[go: up one dir, main page]
More Web Proxy on the site http://driver.im/

CN108866470A - A kind of preparation method of air plasma spraying alloy-ceramic laminar coating - Google Patents

A kind of preparation method of air plasma spraying alloy-ceramic laminar coating Download PDF

Info

Publication number
CN108866470A
CN108866470A CN201810630621.6A CN201810630621A CN108866470A CN 108866470 A CN108866470 A CN 108866470A CN 201810630621 A CN201810630621 A CN 201810630621A CN 108866470 A CN108866470 A CN 108866470A
Authority
CN
China
Prior art keywords
powder
ceramic
plasma spraying
preparation
air plasma
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
Application number
CN201810630621.6A
Other languages
Chinese (zh)
Inventor
张超
黄博
任永先
肖金坤
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.)
YANGZHOU RIGHT PETROLEUM MACHINERY CO Ltd
Yangzhou University
Original Assignee
YANGZHOU RIGHT PETROLEUM MACHINERY CO Ltd
Yangzhou University
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 YANGZHOU RIGHT PETROLEUM MACHINERY CO Ltd, Yangzhou University filed Critical YANGZHOU RIGHT PETROLEUM MACHINERY CO Ltd
Priority to CN201810630621.6A priority Critical patent/CN108866470A/en
Publication of CN108866470A publication Critical patent/CN108866470A/en
Pending legal-status Critical Current

Links

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
    • 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
    • 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

Landscapes

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

Abstract

The present invention relates to a kind of preparation methods of air plasma spraying alloy-ceramic laminar coating.Ceramal powder is directly sprayed in matrix surface using air plasma spraying mode, prepares high-temperature wearable corrosion-inhibiting coating.Present invention process is simple, and cost is relatively low, efficiently solves the problems, such as the big toughness deficiency of ceramic coating brittleness, the service life is longer for coating.

