CN112575327B - High-hardness and high-wear-resistance composite coating applied to surface of valve body, preparation method and valve body - Google Patents

High-hardness and high-wear-resistance composite coating applied to surface of valve body, preparation method and valve body Download PDF

Info

Publication number
CN112575327B
CN112575327B CN202011420407.1A CN202011420407A CN112575327B CN 112575327 B CN112575327 B CN 112575327B CN 202011420407 A CN202011420407 A CN 202011420407A CN 112575327 B CN112575327 B CN 112575327B
Authority
CN
China
Prior art keywords
valve body
hardness
layer
wear
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
Application number
CN202011420407.1A
Other languages
Chinese (zh)
Other versions
CN112575327A (en
Inventor
郑刚
唐华
付永忠
叶兴海
潘天红
滕成龙
杨龙祥
刘振
朱鑫达
赵荣河
邵玲
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Zhenjiang Silian Mechatronic Technology Co ltd
Original Assignee
Hefei Wanfeng Hydraulic Technology Co ltd
Zhenjiang Silian Mechatronic Technology Co ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Hefei Wanfeng Hydraulic Technology Co ltd, Zhenjiang Silian Mechatronic Technology Co ltd filed Critical Hefei Wanfeng Hydraulic Technology Co ltd
Priority to CN202011420407.1A priority Critical patent/CN112575327B/en
Publication of CN112575327A publication Critical patent/CN112575327A/en
Application granted granted Critical
Publication of CN112575327B publication Critical patent/CN112575327B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • CCHEMISTRY; METALLURGY
    • C23COATING 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
    • C23CCOATING 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
    • C23C28/00Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D
    • C23C28/30Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
    • C23C28/32Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one pure metallic layer
    • C23C28/321Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one pure metallic layer with at least one metal alloy layer
    • C23C28/3215Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one pure metallic layer with at least one metal alloy layer at least one MCrAlX layer
    • CCHEMISTRY; METALLURGY
    • C23COATING 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
    • C23CCOATING 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
    • C23C24/00Coating starting from inorganic powder
    • C23C24/08Coating starting from inorganic powder by application of heat or pressure and heat
    • C23C24/10Coating starting from inorganic powder by application of heat or pressure and heat with intermediate formation of a liquid phase in the layer
    • CCHEMISTRY; METALLURGY
    • C23COATING 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
    • C23CCOATING 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
    • C23C28/00Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D
    • C23C28/30Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
    • C23C28/34Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one inorganic non-metallic material layer, e.g. metal carbide, nitride, boride, silicide layer and their mixtures, enamels, phosphates and sulphates
    • CCHEMISTRY; METALLURGY
    • C23COATING 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
    • C23CCOATING 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
    • C23C4/00Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
    • C23C4/04Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge characterised by the coating material
    • C23C4/06Metallic material
    • C23C4/073Metallic material containing MCrAl or MCrAlY alloys, where M is nickel, cobalt or iron, with or without non-metal elements
    • CCHEMISTRY; METALLURGY
    • C23COATING 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
    • C23CCOATING 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
    • C23C4/00Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
    • C23C4/12Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge characterised by the method of spraying
    • C23C4/134Plasma spraying

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Physics & Mathematics (AREA)
  • Plasma & Fusion (AREA)
  • Inorganic Chemistry (AREA)
  • Coating By Spraying Or Casting (AREA)
  • Other Surface Treatments For Metallic Materials (AREA)

Abstract

The invention provides a high-hardness and high-wear-resistance composite coating applied to the surface of a valve body, a preparation method and the valve body, wherein Si-doped W is introduced into the surface of the valve body 2 N-layer or Si-doped Mo 2 The N layer and the WC and the novel high-entropy alloy AlMoCrFeNi multilayer composite coating combine the advantages of high-temperature ceramics and high-entropy alloy, and the W is respectively enhanced by doping Si and strengthening WC particles 2 N layer or Mo 2 The N layer and the high-entropy alloy AlMoCrFeNi have the hardness and toughness and have high hardness and high wear resistance. The coating prepared by the invention has a compact and uniform structure, high hardness, high strength, high toughness, high wear resistance and good corrosion resistance, and is suitable for the surface of a valve body.

