CN108559957A - A kind of titanium alloy cutting cutter material and preparation method thereof with PVD coatings - Google Patents

A kind of titanium alloy cutting cutter material and preparation method thereof with PVD coatings Download PDF

Info

Publication number
CN108559957A
CN108559957A CN201810372099.6A CN201810372099A CN108559957A CN 108559957 A CN108559957 A CN 108559957A CN 201810372099 A CN201810372099 A CN 201810372099A CN 108559957 A CN108559957 A CN 108559957A
Authority
CN
China
Prior art keywords
coatings
coating
nitrogen
tialzr
targets
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.)
Granted
Application number
CN201810372099.6A
Other languages
Chinese (zh)
Other versions
CN108559957B (en
Inventor
刘杰
邓欣
伍尚华
梅海娟
王瑞
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.)
Guangdong University of Technology
Original Assignee
Guangdong University of Technology
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 Guangdong University of Technology filed Critical Guangdong University of Technology
Priority to CN201810372099.6A priority Critical patent/CN108559957B/en
Publication of CN108559957A publication Critical patent/CN108559957A/en
Application granted granted Critical
Publication of CN108559957B publication Critical patent/CN108559957B/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • C23C14/00Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
    • C23C14/22Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the process of coating
    • C23C14/24Vacuum evaporation
    • C23C14/32Vacuum evaporation by explosion; by evaporation and subsequent ionisation of the vapours, e.g. ion-plating
    • C23C14/325Electric arc evaporation
    • 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
    • C23C14/00Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
    • C23C14/0021Reactive sputtering or evaporation
    • 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
    • C23C14/00Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
    • C23C14/0021Reactive sputtering or evaporation
    • C23C14/0036Reactive sputtering
    • C23C14/0057Reactive sputtering using reactive gases other than O2, H2O, N2, NH3 or CH4
    • 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
    • C23C14/00Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
    • C23C14/02Pretreatment of the material to be coated
    • C23C14/024Deposition of sublayers, e.g. to promote adhesion of the coating
    • 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
    • C23C14/00Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
    • C23C14/06Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the coating material
    • 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
    • C23C14/00Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
    • C23C14/06Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the coating material
    • C23C14/0641Nitrides
    • 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
    • C23C14/00Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
    • C23C14/06Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the coating material
    • C23C14/0664Carbonitrides
    • 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
    • C23C14/00Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
    • C23C14/06Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the coating material
    • C23C14/14Metallic material, boron or silicon
    • C23C14/18Metallic material, boron or silicon on other inorganic substrates
    • 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
    • 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
    • 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
    • C23C28/347Coatings 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 with layers adapted for cutting tools or wear applications

Landscapes

  • Chemical & Material Sciences (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Inorganic Chemistry (AREA)
  • Cutting Tools, Boring Holders, And Turrets (AREA)
  • Physical Vapour Deposition (AREA)

Abstract

The present invention relates to a kind of titanium alloy cutting cutter material and preparation method thereof with PVD coatings, multi-element coating is prepared using the cathodic arc evaporation technique in physical vapour deposition (PVD) PVD, including:Cleaning is polished to sample cutter;Prepare TiN bond coatings;Prepare TiCNO and TiCN multi-element coatings;Protective coating is prepared, can be TiAlZr/TiAlZrCr coatings, TiAlZr/CrN coatings, TiAlZr/ZrN coatings, TiAl/CrN coatings or TiAl/TiAlCr coatings.A variety of alloying elements are added in cutter coat in the present invention, multi-element coating system is formed, improves the hardness of coating, improve the wearability and toughness of coating, reduce the bonding tendency and friction coefficient with titanium alloy.Meanwhile there is cutter resistance to mechanical impact and good thermal stability, good combination property effectively to extend titanium alloy cutting cutting-tool's used life.

