CN106283053B - For the multi-layer composite coatings of cutter, cutter and preparation method thereof - Google Patents
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- CN106283053B CN106283053B CN201610782688.2A CN201610782688A CN106283053B CN 106283053 B CN106283053 B CN 106283053B CN 201610782688 A CN201610782688 A CN 201610782688A CN 106283053 B CN106283053 B CN 106283053B
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- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C28/00—Coating 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
- C23C28/04—Coating 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 only coatings of inorganic non-metallic material
- C23C28/044—Coating 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 only coatings of inorganic non-metallic material coatings specially adapted for cutting tools or wear applications
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- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C28/00—Coating 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
- C23C28/04—Coating 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 only coatings of inorganic non-metallic material
- C23C28/042—Coating 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 only coatings of inorganic non-metallic material including a refractory ceramic layer, e.g. refractory metal oxides, ZrO2, rare earth oxides
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C28/00—Coating 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
- C23C28/40—Coatings including alternating layers following a pattern, a periodic or defined repetition
- C23C28/42—Coatings including alternating layers following a pattern, a periodic or defined repetition characterized by the composition of the alternating layers
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- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C28/00—Coating 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
- C23C28/40—Coatings including alternating layers following a pattern, a periodic or defined repetition
- C23C28/44—Coatings including alternating layers following a pattern, a periodic or defined repetition characterized by a measurable physical property of the alternating layer or system, e.g. thickness, density, hardness
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- Engineering & Computer Science (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Inorganic Chemistry (AREA)
- Ceramic Engineering (AREA)
- Cutting Tools, Boring Holders, And Turrets (AREA)
- Drilling Tools (AREA)
- Physical Vapour Deposition (AREA)
Abstract
The multi-layer composite coatings that the invention discloses a kind of for cutter, cutter and preparation method thereof, the multi-layer composite coatings include multiple coated elements of periodical alternating deposit, and the coated elements include the Cr for the alternating deposit being sequentially depositing1‑xAlxN layers, Cr1‑ yZryN layers, ZrN layers and Cr1‑yZryN layers；Wherein, 0≤x≤0.70,0.30≤y≤0.70；The method that the method uses the more target alternating deposits of physical vapour deposition (PVD), passes through CrAl targets, CrZr targets, Zr targets and CrZr target alternating deposits Cr respectively on cutter body1‑xAlxN layers, Cr1‑yZryN layers, ZrN layers and Cr1‑yZryN layers, obtain into the Cr of periodical alternating deposit1‑xAlxN/Cr1‑yZryN/ZrN/Cr1‑yZryN MULTILAYER COMPOSITEs apply.
Description
Technical field
The invention belongs to material surface modifying technology fields, and in particular to a kind of multi-layer composite coatings, knife for cutter
Tool and preparation method thereof.
Background technology
CrAlN coatings are widely used in cutter, mold as protection materials.CrAlN substitutes the Cr in CrN by Al and is formed
Cubic structure metastable phase CrAlN coatings, crystal structure and mechanical property can change with the variation of Al content.It is keeping
When the face-centred cubic structure of CrN, and the mechanical property of coating can rise with the rising of Al content, when Al content is more than consolidating for CrN
When solubility, the structure of coating converts to the AlN of hexagonal structure and its mechanics and hot property is made to be remarkably decreased.
CrAlN coatings are often applied to high temperature applicationss as protection materials, and therefore, high-temperature behavior is extremely important.
The high-temperature oxidation resistance of CrAlN coatings is preferable, is higher than 1000 DEG C.But the CrAlN coatings of metastable phase are in high temperature (being higher than 900 DEG C)
Shi Huixiang its stable phase Cr and the AlN of close-packed hexagonal conversion and make its mechanical properties decrease, wherein the generation of Cr need by
Cr2N transition complete, the unstable release N atoms of Cr-N keys especially in coating thermal decomposition process and keep its mechanical property notable
It reduces.
Multi-element alloyed and multilayered structure optimization based on CrAlN coatings is the effective means for improving its performance at present.
Zr is added in CrAlN coatings, since the bond energy between Zr-N is higher than Cr-N keys and Al-N keys, CrAlN coatings can be significantly improved
Thermal stability.After adding Zr, in Cr0.48Al0.52The initial temperature of N coatings thermal decomposition increases, and the hardness of coating also rises therewith
It is high.But the addition of Zr can reduce the solid solubility of A1 in CrAlN coatings, and excessively high Zr additions can be such that the structure of coating turns to hexagonal phase
Change and its performance is made to decline.