Description

High-hardness and high-wear-resistance composite coating applied to surface of valve body, preparation method and valve body
Technical Field
The invention relates to the technical field of surface engineering, in particular to a high-hardness and high-wear-resistance composite coating applied to the surface of a valve body, a preparation method and the valve body, belonging to the technical field of surface strengthening treatment.
Background
The valve body is used as a main part of the valve, and the pressure resistance, the wear resistance, the corrosion resistance and other properties of the valve body play an important role in the quality of the valve. The existing valve body is made of various materials, wherein high-quality tool steel, stainless steel and aluminum alloy are widely applied due to wear resistance and corrosion resistance, and the valve body made of the stainless steel is a mainstream product of the valve sold in the market at present. The common valve has poor sealing performance, easy leakage, easy perforation of a shell and short service life under the process conditions of strong corrosion, toxicity and harm, and can not meet the special requirement of effectively conveying toxic media for a long time. Therefore, the exploration and development of high-wear-resistance and corrosion-resistance valve body materials and processes are important guarantees for obtaining high-quality or special requirements of valves.
In recent years, high-hardness and high-wear-resistance coating materials are widely applied to coating of substrate materials so as to further enhance the performance of the substrate, for example, two-dimensional materials, ceramics, high-entropy alloys and the like form composite coatings on the surfaces of substrates by the technologies of thermal spraying, ion spraying, laser cladding and the like. Hong et al reported a layered 2D structure of MoSi 2 N 4 The preparation method of the film (Science369, 670-674 (2020)) has better mechanical property and stability than the traditional two-dimensional ceramic material, and provides a brand new idea for designing the ultrahigh-hardness and high-wear-resistance composite coating. In addition, the high-entropy alloy is widely applied to metal coatings and thin films due to high strength, high hardness, high wear resistance and high corrosion resistance, the preparation method and the spraying technology of the high-entropy alloy are greatly developed, and Chinese patent applications CN111593248A, CN111549344A, CN111364040A and CN111593339A provide a high-entropy alloy synthesis method and a multilayer coating preparation process and provide a composite coating for designing and developing a two-dimensional ceramic material and the high-entropy alloyThe theoretical basis and the technical guarantee of the valve body have great potential for improving the material performance of the valve body.
Disclosure of Invention
Based on the prior art, the invention provides the high-hardness and high-wear-resistance composite coating applied to the surface of the valve body, which is low in cost, simple in process and high in yield, the preparation method thereof and the valve body with the composite coating. Introducing Si doped W on the surface of the valve body 2 N-layer or Si-doped Mo 2 The multilayer composite coating of the N layer, WC and high-entropy alloy AlMoCrFeNi is used for improving the hardness and the wear resistance of the surface of the coating.
The present invention achieves the above-described object by the following means.
The high-hardness and high-wear-resistance composite coating applied to the surface of the valve body is characterized by comprising Si-doped W which is adhered to the surface of the valve body and is alternately laminated 2 N-layer or Si-doped Mo 2 The composite layer is a high-entropy alloy AlMoCrFeNi layer dispersed with WC particles, wherein the mass percentage of the WC particles is 5-10%, the particle size of the WC particles is 100-200 meshes, and the balance is the high-entropy alloy AlMoCrFeNi.
Further, the content of each element in the high-entropy alloy AlMoCrFeNi is calculated by the atomic percentage: 18-22% of Al, 18-22% of Cr, 18-22% of Mo, 18-22% of Fe and 18-22% of Ni, and the grain diameter of the alloy is 50-100 meshes.
Further, the method comprises the following steps:
(1) Carrying out polishing, oil removal, acid pickling and sand blasting treatment on a valve body base material;
(2) Cladding W, si powder or mixed powder of Mo and Si on the surface of the valve body base material treated in the step (1) by adopting a laser cladding technology, placing the cladding material in a muffle furnace, preserving heat for 15-30min at 700-850 ℃ under the protection of inert gas, and naturally cooling to room temperature; then transferring into a tube furnace at 1000-1200 ℃ and N 2 And NH 3 Keeping the temperature for 1 to 3 hours under the atmosphere of the mixed gas to obtain Si-doped W 2 N-layer or Si-doped Mo 2 N layers;
(3) Mixing Al, cr, mo, fe and Ni in a nearly equimolar ratio to obtain multi-component mixed powder, adding the multi-component mixed powder into WC particles, and carrying out ball-milling mixing to obtain multi-component mixed powder containing WC;
(4) Spraying the multi-element mixed powder prepared in the step (3) on Si-doped W by adopting an atmospheric plasma spraying technology 2 N-layer or Si-doped Mo 2 Preparing a WC-AlMoCrFeNi composite layer on the surface of the N layer; placing the ion-sprayed mixture in a muffle furnace, preserving the heat for 15-30min at 350-500 ℃ under the protection of inert gas, and naturally cooling to room temperature.
