CN111676478A - A kind of preparation method of corrosion-resistant alloy layer on the surface of GCr15 steel - Google Patents
A kind of preparation method of corrosion-resistant alloy layer on the surface of GCr15 steel Download PDFInfo
- Publication number
- CN111676478A CN111676478A CN202010547989.3A CN202010547989A CN111676478A CN 111676478 A CN111676478 A CN 111676478A CN 202010547989 A CN202010547989 A CN 202010547989A CN 111676478 A CN111676478 A CN 111676478A
- Authority
- CN
- China
- Prior art keywords
- powder
- corrosion
- gcr15 steel
- alloy layer
- laser
- 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
- 238000005260 corrosion Methods 0.000 title claims abstract description 74
- 229910000831 Steel Inorganic materials 0.000 title claims abstract description 60
- 239000010959 steel Substances 0.000 title claims abstract description 60
- 230000007797 corrosion Effects 0.000 title claims abstract description 45
- 239000000956 alloy Substances 0.000 title claims abstract description 39
- 229910045601 alloy Inorganic materials 0.000 title claims abstract description 39
- 238000002360 preparation method Methods 0.000 title claims abstract description 12
- 239000000843 powder Substances 0.000 claims abstract description 58
- 239000011248 coating agent Substances 0.000 claims abstract description 46
- 238000000576 coating method Methods 0.000 claims abstract description 46
- 238000000034 method Methods 0.000 claims abstract description 32
- 239000000463 material Substances 0.000 claims abstract description 31
- 239000011159 matrix material Substances 0.000 claims abstract description 7
- 238000004093 laser heating Methods 0.000 claims abstract description 3
- 239000002131 composite material Substances 0.000 claims description 18
- 239000000203 mixture Substances 0.000 claims description 17
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 claims description 16
- 239000007789 gas Substances 0.000 claims description 13
- 229910052786 argon Inorganic materials 0.000 claims description 8
- 239000011230 binding agent Substances 0.000 claims description 8
- 239000003822 epoxy resin Substances 0.000 claims description 6
- 229920000647 polyepoxide Polymers 0.000 claims description 6
- 239000000835 fiber Substances 0.000 claims description 4
- 239000002245 particle Substances 0.000 claims description 4
- 239000011812 mixed powder Substances 0.000 claims description 2
- 229920005989 resin Polymers 0.000 claims description 2
- 239000011347 resin Substances 0.000 claims description 2
- 239000000853 adhesive Substances 0.000 claims 2
- 230000001070 adhesive effect Effects 0.000 claims 2
- 238000005275 alloying Methods 0.000 abstract description 12
- 230000007547 defect Effects 0.000 abstract 1
- 239000000758 substrate Substances 0.000 description 24
- 230000010287 polarization Effects 0.000 description 13
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 4
- LFQSCWFLJHTTHZ-UHFFFAOYSA-N Ethanol Chemical compound CCO LFQSCWFLJHTTHZ-UHFFFAOYSA-N 0.000 description 4
- 239000010953 base metal Substances 0.000 description 4
- 230000003247 decreasing effect Effects 0.000 description 4
- 238000009826 distribution Methods 0.000 description 4
- 238000005516 engineering process Methods 0.000 description 4
- 238000005468 ion implantation Methods 0.000 description 4
- 238000005728 strengthening Methods 0.000 description 4
- 239000010936 titanium Substances 0.000 description 3
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 2
- 238000010438 heat treatment Methods 0.000 description 2
- 238000002513 implantation Methods 0.000 description 2
- 229910052757 nitrogen Inorganic materials 0.000 description 2
- 229910052719 titanium Inorganic materials 0.000 description 2
- 229910018509 Al—N Inorganic materials 0.000 description 1
- VEXZGXHMUGYJMC-UHFFFAOYSA-M Chloride anion Chemical compound [Cl-] VEXZGXHMUGYJMC-UHFFFAOYSA-M 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 206010016256 fatigue Diseases 0.000 description 1
- 150000002500 ions Chemical class 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 238000007750 plasma spraying Methods 0.000 description 1
- 238000010791 quenching Methods 0.000 description 1
- 230000000171 quenching effect Effects 0.000 description 1
- 238000005496 tempering Methods 0.000 description 1
Images
Classifications
-
- 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
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C27/00—Alloys based on rhenium or a refractory metal not mentioned in groups C22C14/00 or C22C16/00
- C22C27/06—Alloys based on chromium
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C32/00—Non-ferrous alloys containing at least 5% by weight but less than 50% by weight of oxides, carbides, borides, nitrides, silicides or other metal compounds, e.g. oxynitrides, sulfides, whether added as such or formed in situ
- C22C32/0047—Non-ferrous alloys containing at least 5% by weight but less than 50% by weight of oxides, carbides, borides, nitrides, silicides or other metal compounds, e.g. oxynitrides, sulfides, whether added as such or formed in situ with carbides, nitrides, borides or silicides as the main non-metallic constituents
- C22C32/0052—Non-ferrous alloys containing at least 5% by weight but less than 50% by weight of oxides, carbides, borides, nitrides, silicides or other metal compounds, e.g. oxynitrides, sulfides, whether added as such or formed in situ with carbides, nitrides, borides or silicides as the main non-metallic constituents only carbides
- C22C32/0057—Non-ferrous alloys containing at least 5% by weight but less than 50% by weight of oxides, carbides, borides, nitrides, silicides or other metal compounds, e.g. oxynitrides, sulfides, whether added as such or formed in situ with carbides, nitrides, borides or silicides as the main non-metallic constituents only carbides based on B4C
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Powder Metallurgy (AREA)
- Other Surface Treatments For Metallic Materials (AREA)
Abstract
Description
技术领域technical field
本发明属于材料表面改性技术领域,具体涉及一种GCr15钢表面耐蚀合金层的制备方法。The invention belongs to the technical field of material surface modification, in particular to a preparation method of a corrosion-resistant alloy layer on the surface of GCr15 steel.