Description

A kind of titanium alloy cutting cutter material and preparation method thereof with PVD coatings
Technical field
The present invention relates to metal cutting investigation of materials field, more particularly to a kind of titanium alloy cutting knife with PVD coatings Has material and preparation method thereof.
Background technology
With the development of Machine Manufacturing Technology, foreign-made had started largely to use high cutting speed, high feed speed already With the Novel numerical control machine of high structural rigidity, such as the automobile of mass production and airplane industry field.And these are high performance Lathe proposes new requirement for the material, coating process and cutter structure of cutter.
Currently, hard alloy coating technology is broadly divided into physical gas phase deposition technology (PVD) and chemical vapor deposition (CVD), CVD or PVD process by single-layer or multi-layer described in abrasion resistant protective coating is applied to made of hard material In main body.PVD process includes magnetron sputtering, arc vapor deposition (electric arc PVD), ion plating, electron-beam vapor deposition and laser Ablation.However, the product hardness using PVD preparation processes is low compared with the product by CVD preparation processes, coating film-substrate cohesion also compared with It is low.In addition, the performance of the coating of cutting element is related to the design of its protective coating, currently, the coating material of high speed cutting tool In material, most widely used coating is TiN.According to incompletely statistics, utilization rate of the TiN coatings on high-speed steel tool be 50%~ 70%, and the utilization rate on complex cutting tool is then more than 90%.However, TiN coating oxidation resistent susceptibilities are poor, when temperature in use is super When crossing 500 DEG C, apparent oxidation is burnt by coating surface;TiN coating hardness is relatively low simultaneously, can not adapt to cutting high speed pair The high request of cutter coat.TiC coated cutting tools have preferable chemical stability and anti-oxidant abrasiveness.The knot of coating and matrix It is high to close intensity, anti-stick, durability is higher, when cutting is small to the abrasion of cutter.However, will produce between TiC coatings and matrix de- Carbon-coating, that is, brittlement phase, this decarburized layer can be thickened as coating layer thickness increases, and the reduction of blade bending strength, brittleness is caused to increase, Crushing knife is easy when cutting.Al2O3Coating has good thermal stability and chemical property, high mechanical strength.However, due to Al2O3 Too big, single Al is differed with the physics of hard alloy substrate, chemical property2O3Coating can not expire group high-performance, high cutting speed Requirement of the cutter for coating.
TiCN coatings have both the advantages of TiC coatings are with TiN coatings, the wearability of adhesive strength and TiC with TiN, firmly Degree is than TiN high, and friction coefficient is small, there is certain inhibiting effect for cohesiveness.With the raising of cutting rate, cutting Phenomena such as tool surface may locally will produce a large amount of heat in journey, and coated cutting tool oxidation, hardness decline, instantaneous wear out failure is tight Weight.And when continuous high speed cutting, cutter is exposed under hot conditions for a long time, tissue and microstructure change so that property It can reduce.
In addition, in Tool in Cutting field, it is difficult the metal material cut that titanium alloy, which is a kind of,.This is because titanium alloy is chemical Activity is higher, cutting temperature is high, unit area cutting force causes to generate between titanium alloy and cutter greatly and stings weldering, bond, spread and Oxidative wear is serious.Therefore, how to design and prepare a kind of good combination property and can efficiently realize the painting of titanium alloy cutting Layer cutter more gradually becomes cutting tool field project in the urgent need to address.
Patent ZL200510071119.2 discloses a kind of cutting tool coating and its manufacturing method, and which disclose one The production method of kind TiAiCN nonmetalloid linear gradient's coatings is to carry out coating treatment, the coating using PVD methods Processing procedure is divided into continuous four periods, be within second period, while be passed through into furnace chamber argon gas, nitrogen, Acetylene gas, wherein argon Ar flow remain unchanged, the flow uniform descent of nitrogen or rising, and the flow of acetylene gas is then at the uniform velocity It rises or falls;To form the TiAlCN gradient layers of a nonmetalloid linear change.Production method in the patent is multiple It is miscellaneous, it needs that the flow of argon gas, nitrogen, acetylene gas is kept monitoring at any time in reaction process, and be accordingly adjusted, and due to Rate changes and what gas reaction consumed does not know, and is easy to cause furnace gas partial pressure and ratio is uneven, cause air pressure insufficient, And then cause the cutter material performance of production bad.
Patent 201180020600.0 discloses a kind of PVD coatings for intermetallic composite coating, and the coating passes through physics gas Mutually deposition (PVD) and deposit, including at least two layers, described two layers have different grain size, but with of the same nature Ingredient.The granularity of two coatings in the patent has larger difference, has apparent boundary in microscopic structure, is tied between two coatings Conjunction property is poor, and the hardness and film-substrate cohesion of coating are low, and the hardness of cutter entirety is low, and stability is poor.
Patent 201380049876.9 discloses a kind of tool with TiAlCrSiNPVD coatings;Specifically closed by hard Main body made of gold, cermet, ceramics, steel or high-speed steel and it is applied to the multi-layer wear-resistant in the main body using PVD process Protective coating, protective coating include at least one layer (A):TiaAl(1-a)N, wherein 0.33 < a <, 1 thickness is 20nm to 3 μ m;With at least one layer (B), it includes the Ti that a series of at least four is alternately stacked arrangementbSi(1-b)N and AlcCr(1-c)N sublayers And layer thickness is 0.5nm to 15nm, wherein 0.70 < b < 0.98 and 0.3 < c < 0.75, also include layer (C):TidSi(1-d) N, wherein 0.70 < d < 0.98 and layer thickness are 50nm to 1 μm.Have strictly really for the composition of coating in the patent It is fixed, and the thickness of coating and component are easy affected by various factors in the production process, make such as temperature, bias, the time, introduced The arrangement of target is arranged in partial pressure of gas etc., this just increases the manufacture difficulty and cost of manufacture of coating, is unfavorable for industrially pushing away Wide application.