Description

A kind of preparation method of air plasma spraying alloy-ceramic laminar coating
Technical field
The present invention relates to technical field of surface coating, in particular to a kind of air plasma spraying alloy-ceramic laminar applies The preparation method of layer.
Background technique
With the fast development of modern industrial technology, in the fields such as metallurgy, chemical industry, the energy, military project, high temperature equipment is obtained It is widely applied, especially in the corrosive medium of high temperature, high pressure and complexity, the Anticorrosion solution of these equipment is bad not only Huge economic loss is caused, while can also bring many hidden danger to safety in production, therefore carries out the high-temperature anticorrosion work of equipment It can not only guarantee safe production, moreover it is possible to extend the service life of equipment, save fund.Alloy-ceramics prepared by the present invention Stratiform coating just has good high-temperature corrosion resistance performance, and matrix can be protected from the attrition and attack under hot environment, extended Its service life.
NiCrBSi powder of the present invention is the Ni base self-fluxing powder using Ni, Cr as main component, and Cr improves Ni The high temperature corrosion-resisting performance and high temperature oxidation resistance of matrix, and chromium boride hard phase is formed with boron, improve its hardness and wear-resisting Property, B and Si element can reduce alloy melting point, significantly improve the wettability of matrix surface.Ni base self-fluxing powder has excellent Different wear-resisting property and wettability, and there is good backup capability, it is ideal coated substrate material.Ceramal Composite material has had both the high tenacity of alloy substrate and the high rigidity of ceramic phase reinforcement and has been widely used in wear-resistant coating.The present invention YSZ hard ceramic powder is added in Ni base coating basis material, is not only acted as the effect of hard phase, is mentioned coating hardness significantly Height, still very excellent barrier material, improves the high-temperature wearable antiseptic property of coated substrate.
Atmospheric plasma spraying technology is a kind of important surface strengthening technology, it is to be sent into metal powder or non-metal powder Fusing or semi-molten state are heated in plasma arc flame stream, plasma arc flame stream temperature is up to 12000 ~ 16000 DEG C, flame flow velocity Degree is 200 ~ 1200 m/s, metal powder and ceramic powders can be made to melt sufficiently, and arrive with plasma arc flame stream high-velocity spray The matrix surface of sandblasting, in the cooling rate of superelevation(105-107K/s)Under, metal ceramic wear-resisting required for preparing applies Layer.
Traditional air plasma spraying ceramal composite coating technology is that alloyed powder and ceramic powder are carried out ball milling in advance Mixing, practice have shown that, when alloyed powder differs larger with ceramic powder density or partial size, two kinds of powder are unable to fully be blended in one It rises, starting powder can be also destroyed in mechanical milling process, powder waste is than more serious in spraying.Though another method uses reunion powder Right spraying effect is preferable, but higher cost, is not useable for producing in enormous quantities.The method that the present invention uses two-way powder feeding, solves Ceramic powders are unable to fully deposit to the defect on coated substrate, and design perpendicular to plasma arc flame stream, are parallel to each other Alloyed powder and ceramic powder powder feeding pipe, and alloyed powder powder feeding pipe away from plasma arc nozzle farther out, ceramic powder powder feeding pipe is away from plasma Arc nozzle is closer, solves the problems, such as that dystectic ceramic powder can not sufficiently melt in plasma arc flame stream, makes alloy Ceramic powder even compact is deposited on matrix surface.
CN106756713A provides a kind of coating for improving combustion engine compressor drum barrel wearability peculiar to vessel and its preparation side Method.The invention first pre-processes combustion engine compressor drum barrel alloy substrate and ceramic fibre, according still further to 18% ~ 80%YSZ powder Body, 18% ~ 80%Al2O3The quality of powder and 2% ~ 20% ceramic fibre is mixed than composition ratio, is then carried out ball-milling treatment and is obtained To ceramic composite powder.One layer of adhesive layer is sprayed in matrix surface by atmospheric plasma spraying technology again, then one layer of spraying Ceramic Composite working lining.The invention biggest advantage is solve the big toughness of ceramic coating brittleness not by adding ceramic fibre The problem of foot, realization is fiber reinforced, improves the wearability of coating.
CN104032256A discloses a kind of preparation method of wear resistant corrosion resistant ni base alloy coating, which treats first The workpiece surface of spraying carries out sandblasting roughening treatment, using ultrasonic cleaning and drying, then uses Supersonic Plasma Spraying The technological parameter of system and plasma gun, spraying is:30 ~ 40 KW of spray power, 20 ~ 30 g/min of powder feeding rate, throughput 90 ~ 110 L/min, 90 ~ 110 mm of spray distance.Then the nickel-base alloy that a layer thickness is 40 ~ 60 μm is sprayed in matrix surface Coating, natural cooling obtains ni base alloy coating in air.The Supersonic Plasma Spraying technology preparation that the invention uses The highly uniform densification of ni base alloy coating, bond strength is higher with coating hardness, in high temperature(300℃)Under the conditions of have it is excellent Wear-corrosion resistance.