背景技术Background technique
GCrl5钢是一种应用范围最广的轴承钢,其具有较高的硬度和耐磨性,在航天航空、轨道交通、核工业等高新技术领域具有重要的应用。但GCr15钢耐蚀性较差,在严苛环境条件下GCr15钢制备的轴承关键部件常因腐蚀发生早期疲劳失效,尤其是在海洋装备中服役时,由于氯离子等侵蚀性离子的作用,其使用寿命较短。因此,提高GCr15钢制备的轴承关键部件的耐蚀性对提高轴承寿命和可靠性具有重要意义。GCrl5 steel is one of the most widely used bearing steels. It has high hardness and wear resistance, and has important applications in high-tech fields such as aerospace, rail transit, and nuclear industry. However, GCr15 steel has poor corrosion resistance. Under harsh environmental conditions, key components of bearings made of GCr15 steel often suffer early fatigue failure due to corrosion, especially when serving in marine equipment, due to the action of corrosive ions such as chloride ions. Short service life. Therefore, improving the corrosion resistance of key components of bearings made of GCr15 steel is of great significance to improve bearing life and reliability.
为解决上述问题,研究学者尝试利用等离子喷涂、热处理、离子注入等方法对GCr15钢表面进行改性,在一定程度上有效提高了其表面耐蚀性能。现有技术中,申请号为200710193136.9的中国专利文献报道了一种GCr15轴承钢球表面强化的离子注入工艺,选用氮和钛两种注入元素,采用100keV的注入能量,先注入钛后注入氮,剂量控制在2.0~3.0×1017Ti+2.0~3.0×1017N,从而获得较高的硬度、较好的耐磨耐蚀性能;申请号为201110317942.9的中国专利文献报道了经表面改性的GCr15压缩机叶片及其制备工艺,在GCr15轴承钢叶片进行整体热处理(淬火+低温回火)后对其表面采用PVD沉积Cr-Al-N膜,提高叶片的耐磨性和抗腐蚀能力。但是上述技术存在流程复杂、效率低、成本较高、无法进行局部强化等缺点。In order to solve the above problems, researchers have tried to use plasma spraying, heat treatment, ion implantation and other methods to modify the surface of GCr15 steel, which has effectively improved its surface corrosion resistance to a certain extent. In the prior art, the Chinese patent document with the application number of 200710193136.9 reported a kind of ion implantation process for surface strengthening of GCr15 bearing steel balls, selecting nitrogen and titanium two kinds of implantation elements, using the implantation energy of 100keV, first implanting titanium and then implanting nitrogen, The dosage is controlled at 2.0~3.0×10 17 Ti+2.0~3.0×10 17 N, so as to obtain higher hardness and better wear and corrosion resistance; Chinese patent document with application number 201110317942.9 reported that the surface-modified GCr15 compressor blade and its preparation process, after the overall heat treatment (quenching + low temperature tempering) of GCr15 bearing steel blade, PVD is used to deposit Cr-Al-N film on the surface to improve the wear resistance and corrosion resistance of the blade. However, the above technologies have disadvantages such as complex process, low efficiency, high cost, and inability to perform local strengthening.
为此,本发明提供了一种提高GCr15钢表面耐蚀性能的方法。本发明所述方法利用激光在GCr15钢表面制备耐蚀合金层。相较于离子注入、PVD等技术,本发明所述方法操作简单、效率高,易于自动化控制,并且可实现局部强化等。因此,可通过本发明所述方法改善GCr15钢制备的轴承关键部件的耐蚀性。Therefore, the present invention provides a method for improving the surface corrosion resistance of GCr15 steel. The method of the invention utilizes a laser to prepare a corrosion-resistant alloy layer on the surface of GCr15 steel. Compared with ion implantation, PVD and other technologies, the method of the present invention has simple operation, high efficiency, easy automatic control, and can realize local strengthening and the like. Therefore, the corrosion resistance of the key components of the bearing made of GCr15 steel can be improved by the method of the present invention.