Invention content
The shortcomings that it is a primary object of the present invention to overcome the prior art and a kind of insufficient, titanium with PVD coatings of proposition Alloy cutter material and preparation method thereof.A variety of alloying elements are added in cutter coat in the present invention, are formed polynary Coating system improves the hardness of coating, improves the abrasion resistance and toughness of coating, and with the impact of good resistance to mechanical and Thermal stability, good combination property effectively extend titanium alloy cutting cutting-tool's used life.
The present invention specifically provides a kind of preparation method of the titanium alloy cutting cutter material with PVD coatings, using physics Cathodic arc evaporation technique in physical vapour deposition (PVD) PVD prepares multi-element coating, and above-mentioned technical process includes the following steps:
Cleaning is polished to sample cutter:It is polished step by step using silicon carbide paper successively, polishing treatment, sandblast makes Ultrasonic cleaning is carried out to sample cutter respectively with the third bronze medal and ethyl alcohol;
Prepare bonding bottom:Ti targets are installed, after the cutter after cleaning is placed on work rest, vacuum chamber is sent into, makes matrix Vertical range between arc source is 200~300mm, is evacuated to less than 10-3Pa, and carrying out heating to workpiece simultaneously makes it reach To preset temperature;It is passed through nitrogen, nitrogen flow is 600~650sccm, applies substrate bias -80V~-220V, in specimen surface Depositing TiN bond coating;
Prepare main coating:The main coating is TiCNO and TiCN multi-element coatings:The Ti targets of use, Ti target arc currents are 60~65A, depositing temperature are 260~270 DEG C, and substrate bias is -80V~-220V, keeps and be passed through nitrogen, C2H2And CO mixing It is reacted in gas to reative cell, the flow of nitrogen is 400~500sccm, C2H2Flow be 150~300sccm, the flow of CO For 80~200sccm, generates and prepare TiCNO and TiCN mixed coatings;
Prepare protective coating:The protective coating is TiAlZr/TiAlZrCr coatings, TiAlZr/CrN coatings, TiAlZr/ ZrN coatings, TiAl/CrN coatings or TiAl/TiAlCr coatings are taken corresponding with coating when preparing above-mentioned multi-element coating Target and target arc current are passed through nitrogen or argon gas, and depositing temperature is 260~270 DEG C, and substrate bias is -80V~-220V.
Further, further include Ion Cleaning step, it is -350V specially to apply substrate bias to sample cutter, is passed through Arc initiation device, the striking under condition of high vacuum degree are opened, the ion that Ti targets are emitted reaches specimen surface, and ion is carried out to specimen surface Sputter clean, scavenging period are 5~10 minutes.
Further, the preparation method of the TiAlZr/TiAlZrCr coatings is:Using TiAlZr targets, arc current is 50~60A, depositing temperature are 260~270 DEG C, and substrate bias is -80V~-220V, and is passed through argon gas, and the flow of argon gas is 500 The thickness of~650sccm, depositing Ti AlZr coatings, TiAlZr coatings are 300~500 μm;TiAlZr targets and Cr targets are then used, TiAl target arc currents are 50~60A, and Cr target arc currents are 40A, and depositing temperature is 260~270 DEG C, and substrate bias is -80V ~-220V, and be passed through argon gas and nitrogen, the flow of argon gas fall to 300~400sccm, and the flow of nitrogen is 200~ 400sccm, depositing Ti AlZrCr coatings, TiAlZrCr coating layer thicknesses are 200~400 μm.
Further, the preparation method of the TiAlZr/CrN coatings is:Using TiAlZr targets, using TiAlZr targets, electricity Arc current is 50~60A, and depositing temperature is 260~270 DEG C, and substrate bias is -80V~-220V, and is passed through argon gas, argon gas Flow is 500~650sccm, and the thickness of depositing Ti AlZr coatings, TiAlZr coatings is 200~500 μm;Then Zr targets are used, Zr target arc currents are 60A, and depositing temperature is 260~270 DEG C, and substrate bias is -80V~-220V, and is passed through argon gas and nitrogen The flow of gas, argon gas falls to 300~400sccm, and the flow of nitrogen is 200~400sccm, deposits ZrN coatings, ZrN coatings Thickness is 200~400 μm.
Further, the preparation method of the TiAlZr/ZrN coatings is:Using TiAlZr targets, using TiAlZr targets, electricity Arc current is 50~60A, and depositing temperature is 260~270 DEG C, and substrate bias is -80V~-220V, and is passed through argon gas, argon gas Flow is 500~650sccm, and the thickness of depositing Ti AlZr coatings, TiAlZr coatings is 200~500 μm;Then Zr paintings are prepared Layer, using Zr targets, Zr target arc currents are 60A, and depositing temperature is 260~270 DEG C, and substrate bias is -80V~-220V, and is led to Enter argon gas and nitrogen, the flow of argon gas falls to 300~400sccm, and the flow of nitrogen is 200~400sccm, and deposition ZrN is applied Layer, ZrN coating layer thicknesses are 200~400 μm.
Further, the preparation method of the TiAl/CrN coatings is:First use TiAl targets, arc current be 60~ 65A, depositing temperature are 260~270 DEG C, and substrate bias is -80V~-220V, and is passed through nitrogen, the flow of nitrogen is 500~ The thickness of 700sccm, depositing Ti Al coatings, TiAl coatings are 200~500 μm;Then Cr coatings are prepared, using Cr targets, Cr targets Arc current is 60A, and depositing temperature is 260~270 DEG C, and substrate bias is -80V~-220V, and is passed through nitrogen, the stream of nitrogen Amount is 500~700sccm, deposits CrN coatings, and CrN coating layer thicknesses are 200~400 μm.
Further, the preparation method of the TiAl/TiAlCr coatings is:Using TiAl targets, arc current is 60~ 65A, depositing temperature are 260~270 DEG C, and substrate bias is -80V~-220V, and is passed through nitrogen, the flow of nitrogen is 500~ The thickness of 700sccm, depositing Ti Al coatings, TiAl coatings are 200~500 μm;Then it prepares TiAlCr and uses TiAl targets and Cr Target, TiAl target arc currents be 60~65A, Cr target arc currents be 40A, depositing temperature be 260~270 DEG C, substrate bias be- 80V~-220V, and it is passed through nitrogen, the flow of nitrogen is 500~700sccm, depositing Ti AlCr coatings, TiAlCr coating layer thicknesses It is 200~400 μm.