Another means multilayered structure that coating material is modified can combine the advantage of different materials, especially when MULTILAYER COMPOSITE applies
For each layer of thickness control of layer in nanoscale, a kind of material can be that template coherent strengthening (be also known as using another material
Position superstructure coating), interface enhancing effect can be such that the hardness of coating steeply rises.The state of interface of multi-layer composite coatings removes
It is closely related outer with its modulation period and modulation ratio, also (for example by each coating material intrinsic performance：Lattice constant, mould
Amount etc.) influence.Due to Cr0.32A0.68The lattice constant difference of two kinds of materials of N and ZrN is too big (~12%), leads to its strain energy
Superstructure coating that is too big and being hardly formed complete coherent growth.When the modulation period of CrAlN/ZrN coatings is 9nm, CrAlN
Layer and the ZrN layers of multi-layer composite coatings for complete non-coherence, at this time ZrN layers of introducing do not have the performance of CrAlN coatings substantially
It influences.5nm is reduced to when the modulation period of CrAlN/ZrN coatings, the interface between CrAlN layers and ZrN layers is part coherence circle
Face, at this point, the hardness of coating and thermal stable temperature have promotion.
Invention content
In order to solve the above technical problems, the multi-layer composite coatings that the purpose of the present invention is to provide a kind of on cutter,
Cutter and preparation method thereof has high hardness and excellent heat to which the multi-layer composite coatings are combined with the advantage of a variety of materials
Stability improves the performance and application field of coating.
In order to achieve the above objectives, technical scheme is as follows：
On the one hand, the present invention provides a kind of multi-layer composite coatings for cutter, including periodical alternating deposit is multiple
Coated elements, the coated elements include the Cr for the alternating deposit being sequentially depositing1-xAlxN layers, Cr1-yZryN layers, ZrN layers and Cr1- yZryN layers；Wherein, 0≤x≤0.70,0.30≤y≤0.70.
Preferably, the Cr1-xAlxN layers, Cr1-yZryN layers, ZrN layers of thickness in monolayer be 2~10nm, thickness in monolayer is too
It is low, it is difficult to control in industrialized production；Thickness in monolayer is too high, and accumulative strain energy is excessive during each monolayer growth, it is difficult to
The laminated coating of coherent strengthening is obtained, in the thickness range, the multilayer that can obtain coherent strengthening applies each single layer
Layer.
Preferably, the overall thickness of the multi-layer composite coatings is 1 μm~12.0 μm.
Preferably, the overall thickness of the multi-layer composite coatings is 1 μm~6.0 μm, and preferably 3 μm, multi-layer composite coatings are such as
Fruit is excessively thin, influences whether the protective value and protecting effect of composite coating, but blocked up composite coating not only will produce it is excessively high
Stress causes coating easily to peel off, and cost is consequently increased, the coating in the thickness range have preferably protective value,
Protecting effect is not easy to peel off, at low cost.
Preferably, it is additionally provided with Cr between described matrix and the multi-layer composite coatings1-xAlxN transition zones, Cr1-xAlxN transition
The introducing of layer can improve the bond strength between coating and matrix.
Preferably, the Cr1-xAlxThe thickness of N transition zones is 50nm~1000nm.
Preferably, the Cr1-xAlxN layers, Cr1-yZryN layers and ZrN layers are face-centred cubic structure, are keeping face-centered cubic
When structure, the performance that coating has had, and Cr1-xAlxN layers and Cr1-yZryCoherent boundary is more readily formed between N layers.
On the other hand, the present invention also provides a kind of cutter, above-mentioned multi-layer composite coatings further include tool matrix, described more
Layer composite coating is located on the tool matrix.
On the other hand, the present invention also provides a kind of preparation method of above-mentioned cutter, the method is heavy using physical vapor
The method of the more target alternating deposits of product, passes through CrAl targets, CrZr targets, Zr targets and CrZr target alternating deposits respectively on cutter body
Cr1-xAlxN layers, Cr1-yZryN layers, ZrN layers and Cr1-yZryN layers, obtain into the Cr of periodical alternating deposit1-xAlxN/Cr1- yZryN/ZrN/Cr1-yZryN multi-layer composite coatings.