Further, the method also comprises the step (5): repeating the steps (2) to (4) once or more times to obtain the multilayer laminated composite coating.
Further, the specific process of the step (1) is as follows:
polishing: polishing the sample by using 100-2000-mesh abrasive paper step by step until the surface of the sample is bright and flat;
oil removal: placing the valve body substrate in alcohol or acetone for ultrasonic cleaning and oil removal;
acid washing: removing scratches and a hardened layer on the surface of the substrate by using a solution containing 5% hydrofluoric acid, 40% nitric acid and 55% deionized water;
sand blasting: the abrasive material for sand blasting is brown corundum with granularity of 60-100 meshes, the time for sand blasting is 5-10s, the distance for sand blasting is 30-60mm, and the air pressure is 0.5-1MPa.
Furthermore, the valve body is made of 20Cr, 45 steel or GCr15; the ball milling parameters of the multi-element mixed powder in the step (3) are as follows: mixing for 1-2h at the rotating speed of 60-120 rpm; the protective gas is nitrogen or argon.
Further, the Si-doped W prepared in the step (2) 2 N-coating or Si-doped Mo 2 The thickness of the N layer is 50-150 mu m; the thickness of the WC-AlMoCrFeNi composite layer prepared in the step (4) is 40-100 mu m.
Further, the laser cladding conditions in the step (2) are as follows: the laser power is 1.5-2kW, the protective gas is argon, the flow rate is 100-150mL/min, the tungsten source is metal tungsten, the silicon source is simple substance silicon, the powder feeding mode is coaxial powder feeding, the defocusing amount is 45-50mm, the spot size is 4-5mm, the scanning speed is 15-20mm/s, the lap joint rate is 50-75%, and the powder feeding amount is 20g/min; the heat preservation temperature of the tubular furnace is 1000-1200 ℃, and the heat preservation time is 3-5h.
Further, in the step (4), during the atmospheric plasma spraying, the used fuel gas is propane, the combustion-supporting gas is oxygen, the powder feeding gas is nitrogen, the flow rate of the fuel gas is 20-80mL/min, the flow rate of the combustion-supporting gas is 200-400mL/min, and the flow rate of the powder feeding gas is 20-80mL/min.
The valve body is provided with the high-hardness and high-wear-resistance composite coating applied to the surface of the valve body.
The high-hardness and high-wear-resistance composite coating prepared by the invention introduces Si-doped W on the surface of the valve body by utilizing the high strength, high hardness, high wear resistance and high corrosion resistance of the two-dimensional ceramic material and the high-entropy alloy 2 N, WC and a novel high-entropy alloy AlMoCrFeNi multilayer composite coating in the traditional W 2 Si and WC are respectively doped in the N coating and the high-entropy alloy coating, and the hardness and toughness of the two coatings are further improved in a doping mode, so that the wear resistance is improved. Meanwhile, the preparation method of the coating comprises the steps of cladding the mixed powder of simple substance silicon and tungsten on the surface of the matrix in a laser cladding mode, and then cladding the mixed powder of simple substance silicon and tungsten on the surface of the matrix by NH 3 Reacting W in the mixed layer as a nitrogen source and cladding to generate W 2 N, the preparation process makes silicon in W 2 The dispersion in N is more uniform, the conditions of segregation and uneven distribution do not exist, and the doping strengthening effect is improved. In the preparation process of the WC-AlMoCrFeNi composite layer, the mixed micro powder of the WC and the AlMoCrFeNi composite layer is sprayed on the silicon-doped W in a plasma spraying mode 2 On the N layer, the bonding strength between the two coatings is improved, and the distribution of WC in the high-entropy alloy is more uniform. The composite coating combines the advantages of high-temperature ceramics and high-entropy alloy, so that the composite coating has high hardness and high wear resistance, and is suitable for preparing a coating which has a compact and uniform structure and has high hardness, high strength, high toughness, high wear resistance and good corrosion resistance. According to the invention, a multilayer film structure is formed on the surface of the valve body through a simple coating process, the hardness and the friction performance of the valve body are effectively improved by about 10% compared with the traditional valve body, and the valve body has a wide practical application prospect.
In addition, in the preparation process, all reagents are commercial products, the re-preparation is not needed, the process is simple, the cost is low, the production process is simple and easy to control, the product difference rate is high, and the method is suitable for large-scale industrial production. The hardness and the wear resistance of the prepared composite coating are greatly improved.
Drawings
FIG. 1 is Si-doped W prepared in example 1 2 TEM image of N.
FIG. 2 is a metallographic view of the WC-AlMoCrFeNi composite layer prepared in example 1.
FIG. 3 is an SEM image of the wear scar of the substrate after the rubbing test with example 1.
Detailed Description
The present invention will be further described with reference to specific examples, but the scope of the present invention is not limited thereto.
Example 1:
a20 Cr valve body is used as a base material, and a high-hardness and high-wear-resistance composite coating is prepared on the surface of the valve body, and the method comprises the following specific steps:
(1) Using 20Cr as a base material, and gradually polishing the surface of a sample by using 100-mesh, 200-mesh, 500-mesh and 1500-mesh sand paper until the surface of the sample is bright and flat; then, the 20Cr substrate is placed in alcohol or acetone for ultrasonic cleaning and oil removal, a solution containing 5% hydrofluoric acid, 40% nitric acid and 55% deionized water is adopted to remove scratches and a hardened layer on the surface of the substrate, and then surface sand blasting treatment is carried out, wherein the sand blasting abrasive is brown corundum, the granularity is 60 meshes, the sand blasting time is 5s, the sand blasting distance is 30mm, and the air pressure is 0.5MPa; obtaining the 20Cr substrate with smooth surface.
(2) And (2) cladding W, si mixed powder on the surface of the 20Cr substrate treated in the step (1) by adopting a laser cladding technology, wherein the laser power is 1.7kW, the protective gas is argon, the flow rate is 100mL/min, the powder feeding mode is coaxial powder feeding, the diameter of a light spot is 2.5mm, the positive defocusing amount is 5mm, the scanning speed is 15mm/s, the lap joint rate is 50%, and the powder feeding amount is 15g/min. After laser cladding, the mixture is placed in a muffle furnace at 1000 ℃ and N 2 And NH 3 Keeping the temperature for 1h in the mixed gas atmosphere, and naturally cooling to room temperature to obtain Si-doped W 2 And (4) coating N. Prepared Si-doped W 2 The thickness of the N coating was 70 μm. The TEM image of the above sample was measured by TEM as shown in FIG. 1, and it was observedA distinct layered structure.
(3) Mixing Cr, mo, fe, al and Ni with the purity of more than or equal to 99.0 percent and the granularity of less than 100 meshes in an approximately equimolar ratio, wherein the atomic number contents of the Cr, the Mo, the Fe, the Al and the Ni are respectively 18-22 percent, 18-22 percent and 18-22 percent, adding WC particles with the purity of more than or equal to 99.0 percent and the granularity of less than 200 meshes, wherein the adding amount of the WC particles is 5 percent of the total mass of the mixed powder of the Cr, the Mo, the Fe, the Al and the Ni, placing the mixture into a grinding tank, and performing ball-milling and mixing for 1 hour to obtain the multi-element mixed powder containing WC.
(4) Spraying the WC-containing multi-component mixed powder prepared in the step (3) on Si-doped W by adopting an atmospheric plasma spraying technology 2 Preparing a WC-AlMoCrFeNi composite layer with the thickness of 80 mu m on the surface of the N coating. Spraying conditions are as follows: the used fuel gas is propane, the gas flow of the fuel gas is 35mL/min, the combustion-supporting gas is oxygen, the gas flow of the combustion-supporting gas is 150mL/min, the powder feeding gas is nitrogen, the gas flow of the powder feeding gas is 40mL/min, the spraying distance is 80mm, and the length of the spraying pipe is 60mm.
And (3) performing a metallographic experiment on the WC-AlMoCrFeNi composite layer prepared in the step (4), wherein the composite layer is composed of an irregular latticed structure and has good quality and no defects such as holes and cracks, as shown in figure 2.
Example 2:
(1) Taking 45 steel as a base material, and gradually polishing the surface of a sample by adopting 150-mesh, 400-mesh, 1200-mesh and 2000-mesh sand paper until the surface of the sample is bright and flat; and then placing the 45 steel substrate in alcohol or acetone for ultrasonic cleaning and oil removal, removing scratches and a hardened layer on the surface of the substrate by adopting a solution containing 5% hydrofluoric acid, 40% nitric acid and 55% deionized water, and then carrying out surface sand blasting treatment to obtain the 45 steel substrate. The abrasive material for sand blasting is brown corundum, the granularity is 80 meshes, the sand blasting time is 70s, the sand blasting distance is 50mm, and the air pressure is 0.7MPa.
(2) And cladding the W, si mixed powder on the surface of a 45 steel substrate by a laser cladding method. The laser power is 1.5kW, the protective gas is argon, the flow rate is 120mL/min, the powder feeding mode is coaxial powder feeding, the diameter of a light spot is 2.5mm, the positive defocusing amount is 5mmL/min, the scanning speed is 18mm/s, the lap joint rate is 60%, and the powder feeding amount is 15g/min. After cladding, the workpiece is placed in a muffle furnace at 800 ℃ and N 2 And NH 3 Keeping the temperature for 2h in the mixed gas atmosphere, and naturally cooling to room temperature to obtain Si-doped W 2 And (4) coating N. Prepared Si-doped W 2 The thickness of the N coating was 120. Mu.m.
(3) Mixing Cr, mo, fe, al and Ni with the purity of more than or equal to 99.0 percent and the granularity of less than 100 meshes in nearly equal molar ratio, wherein the atomic number content of the Cr, the Mo, the Fe, the Al and the Ni is respectively 18-22 percent, 18-22 percent and 18-22 percent, adding WC particles with the purity of more than or equal to 99.0 percent and the granularity of less than 200 meshes, wherein the adding amount of the WC particles is 8 percent of the total mass of the mixed powder of the Cr, the Mo, the Fe, the Al and the Ni, placing the mixture in a grinding tank for ball milling and mixing for 1h, and placing the mixture in the grinding tank for ball milling and mixing for 1h to obtain the multi-component mixed powder containing WC.