The present invention also provides a kind of titanium alloy cutting cutter materials using with PVD coatings obtained by above-mentioned preparation method Material, the PVD coatings of stating are multi-element coating, and the multi-element coating includes main coating and protective coating, and the main coating is TiCN With TiCNO multi-element coatings, in the multi-element coating, the oxygen atom of incorporation is instead of the carbon atom or nitrogen original in the TiCN of part Son, multi-element coating are face-centred cubic structure, and thickness is 500~800 μm;The protective coating is TiAlZr/TiAlZrCr coatings, TiAlZr/CrN coatings, TiAlZr/ZrN coatings, TiAl/CrN coatings or TiAl/TiAlCr coatings, thickness are 400~800 μm.
Further, further include TiN bond coatings between the main coating and sample tool surface, thickness is 80~ 120 μm of TiN bond coatings play a transition role between TiCNO and TiCN coatings and matrix, improve interface binding power and film/ Binding performance between matrix.
Further, TiCN the and TiCNO multi-element coatings are TiC0.78N0.52And TiC0.63N0.471O0.21Multi-element coating.
Compared with prior art, the present invention having the following advantages that and advantageous effect:
Main coating in the present invention is TiCN and TiCNO multi-element coatings, which is provided simultaneously with TiCN and Al2O3It applies Layer the advantages of, the coated grains shape uniformly, crystallite dimension refinement, crystal grain marshalling and it is close, with refined crystalline strengthening work With;Along with the TICN lattices that enter of oxygen atom generate distortion of lattice, play the role of solution strengthening.Generally so that apply The dense structure of layer, hardness improve.
PVD coatings are provided with TiN bond coatings in the present invention, and TiN bond coatings play matrix and the transition of main coating is made With the interface binding power between raising main coating and matrix improves the binding performance between film/matrix.PVD coatings are set in the present invention It is set to multi-element coating cutter, the growth of the column crystal in coating interface has been interrupted due to multi-element coating, so that coating interface It is strengthened, it is intercrystalline to be tightly combined, to improve the hardness of coating.Further, since the microhardness and film/base of coating The promotion of binding force largely also improves the abrasion resistance energy of coating.
Contain Zr elements in multi-element coating, the bonding abrasion degree between cutter and titanium alloy can be reduced, bonding abrasion is The main failure forms of machining titanium alloy cutter, so, the addition of Zr greatly improves the wearability of cutter.In multi-element coating Coating containing Cr can be improved appearance surface hardness, film/base junction resultant force and inoxidizability, reduce friction coefficient, extends cutter and use Service life.
Description of the drawings
Fig. 1 is the room temperature friction coefficient curve figure of the titanium alloy cutting cutter material with PVD coatings;
Fig. 2 be before processing and treated cutter sample in 500~900 DEG C of oxidation weight gain curve figures.
Specific implementation mode
The present invention is more specifically described in detail with reference to specific embodiment and Figure of description.
Tool matrix in the present embodiment is W18Cr4V tool steel.The equipment that the present embodiment uses is Swiss-PVD coating Company model is the coating apparatus depositing coating of SP1500.
Embodiment 1:
For the preparation method of the titanium alloy cutting cutter material with PVD coatings in the present embodiment, using physical Cathodic arc evaporation technique in vapor deposition PVD prepares multi-element coating, specifically includes following steps:
First, sample is cleaned, removes greasy dirt, rusty stain, dust of workpiece etc., it is ensured that workpiece obtains good coat knot With joint efforts.It is first polished step by step with silicon carbide paper, then the polishing treatment to specimen surface.Carry out sandblast, can be used corundum, SiO2Equal sand grains sandblast, and obtain surface clean, that essence is rough.Then sample cutter is surpassed respectively using the third bronze medal and ethyl alcohol Sound wave cleans.It carries out Ion Cleaning and prepares bond coating:Installation Ti targets are sent after the cutter after cleaning is placed on work rest Enter to vacuum chamber, it is 200~300mm to make the vertical range between matrix and arc source, is evacuated to less than 10-3Pa, and it is right simultaneously Workpiece carries out heating and reaches preset temperature.It is -350V to apply substrate bias to sample cutter, is passed through unlatching arc initiation device, The striking under condition of high vacuum degree, the ion that Ti targets are emitted reach specimen surface, and ion sputtering cleaning, cleaning are carried out to specimen surface Time is 5~10 minutes.Then, it is passed through nitrogen, nitrogen flow is 600~650sccm, applies substrate bias -80V~-220V, In specimen surface depositing TiN bond coating, thickness is 80~120 μm.
Prepare main coating, that is, TiCNO and TiCN coatings:It is prepared using the cathodic arc evaporation in physical vapour deposition (PVD) PVD TiCNO and TiCN coatings.The Ti targets of use, Ti target arc currents are 60~65A, and depositing temperature is 260~270 DEG C, and matrix is inclined Pressure is -80V~-220V, keeps and be passed through nitrogen, C2H2And reacted in CO mixed gas to reative cell, the flow of nitrogen is 400 ~500sccm, C2H2Flow be 150~300sccm, the flow of CO is 80~200sccm, generates that prepare TiCNO and TiCN mixed Coating is closed, the thickness of TiCNO and TiCN coatings is 500~800 μm.
In above-mentioned steps, the volume ratio of nitrogen and other gases is 2: 1~3: 1, can the accounting appropriate that improve nitrogen. In the present embodiment, when nitrogen accounts for it is relatively high when, in deposition, arc macular area nearby easily generates nitride deposition on target surface, and nitrogenizes The fusing point of object is high, can reduce hole size of burning, the generation of drop, limits for cathode surface when reducing cathodic vacuum arc discharge Ablation.