CN104195494A relates to a kind of preparation method of cermet composite coating, coating used in the method Material is iron, Ni-based chromium carbide compounded material, is pre-processed first to substrate, then prepares metal using plasma cladding method Ceramic composite coating, institute are using technological parameter:150 ~ 200 A of electric current, 45 ~ 60 V of voltage, 100 ~ 120 g/min of powder sending quantity, 300 ~ 500 mm/min of scanning speed, two pass scanning.The cermet composite coating dense structure of this method preparation, surface are flat It is whole, and hardness is high, excellent wear-resisting property, and application performance is good.
Summary of the invention
Present invention aims to overcome that drawbacks described above, a kind of air plasma spraying alloy-ceramic laminar coating is developed Preparation method.
The technical scheme adopted by the invention is that:A kind of preparation side of air plasma spraying alloy-ceramic laminar coating Method has following steps:Ceramal powder is directly sprayed in matrix surface using air plasma spraying mode, prepares high temperature Wear-and corrosion-resistant coating.
Metal powder in the ceramal powder is NiCrBSi powder, and ceramic powder is YSZ powder.
Alloyed powder and ceramic powder are sent into plasma arc simultaneously using two-way automatic powder feeding system.
Ceramic powder powder feeding pipe is closer away from plasma-arc nozzle, alloy powder feeding pipe away from plasma-arc nozzle farther out.
Plasma spray coating process electric current is 500-550 A, and voltage is 55-65 V, and it is 40-60 that plasma, which generates gas Ar flow, L/min, H2Flow is 5-10 L/min, and ceramic powder powder feed rate is 3-10 g/min, and alloyed powder powder feed rate is 30 g/min, It is 300-450 μm that coating layer thickness, which is made,.
The NiCrBSi powder density is 7.5 g/cm3, YSZ powder density is 6.1 g/cm3, 80-100 DEG C of oven temperature, do The dry time is 2h.
The mass percent of ceramic powder YSZ powder is 10 ~ 30% in ceramal powder.
It first treats sprayed surface and carries out ultrasonic cleaning processing and drying with acetone,
Then it is carried out containing following steps:
1)Sandblasting roughening treatment is carried out to matrix surface to be sprayed using Brown Alundum;
2)Quantitative alloyed powder and ceramic powder are weighed respectively is placed in drying for standby in baking oven;
3)Alloyed powder and ceramic powder are sent into plasma arc simultaneously using two-way automatic powder feeding system;
4)Ceramal powder is directly sprayed in matrix surface using air plasma spraying mode, prepares the painting of high-temperature wearable anti-corrosion Layer;
5)Ceramal dusty material includes the NiCrBSi-YSZ ceramal powder of different YSZ contents;
6)The workpiece sprayed is placed in natural cooling in air.
The step 1)Brown Alundum used in middle progress sandblasting roughening treatment is 20 mesh, the Substrate Surface Roughness after roughening Not less than Ra7.0.
Spraying equipment used in air plasma spraying mode includes:
Anode nozzle including generating plasma arc flame stream(1)And cathode(2), and be vertically arranged with the plasma arc flame stream Ceramic powder powder feeding pipe(3)With alloyed powder powder feeding pipe(4), wherein alloyed powder powder feeding pipe(4)And anode nozzle(1)Between distance compared with Far, ceramic powder powder feeding pipe(3)And anode nozzle(1)Between be closer;
In the ceramic powder powder feeding pipe(3)With alloyed powder powder feeding pipe(4)Matrix is set below(8).
Advantages of the present invention and effect are:First, feeding powder used in the present invention is ceramal powder, alloy pottery Ceramic material has both the high tenacity of alloy material and the high rigidity of ceramic material, spray coating obtained have it is very excellent resistance to Abrasion, corrosion-resistant and high temperature resistance.Wherein used alloyed powder is NiCrBSi powder, and this Ni base self-melting alloy is normal Coated substrate material.Used ceramic powder is YSZ powder, and this material has high-melting-point, lower thermal conductivity, high-fracture toughness The excellent thermodynamic property with high thermal expansion coefficient etc. is extraordinary barrier material, while its high-temperature corrosion resistance performance ten It is point excellent, therefore this hard particles are embedded into coated substrate can significantly improve coating high-temp wear-and corrosion-resistant performance, can answer For components such as aero-engine, diesel engine, industry gas turbines, it is with a wide range of applications in the industrial production.
Second, compared to other hot-spraying techniques, plasma spraying technology is easy to operate flexibly, and spray efficiency is higher, answers With more extensively.The technology provides higher plasma arc flame stream temperature(12000~16000℃), higher flame flow velocity degree(200~ 1200 m/s), melt alloyed powder and ceramic powder sufficiently in plasma arc flame stream, deposited to the jet velocity being exceedingly fast Matrix surface, and with the cooling rate of superelevation(105-107K/s)Cooling obtains ceramal coating.
Third, the method that the present invention uses two-way powder feeding, solves ceramic powders and is unable to fully deposit on coated substrate Defect, and design perpendicular to plasma arc flame stream, the alloyed powder being parallel to each other and ceramic powder powder feeding pipe, and alloyed powder is sent Farther out away from plasma arc nozzle, ceramic powder powder feeding pipe is closer away from plasma arc nozzle for tube cell, and ceramic powder particles are in plasma arc flame The flight time is longer in stream, solves the problems, such as that dystectic ceramic powder can not sufficiently melt in plasma arc flame stream, Make molten alloy powder material and ceramic powder material even compact is deposited on matrix surface.