(4) Spraying the WC-containing multi-component mixed powder prepared in the step (3) on Si-doped W by adopting an atmospheric plasma spraying technology 2 Preparing a WC-AlMoCrFeNi composite layer with the thickness of 50 mu m on the surface of the N coating. Spraying conditions are as follows: the used fuel gas is propane, the gas flow of the fuel gas is 20mL/min, the combustion-supporting gas is oxygen, the gas flow of the combustion-supporting gas is 300mL/min, the powder feeding gas is nitrogen, the gas flow of the powder feeding gas is 20mL/min, the spraying distance is 40mm, and the length of the spraying pipe is 120mm.
Example 3:
(1) Using GCr15 as a base material, and gradually polishing by using 100-mesh, 200-mesh, 600-mesh, 1200-mesh and 2000-mesh sand paper until the surface of a sample is bright and flat; and then placing the GCr15 substrate in alcohol or acetone for ultrasonic cleaning and oil removal, removing scratches and a hardened layer on the surface of the substrate by adopting a solution containing 5% hydrofluoric acid, 40% nitric acid and 55% deionized water, and then carrying out surface sand blasting treatment to obtain the GCr15 substrate. The abrasive material for sand blasting is brown corundum, the granularity is 100 meshes, the sand blasting time is 10s, the sand blasting distance is 60mm, and the air pressure is 1MPa.
(2) And (3) cladding W, si powder on the surface of the GCr15 matrix by adopting a laser cladding technology. The laser power is 1.5kW, the protective gas is argon, the flow rate is 150mL/min, the powder feeding mode is coaxial powder feeding, the spot diameter is 2.5mm, the positive defocusing amount is 5mmL/min, the scanning speed is 20mm/s, the lap joint rate is 60%, and the powder feeding amount is 20g/min. After cladding, the mixture is placed in a muffle furnace at 850 ℃ and N 2 And NH 3 Mixed gas ofKeeping the temperature for 3h under the atmosphere, and naturally cooling to room temperature to obtain Si-doped W 2 And (4) coating N. Prepared Si-doped W 2 The thickness of the N coating was 140 μm.
(3) Mixing Cr, mo, fe, al and Ni with the purity of more than or equal to 99.0 percent and the granularity of less than 100 meshes in nearly equal molar ratio, wherein the atomic number content of the Cr, the Mo, the Fe, the Al and the Ni is respectively 18-22 percent, 18-22 percent and 18-22 percent, adding WC particles with the purity of more than or equal to 99.0 percent and the granularity of less than 200 meshes, wherein the adding amount of the WC particles is 5 percent of the total mass of the mixed powder of the Cr, the Mo, the Fe, the Al and the Ni, placing the mixture in a grinding tank, carrying out ball milling and mixing for 1 hour, placing the mixture in the grinding tank, carrying out ball milling and mixing for 2 hours, and obtaining the multi-component mixed powder containing WC.
(4) Spraying the WC-containing multi-component mixed powder prepared in (3) on Si-doped W by adopting an atmospheric plasma spraying technology 2 Preparing a WC-AlMoCrFeNi composite layer with the thickness of 90 mu m on the surface of the N coating. Spraying conditions are as follows: the used fuel gas is propane, the gas flow of the fuel gas is 80mL/min, the combustion-supporting gas is oxygen, the gas flow of the combustion-supporting gas is 400mL/min, the powder feeding gas is nitrogen, the gas flow of the powder feeding gas is 80mL/min, the spraying distance is 120mm, and the length of the spraying pipe is 200mm.
Table 1 shows the hardness of the composite coatings prepared in the three examples and the hardness of the base material, and the hardness of the composite coatings prepared by the invention is improved to a great extent through comparison.
TABLE 1 hardness of each example and comparative example
Figure GDA0003860846740000051
The friction properties of the composite coatings prepared in the above examples were measured using a UMT-2 multipurpose Friction wear tester, from CETR, USA. In the friction experiment process, a ball disc type friction mode is adopted, the upper sample is a 440C stainless steel ball with the diameter of 10mm, and the material hardness is HRC62; the lower samples were made of the base materials having the high-hardness and high-abrasion-resistance composite coatings prepared in examples 1 to 3 of the present invention, respectively
Figure GDA0003860846740000062
A disk. Friction test conditions: the load is 10-30N, the rotating speed is 100rpm, and the experimental time is 1h. The test results are shown in table 2, and experiments prove that the composite coating prepared by the invention has lower friction coefficient, reduces the wear rate under the same conditions and greatly improves the wear resistance of the matrix. In addition, the composite coating prepared in example 1 was subjected to SEM test for wear scar after friction test and compared with the wear scar of the 20Cr substrate, as shown in fig. 3, wherein (a) is the wear scar of the 20Cr substrate after friction test and (b) is the wear scar of the composite coating prepared in example 1 after friction test. It is clear that the composite coating prepared in example 1 has a shallower wear scar and less wear by the friction test, which is consistent with the wear rate data.
TABLE 2 Friction Properties of examples and comparative examples
Figure GDA0003860846740000061
The present invention is not limited to the above-described embodiments, and any obvious improvements, substitutions or modifications can be made by those skilled in the art without departing from the spirit of the present invention.

