CN114250463B - Preparation method of intelligent coating with double energy absorption and impact resistance - Google Patents
Preparation method of intelligent coating with double energy absorption and impact resistance Download PDFInfo
- Publication number
- CN114250463B CN114250463B CN202111543936.5A CN202111543936A CN114250463B CN 114250463 B CN114250463 B CN 114250463B CN 202111543936 A CN202111543936 A CN 202111543936A CN 114250463 B CN114250463 B CN 114250463B
- Authority
- CN
- China
- Prior art keywords
- coating
- absorbing
- self
- energy
- energy absorption
- 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 85
- 239000011248 coating agent Substances 0.000 title claims abstract description 77
- 238000010521 absorption reaction Methods 0.000 title claims abstract description 21
- 238000002360 preparation method Methods 0.000 title claims abstract description 21
- 239000000843 powder Substances 0.000 claims abstract description 61
- 229910052751 metal Inorganic materials 0.000 claims abstract description 39
- 239000002184 metal Substances 0.000 claims abstract description 39
- 238000000498 ball milling Methods 0.000 claims abstract description 26
- 238000004372 laser cladding Methods 0.000 claims abstract description 22
- 239000000758 substrate Substances 0.000 claims abstract description 21
- 238000000034 method Methods 0.000 claims abstract description 20
- 239000000835 fiber Substances 0.000 claims abstract description 16
- 238000005728 strengthening Methods 0.000 claims abstract description 15
- 238000005096 rolling process Methods 0.000 claims abstract description 12
- 230000008569 process Effects 0.000 claims abstract description 9
- 229910045601 alloy Inorganic materials 0.000 claims description 31
- 239000000956 alloy Substances 0.000 claims description 31
- 238000005253 cladding Methods 0.000 claims description 12
- 230000009977 dual effect Effects 0.000 claims description 9
- 239000000463 material Substances 0.000 claims description 9
- 239000011159 matrix material Substances 0.000 claims description 9
- 239000002245 particle Substances 0.000 claims description 8
- 238000004140 cleaning Methods 0.000 claims description 7
- 238000002156 mixing Methods 0.000 claims description 6
- 229910000831 Steel Inorganic materials 0.000 claims description 5
- 229910052782 aluminium Inorganic materials 0.000 claims description 5
- 239000010959 steel Substances 0.000 claims description 5
- 229920000049 Carbon (fiber) Polymers 0.000 claims description 4
- 239000004917 carbon fiber Substances 0.000 claims description 4
- 238000001035 drying Methods 0.000 claims description 4
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 claims description 4
- HBMJWWWQQXIZIP-UHFFFAOYSA-N silicon carbide Chemical compound [Si+]#[C-] HBMJWWWQQXIZIP-UHFFFAOYSA-N 0.000 claims description 4
- 229910010271 silicon carbide Inorganic materials 0.000 claims description 4
- 229910052719 titanium Inorganic materials 0.000 claims description 4
- 239000010936 titanium Substances 0.000 claims description 4
- 229910052802 copper Inorganic materials 0.000 claims description 3
- 229910052721 tungsten Inorganic materials 0.000 claims description 3
- 229910052720 vanadium Inorganic materials 0.000 claims description 3
- 229910052727 yttrium Inorganic materials 0.000 claims description 3
- 229910000851 Alloy steel Inorganic materials 0.000 claims description 2
- 229910052581 Si3N4 Inorganic materials 0.000 claims description 2
- 229910001069 Ti alloy Inorganic materials 0.000 claims description 2
- HQVNEWCFYHHQES-UHFFFAOYSA-N silicon nitride Chemical compound N12[Si]34N5[Si]62N3[Si]51N64 HQVNEWCFYHHQES-UHFFFAOYSA-N 0.000 claims description 2
- 238000005498 polishing Methods 0.000 claims 2
- 230000003014 reinforcing effect Effects 0.000 claims 1
- 230000035939 shock Effects 0.000 claims 1
- 239000010410 layer Substances 0.000 abstract description 63
- 230000003044 adaptive effect Effects 0.000 abstract description 19
- 239000000203 mixture Substances 0.000 abstract description 5
- 239000002344 surface layer Substances 0.000 abstract description 3
- 230000007246 mechanism Effects 0.000 abstract description 2
- 230000007704 transition Effects 0.000 abstract description 2
- 238000000227 grinding Methods 0.000 description 9
- 230000005540 biological transmission Effects 0.000 description 5
- 229910052759 nickel Inorganic materials 0.000 description 5
- 238000012360 testing method Methods 0.000 description 5
- 238000013016 damping Methods 0.000 description 4
- 238000005516 engineering process Methods 0.000 description 4
- 239000012159 carrier gas Substances 0.000 description 3
- 229910052804 chromium Inorganic materials 0.000 description 3
- 239000002131 composite material Substances 0.000 description 3
- 229910052733 gallium Inorganic materials 0.000 description 3
- 229910052748 manganese Inorganic materials 0.000 description 3
- 239000011572 manganese Substances 0.000 description 3
- 229910052758 niobium Inorganic materials 0.000 description 3
- 230000002195 synergetic effect Effects 0.000 description 3
- 229910000617 Mangalloy Inorganic materials 0.000 description 2
- 125000004122 cyclic group Chemical group 0.000 description 2