Preferably, further include the CrAl targets deposition Cr on matrix before depositing multi-layer composite coatings on cutter body1- xAlxThe step of N transition zones.
Preferably, the deposition atmosphere in the method is N2Either N2With the mixed gas of Ar.
The advantage of the invention is that：Due to Cr1-xAlxN/Cr1-yZryN/ZrN/Cr1-yZryN multi-layer composite coatings are each single
Coherent strengthening between layer, therefore, wherein Cr1-yZryZr-N keys in N layers, can also be steady other than strengthening the Cr-N in this layer
Determine Cr1-xAlxCr-N keys in N layers, and the Zr-N keys in ZrN can strengthen Cr1-yZryCr-N keys in N layers, it is final to prevent to apply
The thermal decomposition behavior of layer improves its thermal stability.In addition, the Cr of coherent strengthening1-xAlxN/Cr1-yZryN/ZrN/Cr1-yZryN
The interface enhancing of multi-layer composite coatings is remarkably improved the hardness of coating.
It is combined with the advantage of a variety of materials by multi-layer composite coatings, there is high hardness and superior heat-stability, improves
The performance and application field of coating.And the preparation method of the present invention is simple, equipment requirement is low and production cost is low
It is honest and clean.
Research and experiments have shown that, Cr1-yZryCan the control of the Composition Control of N namely its lattice constant to laminated coating
The superstructure coating for forming complete coherent growth is extremely important.If Zr contents are too high, Cr1-yZryN layers and Cr1-xAlxBetween N layers
Lattice constant difference is too big, it is difficult to form coherent boundary；If Zr contents are too low, Cr1-yZryDot matrix is normal between N layers and ZrN layers
Number difference is too big, it is difficult to form coherent boundary.By Cr1-yZryY in N is controlled in the ranges of 0.30≤y≤0.70, can be formed
The superstructure coating of complete coherent growth.
Description of the drawings
Fig. 1 is the structural schematic diagram of the multi-layer composite coatings provided in an embodiment of the present invention without transition zone；
Fig. 2 is the structural schematic diagram of the multi-layer composite coatings provided in an embodiment of the present invention with transition zone；
1, matrix；
2、Cr1-xAlxN layers；
3、Cr1-yZryN layers；
4, ZrN layers；
5、Cr1-xAlxN transition zones
Specific implementation mode
Unless specifically stated otherwise, drug used in following embodiment can be commercially available from regular channel.
Embodiment 1
By physical gas-phase deposite method deposition (referring to：Correlation between arc evaporation of
Ti-Al-N coatings and corresponding Ti0.50Al0.50target types, Surface＆Coatings
Technology, 275 (2015) 309-315)), utilize CrAl targets, CrZr targets and Zr target alternating deposits " Cr1-xAlxN layers 2 arrive
Cr1-yZryN layers 3 arrive Cr to ZrN layers 41-yZryThe Cr of the cyclically-varying trend of N layers 3 "1-xAlxN/Cr1-yZryN/ZrN/Cr1- yZryN multi-layer composite coatings, Cr1-xAlxAl content in N layers is controlled in 0≤X ＜ 0.70, Cr1-yZryN layers of Zr contents control
In 0.30≤y≤0.70, Cr1-xAlxN layers 2, Cr1-yZryN layers 3, ZrN layers 4 and Cr1-yZryThe thickness in monolayer of N layers 3 is followed successively by
3nm, 8nm, 4nm, 9nm, by 250 periods until the overall thickness of coating is 6.0 μm.
Embodiment 2
By physical gas-phase deposite method (referring to：Correlation between arc evaporation of Ti-
A1-N coatings and corresponding Ti0.50Al0.50Target types, Surface＆Coatings
Technology, 275 (2015) 309-315) deposition, Cr is deposited using CrAl targets first on tool matrix 11-xAlxN transition
Layer 5, then in Cr1-xAlx" Cr is deposited using CrAl targets, CrZr targets and Zr targets using physical gas-phase deposition on N transition zones 51- xAlxN layers 2 arrive Cr1-yZryN layers 3 arrive Gr to ZrN layers 41-yZryThe Cr of the cyclically-varying trend of N layers 3 "1-xAlxN/Cr1-yZryN/
ZrN/Cr1-yZryN multi-layer composite coatings, Cr1-xAlxN layers2In Al content control in 0≤X≤0.70, Cr1-yZryN layers of Zr
Content is controlled in 0.30≤y≤0.70, the Cr1-xAlxN layers 2, Cr1-yZryN layers 3, ZrN layers 4 and Cr1-yZryThe single layer of N layers 3
Thickness is followed successively by 2nm, 7nm, 3nm, 10nm, by 450 periods until the overall thickness of coating is 12 μm.
