high-entropy alloy composite coating is about 2.7 mg.
与对比实施例相比,本实施例中采用激光熔覆的方法制备得到的金刚石增强的高熵合金复合涂层的力学性能得到明显改善。Compared with the comparative example, the mechanical properties of the diamond-enhanced high-entropy alloy composite coating prepared by laser cladding in this example are significantly improved.
实施例10:Example 10:
本实施例与实施例1基本相同,使用304不锈钢基底,所不同的是本实施例中金刚石的质量分数为12%,其他实验条件相同。This example is basically the same as Example 1, using a 304 stainless steel substrate, the difference is that the mass fraction of diamond in this example is 12%, and other experimental conditions are the same.
得到的金刚石磨层的厚度为0.61mm,利用涂层显微硬度测试方法测得上述金刚石增强的高熵合金复合涂层的显微硬度约为1012.3HV,利用涂层的耐磨性测试方法测得上述金刚石增强的高熵合金复合涂层的磨损量约为2.8mg。The thickness of the obtained diamond grinding layer is 0.61mm, and the microhardness of the above-mentioned diamond-enhanced high-entropy alloy composite coating is measured by the coating microhardness test method to be about 1012.3HV, and the wear resistance test method of the coating is used to measure The wear amount of the above-mentioned diamond-enhanced high-entropy alloy composite coating is about 2.8 mg.
与对比实施例相比,本实施例中采用激光熔覆的方法制备得到的金刚石增强的高熵合金复合涂层的力学性能得到明显改善。Compared with the comparative example, the mechanical properties of the diamond-enhanced high-entropy alloy composite coating prepared by laser cladding in this example are significantly improved.
实施例11:Example 11:
本实施例与实施例1基本相同,使用铝合金基底,所不同的是本实施例中金刚石的质量分数为9%,其他实验条件相同。This example is basically the same as Example 1, using an aluminum alloy substrate, except that the mass fraction of diamond in this example is 9%, and other experimental conditions are the same.
得到的金刚石磨层的厚度为0.73mm,利用涂层显微硬度测试方法测得上述金刚石增强的高熵合金复合涂层的显微硬度约为913.4HV,利用涂层的耐磨性测试方法测得上述金刚石增强的高熵合金复合涂层的磨损量约为3.6mg。The thickness of the obtained diamond grinding layer is 0.73mm, and the microhardness of the above-mentioned diamond-enhanced high-entropy alloy composite coating is measured by the coating microhardness test method to be about 913.4HV, and the wear resistance test method of the coating is used to measure The wear amount of the above-mentioned diamond-enhanced high-entropy alloy composite coating is about 3.6 mg.
与对比实施例相比,本实施例中采用激光熔覆的方法制备得到的金刚石增强的高熵合金复合涂层的力学性能得到明显改善。Compared with the comparative example, the mechanical properties of the diamond-enhanced high-entropy alloy composite coating prepared by laser cladding in this example are significantly improved.
实施例12:Example 12:
本实施例与实施例1基本相同,使用铝合金基底,所不同的是本实施例中金刚石的质量分数为10%,其他实验条件相同。This example is basically the same as Example 1, using an aluminum alloy substrate, except that the mass fraction of diamond in this example is 10%, and other experimental conditions are the same.
得到的金刚石磨层的厚度为0.89mm,利用涂层显微硬度测试方法测得上述金刚石增强的高熵合金复合涂层的显微硬度约为1151.4HV,利用涂层的耐磨性测试方法测得上述金刚石增强的高熵合金复合涂层的磨损量约为2.1mg。The thickness of the obtained diamond grinding layer is 0.89mm, and the microhardness of the above-mentioned diamond-enhanced high-entropy alloy composite coating is measured by the coating microhardness test method to be about 1151.4HV, and the wear resistance test method of the coating is used to measure The wear amount of the above-mentioned diamond-enhanced high-entropy alloy composite coating is about 2.1 mg.