- 238000013461 design Methods 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 238000009792 diffusion process Methods 0.000 description 2
- 238000009863 impact test Methods 0.000 description 2
- 230000006872 improvement Effects 0.000 description 2
- 229910052738 indium Inorganic materials 0.000 description 2
- 239000011812 mixed powder Substances 0.000 description 2
- 229910052750 molybdenum Inorganic materials 0.000 description 2
- 229910052710 silicon Inorganic materials 0.000 description 2
- 239000002356 single layer Substances 0.000 description 2
- 229910052718 tin Inorganic materials 0.000 description 2
- 229920002396 Polyurea Polymers 0.000 description 1
- XSQUKJJJFZCRTK-UHFFFAOYSA-N Urea Chemical compound NC(N)=O XSQUKJJJFZCRTK-UHFFFAOYSA-N 0.000 description 1
- 238000005299 abrasion Methods 0.000 description 1
- 239000002250 absorbent Substances 0.000 description 1
- 239000004202 carbamide Substances 0.000 description 1
- 230000000052 comparative effect Effects 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 229910021389 graphene Inorganic materials 0.000 description 1
- 238000011065 in-situ storage Methods 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- CWQXQMHSOZUFJS-UHFFFAOYSA-N molybdenum disulfide Chemical compound S=[Mo]=S CWQXQMHSOZUFJS-UHFFFAOYSA-N 0.000 description 1
- 229910052982 molybdenum disulfide Inorganic materials 0.000 description 1
- 239000002135 nanosheet Substances 0.000 description 1
- 230000000704 physical effect Effects 0.000 description 1
- 238000007750 plasma spraying Methods 0.000 description 1
- 239000011148 porous material Substances 0.000 description 1
- 230000008439 repair process Effects 0.000 description 1
- 239000004576 sand Substances 0.000 description 1
- 230000003313 weakening effect Effects 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
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/02—Ferrous alloys, e.g. steel alloys containing silicon
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/04—Ferrous alloys, e.g. steel alloys containing manganese
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C49/00—Alloys containing metallic or non-metallic fibres or filaments
- C22C49/02—Alloys containing metallic or non-metallic fibres or filaments characterised by the matrix material
- C22C49/08—Iron group metals
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C49/00—Alloys containing metallic or non-metallic fibres or filaments
- C22C49/14—Alloys containing metallic or non-metallic fibres or filaments characterised by the fibres or filaments
-
- 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)
- Powder Metallurgy (AREA)
Abstract
具有双重吸能抗冲击的智能涂层的制备方法,本发明为了解决现有金属机械运动部件在大冲击、高磨损工况条件下磨损严重、易失效和服役寿命短等问题。制备方法:一、将耐高温纤维和NiXY金属粉末球磨混合;二、将强化相粉末和FeMnSiA金属粉末球磨混合;三、打磨金属基体;四、在金属基体上施加超声振动,采用激光熔覆工艺制备自适应吸能层;五、采用激光熔覆工艺制备自硬化耐磨层;六、对双重吸能涂层进行打磨;七、对双重吸能涂层进行超声深滚处理。本发明双重吸能抗冲击智能涂层中的表层通过吸能相变机制将冲击能转变为自身强化的动力,内层将纵向冲击能量吸收后横向传输、扩散,提高涂层综合力学性能。
The preparation method of an intelligent coating with double energy absorption and impact resistance is designed to solve the problems of severe wear, easy failure and short service life of the existing metal mechanical moving parts under the conditions of large impact and high wear. Preparation method: 1. Mix the high temperature resistant fiber and NiXY metal powder by ball milling; 2. Mix the strengthening phase powder and FeMnSiA metal powder by ball milling; 3. Grind the metal substrate; 4. Apply ultrasonic vibration on the metal substrate and adopt laser cladding process Prepare an adaptive energy-absorbing layer; Fifth, prepare a self-hardening wear-resistant layer by laser cladding; Six, polish the double energy-absorbing coating; Seven, perform ultrasonic deep rolling treatment on the double energy-absorbing coating. The surface layer of the double energy-absorbing impact-resistant intelligent coating of the present invention transforms the impact energy into self-strengthening power through the energy-absorbing phase transition mechanism, and the inner layer absorbs the longitudinal impact energy and transmits and diffuses it laterally to improve the comprehensive mechanical properties of the coating.
Description
技术领域technical field
本发明属于表面工程领域,具体涉及一种具有“自适应-自硬化”的双重吸能抗冲击智能涂层的制备方法。The invention belongs to the field of surface engineering, and in particular relates to a preparation method of an "adaptive-self-hardening" double energy-absorbing and impact-resistant intelligent coating.
背景技术Background technique
近年来,由于技术的发展,各种机械设备的功率逐渐提高,使得机械零部件的工作环境越来越复杂恶劣,如大冲击、高磨损恶劣工况,其运动部件频繁发生疲劳、磨损、断裂等失效,因此需要及时进行更换,造成生产成本大幅提高。而目前在材料表面利用表面改性技术制备抗冲击耐磨涂层是延长零部件使用寿命的有效手段。In recent years, due to the development of technology, the power of various mechanical equipment has gradually increased, making the working environment of mechanical parts more and more complex and harsh, such as heavy impact, high wear and harsh working conditions, and its moving parts are frequently fatigued, worn, and broken Waiting for failure, so it needs to be replaced in time, resulting in a significant increase in production costs. At present, the use of surface modification technology to prepare impact-resistant and wear-resistant coatings on the surface of materials is an effective means to prolong the service life of parts.