Prepare protective coating;Protective coating is TiAlZr/TiAlZrCr coatings, uses TiAlZr targets, arc current first For 50~60A, depositing temperature is 260~270 DEG C, and substrate bias is -80V~-220V, and is passed through argon gas, and the flow of argon gas is The thickness of 500~650sccm, depositing Ti AlZr coatings, TiAlZr coatings are 200~500 μm.Then TiAlZrCr uses are prepared TiAlZr targets and Cr targets, TiAl target arc currents are 50~60A, and Cr target arc currents are 40A, and depositing temperature is 260~270 DEG C, substrate bias is -80V~-220V, and is passed through argon gas and nitrogen, and the flow of argon gas falls to 300~400sccm, nitrogen Flow is 200~400sccm, and depositing Ti AlZrCr coatings, TiAlZrCr coating layer thicknesses are 200~400 μm.
Embodiment 2:
The sample of the preparation method of the titanium alloy cutting cutter material with PVD coatings is cleaned in the present embodiment, is viscous It ties bottom preparation and main coating preparation process is same as Example 1;Protective coating is TiAlZr/CrN coatings in the present embodiment. The preparation method of protective coating is:TiAlZr targets are used first, and it is 50~60A, deposition to use TiAlZr targets, arc current first Temperature is 260~270 DEG C, and substrate bias is -80V~-220V, and is passed through argon gas, and the flow of argon gas is 500~650sccm, is sunk The thickness of product TiAlZr coatings, TiAlZr coatings is 200~500 μm.Then Cr coatings are prepared, using Cr targets, Cr targets electric arc electricity Stream is 40A, and depositing temperature is 260~270 DEG C, and substrate bias is -80V~-220V, and is passed through argon gas and nitrogen, the stream of argon gas Amount falls to 300~400sccm, and the flow of nitrogen is 200~400sccm, deposits CrN coatings, and CrN coating layer thicknesses are 200~ 400μm。
Embodiment 3:
The sample of the preparation method of the titanium alloy cutting cutter material with PVD coatings is cleaned in the present embodiment, is viscous It ties bottom preparation and main coating preparation process is same as Example 1;Protective coating is TiAlZr/ZrN coatings in the present embodiment. The preparation method of protective coating is:Protective coating can be TiAlZr/ZrN coatings.TiAlZr targets are used first, are used first TiAlZr targets, arc current are 50~60A, and depositing temperature is 260~270 DEG C, and substrate bias is -80V~-220V, and is passed through The flow of argon gas, argon gas is 500~650sccm, and the thickness of depositing Ti AlZr coatings, TiAlZr coatings is 200~500 μm.So After prepare Zr coatings, using Zr targets, Zr target arc currents are 60A, and depositing temperature is 260~270 DEG C, and substrate bias is -80V ~-220V, and be passed through argon gas and nitrogen, the flow of argon gas fall to 300~400sccm, and the flow of nitrogen is 200~ 400sccm, deposits ZrN coatings, and ZrN coating layer thicknesses are 200~400 μm.
Embodiment 4:
The sample of the preparation method of the titanium alloy cutting cutter material with PVD coatings is cleaned in the present embodiment, is viscous It ties bottom preparation and main coating preparation process is same as Example 1;Protective coating is TiAl/CrN coatings in the present embodiment.It protects Shield coating preparation method be:Protective coating is TiAl/CrN coatings.It is 60~65A to use TiAl targets, arc current first, is sunk Accumulated temperature degree is 260~270 DEG C, and substrate bias is -80V~-220V, and is passed through nitrogen, and the flow of nitrogen is 500~700sccm, The thickness of depositing Ti Al coatings, TiAl coatings is 200~500 μm.Then Cr coatings are prepared.Using Cr targets, Cr target arc currents For 60A, depositing temperature is 260~270 DEG C, and substrate bias is -80V~-220V, and is passed through nitrogen, the flow of nitrogen is 500~ 700sccm, deposits CrN coatings, and CrN coating layer thicknesses are 200~400 μm.
Embodiment 5:
The sample of the preparation method of the titanium alloy cutting cutter material with PVD coatings is cleaned in the present embodiment, is viscous It ties bottom preparation and main coating preparation process is same as Example 1;Protective coating is that TiAl/TiAlCr is applied in the present embodiment Layer.The preparation method of protective coating is:Protective coating can be TiAl/TiAlCr multi-element coatings, use TiAl targets, electric arc electricity first Stream is 60~65A, and depositing temperature is 260~270 DEG C, and substrate bias is -80V~-220V, and is passed through nitrogen, the flow of nitrogen Thickness for 500~700sccm, depositing Ti Al coatings, TiAl coatings is 200~500 μm.Then it prepares TiAlCr and uses TiAl Target and Cr targets, TiAl target arc currents are 60~65A, and Cr target arc currents are 40A, and depositing temperature is 260~270 DEG C, matrix Bias is -80V~-220V, and is passed through nitrogen, and the flow of nitrogen is 500~700sccm, depositing Ti AlCr coatings, TiAlCr paintings Layer thickness is 200~400 μm.
Arc current is ranging from tested and is measured in above-described embodiment 1 to the technique in embodiment 5, needed for conventional coating Arc current value, and the lower value in desirable arc current value range takes smaller current value decrease electric arc appropriate Electric discharge, reduce arc spot number, while reducing micro- molten bath area, reduce number of drops, improve the quality of coating deposition.Even if electric arc The reduction of current value can reduce the rate of evaporation and deposition, and then the deposition efficiency influenced to a certain degree, however, being adopted in the present invention With the technique of multilayer multi-element coating, it can equally reach high arc current value and be formed by compactness possessed by coating surface, High rigidity and wear-resisting characteristic.
Target stretches progress using the technique for mixing hot pressing, hot isostatic pressing, cold pressing and sintering, cast, hot rolling or cold rolling Forming processes, after the heat treatment process such as matter, sintering, carry out mechanical processing combined with backboard it is obtained.