Claims (9)

1. The high-hardness and high-wear-resistance composite coating applied to the surface of the valve body is characterized by comprising Si-doped W which is adhered to the surface of the valve body and is alternately laminated 2 N-layer or Si-doped Mo 2 The composite layer is a high-entropy alloy AlMoCrFeNi layer dispersed with WC particles, wherein the mass percentage of the WC particles is 5-10%, the particle size of the WC particles is 100-200 meshes, and the balance is the high-entropy alloy AlMoCrFeNi.
2. The high-hardness and high-wear-resistance composite coating applied to the surface of the valve body according to claim 1, wherein the content of each element in the high-entropy alloy AlMoCrFeNi is calculated by atomic percent: 18-22% of Al, 18-22% of Cr, 18-22% of Mo, 18-22% of Fe and 18-22% of Ni, and the grain diameter of the alloy is 50-100 meshes.
3. The method for preparing the high-hardness and high-wear-resistance composite coating applied to the surface of the valve body according to claim 1, characterized by comprising the following steps:
(1) Polishing, degreasing, pickling and sand blasting the valve body base material;
(2) Cladding the mixed powder of W and Si or the mixed powder of Mo and Si on the surface of the valve body base material treated in the step (1) by adopting a laser cladding technology, placing the clad material in a muffle furnace, preserving the heat for 15-30min at 700-850 ℃ under the protection of inert gas, and naturally cooling to room temperature; transferring into tubular furnace at 1000-1200 deg.C and N 2 And NH 3 Keeping the temperature for 1 to 3 hours under the atmosphere of the mixed gas to obtain Si-doped W 2 N-layer or Si-doped Mo 2 N layers;
(3) Mixing Al, cr, mo, fe and Ni in a nearly equimolar ratio to obtain multi-component mixed powder, adding the multi-component mixed powder into WC particles, and carrying out ball-milling mixing to obtain multi-component mixed powder containing WC;
(4) Spraying the multi-element mixed powder prepared in the step (3) on Si-doped W by adopting an atmospheric plasma spraying technology 2 N-layer or Si-doped Mo 2 Preparing a WC-AlMoCrFeNi composite layer on the surface of the N layer; placing the ion-sprayed mixture in a muffle furnace, preserving the heat for 15-30min at 350-500 ℃ under the protection of inert gas, and naturally cooling to room temperature;
(5) Repeating the steps (2) - (4) once or more times to obtain the multilayer laminated composite coating.
4. The method for preparing the high-hardness and high-wear-resistance composite coating according to claim 3, wherein the specific process of the step (1) is as follows:
polishing: polishing the sample by using 100-2000-mesh abrasive paper step by step until the surface of the sample is bright and flat;
oil removal: placing the valve body substrate in alcohol or acetone for ultrasonic cleaning and oil removal;
acid washing: removing scratches and a hardened layer on the surface of the substrate by using a solution containing 5% of hydrofluoric acid, 40% of nitric acid and 55% of deionized water;
sand blasting: the abrasive material for sand blasting is brown corundum, the granularity is 60-100 meshes, the sand blasting time is 5-10s, the sand blasting distance is 30-60mm, and the air pressure is 0.5-1MPa.
5. The method for preparing the high-hardness and high-wear-resistance composite coating according to claim 3, wherein the valve body is made of 20Cr, 45 steel or GCr15; the ball milling parameters of the multi-element mixed powder in the step (3) are as follows: mixing for 1-2h at the rotating speed of 60-120 rpm; the protective gas is nitrogen or argon.
6. The method for preparing a high-hardness and high-wear-resistance composite coating according to claim 3, wherein the Si-doped W prepared in the step (2) 2 N-layer or Si-doped Mo 2 The thickness of the N layer is 50-150 mu m; the thickness of the WC-AlMoCrFeNi composite layer prepared in the step (4) is 40-100 mu m.
7. The method for preparing the high-hardness and high-wear-resistance composite coating according to claim 3, wherein the laser cladding conditions in the step (2) are as follows: the laser power is 1.5-2kW, the protective gas is argon, the flow rate is 100-150mL/min, the powder feeding mode is coaxial powder feeding, the defocusing amount is 45-50mm, the spot size is 4-5mm, the scanning speed is 15-20mm/s, the lap joint rate is 50-75%, and the powder feeding amount is 20g/min; the heat preservation temperature of the tubular furnace is 1000-1200 ℃, and the heat preservation time is 3-5h.
8. The preparation method of the high-hardness and high-wear-resistance composite coating according to claim 3, wherein in the step (4), during the atmospheric plasma spraying, the used fuel gas is propane, the combustion-supporting gas is oxygen, the powder feeding gas is nitrogen, the gas flow rate of the fuel gas is 20-80mL/min, the gas flow rate of the combustion-supporting gas is 200-400mL/min, and the gas flow rate of the powder feeding gas is 20-80mL/min.
9. A valve body having the high-hardness, high-abrasion resistant composite coating applied to the surface of the valve body as claimed in claim 1 or 2.
CN202011420407.1A 2020-12-08 2020-12-08 High-hardness and high-wear-resistance composite coating applied to surface of valve body, preparation method and valve body Active CN112575327B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202011420407.1A CN112575327B (en) 2020-12-08 2020-12-08 High-hardness and high-wear-resistance composite coating applied to surface of valve body, preparation method and valve body