4th, the present invention density different from two kinds of materials of ceramic powder using alloyed powder optimizes spraying process, makes two kinds of powder Different spraying profiles is realized in spraying in end, obtains stratiform alloy-ceramic coating, there are certain holes for this layer structure Gap, these holes can effectively reduce the thermal conductivity of coating, enhance its heat-proof quality.In high-temperature corrosion environment, this stratiform knot Structure can also weaken the infiltration of corrosive medium, improve the corrosion resisting property of coating.
Compared to a kind of patent CN106756713A coating for improving combustion engine compressor drum barrel wearability peculiar to vessel provided and Preparation method, the present invention spray Ni base self-fluxing powder as coated substrate, coating toughness significantly improves, hardness with it is wear-resisting Property it is also very excellent, ceramic fibre toughening ceramic composite granule preparation process used in CN106756713A is complicated, and makes pottery Porcelain powder brittleness is larger, and vulnerable to damage in mechanical milling process, and present invention process is simple, and cost is relatively low, efficiently solves ceramic painting The layer big toughness deficiency problem of brittleness, the service life is longer for coating.
Compared to a kind of preparation method of wear resistant corrosion resistant ni base alloy coating disclosed in patent CN104032256A, this hair It is bright that hard YSZ ceramic powder is coated in coated substrate, coating hardness is effectively increased, and YSZ material thermal conductivity is lower, it is heat-resisting Better performances, make the coating wear-resistant, excellent anti-corrosion performance under the conditions of high-temperature service, and the coating application range is more wide It is general.
Compared to a kind of preparation method of the patent CN104195494A cermet composite coating provided, two-way of the present invention The plasma spraying technology of powder feeding can prepare different ceramal coatings according to different demands, solve alloyed powder and ceramic powder The problem of mixed powder hardly possible, production efficiency is higher, and cost is relatively low, can be mass-produced.
Detailed description of the invention
Fig. 1 --- two-way powder feeding Plasma Spraying Process Using schematic diagram of the present invention.
The corresponding component names of each label are as follows in figure:
1 is anode nozzle in figure, and 2 be cathode, and 3 be ceramic powder powder feeding pipe, and 4 be alloyed powder powder feeding pipe, and 5 be plasma arc flame stream, 6 It is coating 7,8 for melt granules 6,7 is matrix.
NiCrBSi-YSZ composite coating section SEM figure in Fig. 2 --- the embodiment of the present invention 1.
NiCrBSi-YSZ composite coating XRD spectrum in Fig. 3 --- the embodiment of the present invention 1.
Specific embodiment
Technical thought of the invention is:
It for the problem that the metal material corrosion-vulnerable under various service conditions, is prone to wear, the present invention is using two-way powder feeding Method prepares ceramal coating, used two-way powder feeding side in matrix surface using plasma spraying surface strengthening technology Method efficiently solves the problems, such as that alloyed powder and ceramic powder since the mixed powder that density difference is larger and generates is difficult, make the molten of two kinds of powder Matrix surface can be sufficiently deposited on by melting particle.The purpose of the present invention is overcoming deficiency in the prior art, one kind is designed Perpendicular to plasma arc flame stream, it is parallel to each other, metal powder in tandem and ceramic powder powder feeding pipe arrangement mode, optimization spray rail Mark obtains the excellent ceramal coating of high-temperature wearable antiseptic property by plasma spray technology.
The present invention is illustrated below with reference to thermal spraying schematic diagram 1.
Plasma torch Anodic 1 gets plasma-arc between cathode 2, formed after the ejection of anode nozzle 1 etc. from Daughter flame stream 5, ceramic powder powder feeding pipe 3 are respectively sent NiCrBSi powder and YSZ powder with radial automatic powder feeding system with alloyed powder powder feeding pipe 4 Enter flame flow center, wherein two powder feeding pipes are parallel to each other, farther out, ceramic powder is sent distance between alloyed powder powder feeding pipe 4 and anode nozzle 1 It is closer between tube cell 3 and anode nozzle 1, the melt granules 6 of subsequent flame flow center are arrived through plasma arc flame stream accelerating jetting 8 surface of matrix forms the ceramal coating 7 of even compact.
Embodiment 1:
1. being cleaned by ultrasonic with acetone to matrix surface to be sprayed, dry 2h is subsequently placed in 80-100 DEG C of baking oven.
2. carrying out sandblasting roughening treatment to matrix surface to be sprayed using the Brown Alundum that granularity is 20 mesh, make matrix surface There are many unevenness, the Substrate Surface Roughness after roughening is not less than Ra7.0.
3. weighing NiCrBSi powder of the 2000 g particle size ranges at -75 ~+40 μm respectively, weight percentage of each component is: Chromium 15 ~ 20%, boron 3 ~ 4.5%, silicon 3.5 ~ 5.5%, carbon 0.5 ~ 1.1%, iron < 5%, surplus are nickel.2000 g particle size ranges -53 ~+ 15 μm of YSZ powder is placed in 80 ~ 100 DEG C of baking ovens dry 2 h to guarantee powder in spraying process and keeps good flowing Property.