For single TiCN coatings, dissolves each other the unlimited solid solution to be formed for TiC and TiN, there is NaCl type face-centered cubics Amorphous carbon is easily precipitated in structure, so that structural transformation progress faster, thermal stability is poor, and defect concentration reduces in coating, Stress release.In main coating, such as TiCN and TiCNO multi-element coatings generated in embodiment 1 to embodiment 5, the oxygen of incorporation Atom is similarly NaCl type face-centred cubic structures, is solid-solution in face-centered cubic instead of the C atoms or N atoms in the TiCN of part, TiO In lattice, TiCNO solid solution is formed.The texture coefficient of TiCN and TiCNO multi-element coatings increases, can in conjunction with XRD spectrum Know, the diffracted intensity of coating is also improved, this is because the interaction of oxygen atom and carbon atom promotes nitrogen-atoms Deposition.For coating morphology, the crystal of TiCN single coatings is coarse, and size is uneven, and there are rib ridges for inside.And TiCN and The grain shape of TiCNO multi-element coatings refines, and grain particles reduce, and grain size is not much different, and crystal grain is neatly tightly combined, and is made Coating hardness is obtained to improve.TiCN and TiCNO multi-element coatings hardness compared with single TiCN coatings is improved, oxygen atom Solution strengthening effect and refined crystalline strengthening effect are produced into TiCN lattices are made so that coating structure is more fine and compact.
Prepared TiCN and TiCNO multi-element coatings are TiC in the present embodiment0.78N0.52And TiC0.63N0.47lO0.21It is polynary Coating.
Contain Zr elements in embodiment 1 and embodiment 2 in multi-element coating, embodiment 3 generates ZrN coatings, embodiment 1-3 institutes The coating of generation can reduce the adhesive wear degree with Ti alloys, and wear-resisting property is greatly improved, can be widely applied to High speed cutting tool effectively reduces the abrasion of cutter, improves the cutting quality of workpiece.It is applied generated in embodiment 4 and embodiment 5 In layer, outermost tunic is the coating containing Cr, since outermost layer coating contains Cr elements so that sample appearance surface hardness, film/base junction Resultant force and inoxidizability are significantly improved, and multicomponent membrane cutter is applicable to the High-speed machining of 400m/min or more, And cutting ability and thermal stability get a promotion, and end wear amount reduces, and service life extends.
The coating hardness of multi-element coating cutter prepared by embodiment 1 to embodiment 5 is higher than the hardness of untreated sample, This is because the multilayer multi-element coating of deposition has interrupted the growth of the column crystal in coating interface, so that coating interface obtains Strengthen.With the increase of coating layer thickness known to following table, and the microhardness for the sample for being coated with multi-element coating is made to significantly increase, This is because with the increase of coating layer thickness, intercrystalline combination is even closer, causes coating finer and close, is applied to improve The hardness of layer.
Coating layer thickness Hardness (HV before processing0.01) Hardness (HV after processing0.01)
1000μm 2650±50 3500±50
1200μm 2650±50 3750±50
1400μm 2650±50 3850±50
Treated multi-element coating cutter both has a higher rigid nature compared with sample before processing, and the film improved/ Binding force between base.Before depositing Ti CNO and TiCN coating, TiN bond coatings are prepared, improve TiCNO and TiCN coatings and matrix Between interface binding power, improve film/matrix between binding performance.Under normal conditions, due to being deposited between multi-element coating and matrix In certain lattice equations, this so that the binding force between coating and matrix is declined.However, due to TiN bond coatings Play matrix and TiCNO and TiCN coating transitional functions, meanwhile, TiAl coatings play TiCNO and TiCN coatings and Cr coatings it Between transitional function.In this way, improving the compatibility between gradient coating composition consecutive variations and each coating, subtract to a certain extent The thermal stress that small multi-element coating is generated due to coefficient of thermal expansion difference so that good combination is presented in interface between each coating State improves the film-substrate cohesion of multi-element coating.
Coating layer thickness Binding force (N) before processing Binding force (N) after processing
1000μm 180±50 > 220
1200μm 180±50 > 220
1400μm 180±50 > 220
Between the 1 average room temperature friction coefficient that can be seen that prepared coating is 0.3~0.4 with reference to the accompanying drawings, and with Deposition thickness difference, friction system is reduced and fluctuates reduction.This is because the microhardness and film of coating/base junction are closed Power greatly enhances the abrasion resistance energy of coating.In addition, for the surface topography of coating abrasion, wear area reduces, Friction groove trace, crackle and the degree mitigation for peeling off hole.
As shown in Fig. 2, for that rear sample will be placed at 500~900 DEG C before treatment, the curve graph of oxidation 5 hours.From figure Can be seen that, the oxidation weight gain of sample after treatment significantly lower than processing before sample, sample after treatment its high temperature resistance gasification property Getable apparent improvement.It can be seen from the figure that at 500~700 DEG C, treated, and sample still increases weight without apparent, and When temperature is more than 700~800 DEG C, treated, and sample increases slowly weightening with temperature, when temperature is more than 800 DEG C, the oxygen of sample Change weightening to be substantially increased, at this point, coating failure.
The above-mentioned measurement for hardness is measured using microhardness testers, and the mode that multigroup sample is averaged is arranged; Coating adhesion scratch test machine is carried out using WS-97 and measures bond strength;Using scanning electron microscope sem and X-ray diffractometer XRD Carry out coating morphology and Phase Structure Analysis.
The implementation of the present invention is not limited to this, and the above according to the invention is known using the ordinary skill of this field Knowledge and customary means, under the premise of not departing from above-mentioned basic fundamental thought of the invention, the present invention can also make other a variety of shapes Modification, replacement or the change of formula, all fall within rights protection scope of the present invention.