Embodiment 3
By physical gas-phase deposite method (referring to：Correlation between arc evaporation of Ti-
Al-N coatings and corresponding Ti0.50Al0.50Target types, Surface＆Coatings
Technology, 275 (2015) 309-315) deposition, " Cr is deposited on tool matrix 10.48Al52N layers 2 arrive Cr0.50Zr0.50N layers
3 arrive Cr to ZrN layers 40.50Zr0.50The Cr of the cyclically-varying trend of N layers 3 "0.48Al52N/Cr0.50Zr0.50N/ZrN/
Cr0.50Zr0.50N multi-layer composite coatings, wherein Cr0.48Al52N layers 2, Cr0.50Zr0.50N layers 3, ZrN layers 4, Cr0.50Zr0.50N layers 3
Thickness is followed successively by 6nm, 5nm, 4nm, 5nm, by 150 periods until the overall thickness of coating is 3.0 μm.
Cr prepared by the present invention0.48Al52N/Cr0.50Zr0.50N/ZrN/Cr0.50Zr0.50N multi-layer composite coatings are single-phase vertical
Square structure, by nano impress method (referring to：Correlation between arc evaporation of Ti-A1-N
coatings and corresponding Ti0.50Al0.50Target types, Surface＆Coatings Technology,
275 (2015) 309-315)) hardness of the coating is measured as~38.6GPa, and the Cr prepared0.48Al52The hardness of N signal layer coatings
Only~28.7GPa.
Reference substance be equally using above-mentioned standard milling cutter as tool matrix, by common physical gas-phase deposite method (referring to：
Correlation between arc evaporation ofTi-Al-N coatings and corresponding
Ti0.50Al0.50Target types, Surface＆Coatings Technology, 275 (2015) 309-315) deposit respectively it is general
The ingredient of logical CrAlN coatings, TiAlN coatings is Ti0.50Al0.50N。
Above-mentioned coating is deposited on the carbide blade base of model TNMG 120408, then uses the present embodiment 3
Composite coating layer cutter and reference substance obtained carry out the contrast experiment of continuous turning stainless steel, cutting parameter：Vc=120m/min,
F=0.3mm/r, ap=1.0mm.
Wherein the working durability of CrAlN coated chips is 8 minutes, and the working durability of coated chip of the present invention is 16 minutes.
Service life of the coated cutting tool of the composite coating of the present invention in turning stainless steel is than the CrAlN coated cutting tools under the prior art
It is significantly improved.
Embodiment 4.
By physical gas-phase deposite method (referring to：Correlation between arc evaporation of Ti-
Al-N coatings and corresponding Ti0.50Al0.50 target types, Surface＆Coatings
Technology, 275 (2015) 309-315) deposition, " Cr is deposited on tool matrix 10.48Al52N layers are arrived Cr0.50Zr0.50N layers
Cr is arrived to ZrN layers0.50Zr0.50N layers " cyclically-varying trend Cr0.48Al52N/Cr0.50Zr0.50N/ZrN/
Cr0.50Zr0.50N multi-layer composite coatings, wherein Cr0.48Al52N layers, Cr0.50Zr0.50N layers, ZrN layers, Cr0.50Zr0.50N layers of thickness
Degree is followed successively by 3nm, 6nm, 5nm, 6nm, by 150 periods until the overall thickness of coating is 3.0 μm.Prepared by the present invention
Cr0.48Al52N/Cr0.50Zr0.50N/ZrN/Cr0.50Zr0.50N multi-layer composite coatings are single phase cubic, by nano impress side
The hardness that method measures the coating is~36.4GPa, and the Cr prepared0.48Al52The hardness of N signal layer coatings is only~28.7GPa.