4. being sent into alloyed powder and ceramic powder in plasma arc simultaneously using two-way automatic powder feeding system, alloyed powder powder feeding pipe is controlled It with ceramic powder powder feeding pipe all perpendicular to plasma arc flame stream, is parallel to each other, alloyed powder powder feeding pipe farther out, is made pottery away from plasma arc nozzle Porcelain powder powder feeding pipe is closer away from plasma arc nozzle, and adjusting distance between two powder feeding pipes is 10 mm.
5. directly preparing stratiform coating, tool in matrix surface spraying ceramal powder using air plasma spraying mode Body way is that dried alloy powder and ceramic powders are respectively put into alloyed powder powder feeder 1 and ceramic powder powder feeder 2, powder feeding 1 powder sending quantity of device is 29.8 g/min, and 2 powder sending quantity of powder feeder is 13.5 g/min.Adjusting plasma spray coating process electric current is 517 A, voltage are 58 V, and it is 50 L/min, H that plasma, which generates gas Ar flow,2Flow is 8 L/min, and spray distance is 120 mm, rifle Translational velocity is 300 mm/s, and it is 3 mm that rifle, which translates spacing, and spraying number of repetition is 5, and the type of cooling is that 0.3 Mpa is air-cooled.
6. the workpiece sprayed is placed in natural cooling in air, then the NiCrBSi-YSZ coating being prepared is led to Overscanning Electronic Speculum observes its Cross Section Morphology, as shown in Fig. 2, discovery coating is well combined with matrix, coating is in typical stratiform knot Structure, coating layer thickness are about 300 μm.
7. pair NiCrBSi-YSZ coating being prepared is hardness test, coating hardness HV0.1Vickers hardness can reach 834。
8. the coating prepared by pair carries out reciprocating friction and wear test, wherein 20 N are loaded, 4 Hz of frequency, polishing scratch length 8 Mm, 1 h of duration, total 72 m of sliding distance, the wear rate of the NiCrBSi-YSZ coating of spraying is 9.7 × 10-2 mm3/N·m。
9. the metal-cermic coating prepared by pair carries out its phase composition of XRD analysis, as a result as shown in figure 3, coating is mainly deposited In γ-Ni phase and((ZrO20.94(Y2O30.060.943Phase.
Embodiment 2:
The present embodiment difference from example 1 is that:1 powder sending quantity of metal powder powder feeder is 29.8 g/min, pottery in step 5 2 powder sending quantity of porcelain powder powder feeder is 3.4 g/min.Adjusting plasma spray coating process electric current is 517 A, and voltage is 58 V, plasma Generation gas Ar flow is 50 L/min, H2Flow is 8 L/min, and spray distance is 120 mm, and rifle translational velocity is 300 mm/s, It is 3 mm that rifle, which translates spacing, and spraying number of repetition is 5, and the type of cooling is that 0.3 Mpa is air-cooled.
Hardness test, coating hardness HV are done to the NiCrBSi-YSZ coating being prepared0.1Vickers hardness can reach 742.
Reciprocating friction and wear test is carried out to prepared coating, wherein 20 N are loaded, 4 Hz of frequency, polishing scratch length 8 Mm, 1 h of duration, total 72 m of sliding distance, the wear rate of the NiCrBSi-YSZ coating of spraying is 4.6 × 10-2 mm3/N·m。
Embodiment 3:
The present embodiment difference from example 1 is that:1 powder sending quantity of metal powder powder feeder is 29.8 g/min, pottery in step 5 2 powder sending quantity of porcelain powder powder feeder is 8.2 g/min.Adjusting plasma spray coating process electric current is 517 A, and voltage is 58 V, plasma Generation gas Ar flow is 50 L/min, H2Flow is 8 L/min, and spray distance is 120 mm, and rifle translational velocity is 300 mm/s, It is 3 mm that rifle, which translates spacing, and spraying number of repetition is 5, and the type of cooling is that 0.3 Mpa is air-cooled.
Hardness test, coating hardness HV are done to the NiCrBSi-YSZ coating being prepared0.1Vickers hardness can reach 754.
Reciprocating friction and wear test is carried out to prepared coating, wherein 20 N are loaded, 4 Hz of frequency, polishing scratch length 8 Mm, 1 h of duration, total 72 m of sliding distance, the wear rate of the NiCrBSi-YSZ coating of spraying is 4.6 × 10-2 mm3/N·m。
Embodiment 4:
The present embodiment difference from example 1 is that:1 powder sending quantity of metal powder powder feeder is 29.8 g/min, pottery in step 5 2 powder sending quantity of porcelain powder powder feeder is 3.4 g/min.Adjusting plasma spray coating process electric current is 517 A, and voltage is 58 V, plasma Generation gas Ar flow is 65 L/min, H2Flow is 8 L/min, and spray distance is 100 mm, and rifle translational velocity is 300 mm/s, It is 3 mm that rifle, which translates spacing, and spraying number of repetition is 5, and the type of cooling is that 0.3 Mpa is air-cooled.
Embodiment 5:
The present embodiment difference from example 1 is that:1 powder sending quantity of metal powder powder feeder is 29.8 g/min, pottery in step 5 2 powder sending quantity of porcelain powder powder feeder is 3.4 g/min.Adjusting plasma spray coating process electric current is 600 A, and voltage is 50 V, plasma Generation gas Ar flow is 50 L/min, H2Flow is 8 L/min, and spray distance is 100 mm, and rifle translational velocity is 300 mm/s, It is 3 mm that rifle, which translates spacing, and spraying number of repetition is 5, and the type of cooling is that 0.3 Mpa is air-cooled.
Embodiment 6:
The present embodiment difference from example 1 is that:In step 3 in NiCrBSi alloy powder each component weight percent Than for chromium 11 ~ 15%, boron 2 ~ 3%, silicon 3 ~ 4.5%, carbon 0.3 ~ 0.6%, iron < 5%, surplus is nickel.
Embodiment 7:
The present embodiment difference from example 1 is that:In step 3 in NiCrBSi alloy powder each component weight percent Than for chromium 7 ~ 10%, boron 1.5 ~ 2.5%, silicon 2 ~ 3.5%, carbon≤0.4%, iron < 4%, surplus is nickel.