Claims (10)

1. a kind of preparation method of the titanium alloy cutting cutter material with PVD coatings, using in physical gas phase deposition technology Cathodic arc evaporation technique prepares multi-element coating, which is characterized in that above-mentioned technical process includes the following steps:
Cleaning is polished to sample cutter:It is polished step by step using silicon carbide paper successively, polishing treatment, sandblast and the third bronze medal And ethyl alcohol carries out ultrasonic cleaning to sample cutter respectively;
Prepare bonding bottom:Ti targets are installed, after the cutter after cleaning is placed on work rest, vacuum chamber is sent into, makes matrix and arc Vertical range between source is 200~300mm, is evacuated to less than 10-3Pa, and simultaneously to workpiece carry out heating reach it is pre- If temperature;It is passed through nitrogen, nitrogen flow is 600~650sccm, applies substrate bias -80V~-220V, is deposited in specimen surface TiN bond coatings;
Prepare main coating:The main coating is TiCNO and TiCN multi-element coatings:The Ti targets of use, Ti target arc currents be 60~ 65A, depositing temperature are 260~270 DEG C, and substrate bias is -80V~-220V, keeps and be passed through nitrogen, C2H2And CO mixed gas To being reacted in reative cell, the flow of nitrogen is 400~500sccm, C2H2Flow be 150~300sccm, the flow of CO is 80 ~200sccm is generated and is prepared TiCNO and TiCN mixed coatings;
Prepare protective coating:The protective coating is TiAlZr/TiAlZrCr coatings, TiAlZr/CrN coatings, TiAlZr/ZrN Coating, TiAl/CrN coatings or TiAl/TiAlCr coatings take target corresponding with coating when preparing above-mentioned multi-element coating Material and target arc current are passed through nitrogen or argon gas, and depositing temperature is 260~270 DEG C, and substrate bias is -80V~-220V.
2. the preparation method of the titanium alloy cutting cutter material according to claim 1 with PVD coatings, feature exist In:Further include Ion Cleaning step, it is -350V specially to apply substrate bias to sample cutter, is passed through unlatching arc initiation device, Striking under condition of high vacuum degree, ion that Ti targets are emitted reach specimen surface, and ion sputtering cleaning is carried out to specimen surface, when cleaning Between be 5~10 minutes.
3. the preparation method of the titanium alloy cutting cutter material according to claim 1 or 2 with PVD coatings, feature It is:The preparation method of the TiAlZr/TiAlZrCr coatings is:Using TiAlZr targets, arc current is 50~60A, deposition Temperature is 260~270 DEG C, and substrate bias is -80V~-220V, and is passed through argon gas, and the flow of argon gas is 500~650sccm, is sunk The thickness of product TiAlZr coatings, TiAlZr coatings is 300~500 μm;Then use TiAlZr targets and Cr targets, TiAl targets electric arc electricity Stream is 50~60A, and Cr target arc currents are 40A, and depositing temperature is 260~270 DEG C, and substrate bias is -80V~-220V, and is led to Enter argon gas and nitrogen, the flow of argon gas falls to 300~400sccm, and the flow of nitrogen is 200~400sccm, deposition TiAlZrCr coatings, TiAlZrCr coating layer thicknesses are 200~400 μm.
4. the preparation method of the titanium alloy cutting cutter material according to claim 1 or 2 with PVD coatings, feature It is:The preparation method of the TiAlZr/CrN coatings is:Using TiAlZr targets, using TiAlZr targets, arc current is 50~ 60A, depositing temperature are 260~270 DEG C, and substrate bias is -80V~-220V, and is passed through argon gas, the flow of argon gas is 500~ The thickness of 650sccm, depositing Ti AlZr coatings, TiAlZr coatings are 200~500 μm;Then Zr targets, Zr target arc currents are used For 60A, depositing temperature is 260~270 DEG C, and substrate bias is -80V~-220V, and is passed through argon gas and nitrogen, the flow of argon gas 300~400sccm is fallen to, the flow of nitrogen is 200~400sccm, deposits ZrN coatings, and ZrN coating layer thicknesses are 200~400 μm。
5. the preparation method of the titanium alloy cutting cutter material according to claim 1 or 2 with PVD coatings, feature It is:The preparation method of the TiAIZr/ZrN coatings is:Using TiAIZr targets, using TiAlZr targets, arc current is 50~ 60A, depositing temperature are 260~270 DEG C, and substrate bias is -80V~-220V, and is passed through argon gas, the flow of argon gas is 500~ The thickness of 650sccm, depositing Ti AlZr coatings, TiAlZr coatings are 200~500 μm;Then Zr coatings are prepared, using Zr targets, Zr target arc currents are 60A, and depositing temperature is 260~270 DEG C, and substrate bias is -80V~-220V, and is passed through argon gas and nitrogen The flow of gas, argon gas falls to 300~400sccm, and the flow of nitrogen is 200~400sccm, deposits ZrN coatings, ZrN coatings Thickness is 200~400 μm.
6. the preparation method of the titanium alloy cutting cutter material according to claim 1 or 2 with PVD coatings, feature It is:The preparation method of the TiAl/CrN coatings is:It is 60~65A to use TiAl targets, arc current first, and depositing temperature is 260~270 DEG C, substrate bias is -80V~-220V, and is passed through nitrogen, and the flow of nitrogen is 500~700sccm, depositing Ti Al The thickness of coating, TiAl coatings is 200~500 μm;Then Cr coatings are prepared, using Cr targets, Cr target arc currents are 60A, are sunk Accumulated temperature degree is 260~270 DEG C, and substrate bias is -80V~-220V, and is passed through nitrogen, and the flow of nitrogen is 500~700sccm, CrN coatings are deposited, CrN coating layer thicknesses are 200~400 μm.
7. the preparation method of the titanium alloy cutting cutter material according to claim 1 or 2 with PVD coatings, feature It is:The preparation method of the TiAl/TiAlCr coatings is:Using TiAl targets, arc current is 60~65A, and depositing temperature is 260~270 DEG C, substrate bias is -80V~-220V, and is passed through nitrogen, and the flow of nitrogen is 500~700sccm, depositing Ti Al The thickness of coating, TiAl coatings is 200~500 μm;Then it prepares TiAlCr and uses TiAl targets and Cr targets, TiAl target arc currents For 60~65A, Cr target arc currents are 40A, and depositing temperature is 260~270 DEG C, and substrate bias is -80V~-220V, and is passed through The flow of nitrogen, nitrogen is 500~700sccm, and depositing Ti AlCr coatings, TiAlCr coating layer thicknesses are 200~400 μm.
8. the titanium alloy cutting cutter material with PVD coatings, institute obtained by a kind of preparation method by described in claim 1 It is multi-element coating to state PVD coatings, and the multi-element coating includes main coating and protective coating, it is characterised in that:The main coating is TiCN and TiCNO multi-element coatings, in the multi-element coating, the oxygen atom of incorporation is instead of the carbon atom or nitrogen in the TiCN of part Atom, multi-element coating are face-centred cubic structure, and thickness is 500~800 μm;The protective coating applies for TiAlZr/TiAlZrCr Layer, TiAlZr/CrN coatings, TiAlZr/ZrN coatings, TiAl/CrN coatings or TiAl/TiAlCr coatings, thickness are 400~800 μm。
9. the titanium alloy cutting cutter material according to claim 7 with PVD coatings, it is characterised in that:In the master Further include TiN bond coatings between coating and sample tool surface, thickness is 80~120 μm of TiN bond coatings in TiCNO And play a transition role between TiCN coatings and matrix, improve the binding performance between interface binding power and film/matrix.
10. the titanium alloy cutting cutter material according to claim 7 with PVD coatings, it is characterised in that:The TiCN It is TiC with TiCNO multi-element coatings0.78N0.52And TiC0.63N0.47O0.21Multi-element coating.
CN201810372099.6A 2018-04-23 2018-04-23 A kind of titanium alloy cutting cutter material and preparation method thereof with PVD coating Expired - Fee Related CN108559957B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201810372099.6A CN108559957B (en) 2018-04-23 2018-04-23 A kind of titanium alloy cutting cutter material and preparation method thereof with PVD coating