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202011420407.1A CN112575327B (en) 2020-12-08 2020-12-08 High-hardness and high-wear-resistance composite coating applied to surface of valve body, preparation method and valve body

Publications (2)

Publication Number Publication Date
CN112575327A CN112575327A (en) 2021-03-30
CN112575327B true CN112575327B (en) 2022-11-18

Family

ID=75127898

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202011420407.1A Active CN112575327B (en) 2020-12-08 2020-12-08 High-hardness and high-wear-resistance composite coating applied to surface of valve body, preparation method and valve body

Country Status (1)

Country Link
CN (1) CN112575327B (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113215466B (en) * 2021-03-31 2022-03-18 中国核动力研究设计院 AlFeNiCrMo high-entropy alloy, preparation method and application thereof

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106894016A (en) * 2017-02-27 2017-06-27 辽宁工程技术大学 Enhanced high-entropy alloy base composite coating of Argon arc cladding titanium carbide and preparation method thereof
CN109972134A (en) * 2019-03-08 2019-07-05 广东工业大学 A method of FeCoNiCrMn high entropy alloy coating is prepared on potassium steel surface

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6242108B1 (en) * 1998-07-02 2001-06-05 The United States Of America As Represented By The United States Department Of Energy Abrasion resistant coating and method of making the same
CN202768994U (en) * 2012-09-28 2013-03-06 温州大学 Corrosion-resistant protective coating structure of valve
CN105463443B (en) * 2015-12-04 2018-06-12 山东开泰抛丸机械股份有限公司 A kind of marine drilling platform corrosion resistant coating production
CN105862035A (en) * 2016-06-25 2016-08-17 芜湖三刀材料科技有限公司 High-entropy alloy coating and preparation method thereof
US20180022929A1 (en) * 2016-07-20 2018-01-25 Guardian Glass, LLC Coated article supporting high-entropy nitride and/or oxide thin film inclusive coating, and/or method of making the same
US11098403B2 (en) * 2017-02-07 2021-08-24 City University Of Hong Kong High entropy alloy thin film coating and method for preparing the same
CN107142475A (en) * 2017-04-22 2017-09-08 南京工程学院 A kind of laser cladding strengthens new A lFeCrCoNiTi alloy-base composite materials coating and preparation method with TiC
CN108220880B (en) * 2018-01-30 2019-11-15 上海新弧源涂层技术有限公司 A kind of high rigidity high corrosion-resistant high-entropy alloy nitride coatings and preparation method thereof
CN111593248A (en) * 2019-02-21 2020-08-28 中国科学院理化技术研究所 High-entropy alloy and preparation thereof, coating comprising alloy and preparation
CN109930053B (en) * 2019-03-30 2022-02-01 扬州睿德石油机械有限公司 FeCoNiCrMn high-entropy alloy and method for preparing wear-resistant coating by using same
CN110205178A (en) * 2019-06-05 2019-09-06 镇江市高等专科学校 Titanium is modified two tungsten selenide nano-lubricating materials, Its Preparation Method And Use
CN110331398B (en) * 2019-07-22 2022-02-01 中南大学 Composite coating of high-entropy alloy composite large-particle tungsten carbide and preparation method and application thereof
CN111593339B (en) * 2020-04-21 2022-06-24 上海工程技术大学 Multilayer high-entropy alloy laser cladding layer containing nano tantalum carbide and preparation method thereof
CN111364040B (en) * 2020-05-13 2022-04-05 南京工程学院 High-hardness high-entropy alloy coating and preparation method and application thereof
CN111441052B (en) * 2020-05-20 2020-11-20 南京工程学院 In-situ synthesized multi-element ceramic reinforced coating and preparation method and application thereof
CN111549344A (en) * 2020-06-29 2020-08-18 中天上材增材制造有限公司 Nickel-based alloy powder for laser cladding