抗冲击涂层的结构设计特点有单层、多层的结构涂层。单层涂层在冲击下易产生边缘裂纹和径向裂纹,服役寿命短。多层涂层在低冲击载荷下表现出较高的抗循环冲击性,而在大冲击载荷下表现出较差的循环冲击性,难以在大冲击、高磨损恶劣工况下长期使用。为了突破大冲击、高磨损工况下抗冲击涂层服役寿命短的问题,公开号为CN113118001A,专利名称为《一种具有抗冲击和耐磨性能复合涂层的制备方法》的专利中采用聚脲与石墨烯负载二硫化钼纳米片原位聚合的方式,制备出聚脲石墨烯复合抗冲击高耐磨涂层,但由于聚脲的物理特性,在超过200℃时,其性能受到严重弱化,不能有效防护零件在大冲击,高磨损工况下长时间使用。公开号CN113235036A,专利名称为《一种机制砂用硬质颗粒增强耐冲击磨损涂层的制备方法》的专利中采用等离子喷涂与激光重熔相结合在高锰钢上制备硬质颗粒增强耐冲击磨损涂层,具有较好的抗冲击性能与耐磨性能,但该涂层受限于高锰钢基体,若更换基体,则难以抵抗大冲击作用。因此,目前亟需一种强结合、耐大冲击、高耐磨的强韧一体化涂层来大幅提高在大冲击、高磨损恶劣工况下零件的服役寿命。The structural design features of impact-resistant coatings include single-layer and multi-layer structural coatings. Single-layer coatings are prone to edge cracks and radial cracks under impact, and their service life is short. Multi-layer coatings exhibit high cyclic impact resistance under low impact loads, but poor cyclic impact resistance under high impact loads, making it difficult to use them for a long time under severe conditions of high impact and high wear. In order to break through the problem of short service life of impact-resistant coatings under high-impact and high-wear conditions, the publication number is CN113118001A, and the patent name is "A Preparation Method for Composite Coatings with Impact and Wear Resistance". Urea and graphene-supported molybdenum disulfide nanosheets are in-situ polymerized to prepare a polyurea-graphene composite impact-resistant and high-wear resistance coating, but due to the physical properties of polyurea, its performance is severely weakened when it exceeds 200 °C , cannot effectively protect the parts from being used for a long time under large impact and high wear conditions. Publication No. CN113235036A, the patent title is "Preparation Method of Hard Particle Reinforced Impact and Wear-Resistant Coating for Machine-made Sand", in which the combination of plasma spraying and laser remelting is used to prepare hard particle-reinforced impact-resistant coating on high manganese steel Abrasion coating has good impact resistance and wear resistance, but the coating is limited by the high manganese steel substrate. If the substrate is replaced, it will be difficult to resist large impact. Therefore, there is an urgent need for a strong and tough integrated coating with strong bonding, high impact resistance and high wear resistance to greatly improve the service life of parts under severe conditions of high impact and high wear.
发明内容Contents of the invention
本发明的目的是为了解决现有金属机械运动部件在大冲击、高磨损工况条件下磨损严重、易失效和服役寿命短等问题,而提供一种具有“自适应-自硬化”的双重吸能抗冲击智能涂层的制备方法。The purpose of the present invention is to solve the problems of severe wear, easy failure and short service life of the existing metal mechanical moving parts under the conditions of large impact and high wear, and to provide a double-absorbent with "adaptive-self-hardening" A method for preparing an impact-resistant intelligent coating.
本发明具有双重吸能抗冲击的智能涂层的制备方法按照以下步骤实现:The preparation method of the intelligent coating with double energy absorption and impact resistance of the present invention is realized according to the following steps:
一、制备自适应吸能层合金粉末:1. Preparation of adaptive energy-absorbing layer alloy powder:
按照重量百分比将3%-8%的耐高温纤维和92%-97%的NiXY金属粉末球磨混合,得到自适应吸能层合金粉末;Mix 3%-8% high temperature resistant fiber and 92%-97% NiXY metal powder by ball milling according to weight percentage to obtain adaptive energy-absorbing layer alloy powder;
二、制备自硬化耐磨层合金粉末;2. Preparation of self-hardening wear-resistant layer alloy powder;
按照重量百分比将10%-20%的强化相粉末和80%-90%的FeMnSiA金属粉末球磨混合,得到自硬化耐磨层合金粉末;Ball milling and mixing 10%-20% of strengthening phase powder and 80%-90% of FeMnSiA metal powder according to weight percentage to obtain self-hardening wear-resistant layer alloy powder;
三、打磨金属基体,清洗后得到表面光洁的金属基体;3. Grinding the metal substrate to obtain a metal substrate with a smooth surface after cleaning;
四、在表面光洁的金属基体上施加超声振动,采用激光熔覆工艺,以自适应吸能层合金粉末作为熔覆粉体,控制激光熔覆参数为:激光波长1053nm、激光功率1000-2000W、扫描速率5-15mm/s,在金属基体表面制备自适应吸能层;4. Apply ultrasonic vibration on the metal substrate with smooth surface, adopt laser cladding process, use adaptive energy-absorbing layer alloy powder as cladding powder, control laser cladding parameters: laser wavelength 1053nm, laser power 1000-2000W, The scan rate is 5-15mm/s, and an adaptive energy-absorbing layer is prepared on the surface of the metal substrate;