与对比实施例相比,本实施例中采用激光熔覆的方法制备得到的金刚石增强的高熵合金复合涂层的力学性能得到明显改善。Compared with the comparative example, the mechanical properties of the diamond-enhanced high-entropy alloy composite coating prepared by laser cladding in this example are significantly improved.
实施例13:Example 13:
本实施例与实施例1基本相同,使用铝合金基底,所不同的是本实施例中金刚石的质量分数为11%,其他实验条件相同。This example is basically the same as Example 1, using an aluminum alloy substrate, except that the mass fraction of diamond in this example is 11%, and other experimental conditions are the same.
得到的金刚石磨层的厚度为0.83mm,利用涂层显微硬度测试方法测得上述金刚石增强的高熵合金复合涂层的显微硬度约为1035.1HV,利用涂层的耐磨性测试方法测得上述金刚石增强的高熵合金复合涂层的磨损量约为2.4mg。The thickness of the obtained diamond grinding layer is 0.83mm, and the microhardness of the above-mentioned diamond-enhanced high-entropy alloy composite coating is measured by the coating microhardness test method to be about 1035.1HV, and the wear resistance test method of the coating is used to measure The wear amount of the above-mentioned diamond-enhanced high-entropy alloy composite coating is about 2.4 mg.
与对比实施例相比,本实施例中采用激光熔覆的方法制备得到的金刚石增强的高熵合金复合涂层的力学性能得到明显改善。Compared with the comparative example, the mechanical properties of the diamond-enhanced high-entropy alloy composite coating prepared by laser cladding in this example are significantly improved.
实施例14:Example 14:
本实施例与实施例1基本相同,使用铝合金基底,所不同的是本实施例中金刚石的质量分数为12%,其他实验条件相同。This example is basically the same as Example 1, using an aluminum alloy substrate, except that the mass fraction of diamond in this example is 12%, and other experimental conditions are the same.
得到的金刚石磨层的厚度为0.81mm,利用涂层显微硬度测试方法测得上述金刚石增强的高熵合金复合涂层的显微硬度约为992.3HV,利用涂层的耐磨性测试方法测得上述金刚石增强的高熵合金复合涂层的磨损量约为2.8mg。The thickness of the obtained diamond grinding layer is 0.81mm, and the microhardness of the above-mentioned diamond-enhanced high-entropy alloy composite coating is measured by the coating microhardness test method to be about 992.3HV, and the wear resistance test method of the coating is used to measure The wear amount of the above-mentioned diamond-enhanced high-entropy alloy composite coating is about 2.8mg.
与对比实施例相比,本实施例中采用激光熔覆的方法制备得到的金刚石增强的高熵合金复合涂层的力学性能得到明显改善。Compared with the comparative example, the mechanical properties of the diamond-enhanced high-entropy alloy composite coating prepared by laser cladding in this example are significantly improved.
图1的结果表明,金刚石含量的增加可以明显的提高熔覆层的硬度。The results in Figure 1 show that the increase in diamond content can significantly increase the hardness of the cladding layer.
图2的结果表明,随着金刚石含量的增加,熔覆层中硬质颗粒数量增多,颗粒间的距离减小,对熔覆层粘结相的保护作用增强,从而能够减少基体相的磨损脱落,提高熔覆层的耐磨性。The results in Figure 2 show that with the increase of diamond content, the number of hard particles in the cladding layer increases, the distance between particles decreases, and the protective effect on the bonding phase of the cladding layer is enhanced, thereby reducing the wear and tear of the matrix phase , improve the wear resistance of the cladding layer.
以上所述,仅为本发明的具体实施方式,但本发明的保护范围并不局限于此,任何不经过创造性劳动想到的变化或替换,都应涵盖在本发明的保护范围之内。因此,本发明的保护范围应该以权利要求书所限定的保护范围为准。The above is only a specific implementation of the present invention, but the scope of protection of the present invention is not limited thereto, and any changes or replacements that do not come to mind through creative work shall be covered within the scope of protection of the present invention. Therefore, the protection scope of the present invention should be determined by the protection scope defined in the claims.