发明内容SUMMARY OF THE INVENTION
针对现有技术中存在的上述问题,本发明的目的是提供一种GCr15钢表面耐蚀合金层的制备方法,在保证一定硬度下提高其耐蚀性能,防止GCr15钢在海洋环境服役时发生由腐蚀引起的早期失效问题。In view of the above-mentioned problems existing in the prior art, the purpose of the present invention is to provide a preparation method of a corrosion-resistant alloy layer on the surface of GCr15 steel, improve its corrosion resistance under a certain hardness, and prevent GCr15 steel from being in service in a marine environment. Early failure problems caused by corrosion.
所述的一种GCr15钢表面耐蚀合金层的制备方法,其特征在于以GCr15钢为基体材料,将用于提高材料表面耐磨性的B4C粉末与提高表面耐蚀性的Cr粉为复合涂层材料涂敷在GCr15钢上,通过激光加热使复合涂层材料与基体材料合金化,得到GCr15钢表面耐蚀合金层。The method for preparing a corrosion-resistant alloy layer on the surface of GCr15 steel is characterized in that the GCr15 steel is used as the base material, and the B 4 C powder for improving the surface wear resistance of the material and the Cr powder for improving the surface corrosion resistance are The composite coating material is coated on the GCr15 steel, and the composite coating material is alloyed with the base material by laser heating to obtain a corrosion-resistant alloy layer on the surface of the GCr15 steel.
所述的GCr15钢表面耐蚀合金层的制备方法,其特征在于包括如下步骤:The preparation method of the corrosion-resistant alloy layer on the surface of the GCr15 steel is characterized in that it comprises the following steps:
S1.将基体材料GCr15钢表面打磨、清洗、吹干、待用;S1. Grind the surface of the base material GCr15 steel, clean it, dry it, and set it aside for use;
S2.将B4C粉末与Cr粉按照质量比混合并球磨至混粉均匀,得到复合涂层粉末;S2. Mix the B 4 C powder and the Cr powder according to the mass ratio and ball-mill until the mixed powder is uniform to obtain the composite coating powder;
S3.用粘结剂把球磨后的复合涂层粉末调成均匀糊状,涂敷在基体材料GCr15钢表面,保持涂层厚度均匀,自然风干,得到预置粉末层;S3. Use a binder to adjust the ball-milled composite coating powder into a uniform paste, coat it on the surface of the base material GCr15 steel, keep the coating thickness uniform, and air dry it naturally to obtain a preset powder layer;
S4.采用光纤激光器对试样进行扫描,复合涂层材料在基体材料表面进行激光合金化,得到GCr15钢表面耐蚀合金层,激光扫描的工作参数包括:激光功率为800~1200W,扫描速度为5~20mm/s,光斑直径保持为4mm,搭接率为30~60%,且激光束扫描过程中吹送氩气,气体流量为15~20L/min。S4. Use a fiber laser to scan the sample, and the composite coating material is laser alloyed on the surface of the base material to obtain a corrosion-resistant alloy layer on the surface of GCr15 steel. The working parameters of the laser scanning include: the laser power is 800-1200W, and the scanning speed is 5~20mm/s, the spot diameter is kept at 4mm, the overlap rate is 30~60%, and argon is blown during the laser beam scanning process, and the gas flow is 15~20L/min.
所述的一种GCr15钢表面耐蚀合金层的制备方法,其特征在于复合涂层材料中,两种组份的质量百分比为:B4C粉末0%~12%,Cr粉88%~100%,优选为B4C粉末5.88%、Cr粉94.12%。The method for preparing a corrosion-resistant alloy layer on the surface of GCr15 steel is characterized in that in the composite coating material, the mass percentages of the two components are: B 4 C powder 0%-12%, Cr powder 88%-100% %, preferably B 4 C powder 5.88% and Cr powder 94.12%.
所述的一种GCr15钢表面耐蚀合金层的制备方法,其特征在于B4C粉末的粒度为90-110nm,优选为100nm;Cr粉的粉末粒度为95-105μm,优选为100μm,纯度≥99%。The method for preparing a corrosion-resistant alloy layer on the surface of GCr15 steel is characterized in that the particle size of the B 4 C powder is 90-110 nm, preferably 100 nm; the powder particle size of the Cr powder is 95-105 μm, preferably 100 μm, and the purity is greater than or equal to 100 μm. 99%.
所述的一种GCr15钢表面耐蚀合金层的制备方法,其特征在于步骤S3中,粘结剂为环氧树脂,粘结剂与复合涂层涂末的质量为1-3:5,优选为2:5。The method for preparing a corrosion-resistant alloy layer on the surface of GCr15 steel is characterized in that in step S3, the binder is epoxy resin, and the quality of the binder and the coating powder of the composite coating is 1-3:5, preferably 2:5.