五、在吸能自适应层上采用激光熔覆工艺制备自硬化耐磨层,以自硬化耐磨层合金粉末作为熔覆粉体,控制激光熔覆参数为:激光波长1053nm、激光功率1500-2200W、扫描速率5-15mm/s,在金属基体表面制备得到双重吸能涂层;5. The self-hardening wear-resistant layer is prepared by laser cladding process on the energy-absorbing adaptive layer, and the self-hardening wear-resistant layer alloy powder is used as the cladding powder. The laser cladding parameters are controlled as follows: laser wavelength 1053nm, laser power 1500- 2200W, scan rate 5-15mm/s, double energy-absorbing coating is prepared on the surface of the metal substrate;
六、对双重吸能涂层进行打磨,清洗,烘干;6. Grinding, cleaning and drying the double energy-absorbing coating;
七、对双重吸能涂层进行超声深滚处理,得到具有双重吸能抗冲击的智能涂层;7. Perform ultrasonic deep rolling treatment on the double energy-absorbing coating to obtain an intelligent coating with double energy-absorbing and impact resistance;
其中步骤一中NiXY合金中的X为Ti、Mn或者Al,Y为Cu、Co、Nb、Ga、In、Sn、W中的一种或多种混合元素;步骤二中所述的强化相为ZrO2、Cr3C2、TiC、SiC、WC中的一种或多种混合粉末,步骤二中FeMnSiA合金中的A为Co、Ni、Mo、Al、V、Cr中的一种或多种混合元素。Wherein in step one, X in the NiXY alloy is Ti, Mn or Al, and Y is one or more mixed elements in Cu, Co, Nb, Ga, In, Sn, W; the strengthening phase described in step two is One or more mixed powders of ZrO 2 , Cr 3 C 2 , TiC, SiC, WC, and A in the FeMnSiA alloy in
本发明设计一种具有“自适应-自硬化”的双重吸能抗冲击智能涂层,双重吸能抗冲击智能涂层分为自硬化(强化)耐磨层与自适应吸能层。其中表层为自硬化耐磨层,在受到大冲击时,借助本身的吸能相变机制将冲击能转变为自身强化的动力,提高涂层强度、硬度等综合性能,同时减弱了向内传导的冲击能。而内层为具有能量传输通道的阻尼自适应吸能层,能够借助能量传输通道将纵向冲击能量吸收后横向传输、扩散,同时借助自身阻尼性能削减冲击能,再次减弱大冲击对零部件内部的损害,使得机械零件不会轻易失效,具有较长时间寿命。The invention designs a double energy-absorbing and impact-resistant intelligent coating with "self-adaptation-self-hardening". The double energy-absorbing and impact-resistant intelligent coating is divided into a self-hardening (reinforced) wear-resistant layer and an adaptive energy-absorbing layer. The surface layer is a self-hardening wear-resistant layer. When subjected to a large impact, it uses its own energy-absorbing phase transition mechanism to convert the impact energy into self-strengthening power, improving the overall performance of the coating strength, hardness, etc., and at the same time weakening the inward conduction. impact energy. The inner layer is a damping self-adaptive energy-absorbing layer with energy transmission channels, which can absorb longitudinal impact energy through energy transmission channels and then transmit and diffuse it horizontally. damage, so that mechanical parts will not easily fail and have a longer lifespan.
本发明涉及一种具有“自适应-自硬化”的双重吸能抗冲击智能涂层的制备方法,其通过超声场辅助激光熔覆技术制备双重吸能抗冲击智能涂层,优化超声场发生器的角度、频率、振幅,通过超声振动调控纤维在自适应吸能层中趋于横向排列,形成横向能量扩散通道,再通过超声深滚处理双重吸能抗冲击智能涂层,预强化自硬化耐磨层,提高涂层综合力学性能,并且赋予涂层表面一定残余压应力,提高材料的抗疲劳性能,最终实现涂层抗大冲击及耐高速磨损性能的协同提升。The present invention relates to a preparation method of an "adaptive-self-hardening" double energy-absorbing and impact-resistant intelligent coating, which prepares a double energy-absorbing and impact-resistant intelligent coating through ultrasonic field-assisted laser cladding technology, and optimizes the ultrasonic field generator The angle, frequency, and amplitude of the ultrasonic vibration control fibers tend to be arranged horizontally in the self-adaptive energy-absorbing layer to form a transverse energy diffusion channel. The grinding layer improves the comprehensive mechanical properties of the coating, and endows the surface of the coating with a certain residual compressive stress, improves the fatigue resistance of the material, and finally realizes the synergistic improvement of the coating's resistance to large impact and high-speed wear.
附图说明Description of drawings
图1为本发明具有双重吸能抗冲击的智能涂层的示意图;Fig. 1 is the schematic diagram that the present invention has double energy-absorbing and impact-resistant intelligent coating;
图2为实施例中具有双重吸能抗冲击的智能涂层与Ni基耐磨层在不同深度的平均显微硬度测试图,其中■代表智能涂层,●代表Ni基耐磨层;Fig. 2 is the average microhardness test figure at different depths of the smart coating with double energy-absorbing impact resistance and the Ni-based wear-resistant layer in the embodiment, wherein ■ represents the smart coating, and ● represents the Ni-based wear-resistant layer;
图3为实施例中具有双重吸能抗冲击的智能涂层与Ni基耐磨层摩擦系数曲线图,其中1代表智能涂层,2代表Ni基耐磨层;Fig. 3 is the curve diagram of the friction coefficient between the smart coating with double energy absorption and impact resistance and the Ni-based wear-resistant layer in the embodiment, wherein 1 represents the smart coating, and 2 represents the Ni-based wear-resistant layer;
图4为实施例中具有双重吸能抗冲击的智能涂层与Ni基耐磨层冲击功柱状图。Fig. 4 is a histogram of the impact energy of the intelligent coating with double energy absorption and impact resistance and the Ni-based wear-resistant layer in the embodiment.