Claims (10)

1. a kind of preparation method of air plasma spraying alloy-ceramic laminar coating, which is characterized in that have following steps: Ceramal powder is directly sprayed in matrix surface using air plasma spraying mode, prepares high-temperature wearable corrosion-inhibiting coating.
2. a kind of preparation method of air plasma spraying alloy-ceramic laminar coating according to claim 1, feature It is, the metal powder in the ceramal powder is NiCrBSi powder, and ceramic powder is YSZ powder.
3. a kind of preparation method of air plasma spraying alloy-ceramic laminar coating according to claim 1, feature It is, is sent into alloyed powder and ceramic powder in plasma arc simultaneously using two-way automatic powder feeding system.
4. a kind of preparation method of air plasma spraying alloy-ceramic laminar coating according to claim 3, feature Be, ceramic powder powder feeding pipe is closer away from plasma-arc nozzle, alloy powder feeding pipe away from plasma-arc nozzle farther out.
5. a kind of preparation method of air plasma spraying alloy-ceramic laminar coating according to claim 3, feature It is, plasma spray coating process electric current is 500-550 A, and voltage is 55-65 V, and it is 40-60 L/ that plasma, which generates gas Ar flow, Min, H2Flow is 5-10 L/min, and ceramic powder powder feed rate is 3-10 g/min, and alloyed powder powder feed rate is 30 g/min, system Obtaining coating layer thickness is 300-450 μm.
6. a kind of preparation method of air plasma spraying alloy-ceramic laminar coating according to claim 2, feature It is, the NiCrBSi powder density is 7.5 g/cm3, YSZ powder density is 6.1 g/cm3, 80-100 DEG C of oven temperature, dry Time is 2h.
7. a kind of preparation method of air plasma spraying alloy-ceramic laminar coating according to claim 2, feature It is, the mass percent of ceramic powder YSZ powder is 10 ~ 30% in ceramal powder.
8. a kind of preparation method of air plasma spraying alloy-ceramic laminar coating according to claim 1, feature It is, first treats sprayed surface with acetone and carry out ultrasonic cleaning processing and drying,
Then it is carried out containing following steps:
1)Sandblasting roughening treatment is carried out to matrix surface to be sprayed using Brown Alundum;
2)Quantitative alloyed powder and ceramic powder are weighed respectively is placed in drying for standby in baking oven;
3)Alloyed powder and ceramic powder are sent into plasma arc simultaneously using two-way automatic powder feeding system;
4)Ceramal powder is directly sprayed in matrix surface using air plasma spraying mode, prepares the painting of high-temperature wearable anti-corrosion Layer;
5)Ceramal dusty material includes the NiCrBSi-YSZ ceramal powder of different YSZ contents;
6)The workpiece sprayed is placed in natural cooling in air.
9. a kind of preparation method of air plasma spraying alloy-ceramic laminar coating according to claim 8, feature It is, the step 1)Brown Alundum used in middle progress sandblasting roughening treatment is 20 mesh, and the Substrate Surface Roughness after roughening is not Lower than Ra7.0.
10. a kind of preparation method of air plasma spraying alloy-ceramic laminar coating according to claim 1, special Sign is that spraying equipment used in air plasma spraying mode includes:
Anode nozzle including generating plasma arc flame stream(1)And cathode(2), and be vertically arranged with the plasma arc flame stream Ceramic powder powder feeding pipe(3)With alloyed powder powder feeding pipe(4), wherein alloyed powder powder feeding pipe(4)And anode nozzle(1)Between distance compared with Far, ceramic powder powder feeding pipe(3)And anode nozzle(1)Between be closer;
In the ceramic powder powder feeding pipe(3)With alloyed powder powder feeding pipe(4)Matrix is set below(8).
CN201810630621.6A 2018-06-19 2018-06-19 A kind of preparation method of air plasma spraying alloy-ceramic laminar coating Pending CN108866470A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201810630621.6A CN108866470A (en) 2018-06-19 2018-06-19 A kind of preparation method of air plasma spraying alloy-ceramic laminar coating