所述的一种GCr15钢表面耐蚀合金层的制备方法,其特征在于步骤S3中,树脂涂层厚度为0.1~0.3mm。The method for preparing a corrosion-resistant alloy layer on the surface of GCr15 steel is characterized in that in step S3, the thickness of the resin coating is 0.1-0.3 mm.
所述的一种GCr15钢表面耐蚀合金层的制备方法,其特征在于步骤S4中,光纤激光器的工作参数:激光功率为800W,速度为5mm/s,搭接率为60%,激光束扫描过程B4C与Cr的质量百分比的组成中吹送氩气,气体流量为15L/min。The method for preparing a corrosion-resistant alloy layer on the surface of GCr15 steel is characterized in that in step S4, the working parameters of the fiber laser are: the laser power is 800W, the speed is 5mm/s, the lap rate is 60%, and the laser beam scans In the composition of the mass percentage of B 4 C and Cr in the process, argon gas was blown, and the gas flow rate was 15 L/min.
通过采用上述技术,与现有技术相比,本发明的有益效果如下:By adopting the above-mentioned technology, compared with the prior art, the beneficial effects of the present invention are as follows:
本发明利用B4C粉末与Cr粉作为混合涂层材料,在GCr15钢表面进行激光合金化,在本发明限定的工艺参数下,制备出硬度较高的耐蚀合金化层,与离子注入、PVD等技术相比较,本发明所述方法制备的耐蚀合金层表面较为平整,合金层和基体之间具有冶金结合特点,并且通过引入B4C、Cr两种粉末,可获得硬度更高的耐蚀合金层,而且,本发明所述方法采用的B4C粉末、Cr粉价格较低、工艺流程简单、操作方便、效率高,并且可在零件表面实现局部选择性强化,能避免GCr15钢在海洋环境服役时发生由腐蚀引起的早期失效问题,从而提高其使用寿命。The present invention utilizes B 4 C powder and Cr powder as mixed coating materials, carries out laser alloying on the surface of GCr15 steel, and prepares a corrosion-resistant alloying layer with higher hardness under the process parameters defined in the present invention, which is combined with ion implantation, Compared with PVD and other technologies, the surface of the corrosion - resistant alloy layer prepared by the method of the present invention is relatively smooth, and the alloy layer and the substrate have metallurgical bonding characteristics. Corrosion-resistant alloy layer, and the B 4 C powder and Cr powder used in the method of the present invention are low in price, simple in process flow, convenient in operation, and high in efficiency, and can achieve local selective strengthening on the surface of parts, which can avoid GCr15 steel. Early failures caused by corrosion occur during service in marine environments, thereby increasing their service life.
附图说明Description of drawings
图1为GCr15钢表面涂层质量百分比组成为B4C粉末11.1%、Cr粉88.9%激光合金层的微观组织形貌图;Figure 1 shows the microstructure and morphology of the laser alloy layer composed of B 4 C powder 11.1% and Cr powder 88.9% by mass percentage of GCr15 steel surface coating;
图2为GCr15钢表面涂层质量百分比组成为B4C粉末11.1%、Cr粉88.9%激光合金层的硬度分布曲线图;Figure 2 shows the hardness distribution curve of the laser alloy layer with the composition of the surface coating mass percentage of GCr15 steel: B 4 C powder 11.1% and Cr powder 88.9%;
图3为GCr15钢表面涂层质量百分比组成为B4C粉末5.88%、Cr粉94.12%激光合金层的微观组织形貌图;Figure 3 shows the microstructure and morphology of the laser alloy layer with the mass percentage composition of B 4 C powder 5.88% and Cr powder 94.12% on the surface of GCr15 steel;
图4为GCr15钢表面涂层质量百分比组成为B4C粉末5.88%、Cr粉94.12%激光合金层的硬度分布曲线图;Fig. 4 is the hardness distribution curve of the laser alloy layer composed of B 4 C powder 5.88% and Cr powder 94.12% by mass percentage of GCr15 steel surface coating;
图5为GCr15钢表面涂层质量百分比组成为B4C粉末1.56%、Cr粉98.44%激光合金层的微观组织形貌图;Figure 5 shows the microstructure and morphology of the laser alloy layer with the composition of the surface coating of GCr15 steel with a mass percentage of B 4 C powder of 1.56% and Cr powder of 98.44%;
图6为GCr15钢表面涂层质量百分比组成为B4C粉末1.56%、Cr粉98.44%激光合金层的硬度分布曲线图;Figure 6 is a graph showing the hardness distribution of the laser alloy layer with the mass percentage composition of the surface coating of GCr15 steel: B 4 C powder 1.56% and Cr powder 98.44%;
图7为GCr15钢表面涂层质量百分比组成为B4C粉末0%、Cr粉100%激光合金层的微观组织形貌图;Fig. 7 is the microstructure and morphology of the laser alloy layer composed of B 4 C powder 0% and
图8为GCr15钢表面涂层质量百分比组成为B4C粉末0%、Cr粉100%激光合金层的硬度分布曲线图;Fig. 8 is a graph showing the hardness distribution of the laser alloy layer with the mass percentage composition of the surface coating of GCr15 steel: 0% of B 4 C powder and 100% of Cr powder;
图9为GCr15钢基体的微观组织形貌图;Fig. 9 is the microstructure and morphology of GCr15 steel matrix;
图10为GCr15钢不同质量比下及基体的极化曲线对比图。Figure 10 is a comparison diagram of polarization curves of GCr15 steel with different mass ratios and the matrix.