具体实施方式Detailed ways
具体实施方式一:本实施方式具有双重吸能抗冲击的智能涂层的制备方法按照以下步骤实施:Specific Embodiment 1: The preparation method of the intelligent coating with double energy absorption and impact resistance in this embodiment is implemented according to the following steps:
一、制备自适应吸能层合金粉末:1. Preparation of adaptive energy-absorbing layer alloy powder:
按照重量百分比将3%-8%的耐高温纤维和92%-97%的NiXY金属粉末球磨混合,得到自适应吸能层合金粉末;Mix 3%-8% high temperature resistant fiber and 92%-97% NiXY metal powder by ball milling according to weight percentage to obtain adaptive energy-absorbing layer alloy powder;
二、制备自硬化耐磨层合金粉末;2. Preparation of self-hardening wear-resistant layer alloy powder;
按照重量百分比将10%-20%的强化相粉末和80%-90%的FeMnSiA金属粉末球磨混合,得到自硬化耐磨层合金粉末;Ball milling and mixing 10%-20% of strengthening phase powder and 80%-90% of FeMnSiA metal powder according to weight percentage to obtain self-hardening wear-resistant layer alloy powder;
三、打磨金属基体,清洗后得到表面光洁的金属基体;3. Grinding the metal substrate to obtain a metal substrate with a smooth surface after cleaning;
四、在表面光洁的金属基体上施加超声振动,采用激光熔覆工艺,以自适应吸能层合金粉末作为熔覆粉体,控制激光熔覆参数为:激光波长1053nm、激光功率1000-2000W、扫描速率5-15mm/s,在金属基体表面制备自适应吸能层;4. Apply ultrasonic vibration on the metal substrate with smooth surface, adopt laser cladding process, use adaptive energy-absorbing layer alloy powder as cladding powder, control laser cladding parameters: laser wavelength 1053nm, laser power 1000-2000W, The scan rate is 5-15mm/s, and an adaptive energy-absorbing layer is prepared on the surface of the metal substrate;
五、在吸能自适应层上采用激光熔覆工艺制备自硬化耐磨层,以自硬化耐磨层合金粉末作为熔覆粉体,控制激光熔覆参数为:激光波长1053nm、激光功率1500-2200W、扫描速率5-15mm/s,在金属基体表面制备得到双重吸能涂层;5. The self-hardening wear-resistant layer is prepared by laser cladding process on the energy-absorbing adaptive layer, and the self-hardening wear-resistant layer alloy powder is used as the cladding powder. The laser cladding parameters are controlled as follows: laser wavelength 1053nm, laser power 1500- 2200W, scan rate 5-15mm/s, double energy-absorbing coating is prepared on the surface of the metal substrate;
六、对双重吸能涂层进行打磨,清洗,烘干;6. Grinding, cleaning and drying the double energy-absorbing coating;
七、对双重吸能涂层进行超声深滚处理,得到具有双重吸能抗冲击的智能涂层;7. Perform ultrasonic deep rolling treatment on the double energy-absorbing coating to obtain an intelligent coating with double energy-absorbing and impact resistance;
其中步骤一中NiXY合金中的X为Ti、Mn或者Al,Y为Cu、Co、Nb、Ga、In、Sn、W中的一种或多种混合元素;步骤二中所述的强化相为ZrO2、Cr3C2、TiC、SiC、WC中的一种或多种混合粉末,步骤二中FeMnSiA合金中的A为Co、Ni、Mo、Al、V、Cr中的一种或多种混合元素。Wherein in step one, X in the NiXY alloy is Ti, Mn or Al, and Y is one or more mixed elements in Cu, Co, Nb, Ga, In, Sn, W; the strengthening phase described in step two is One or more mixed powders of ZrO 2 , Cr 3 C 2 , TiC, SiC, WC, and A in the FeMnSiA alloy in
本实施方式步骤一中NiXY金属粉末和步骤二中FeMnSiA金属粉末均采用单质的金属粉末。In this embodiment, the NiXY metal powder in
本实施方式双重吸能抗冲击智能涂层分为自适应吸能层与自硬化耐磨层,其中表层为自硬化耐磨层,在受到大冲击时,借助本身的吸能相变机制将冲击能转变为自身强化的动力,提高涂层强度、硬度等综合性能,同时减弱了向内传导的冲击能。而内层为具有能量传输通道的阻尼自适应吸能层,能够借助能量传输通道将纵向冲击能量吸收后横向传输、扩散,同时借助自身阻尼性能削减冲击能。在超声场协同作用下激光熔覆制备智能涂层,调控纤维在自适应吸能层中趋于横向排列,形成横向能量扩散通道,减少涂层内部气孔、裂纹缺陷,并借助超声深滚技术处理双重吸能抗冲击智能涂层,预强化自硬化耐磨层,提高涂层综合力学性能,并可以在一定程度上修复表面微裂纹、蚀坑等损伤,提高涂层抗疲劳性能,最终实现涂层抗大冲击及耐高速磨损性能的协同提升。In this embodiment, the dual energy-absorbing and impact-resistant intelligent coating is divided into an adaptive energy-absorbing layer and a self-hardening wear-resistant layer. The surface layer is a self-hardening wear-resistant layer. It can be converted into self-strengthening power, improve the overall performance of coating strength, hardness, etc., and at the same time weaken the impact energy transmitted inward. The inner layer is a damping adaptive energy-absorbing layer with energy transmission channels, which can absorb longitudinal impact energy through energy transmission channels and then transmit and diffuse it laterally, while reducing impact energy with its own damping performance. Under the synergistic effect of ultrasonic field, laser cladding prepares smart coatings, regulates the fibers to be arranged horizontally in the self-adaptive energy-absorbing layer, forms transverse energy diffusion channels, reduces internal pores and crack defects in the coating, and is treated with the help of ultrasonic deep rolling technology Double energy-absorbing impact-resistant intelligent coating, pre-strengthened self-hardening wear-resistant layer, improves the comprehensive mechanical properties of the coating, and can repair surface micro-cracks, corrosion pits and other damage to a certain extent, improve the fatigue resistance of the coating, and finally realize the coating The synergistic improvement of layer resistance to large impact and high-speed wear resistance.