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201810372099.6A CN108559957B (en) 2018-04-23 2018-04-23 A kind of titanium alloy cutting cutter material and preparation method thereof with PVD coating

Publications (2)

Publication Number Publication Date
CN108559957A true CN108559957A (en) 2018-09-21
CN108559957B CN108559957B (en) 2019-09-20

Family

ID=63536445

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201810372099.6A Expired - Fee Related CN108559957B (en) 2018-04-23 2018-04-23 A kind of titanium alloy cutting cutter material and preparation method thereof with PVD coating

Country Status (1)

Country Link
CN (1) CN108559957B (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109763102A (en) * 2019-03-22 2019-05-17 中国航空制造技术研究院 A method of improving the antifatigue polishing machine of blade
CN113097520A (en) * 2021-03-29 2021-07-09 深圳扑浪创新科技有限公司 Stainless steel bipolar plate and preparation method thereof
CN114311963A (en) * 2021-12-24 2022-04-12 西安理工大学 Textured wear-resistant doctor blade of gravure printing machine and preparation method

Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4337300A (en) * 1979-08-09 1982-06-29 Mitsubishi Kinzoku Kabushiki Kaisha Surface-coated blade member for cutting tools and process for producing same
CN1616169A (en) * 2003-10-30 2005-05-18 三菱综合材料株式会社 Hard coated layer with good anti-tipping property surface coated with metal ceramic made cutting tool
CN1636657A (en) * 2003-12-22 2005-07-13 三菱综合材料株式会社 Surface-coated cermet cutting tool with hard coating layer having excellend chipping resistance
JP2006289546A (en) * 2005-04-11 2006-10-26 Mitsubishi Materials Corp Surface-coated cermet cutting tool having hard coating layer for exhibiting superior chipping resistance in high speed intermittent cutting work
CN102380629A (en) * 2010-09-01 2012-03-21 三菱综合材料株式会社 Surface-coated cutting tool with hard coating layer having excellent cutting resistance and wear resistance
CN103171178A (en) * 2011-12-23 2013-06-26 株洲钻石切削刀具股份有限公司 Cutting tool for improving coating structure, and preparation method thereof
JP2014231116A (en) * 2013-05-29 2014-12-11 京セラ株式会社 Surface coating member
CN104582881A (en) * 2012-08-28 2015-04-29 三菱综合材料株式会社 Surface-coated cutting tool
CN104703734A (en) * 2012-10-01 2015-06-10 日立工具股份有限公司 Hard film coating tool and method for manufacturing said tool

Patent Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4337300A (en) * 1979-08-09 1982-06-29 Mitsubishi Kinzoku Kabushiki Kaisha Surface-coated blade member for cutting tools and process for producing same
CN1616169A (en) * 2003-10-30 2005-05-18 三菱综合材料株式会社 Hard coated layer with good anti-tipping property surface coated with metal ceramic made cutting tool
CN1636657A (en) * 2003-12-22 2005-07-13 三菱综合材料株式会社 Surface-coated cermet cutting tool with hard coating layer having excellend chipping resistance
JP2006289546A (en) * 2005-04-11 2006-10-26 Mitsubishi Materials Corp Surface-coated cermet cutting tool having hard coating layer for exhibiting superior chipping resistance in high speed intermittent cutting work
CN102380629A (en) * 2010-09-01 2012-03-21 三菱综合材料株式会社 Surface-coated cutting tool with hard coating layer having excellent cutting resistance and wear resistance
CN103171178A (en) * 2011-12-23 2013-06-26 株洲钻石切削刀具股份有限公司 Cutting tool for improving coating structure, and preparation method thereof
CN104582881A (en) * 2012-08-28 2015-04-29 三菱综合材料株式会社 Surface-coated cutting tool
CN104703734A (en) * 2012-10-01 2015-06-10 日立工具股份有限公司 Hard film coating tool and method for manufacturing said tool
JP2014231116A (en) * 2013-05-29 2014-12-11 京セラ株式会社 Surface coating member

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109763102A (en) * 2019-03-22 2019-05-17 中国航空制造技术研究院 A method of improving the antifatigue polishing machine of blade
CN113097520A (en) * 2021-03-29 2021-07-09 深圳扑浪创新科技有限公司 Stainless steel bipolar plate and preparation method thereof
CN113097520B (en) * 2021-03-29 2022-11-01 深圳扑浪创新科技有限公司 Stainless steel bipolar plate and preparation method thereof
CN114311963A (en) * 2021-12-24 2022-04-12 西安理工大学 Textured wear-resistant doctor blade of gravure printing machine and preparation method

Also Published As

Publication number Publication date
CN108559957B (en) 2019-09-20

Similar Documents

Publication Publication Date Title
JP6222675B2 (en) Surface-coated cutting tool and method for manufacturing the same
CN108220880B (en) A kind of high rigidity high corrosion-resistant high-entropy alloy nitride coatings and preparation method thereof
JP5246165B2 (en) Method for producing hard coating member
JP3934136B2 (en) Hard film coating member and coating method thereof
US8247092B2 (en) Coated cutting tool and a method of making thereof
US20060292399A1 (en) Composite coating for finishing of hardened steels
WO2017156996A1 (en) Composite functional cutter coating for cutting titanium alloy and preparation method therefor
EP1988190A2 (en) Coated cutting tool
CN106987816A (en) A kind of super fine and close Al Cr Si N preparation technology of coating of high aluminium content
JPH07310173A (en) Hard film coated tool and hard film coated member excellent in adhesion
CN108559957B (en) A kind of titanium alloy cutting cutter material and preparation method thereof with PVD coating
JP2017148930A (en) Coated cutting tool
Zhang et al. Microstructure evolution and wear resistance of nitride/aluminide coatings on the surface of Ti-coated 2024 Al alloy during plasma nitriding
JP3963354B2 (en) Coated cutting tool
CN109881148A (en) A kind of AlCrTiSiN high-entropy alloy nitride coatings of single phase solid solution structure and its preparation method and application
JP6641610B1 (en) Cutting tool and manufacturing method thereof
US6589602B2 (en) Highly adhesive surface-coated cemented carbide and method for producing the same
JP5765627B2 (en) Coated tool having excellent durability and method for producing the same
KR102085536B1 (en) Coated cutting insert
JP6641611B1 (en) Cutting tool and manufacturing method thereof
WO2020075356A1 (en) Cutting tool and manufacturing method therefor
JP2018176381A (en) Coated carbide alloy tool with high defect resistance
JP6583763B1 (en) Surface-coated cutting tool and manufacturing method thereof
JP5614405B2 (en) Hard film coated tool and manufacturing method thereof
Gorokhovsky Lafad‐Assisted Plasma Surface Engineering Processes for Wear and Corrosion Protection: A Review

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
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20190920

Termination date: 20200423

CF01 Termination of patent right due to non-payment of annual fee