具体实施方式Detailed ways
下面通过具体实施例对本发明作进一步的说明,但本发明的保护范围并不仅限于此。The present invention will be further described below through specific embodiments, but the protection scope of the present invention is not limited thereto.
实施例1Example 1
以GCr15钢作为基体材料,所用的涂层材料质量组成为B4C粉末11.1%、Cr粉88.9%。Taking GCr15 steel as the base material, the mass composition of the used coating material is 11.1% of B 4 C powder and 88.9% of Cr powder.
1)使用角磨机对基体表面打磨,经无水乙醇清洗,吹干、待用;1) Grind the surface of the substrate with an angle grinder, clean it with anhydrous ethanol, dry it and set it aside for use;
2)用球磨机将上述质量百分比的B4C、Cr混合均匀,环氧树脂作为粘结剂,与复合涂层质量比为2:5,均匀涂敷在基体金属表面,保持厚度均匀,晾干后待用;2) Mix the above mass percentages of B 4 C and Cr evenly with a ball mill, and use epoxy resin as a binder, with a mass ratio of 2:5 to the composite coating, uniformly coat it on the surface of the base metal, keep the thickness uniform, and let it dry. to be used later;
3)采用连续激光器对试样进行扫描,使用功率为800W,光斑直径保持为4mm,扫描速度5mm/s,激光束扫描过程中吹送氩气以保护熔池及激光器镜筒,气体流量为15L/min。3) Scan the sample with a continuous laser, the power is 800W, the spot diameter is kept at 4mm, the scanning speed is 5mm/s, and argon gas is blown during the laser beam scanning process to protect the molten pool and the laser lens barrel, and the gas flow rate is 15L/ min.
4)对制备的合金化层进行观察、并进行硬度测试及耐蚀测试(从分析软件中得到极化曲线中的自腐蚀电位以及自腐蚀电流密度)。4) Observing the prepared alloy layer, and performing hardness test and corrosion resistance test (obtain the self-corrosion potential and self-corrosion current density in the polarization curve from the analysis software).
5)图1为实例1激光工艺下试样的组织形貌。合金化层与基体结合较为紧密。5) Figure 1 shows the microstructure of the sample under the laser process of Example 1. The alloying layer is closely combined with the substrate.
6)图2为激光表面Cr合金化涂层的显微硬度,合金化层硬度最高为800HV0.2,远远高于基体硬度200-250HV0.2。6) Figure 2 shows the microhardness of the Cr alloyed coating on the laser surface. The highest hardness of the alloyed layer is 800HV 0.2 , which is much higher than the hardness of the substrate by 200-250HV 0.2 .
7)激光表面合金化涂层的极化曲线与基体的极化曲线如图10所示,基体的自腐蚀电位为-0.5773V,自腐蚀电流密度为6.714×10-6A·cm-2,而激光合金化后自腐蚀电位偏移为-0.5459V,较基体提高了5.44%,自腐蚀电流密度减小至3.706×10-6A·cm-2,自腐蚀电流密度降低了44.8%,表面激光合金化后耐蚀性能显著提高。7) The polarization curve of the laser surface alloyed coating and the polarization curve of the substrate are shown in Figure 10. The self-corrosion potential of the substrate is -0.5773V, and the self-corrosion current density is 6.714×10 -6 A·cm -2 . After laser alloying, the self-corrosion potential shift was -0.5459V, which was 5.44% higher than that of the substrate. The self-corrosion current density decreased to 3.706×10 -6 A·cm -2 , and the self-corrosion current density decreased by 44.8%. Corrosion resistance is significantly improved after laser alloying.
实施例2Example 2
以GCr15钢作为基体材料,所用的涂层材料质量组成为B4C粉末5.88%、Cr粉94.12%。Taking GCr15 steel as the base material, the mass composition of the used coating material is 5.88% of B 4 C powder and 94.12% of Cr powder.
1)使用角磨机对基体表面打磨,经无水乙醇清洗,吹干、待用;1) Grind the surface of the substrate with an angle grinder, clean it with anhydrous ethanol, dry it and set it aside for use;
2)用球磨机将上述质量百分比的B4C、Cr混合均匀,环氧树脂作为粘结剂,与复合涂层质量比为2:5,均匀涂敷在基体金属表面,保持厚度均匀,晾干后待用;2) Mix the above mass percentages of B 4 C and Cr evenly with a ball mill, and use epoxy resin as a binder, with a mass ratio of 2:5 to the composite coating, uniformly coat it on the surface of the base metal, keep the thickness uniform, and let it dry. to be used later;
3)采用连续激光器对试样进行扫描,使用功率为800W,光斑直径保持为4mm,扫描速度5mm/s,激光束扫描过程中吹送氩气以保护熔池及激光器镜筒,气体流量为15L/min。3) Scan the sample with a continuous laser, the power is 800W, the spot diameter is kept at 4mm, the scanning speed is 5mm/s, and argon gas is blown during the laser beam scanning process to protect the molten pool and the laser lens barrel, and the gas flow rate is 15L/ min.