具体实施方式二:本实施方式与具体实施方式一不同的是步骤一中所述的耐高温纤维的直径为5-10μm,长度为45-105μm。Embodiment 2: This embodiment differs from
具体实施方式三:本实施方式与具体实施方式一或二不同的是步骤一中所述的耐高温纤维为碳纤维、碳化硅纤维、氮化硅纤维中的一种或多种混合纤维。Embodiment 3: The difference between this embodiment and
具体实施方式四:本实施方式与具体实施方式一至三之一不同的是步骤二中强化相粉末的粒径为6-45μm。Embodiment 4: This embodiment differs from
具体实施方式五:本实施方式与具体实施方式一至四之一不同的是步骤一和步骤二中所述的球磨混合是以GCr15钢球为球磨介质,控制球料质量比为2:1,转速为300-350r/min,球磨时间为3-4h。Specific embodiment five: what this embodiment is different from one of specific embodiments one to four is that the ball mill mixing described in
具体实施方式六:本实施方式与具体实施方式一至五之一不同的是步骤三所述的金属基体的材质为合金钢或者钛合金。Embodiment 6: This embodiment differs from
具体实施方式七:本实施方式与具体实施方式一至六之一不同的是步骤四中控制超声场参数为:频率20000-35000Hz、振幅5mm-20mm。Embodiment 7: This embodiment differs from
具体实施方式八:本实施方式与具体实施方式一至七之一不同的是步骤四中自适应吸能层的厚度为0.5-2mm。Embodiment 8: This embodiment differs from
具体实施方式九:本实施方式与具体实施方式一至八之一不同的是步骤五中自硬化耐磨层的厚度为0.5-2mm。Embodiment 9: This embodiment differs from
具体实施方式十:本实施方式与具体实施方式一至九之一不同的是步骤六中控制超声深滚参数为:超声波震动频率为20-30kHz,超声深滚5-15遍,轴向的纵向进给速度为15-30mm/min,横向进给步距为0.1-0.3mm,作用力为200-300N。Embodiment 10: This embodiment differs from
实施例:本实施例具有双重吸能抗冲击的智能涂层的制备方法按照以下步骤实施:Embodiment: In this embodiment, the preparation method of an intelligent coating with double energy absorption and impact resistance is implemented according to the following steps:
一、制备自适应吸能层合金粉末:1. Preparation of adaptive energy-absorbing layer alloy powder:
按照重量百分比将碳纤维5%、Ni 45%、Ti 43%、Nb 5%、Ga 2%球磨混合,其中金属粉末粒径均为70μm左右;碳纤维直径为8μm左右,长度为70μm左右;球磨参数为:球磨介质为GCr15钢球、球料比为2:1、转速为300r/min、球磨时间为3h,球磨后置于120℃烘箱中烘干处理2.5h,得到自适应吸能层合金粉末;Mix carbon fiber 5%, Ni 45%, Ti 43%, Nb 5%, and
二、制备自硬化耐磨层合金粉末;2. Preparation of self-hardening wear-resistant layer alloy powder;
按照重量百分比将ZrO2 15%、Fe 42%、Mn 17%、Si 4%、Cr 12%、Ni 6%、Mo4%球磨混合,其中金属粉末粒径均为70μm左右,ZrO2粉末粒径为30μm,球磨参数为:球磨介质为GCr15钢球、球料比为2:1、转速为300r/min、球磨时间为3h,球磨后置于120℃烘箱中烘干处理2.5h,得到自硬化耐磨层合金粉末;According to the percentage by weight, ZrO 2 15%, Fe 42%, Mn 17%, Si 4%, Cr 12%, Ni 6%, Mo4% are ball milled and mixed, and the particle size of the metal powder is about 70 μm, and the particle size of the ZrO 2 powder is 30μm, the ball milling parameters are: the ball milling medium is GCr15 steel balls, the ball-to-material ratio is 2:1, the rotating speed is 300r/min, the ball milling time is 3h, and after the ball milling, it is dried in an oven at 120°C for 2.5h to obtain self-hardening resistant Grinding layer alloy powder;
三、打磨38CrMoAl基体,除氧化皮,得到表面光洁的38CrMoAl基体;3. Grinding the 38CrMoAl matrix to remove the scale to obtain a 38CrMoAl matrix with a smooth surface;
四、在表面光洁的金属基体上施加超声振动,施加超声振动方式是采用超声枪紧压基体材料表面,再采用激光熔覆工艺,以自适应吸能层合金粉末作为熔覆粉体,控制超声场参数为:超声场发生器与基体夹角12°、频率25000Hz、振幅10mm,控制激光熔覆参数为:激光波长1053nm、激光功率1200W、扫描速率10mm/s、搭接率35%、光斑直径4mm、熔覆距离40mm、送粉速率0.15g/s、载气流量为25L/min,在金属基体表面制备自适应吸能层;4. Apply ultrasonic vibration on the metal substrate with a smooth surface. The method of applying ultrasonic vibration is to use an ultrasonic gun to press the surface of the substrate material tightly, and then use the laser cladding process to use the self-adaptive energy-absorbing layer alloy powder as the cladding powder to control the ultrasonic vibration. The field parameters are: the angle between the ultrasonic field generator and the substrate is 12°, the frequency is 25000Hz, and the amplitude is 10mm. The parameters for controlling laser cladding are: laser wavelength 1053nm, laser power 1200W, scan rate 10mm/s, lap rate 35%, spot diameter 4mm, cladding distance 40mm, powder feeding rate 0.15g/s, carrier gas flow rate 25L/min, prepare an adaptive energy-absorbing layer on the surface of the metal substrate;
五、在吸能自适应层上采用激光熔覆工艺制备自硬化耐磨层,以自硬化耐磨层合金粉末作为熔覆粉体,控制激光熔覆参数为:激光波长1053nm、激光功率1800W、扫描速率11mm/s、搭接率33%、光斑直径4mm、熔覆距离40mm、送粉速率0.15g/s、载气流量为25L/min,在金属基体表面制备得到双重吸能涂层;5. The self-hardening wear-resistant layer is prepared by laser cladding on the energy-absorbing self-adaptive layer, and the self-hardening wear-resistant layer alloy powder is used as the cladding powder. The laser cladding parameters are controlled as follows: laser wavelength 1053nm, laser power 1800W, The scan rate is 11mm/s, the overlap rate is 33%, the spot diameter is 4mm, the cladding distance is 40mm, the powder feeding rate is 0.15g/s, the carrier gas flow rate is 25L/min, and the double energy-absorbing coating is prepared on the surface of the metal substrate;
六、对双重吸能涂层进行打磨,清洗,烘干;6. Grinding, cleaning and drying the double energy-absorbing coating;
七、对双重吸能涂层进行超声深滚处理,控制超声深滚参数为:超声波震动频率为20kHz,超声深滚10遍,轴向的纵向进给速度为30mm/min,横向进给步距为0.2mm,作用力为200N,得到具有双重吸能抗冲击的智能涂层。7. Perform ultrasonic deep rolling treatment on the double energy-absorbing coating, and control the ultrasonic deep rolling parameters as follows: ultrasonic vibration frequency is 20kHz, ultrasonic deep rolling is 10 times, the axial longitudinal feed speed is 30mm/min, and the transverse feed step The thickness is 0.2mm, and the force is 200N, and a smart coating with double energy absorption and impact resistance is obtained.