Compared with Example 3, the variation of multi-layer composite coatings is that the thickness of each single layer is changed, the knot of coating
Structure is still single phase cubic, and hardness is declined slightly.
Reference substance be equally using above-mentioned standard milling cutter as tool matrix, by common physical gas-phase deposite method (referring to：
Correlation between arc evaporation of Ti-Al-N coatings and corresponding
Ti0.50Al0.50target types, Surface＆Coatings Technology, 275 (2015) 309-315) it sinks respectively
The ingredient of the common CrAlN coatings of product, TiAlN coatings is Ti0.50Al0.50N。
Above-mentioned coating is deposited on the carbide blade base of model TNMG120408, then uses the present embodiment 4
Composite coating layer cutter and reference substance obtained carry out the contrast experiment of continuous turning stainless steel, cutting parameter：Vc=120m/min,
F=0.3mm/r, ap=1.0mm.
Wherein the working durability of CrAlN coated chips is 8 minutes, and the working durability of coated chip of the present invention is 14 minutes.
Service life of the coated cutting tool of the composite coating of the present invention in turning stainless steel is than the CrAlN coated cutting tools under the prior art
It is improved, but is declined compared with embodiment 3.
Embodiment 5
By physical gas-phase deposite method (referring to：Correlation between arc evaporationof Ti-
Al-N coatings and corresponding Ti0.50Al0.50target types, Surface＆Coatings
Technology, 275 (2015) 309-315) deposition, " Cr is deposited on tool matrix 10.48Al52N layers are arrived Cr0.50Zr0.50N layers
Cr is arrived to ZrN layers0.50Zr0.50N layers " cyclically-varying trend Cr0.48Al52N/Cr0.50Zr0.50N/ZrN/Cr0.50Zr0.50N
Multi-layer composite coatings, wherein Cr0.48Al52N layers, Cr0.50Zr0.50N layers, ZrN layers, Cr0.50Zr0.50N layers of thickness be followed successively by 6nm,
5nm, 4nm, 5nm, by 300 periods until the overall thickness of coating is 3.0 μm.
Cr prepared by the present invention0.48Al52N/Cr0.50Zr0.50N/ZrN/Cr0.50Zr0.50N multi-layer composite coatings are single-phase vertical
Square structure, the hardness that the coating is measured by nano impress method is~36.8GPa, and the Cr prepared0.48Al52N signal layer coatings
Hardness be only~28.7GPa.
Compared with Example 3, the variation of multi-layer composite coatings is that the thickness of each single layer is changed, the knot of coating
Structure is still single phase cubic, and hardness is held essentially constant.
Reference substance be equally using above-mentioned standard milling cutter as tool matrix, by common physical gas-phase deposite method (referring to：
Correlation between arc evaporation of Ti-A1-N coatings and corresponding
Ti0.50Al0.50target types, Surface＆Coatings Technology, 275 (2015) 309-315) it sinks respectively
The ingredient of the common CrAlN coatings of product, TiAlN coatings is Ti0.50Al0.50N。
Above-mentioned coating is deposited on the carbide blade base of model TNMG120408, then uses the present embodiment 5
Composite coating layer cutter and reference substance obtained carry out the contrast experiment of continuous turning stainless steel, cutting parameter：Vc=120m/min,
F=0.3mm/r, ap=1.0mm.Wherein the working durability of CrAlN coated chips is 8 minutes, the cutting of coated chip of the present invention
Service life is 15 minutes.Service life of the coated cutting tool of the composite coating of the present invention in turning stainless steel is than under the prior art
CrAlN coated cutting tools are improved, substantially quite with embodiment 3.
Embodiment 6
By physical gas-phase deposite method (referring to：Correlation between arc evaporationof Ti-
A1-N coatings and corresponding Ti0.50Al0.50target types, Surface＆Coatings
Technology, 275 (2015) 309-315) deposition, the Cr that deposition thickness is 200 nanometers on tool matrix 10.32Al68N mistakes
Layer is crossed, then in Cr0.32Al68Deposition deposition " Cr on N transition zones0.32Al68N layers are arrived Cr0.60Zr0.40N layers to ZrN layers are arrived
Cr0.60Zr0.40N layers " cyclically-varying trend Cr0.32Al68N/Cr0.60Zr0.40N/ZrN/Cr0.60Zr0.40N MULTILAYER COMPOSITEs apply
Layer, wherein Cr0.32Al68N layers, Cr0.60Zr0.40N layers, ZrN layers, Cr0.60Zr0.40N layers of thickness be followed successively by 6nm, 5nm, 4nm,
5nm, by 150 periods until the overall thickness of coating is 3.0 μm.Cr prepared by the present invention0.32Al68N/Cr0.60Zr0.40N/
ZrN/Cr0.60Zr0.40N multi-layer composite coatings be single phase cubic, by nano impress method measure the coating hardness be~
40.6GPa, and the Cr prepared0.48Al52The hardness of N signal layer coatings is only~28.7GPa.