4)对制备的合金化层进行观察、并进行硬度测试及耐蚀测试(从分析软件中得到极化曲线中的自腐蚀电位以及自腐蚀电流密度)。4) Observing the prepared alloy layer, and performing hardness test and corrosion resistance test (obtain the self-corrosion potential and self-corrosion current density in the polarization curve from the analysis software).
5)图3为实例2激光工艺下试样的组织形貌。合金化层与基体结合较为紧密。5) Figure 3 shows the microstructure of the sample under the laser process of Example 2. The alloying layer is closely combined with the substrate.
6)图4为激光表面Cr合金化涂层的显微硬度,合金化层硬度最高为642HV0.2,远远高于基体硬度200-250HV0.2。6) Figure 4 shows the microhardness of the Cr alloyed coating on the laser surface. The highest hardness of the alloyed layer is 642HV 0.2 , which is much higher than the hardness of the substrate by 200-250HV 0.2 .
7)激光表面合金化涂层的极化曲线与基体的极化曲线如图10所示,基体的自腐蚀电位为-0.5773V,自腐蚀电流密度为6.714×10-6A·cm-2,而激光合金化后自腐蚀电位偏移为-0.5378V,较基体提高了6.9%,自腐蚀电流密度减小至2.022×10-6A·cm-2,自腐蚀电流密度降低了70.9%。7) The polarization curve of the laser surface alloyed coating and the polarization curve of the substrate are shown in Figure 10. The self-corrosion potential of the substrate is -0.5773V, and the self-corrosion current density is 6.714×10 -6 A·cm -2 . After laser alloying, the self-corrosion potential shift is -0.5378V, which is 6.9% higher than that of the substrate, the self-corrosion current density is reduced to 2.022×10 -6 A·cm -2 , and the self-corrosion current density is reduced by 70.9%.
实施例3Example 3
以GCr15钢作为基体材料,所用的涂层材料质量组成为B4C粉末1.56%、Cr粉98.44%。Taking GCr15 steel as the base material, the mass composition of the used coating material is 1.56% of B 4 C powder and 98.44% of Cr powder.
1)使用角磨机对基体表面打磨,经无水乙醇清洗,吹干、待用;1) Grind the surface of the substrate with an angle grinder, clean it with anhydrous ethanol, dry it and set it aside for use;
2)用球磨机将上述质量百分比的B4C、Cr混合均匀,环氧树脂作为粘结剂,与复合涂层质量比为2:5,均匀涂敷在基体金属表面,保持厚度均匀,晾干后待用;2) Mix the above mass percentages of B 4 C and Cr evenly with a ball mill, and use epoxy resin as a binder, with a mass ratio of 2:5 to the composite coating, uniformly coat it on the surface of the base metal, keep the thickness uniform, and let it dry. to be used later;
3)采用连续激光器对试样进行扫描,使用功率为800W,光斑直径保持为4mm,扫描速度5mm/s,激光束扫描过程中吹送氩气以保护熔池及激光器镜筒,气体流量为15L/min。3) Scan the sample with a continuous laser, the power is 800W, the spot diameter is kept at 4mm, the scanning speed is 5mm/s, and argon gas is blown during the laser beam scanning process to protect the molten pool and the laser lens barrel, and the gas flow rate is 15L/ min.
4)对制备的合金化层进行观察、并进行硬度测试及耐蚀测试(从分析软件中得到极化曲线中的自腐蚀电位以及自腐蚀电流密度)。4) Observing the prepared alloy layer, and performing hardness test and corrosion resistance test (obtain the self-corrosion potential and self-corrosion current density in the polarization curve from the analysis software).
5)图5为实例3激光工艺下试样的组织形貌。合金化层与基体结合较为紧密。5) Figure 5 shows the microstructure of the sample under the laser process of Example 3. The alloying layer is closely combined with the substrate.
6)图6为激光表面Cr合金化涂层的显微硬度,合金化层硬度最高为586HV0.2,远远高于基体硬度200-250HV0.2。6) Figure 6 shows the microhardness of the Cr alloyed coating on the laser surface. The highest hardness of the alloyed layer is 586HV 0.2 , which is much higher than the hardness of the substrate by 200-250HV 0.2 .