Claims (4)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202210319022.9A CN114836666B (en) | 2022-03-29 | 2022-03-29 | High-entropy alloy composite coating for improving surface hardness and wear resistance of metal substrate and processing method |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202210319022.9A CN114836666B (en) | 2022-03-29 | 2022-03-29 | High-entropy alloy composite coating for improving surface hardness and wear resistance of metal substrate and processing method |
Publications (2)
Publication Number | Publication Date |
---|---|
CN114836666A CN114836666A (en) | 2022-08-02 |
CN114836666B true CN114836666B (en) | 2023-08-15 |
Family
ID=82563249
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN202210319022.9A Active CN114836666B (en) | 2022-03-29 | 2022-03-29 | High-entropy alloy composite coating for improving surface hardness and wear resistance of metal substrate and processing method |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN114836666B (en) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN118854137B (en) * | 2024-09-26 | 2024-12-27 | 南通理工学院 | Si-containing high-entropy alloy material resistant to molten chloride corrosion and preparation method thereof |
Citations (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5268217A (en) * | 1990-09-27 | 1993-12-07 | Diamonex, Incorporated | Abrasion wear resistant coated substrate product |
CN105506716A (en) * | 2015-12-25 | 2016-04-20 | 苏州宏久航空防热材料科技有限公司 | Preparation method for high-bonding wearproof composite coating |
CN107034462A (en) * | 2017-06-09 | 2017-08-11 | 上海工程技术大学 | One kind is used for stainless steel surfaces acieral coating and preparation method thereof |
CN107299342A (en) * | 2017-07-05 | 2017-10-27 | 暨南大学 | A kind of high-entropy alloy coating and its production and use |
CN108315686A (en) * | 2017-12-08 | 2018-07-24 | 水利部杭州机械设计研究所 | A kind of puppet high-entropy alloy coating formula and its coating production |
CN108893738A (en) * | 2018-08-07 | 2018-11-27 | 华东交通大学 | A kind of superhard Fe-Ni based alloy wear-resistant coating of equiax crystal and preparation method thereof |
CN109468638A (en) * | 2019-01-09 | 2019-03-15 | 苏州科技大学 | A kind of preparation method of diamond reinforced high-entropy alloy composite coating |
CN113278965A (en) * | 2021-05-07 | 2021-08-20 | 太原理工大学 | Preparation method of high-wear-resistance diamond/metal carbide composite coating |
CN114196952A (en) * | 2021-12-07 | 2022-03-18 | 哈尔滨工程大学 | High-entropy alloy biomimetic gradient structure composite coating with eutectic interface and preparation method thereof |
Family Cites Families (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7354660B2 (en) * | 2005-05-10 | 2008-04-08 | Exxonmobil Research And Engineering Company | High performance alloys with improved metal dusting corrosion resistance |
US12012647B2 (en) * | 2019-06-21 | 2024-06-18 | United States Government Administrator Of Nasa | Additively manufactured oxide dispersion strengthened medium entropy alloys for high temperature applications |
-
2022
- 2022-03-29 CN CN202210319022.9A patent/CN114836666B/en active Active
Patent Citations (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5268217A (en) * | 1990-09-27 | 1993-12-07 | Diamonex, Incorporated | Abrasion wear resistant coated substrate product |
CN105506716A (en) * | 2015-12-25 | 2016-04-20 | 苏州宏久航空防热材料科技有限公司 | Preparation method for high-bonding wearproof composite coating |
CN107034462A (en) * | 2017-06-09 | 2017-08-11 | 上海工程技术大学 | One kind is used for stainless steel surfaces acieral coating and preparation method thereof |
CN107299342A (en) * | 2017-07-05 | 2017-10-27 | 暨南大学 | A kind of high-entropy alloy coating and its production and use |
CN108315686A (en) * | 2017-12-08 | 2018-07-24 | 水利部杭州机械设计研究所 | A kind of puppet high-entropy alloy coating formula and its coating production |