对比实施例:本实施例Ni基耐磨层的制备方法按照以下步骤实施:Comparative example: the preparation method of the Ni-based wear-resistant layer of this embodiment is implemented according to the following steps:
一、将38CrMoAl基体进行打磨,除氧化皮,获得表面光洁的38CrMoAl基体。1. Grinding the 38CrMoAl matrix to remove scale to obtain a 38CrMoAl matrix with a smooth surface.
二、Ni基耐磨涂层合金粉末制备:2. Preparation of Ni-based wear-resistant coating alloy powder:
按照重量百分比将Cr 17%、B 3.5%、Si 3.5%、Ni 56%、WC 20%球磨混合,其中金属粉末粒径均为70μm左右,WC粉末粒径为25μm,球磨参数为:球磨介质为GCr15钢球、球料比为2:1、转速为350r/min、球磨时间为3h,球磨后置于150℃烘箱中烘干处理2h,得到干燥粉末;Cr 17%, B 3.5%, Si 3.5%, Ni 56%, and
三、强化相强化Ni基耐磨涂层制备:利用激光熔覆工艺,以干燥粉末作为熔覆粉体,控制激光熔覆参数为:激光波长1053nm、激光功率1500W、扫描速率10mm/s、搭接率33%、光斑直径4mm、熔覆距离40mm、送粉速率0.15g/s、载气流量为25L/min,得到强化相强化Ni基耐磨涂层。3. Preparation of strengthening phase strengthened Ni-based wear-resistant coating: use laser cladding process, use dry powder as cladding powder, control laser cladding parameters: laser wavelength 1053nm, laser power 1500W, scanning speed 10mm/s, lapping The bonding rate is 33%, the spot diameter is 4mm, the cladding distance is 40mm, the powder feeding rate is 0.15g/s, and the carrier gas flow rate is 25L/min, and the strengthening phase strengthened Ni-based wear-resistant coating is obtained.
本实施例双重吸能抗冲击智能涂层从上到下分为自硬化耐磨层和自适应吸能层;自硬化耐磨层受到大冲击时,借助本身的吸能相变机制将冲击能转变为自身强化的动力,提高涂层强度、硬度等综合性能,同时减弱了向内传导的冲击能;自适应吸能层借助能量传输通道将纵向冲击能量吸收后横向传输、扩散,同时借助自身阻尼性能削减冲击能,再次减弱大冲击对零部件内部的损害,使得机械零件不会轻易失效,具有较长时间寿命。In this embodiment, the dual energy-absorbing and impact-resistant intelligent coating is divided into a self-hardening wear-resistant layer and an adaptive energy-absorbing layer from top to bottom; It transforms into self-strengthening power, improves the overall performance of coating strength and hardness, and at the same time weakens the impact energy transmitted inward; the adaptive energy-absorbing layer absorbs the longitudinal impact energy with the help of energy transmission channels and then transmits and diffuses it laterally. The damping performance reduces the impact energy, and again weakens the damage to the internal components of the large impact, so that the mechanical parts will not easily fail and have a longer service life.
本实施例得到双重吸能抗冲击智能涂层与Ni基耐磨层,对其进行打磨、抛光,在显微硬度仪上进行硬度测试,测量不同深度硬度的平均值,测试结果如图2所示;在摩擦磨损实验仪上进行摩擦系数曲线测试,测试结果如图3所示,对双重吸能抗冲击智能涂层与Ni基耐磨层的试样进行室温下标准夏比冲击实验,冲击功值如图4所示。根据试验结果可以看出:复合涂层试样截面硬度沿深度方向呈梯度分布,吸能自强化涂层表面硬度最高(平均硬度为834.4Hv),其平均摩擦系数为0.43;Ni基耐磨涂层表面硬度最高(平均硬度为732.2Hv),其平均摩擦系数为0.43;根据冲击实验,可以看出双重吸能抗冲击智能涂层的试样具有较高冲击功,双重吸能抗冲击智能涂层冲击功为76J,Ni基耐磨层冲击功为32J。综上所述,双重吸能抗冲击智能涂层具有优异的抗冲击性能与耐磨性能,从而延长了金属基体材料的使用寿命。In this embodiment, a double energy-absorbing impact-resistant intelligent coating and a Ni-based wear-resistant layer are obtained, which are polished and polished, and the hardness is tested on a microhardness tester to measure the average value of hardness at different depths. The test results are shown in Figure 2 shown; the friction coefficient curve test was carried out on the friction and wear tester, and the test results are shown in Figure 3. The standard Charpy impact test at room temperature was carried out on the samples of the double energy-absorbing impact-resistant smart coating and the Ni-based wear-resistant layer. Work value as shown in Figure 4. According to the test results, it can be seen that the cross-sectional hardness of the composite coating sample is distributed in a gradient along the depth direction, and the surface hardness of the energy-absorbing self-strengthening coating is the highest (average hardness is 834.4Hv), and its average friction coefficient is 0.43; Ni-based wear-resistant coating The surface hardness of the layer is the highest (the average hardness is 732.2Hv), and its average friction coefficient is 0.43; according to the impact test, it can be seen that the sample of the double energy-absorbing and impact-resistant intelligent coating has relatively high impact energy, and the double energy-absorbing and impact-resistant intelligent coating The impact energy of the layer is 76J, and the impact energy of the Ni-based wear-resistant layer is 32J. To sum up, the dual energy-absorbing and impact-resistant intelligent coating has excellent impact resistance and wear resistance, thereby prolonging the service life of the metal matrix material.