7)激光表面合金化涂层的极化曲线与基体的极化曲线如图10所示,基体的自腐蚀电位为-0.5773V,自腐蚀电流密度为6.714×10-6A·cm-2,而激光合金化后自腐蚀电位偏移为-0.5675V,较基体提高了1.69%,自腐蚀电流密度减小至3.022×10-6A·cm-2,自自腐蚀电流密度降低了54.9%。7) The polarization curve of the laser surface alloyed coating and the polarization curve of the substrate are shown in Figure 10. The self-corrosion potential of the substrate is -0.5773V, and the self-corrosion current density is 6.714×10 -6 A·cm -2 . However, after laser alloying, the self-corrosion potential shift was -0.5675V, which was 1.69% higher than that of the substrate. The self-corrosion current density decreased to 3.022×10 -6 A·cm -2 , and the self-corrosion current density decreased by 54.9%.
实施例4Example 4
以GCr15钢作为基体材料,所用的涂层材料质量组成为B4C粉末0%、Cr粉100%。Taking GCr15 steel as the base material, the mass composition of the used coating material is 0% of B 4 C powder and 100% of Cr powder.
1)使用角磨机对基体表面打磨,经无水乙醇清洗,吹干、待用;1) Grind the surface of the substrate with an angle grinder, clean it with anhydrous ethanol, dry it and set it aside for use;
2)用球磨机将上述质量百分比的B4C、Cr混合均匀,环氧树脂作为粘结剂,与复合涂层质量比为2:5,均匀涂敷在基体金属表面,保持厚度均匀,晾干后待用;2) Mix the above mass percentages of B 4 C and Cr evenly with a ball mill, and use epoxy resin as a binder, with a mass ratio of 2:5 to the composite coating, uniformly coat it on the surface of the base metal, keep the thickness uniform, and let it dry. to be used later;
3)采用连续激光器对试样进行扫描,使用功率为800W,光斑直径保持为4mm,扫描速度5mm/s,激光束扫描过程中吹送氩气以保护熔池及激光器镜筒,气体流量为15L/min。3) Scan the sample with a continuous laser, the power is 800W, the spot diameter is kept at 4mm, the scanning speed is 5mm/s, argon gas is blown during the laser beam scanning process to protect the molten pool and the laser barrel, and the gas flow rate is 15L/ min.
4)对制备的合金化层进行观察、并进行硬度测试及耐蚀测试(从分析软件中得到极化曲线中的自腐蚀电位以及自腐蚀电流密度)。4) Observing the prepared alloy layer, and performing hardness test and corrosion resistance test (obtain the self-corrosion potential and self-corrosion current density in the polarization curve from the analysis software).
5)图7为实例4激光工艺下试样的组织形貌。合金化层与基体结合较为紧密。5) Figure 7 shows the microstructure of the sample under the laser process of Example 4. The alloying layer is closely combined with the substrate.
6)图8为激光表面Cr合金化涂层的显微硬度,合金化层硬度最高为530HV0.2,远远高于基体硬度200-250HV0.2。6) Figure 8 shows the microhardness of the Cr alloyed coating on the laser surface. The highest hardness of the alloyed layer is 530HV 0.2 , which is much higher than that of the matrix by 200-250HV 0.2 .
7)激光表面合金化涂层的极化曲线与基体的极化曲线如图10所示,基体的自腐蚀电位为-0.5773V,自腐蚀电流密度为6.714×10-6A·cm-2,而合金化后自腐蚀电位偏移为-0.5655V,较基体提高了2.04%,自腐蚀电流密度减小至6.510×10-6A·cm-2,自腐蚀电流密度降低了3.31%。7) The polarization curve of the laser surface alloyed coating and the polarization curve of the substrate are shown in Figure 10. The self-corrosion potential of the substrate is -0.5773V, and the self-corrosion current density is 6.714×10 -6 A·cm -2 . After alloying, the self-corrosion potential shift is -0.5655V, which is 2.04% higher than that of the substrate, the self-corrosion current density is reduced to 6.510×10 -6 A·cm -2 , and the self-corrosion current density is reduced by 3.31%.