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201810630621.6A CN108866470A (en) 2018-06-19 2018-06-19 A kind of preparation method of air plasma spraying alloy-ceramic laminar coating

Publications (1)

Publication Number Publication Date
CN108866470A true CN108866470A (en) 2018-11-23

Family

ID=64339638

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201810630621.6A Pending CN108866470A (en) 2018-06-19 2018-06-19 A kind of preparation method of air plasma spraying alloy-ceramic laminar coating

Country Status (1)

Country Link
CN (1) CN108866470A (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109778104A (en) * 2019-03-06 2019-05-21 扬州大学 A kind of cylinder liner internal wall heat insulation and wear resistance composite coating and preparation method
CN110423919A (en) * 2019-08-05 2019-11-08 西安热工研究院有限公司 A kind of last stage vane of steam turbine water erosion protective coating and preparation method thereof
CN112279682A (en) * 2020-04-26 2021-01-29 广东省新材料研究所 Silicon-based composite coating, preparation method and application thereof, and aircraft engine
CN113265608A (en) * 2021-04-22 2021-08-17 西安石油大学 Bionic gradient antifouling composite coating and preparation method thereof
CN114147436A (en) * 2022-01-04 2022-03-08 中国兵器工业第五九研究所 Preparation method of composite component with periodic gradient structure
CN114959546A (en) * 2022-06-09 2022-08-30 昆明理工大学 Preparation method of continuous transition coating with single-way powder feeding
CN115305433A (en) * 2022-07-25 2022-11-08 广东羚光新材料股份有限公司 Nickel net and preparation method and application thereof

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104438339A (en) * 2014-10-16 2015-03-25 绍兴斯普瑞微纳科技有限公司 Roller repair layer and roller repair method
CN104651773A (en) * 2015-03-17 2015-05-27 郴州市泰益表面涂层技术有限公司 Roller repairing layer and method for repairing roller by utilizing roller repairing layer
CN104711506A (en) * 2015-03-23 2015-06-17 江苏科技大学 Spraying method of high-thickness high-performance coating
CN107893207A (en) * 2017-11-20 2018-04-10 河北工业大学 A kind of method for preparing pore self-sealing self-lubricating coat in use in situ
FR3057580A1 (en) * 2016-10-18 2018-04-20 Commissariat A L'energie Atomique Et Aux Energies Alternatives METHOD FOR COATING A SURFACE OF A SOLID SUBSTRATE WITH A LAYER COMPRISING A CERAMIC COMPOUND, AND THE COATED SUBSTRATE THUS OBTAINED