Claims (10)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202111543936.5A CN114250463B (en) | 2021-12-16 | 2021-12-16 | Preparation method of intelligent coating with double energy absorption and impact resistance |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202111543936.5A CN114250463B (en) | 2021-12-16 | 2021-12-16 | Preparation method of intelligent coating with double energy absorption and impact resistance |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN114250463A CN114250463A (en) | 2022-03-29 |
| CN114250463B true CN114250463B (en) | 2023-06-06 |
Family
ID=80795392
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202111543936.5A Active CN114250463B (en) | 2021-12-16 | 2021-12-16 | Preparation method of intelligent coating with double energy absorption and impact resistance |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN114250463B (en) |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104099540A (en) * | 2014-08-06 | 2014-10-15 | 哈尔滨工程大学 | Preparation method of NiTi fiber reinforced intermetallic compound-based laminar composite material for vibration and noise reduction |
| CN108746585A (en) * | 2018-05-21 | 2018-11-06 | 江苏大学 | Low damage type FeMnSi micro-nano powder cored filament materials of laser gain material manufacture function and preparation method thereof |
| EP3590643A1 (en) * | 2018-07-02 | 2020-01-08 | Höganäs AB (publ) | Wear-resistant iron-based alloy compositions comprising nickel |
| CN111962064A (en) * | 2020-07-28 | 2020-11-20 | 江苏大学 | A method of jet cavitation strengthening shape memory alloy coating on the surface of axial flow pump blades |
-
2021
- 2021-12-16 CN CN202111543936.5A patent/CN114250463B/en active Active
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104099540A (en) * | 2014-08-06 | 2014-10-15 | 哈尔滨工程大学 | Preparation method of NiTi fiber reinforced intermetallic compound-based laminar composite material for vibration and noise reduction |
| CN108746585A (en) * | 2018-05-21 | 2018-11-06 | 江苏大学 | Low damage type FeMnSi micro-nano powder cored filament materials of laser gain material manufacture function and preparation method thereof |
| EP3590643A1 (en) * | 2018-07-02 | 2020-01-08 | Höganäs AB (publ) | Wear-resistant iron-based alloy compositions comprising nickel |
| CN111962064A (en) * | 2020-07-28 | 2020-11-20 | 江苏大学 | A method of jet cavitation strengthening shape memory alloy coating on the surface of axial flow pump blades |
Also Published As
| Publication number | Publication date |
|---|---|
| CN114250463A (en) | 2022-03-29 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN111139466B (en) | Titanium alloy petroleum drill pipe wear-resistant belt and preparation method thereof | |
| CN114045484A (en) | A kind of multi-scale ceramic particle coupling enhanced laser cladding iron-based wear-resistant coating and preparation method thereof | |
| CN104148806B (en) | A kind of cast steel with high chromium roll top layer fatigue statistic rapid laser repair method | |
| CN106367707A (en) | Laser remelting method for ultrasonic spraying of WC-12Co coating | |
| CN110923707B (en) | Titanium alloy surface high-temperature-resistant composite coating material based on laser cladding | |
| CN110066995A (en) | A kind of cladding alloy powder and the laser cladding method for carrying out H13 mould steel | |
| CN117779016A (en) | Gradient wear-resistant zone, drill pipe and preparation method of downhole titanium alloy drill pipe | |
| CN115673314A (en) | Iron-based laser cladding material and wear-resistant iron-based laser cladding layer | |
| CN114250463B (en) | Preparation method of intelligent coating with double energy absorption and impact resistance | |
| CN117004942A (en) | High-performance laser cladding alloy cutter | |
| CN114293187A (en) | Preparation method of NbC-reinforced iron-based alloy high-strength wear-resistant coating | |
| CN113584478A (en) | Preparation method of self-lubricating hard composite coating on surface of shield machine cutter | |
| CN109576604B (en) | Impact-resistant wear-resistant material for laser manufacturing | |
| CN111593345B (en) | A composite powder and a preparation method thereof, an anti-contact fatigue coating and a preparation method thereof | |
| Liu et al. | Microstructures and high-temperature friction and wear behavior of high-velocity oxygen-fuel-sprayed WC-12% Co-6% Cr coatings before and after sealing | |
| CN106283035A (en) | The application on elevator traction sheave of a kind of TiC/ cobalt-base alloys composite coating | |
| CN103920872B (en) | Laser alloying powder and the application in steel cylinder ring mould laser surface alloying thereof | |
| Gao et al. | Microstructure, interfacial characteristics, and wear performances of Cu–Fe–SiC cermet composites | |
| CN110499505B (en) | A kind of high-temperature self-lubricating cobalt-based wear-resistant composite layer, preparation method and application | |
| CN114559031B (en) | High-speed laser cladding alloy powder, its preparation method, coating and application | |
| CN117364075B (en) | A graphene-modified titanium alloy oil drill pipe wear-resistant belt and its preparation method | |
| CN116265608B (en) | High-strength wear-resistant belt for titanium alloy drill rod joint and preparation method thereof | |
| CN113604802B (en) | Manufacturing method of plunger rod of ultrahigh-pressure plunger pump | |
| Biryukov | Optimization of Laser Surfacing Technology and Its Effect on Coating Properties | |
| CN116426920A (en) | Yttrium oxide modified gradient wear-resistant coating for titanium alloy 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 | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| OL01 | Intention to license declared | ||
| OL01 | Intention to license declared |