CN108893738A (en) * | 2018-08-07 | 2018-11-27 | 华东交通大学 | A kind of superhard Fe-Ni based alloy wear-resistant coating of equiax crystal and preparation method thereof |
CN109468638A (en) * | 2019-01-09 | 2019-03-15 | 苏州科技大学 | A kind of preparation method of diamond reinforced high-entropy alloy composite coating |
CN113278965A (en) * | 2021-05-07 | 2021-08-20 | 太原理工大学 | Preparation method of high-wear-resistance diamond/metal carbide composite coating |
CN114196952A (en) * | 2021-12-07 | 2022-03-18 | 哈尔滨工程大学 | High-entropy alloy biomimetic gradient structure composite coating with eutectic interface and preparation method thereof |
Non-Patent Citations (1)
Title |
---|
宋鹏芳等.激光熔覆制备高熵合金涂层研究进展:强化机理与性能.青岛理工大学学报.2020,(第04期),106-114. * |
Also Published As
Publication number | Publication date |
---|---|
CN114836666A (en) | 2022-08-02 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
EP1231299B1 (en) | Light alloy-based composite protective multifunction coating | |
CN106757013B (en) | Polynary high-temperature alloy layer of a kind of titanium alloy laser surface silicide enhancing and preparation method thereof | |
EP1646736B1 (en) | Coating | |
CN110565047B (en) | Titanium alloy surface nitriding process | |
CN113652642B (en) | A kind of gradient ceramic high-entropy alloy coating and preparation method thereof | |
CN114836666B (en) | High-entropy alloy composite coating for improving surface hardness and wear resistance of metal substrate and processing method | |
EP0946772A1 (en) | Method of controlling infiltration of complex-shaped ceramic-metal composite articles and the products produced thereby | |
CN111270234A (en) | A kind of method for preparing titanium-aluminum enhanced coating on titanium alloy surface | |
CN113088836A (en) | Method for preparing carbon fiber reinforced aluminum matrix composite material by electric arc spraying | |
CN108220957B (en) | Titanium alloy surface high-temperature-resistant coating and preparation method thereof | |
CN110241412B (en) | Laminated coating self-lubricating bearing and preparation method thereof | |
CN112779533B (en) | Method for preparing metal-based composite coating on surface of stainless steel | |
US5930581A (en) | Method of preparing complex-shaped ceramic-metal composite articles and the products produced thereby | |
CN111804907B (en) | A kind of modified ceramic particle reinforced iron-based composite material and preparation method thereof | |
CN117286493B (en) | Laser cladding nickel-aluminum-based wear-resistant coating and preparation method thereof | |
CN108825841A (en) | A kind of G-M type Cryo Refrigerator rotary valve and preparation method thereof | |
CN114318202B (en) | A kind of nickel-based alloy surface wear-resistant coating and preparation method thereof | |
CN114672720A (en) | Alloy powder, part surface treatment method and application thereof | |
CN119177415B (en) | Preparation method of TC19 titanium alloy | |
CN110438441A (en) | A kind of Si-Co-Y co-penetration layer and preparation method thereof of Ti alloy surface nanosizing auxiliary preparation | |
TWI412614B (en) | Method for manufacturing nano-network hybrid coating | |
CN116445018A (en) | High-temperature oxidation resistant protective coating for titanium alloy surface and preparation method thereof | |
CN119592108A (en) | Composite coating for FPC reinforced austenitic stainless steel surface and preparation method thereof | |
CN106148886A (en) | Metallic titanium surface Fe powder urges the salt bath oozed ooze niobium agent and ooze niobium method | |
CN117403200A (en) | A highly wear-resistant alloy component and its surface treatment method |
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 | ||
GR01 | Patent grant | ||
GR01 | Patent grant |