Claims (7)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202010547989.3A CN111676478A (en) | 2020-06-16 | 2020-06-16 | A kind of preparation method of corrosion-resistant alloy layer on the surface of GCr15 steel |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202010547989.3A CN111676478A (en) | 2020-06-16 | 2020-06-16 | A kind of preparation method of corrosion-resistant alloy layer on the surface of GCr15 steel |
Publications (1)
Publication Number | Publication Date |
---|---|
CN111676478A true CN111676478A (en) | 2020-09-18 |
Family
ID=72455134
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN202010547989.3A Pending CN111676478A (en) | 2020-06-16 | 2020-06-16 | A kind of preparation method of corrosion-resistant alloy layer on the surface of GCr15 steel |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN111676478A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN113894291A (en) * | 2021-09-23 | 2022-01-07 | 石家庄铁道大学 | Method for melting and forming GCr15 bearing steel for high-speed rail in selective laser area |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN101876327A (en) * | 2009-03-06 | 2010-11-03 | 通用电气公司 | Anti-erosion and corrosion resistant turbine compressor airfoil and manufacture method thereof |
CN103920872A (en) * | 2014-04-26 | 2014-07-16 | 武汉高斯激光技术有限公司 | Laser alloying powder and application of laser alloying powder in steel cylinder circular mould laser surface alloying |
CN107201515A (en) * | 2017-05-24 | 2017-09-26 | 山东大学 | A kind of nanometer B4C is modified anti-friction wear-resistant laser cladding layer and preparation method thereof |
-
2020
- 2020-06-16 CN CN202010547989.3A patent/CN111676478A/en active Pending
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN101876327A (en) * | 2009-03-06 | 2010-11-03 | 通用电气公司 | Anti-erosion and corrosion resistant turbine compressor airfoil and manufacture method thereof |
CN103920872A (en) * | 2014-04-26 | 2014-07-16 | 武汉高斯激光技术有限公司 | Laser alloying powder and application of laser alloying powder in steel cylinder circular mould laser surface alloying |
CN107201515A (en) * | 2017-05-24 | 2017-09-26 | 山东大学 | A kind of nanometer B4C is modified anti-friction wear-resistant laser cladding layer and preparation method thereof |
Non-Patent Citations (4)
Title |
---|
孙有政: ""激光表面处理Cr5钢的组织与性能"", 《中国博士学位论文全文数据库 工程科技I辑》 * |
孙有政: ""激光表面处理Cr5钢的组织与性能"", 《中国博士学位论文全文数据库 工程科技I辑》, 16 May 2019 (2019-05-16), pages 42 - 67 * |
肖海兵,钟正根,宋长辉主编: "《先进激光制造设备》", 31 March 2019, pages: 121 * |
董允,张廷森,林晓娉: "《现代表面工程技术》", 31 March 2000, pages: 306 - 307 * |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN113894291A (en) * | 2021-09-23 | 2022-01-07 | 石家庄铁道大学 | Method for melting and forming GCr15 bearing steel for high-speed rail in selective laser area |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
Deng et al. | Mechanical and chemical properties of CoCrFeNiMo0. 2 high entropy alloy coating fabricated on Ti6Al4V by laser cladding | |
CN101974724B (en) | Iron-based alloy powder for high strength and toughness laser deposited coating | |
CN101519778B (en) | Laser cladding method for strengthening surface of piercing point | |
CN111218682A (en) | Corrosion-resistant and wear-resistant iron-based laser cladding powder and laser cladding method | |
CN110791754A (en) | High-wear-resistance conductive strong-bonding coating and preparation method thereof | |
CN106757013B (en) | Polynary high-temperature alloy layer of a kind of titanium alloy laser surface silicide enhancing and preparation method thereof | |
CN109355652A (en) | Laser melting coating Co-based alloy powder and preparation method thereof | |
CN111020571B (en) | Alloy powder for laser cladding of stainless steel surface and application thereof | |
Wan et al. | A comparative study of the microstructure, mechanical properties and corrosion resistance of Ni-or Fe-based composite coatings by laser cladding | |
Abdi et al. | Study on the effect of the crack closing of AlCoCrFeMnNi high entropy alloy electro-spark deposited coating by plasma nitriding on the corrosion resistance | |
CN110747464A (en) | Preparation method of centrifugal fan steel spindle coating based on high-speed laser cladding technology | |
CN116121751B (en) | Self-lubricating wear-resistant composite coating and ultra-high-speed laser cladding method thereof | |
CN110158083B (en) | High-speed laser cladding alloy powder for surface strengthening of centrifugal compressor and method | |
CN111676478A (en) | A kind of preparation method of corrosion-resistant alloy layer on the surface of GCr15 steel | |
CN108326287A (en) | Corrosion-resistant laser cladding powder and its cladding method and purposes | |
CN102021567A (en) | Nickel base alloy powder for manufacturing anticorrosive coating of boiler tube | |
CN119040881A (en) | Laser cladding nickel-based superalloy wear-resistant gradient coating and preparation method thereof | |
Chenglong et al. | Microstructure, Tribocorrosion and Corrosion Performances of Laser Cladded Ni625-x TiC Coatings in 3.5% NaCl Solution | |
Zhicheng et al. | Effect of laser remelting on microstructure, salt spray corrosion and electrochemical performance of plasma sprayed CoCrFeNiMo HEA coating | |
CN118895499A (en) | A Fe-WC composite coating and preparation method thereof | |
CN118086894A (en) | Intermediate entropy alloy laser metal deposition layer and preparation method thereof | |
CN110904450A (en) | Method for regulating stress of multi-component laser cladding layer | |
CN1515705A (en) | Method for in-situ growth of high hardness and wear-resistant ceramic coating on titanium alloy surface | |
CN116397225A (en) | Cavitation erosion resistant laser cladding material and application thereof in surface repair of hydropower station overcurrent part | |
Tarelnyk et al. | New method for nitrocarburizing steel parts |
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 | ||
RJ01 | Rejection of invention patent application after publication | ||
RJ01 | Rejection of invention patent application after publication |
Application publication date: 20200918 |