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104438339A (en) * 2014-10-16 2015-03-25 绍兴斯普瑞微纳科技有限公司 Roller repair layer and roller repair method
CN104651773A (en) * 2015-03-17 2015-05-27 郴州市泰益表面涂层技术有限公司 Roller repairing layer and method for repairing roller by utilizing roller repairing layer
CN104711506A (en) * 2015-03-23 2015-06-17 江苏科技大学 Spraying method of high-thickness high-performance coating
FR3057580A1 (en) * 2016-10-18 2018-04-20 Commissariat A L'energie Atomique Et Aux Energies Alternatives METHOD FOR COATING A SURFACE OF A SOLID SUBSTRATE WITH A LAYER COMPRISING A CERAMIC COMPOUND, AND THE COATED SUBSTRATE THUS OBTAINED
CN107893207A (en) * 2017-11-20 2018-04-10 河北工业大学 A kind of method for preparing pore self-sealing self-lubricating coat in use in situ

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
YAN WANG ET.AL: "APS prepared NiCrBSi-YSZ composite coatings for protection against cavitation erosion", 《JOURNAL OF ALLOYS AND COMPOUNDS》 *

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109778104A (en) * 2019-03-06 2019-05-21 扬州大学 A kind of cylinder liner internal wall heat insulation and wear resistance composite coating and preparation method
CN110423919A (en) * 2019-08-05 2019-11-08 西安热工研究院有限公司 A kind of last stage vane of steam turbine water erosion protective coating and preparation method thereof
CN110423919B (en) * 2019-08-05 2021-07-30 西安热工研究院有限公司 Water erosion protective coating for last-stage blade of steam turbine and preparation method thereof
CN112279682A (en) * 2020-04-26 2021-01-29 广东省新材料研究所 Silicon-based composite coating, preparation method and application thereof, and aircraft engine
CN113265608A (en) * 2021-04-22 2021-08-17 西安石油大学 Bionic gradient antifouling composite coating and preparation method thereof
CN114147436A (en) * 2022-01-04 2022-03-08 中国兵器工业第五九研究所 Preparation method of composite component with periodic gradient structure
CN114959546A (en) * 2022-06-09 2022-08-30 昆明理工大学 Preparation method of continuous transition coating with single-way powder feeding
CN115305433A (en) * 2022-07-25 2022-11-08 广东羚光新材料股份有限公司 Nickel net and preparation method and application thereof
CN115305433B (en) * 2022-07-25 2024-01-09 广东羚光新材料股份有限公司 Nickel screen and preparation method and application thereof

Similar Documents

Publication Publication Date Title
CN108866470A (en) A kind of preparation method of air plasma spraying alloy-ceramic laminar coating
Fauchais et al. Thermal sprayed coatings used against corrosion and corrosive wear
CN110144582B (en) Metal-based material for preparing crystallizer or tuyere and preparation method thereof
CN103374693B (en) Nano thermal barrier coating on surface of high-temperature furnace roller and preparation method thereof
CN109321861B (en) Corrosion-resistant and wear-resistant coating with lamellar and columnar composite structure and preparation method thereof
CN113122841B (en) Corrosion-resistant and wear-resistant coating with gradient composite structure and preparation method thereof
CN111235511B (en) Preparation method of multi-element ceramic composite coating
CN106191753B (en) A kind of method that plasma spraying cladding prepares metallurgical binding coating
CN111334742B (en) Method for preparing ceramic composite coating of refractory transition metal compound
CN106893961A (en) A kind of supersonic flame spraying method for strengthening turbine blade surface
Heimann et al. Recently patented work on thermally sprayed coatings for protection against wear and corrosion of engineered structures
Kumar et al. Evolution and adoption of microwave claddings in modern engineering applications
CN109811294A (en) A method of enhancing turbine blade surface with supersonic flame spraying
CN104711506A (en) Spraying method of high-thickness high-performance coating
CN108531844A (en) A kind of preparation method of the resistance to high temperature oxidation and wear-resistant coating of rare earth oxide doping for the protection of H13 steel surfaces
Lakkannavar et al. Thermal spray coatings on high-temperature oxidation and corrosion applications–a comprehensive review
CN109652798A (en) A kind of preparation method of Sintered NdFeB magnet surface composite coating
CN101691647A (en) Hot-spraying coating with high performance
Henao et al. Principles and applications of thermal spray coatings
Matikainen et al. Advanced coatings by novel high-kinetic thermal spray processes
CN107254655B (en) A kind of Ausmelt furnace lance head and its manufacture craft
Pavan et al. Review of ceramic coating on mild steel methods, applications and opportunities
CN110195205A (en) A kind of preparation method of material surface anticorrosion antiwear alloy coat
CN101768712A (en) Preparation process method for high-temperature protective coating of IMC (intermetallic compound) alloy
Tucker Introduction to thermal spray technology

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: 20181123