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106894016A (en) * 2017-02-27 2017-06-27 辽宁工程技术大学 Enhanced high-entropy alloy base composite coating of Argon arc cladding titanium carbide and preparation method thereof
CN109972134A (en) * 2019-03-08 2019-07-05 广东工业大学 A method of FeCoNiCrMn high entropy alloy coating is prepared on potassium steel surface

Also Published As

Publication number Publication date
CN112575327A (en) 2021-03-30

Similar Documents

Publication Publication Date Title
CN111270234B (en) Method for preparing titanium-aluminum enhanced coating on surface of titanium alloy
CN113832461B (en) Nickel-based alloy powder for laser cladding, ceramic particle reinforced composite powder and application
CN110629153B (en) Preparation method of graphene nanosheet/amorphous iron-based composite coating
CN115233137B (en) Low-friction supersonic flame spraying wear-resistant coating material, preparation method and application
CN107236331B (en) High-temperature corrosion resistance coating and preparation method thereof and high-temperature corrosion resistance coating and preparation method thereof
CN112575327B (en) High-hardness and high-wear-resistance composite coating applied to surface of valve body, preparation method and valve body
CN106835112A (en) A kind of preparation method of the stainless steel composite coating of Mg alloy surface cold spraying 420
CN112899604A (en) NiCrBSi-ZrB for high-temperature protection2Metal ceramic powder, composite coating and preparation method thereof
CN111575629B (en) Anti-corrosion composite layer, application and preparation method of anti-corrosion composite lining layer
CN112342485A (en) Anti-cavitation composite coating for hydraulic machinery and preparation method thereof
CN115121789A (en) Thermal shock resistance high wear-resistant coating material and preparation method thereof
JP2006274326A (en) METHOD FOR FORMING Ti FILM
CN114411145A (en) Method for reducing stainless steel surface cladding coating cracks under high-temperature service
CN112626442A (en) High-temperature oxidation-resistant and corrosion-resistant coating and preparation method thereof
CN111926284B (en) Steam turbine high-medium pressure inner cylinder steam oxidation resistant coating and preparation method thereof
CN110791723B (en) Wear-resistant high-temperature hydrophobic Cr3C2-NiCr coating, preparation method thereof and workpiece
CN110819931B (en) Powder-cored welding wire, preparation method and application thereof, porous coating and preparation method thereof
CN111485191B (en) Composite coating powder for plasma spraying, preparation method and application thereof, amorphous composite coating and preparation method thereof
CN112626515A (en) Method for improving performance of Inconel625 nickel-based powder laser cladding layer
CN102071388A (en) Method for preparing anticorrosive coating for magnesium and lithium alloy
CN113774309B (en) Preparation method of composite powder, dynamic friction sealing coating and preparation method
CN111411318B (en) Titanium alloy shaft part and preparation method and application thereof
CN112281106A (en) Preparation method of graphene-doped nanosheet nano-alumina coating
CN111187554A (en) Anticorrosive paint for large-diameter high-temperature-resistant thermal steel pipe and spraying method
CN110872712A (en) Preparation and test method of zinc-aluminum corrosion-resistant coating on inner wall of SA106B pipe

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
TR01 Transfer of patent right

Effective date of registration: 20230824

Address after: 212000 building 26, No. 99, dingmaojing 15th Road, Zhenjiang New District, Jiangsu Province

Patentee after: ZHENJIANG SILIAN MECHATRONIC TECHNOLOGY Co.,Ltd.

Address before: 212000 building 26, No. 99, dingmaojing 15th Road, Zhenjiang New District, Jiangsu Province

Patentee before: ZHENJIANG SILIAN MECHATRONIC TECHNOLOGY Co.,Ltd.

Patentee before: Hefei Wanfeng Hydraulic Technology Co.,Ltd.

TR01 Transfer of patent right