Compared with Example 5,200 nanometers of Cr is only introduced between periodical coating and matrix0.32A168N transition zones,
Other to remain unchanged, the structure of coating is still single phase cubic, and hardness is kept substantially.
Reference substance be equally using above-mentioned standard milling cutter as tool matrix, by common physical gas-phase deposite method (referring to：
Correlation between arc evaporation of Ti-A1-N coatings and corresponding
Ti0.50Al0.50target types, Surface＆Coatings Technology, 275 (2015) 309-315) it sinks respectively
The ingredient of the common CrAlN coatings of product, TiAlN coatings is Ti0.50Al0.50N。
Above-mentioned coating is deposited on the carbide blade base of model TNMG120408, then uses the present embodiment 6
Composite coating layer cutter and reference substance obtained carry out the contrast experiment of continuous turning stainless steel, cutting parameter：Vc=120m/min,
F=0.3mm/r, ap=1.0mm.Wherein the working durability of CrAlN coated chips is 8 minutes, the cutting of coated chip of the present invention
Service life is 17 minutes.Service life of the coated cutting tool of the composite coating of the present invention in turning stainless steel is than under the prior art
CrAlN coated cutting tools are significantly improved, and are improved compared with embodiment 5.
Embodiment 7
By physical gas-phase deposite method (referring to：Correlation between arc evaporation of Ti-
Al-N coatings and corresponding Ti0.50Al0.50target types, Surface＆Coatings
Technology, 275 (2015) 309-315) deposition, the CrN transition zones that deposition thickness is 200 nanometers on tool matrix 1, so
" CrN layers are arrived Cr to deposition deposition on CrN transition zones afterwards0.30Zr0.70N layers to ZrN layers are arrived Cr0.30Zr0.70N layers " periodical become
The CrN/Cr of change trend0.30Zr0.70N/ZrN/Cr0.30Zr0.70NN multi-layer composite coatings, wherein CrN layer, Cr0.30Zr0.70N layers,
ZrN layers, Cr0.30Zr0.70N layers of thickness is followed successively by 6nm, 5nm, 4nm, 5nm, by 150 periods until the overall thickness of coating is
3.0μm.CrN/Cr prepared by the present invention0.30Zr0.70N/ZrN/Cr0.30Zr0.70NN multi-layer composite coatings are single phase cubic,
The hardness that the coating is measured by nano impress method is~30.1GPa, and the Cr prepared0.48Al52The hardness of N signal layer coatings is only
For~28.7GPa.
Compared with Example 6, transition zone Cr1-xAlxCr in N and periodical coating1-xAlxN and Cr1-yZryN layers of ingredient
Changed, the structure of coating is still single phase cubic, and hardness is decreased obviously.
Reference substance be equally using above-mentioned standard milling cutter as tool matrix, by common physical gas-phase deposite method (referring to：
Correlation between arc evaporation of Ti-Al-N coatings and corresponding
Ti0.50A10.50target types, Surface＆Coatings Technology, 275 (2015) 309-315) it sinks respectively
The ingredient of the common CrAlN coatings of product, TiAlN coatings is Ti0.50Al0.50N。
Above-mentioned coating is deposited on the carbide blade base of model TNMG120408, then uses the present embodiment 7
Composite coating layer cutter and reference substance obtained carry out the contrast experiment of continuous turning stainless steel, cutting parameter：Vc=120m/min,
F=0.3mm/r, ap=1.0mm.Wherein the working durability of CrAlN coated chips is 8 minutes, the cutting of coated chip of the present invention
Service life is 11 minutes.Service life of the coated cutting tool of the composite coating of the present invention in turning stainless steel is than under the prior art
CrAlN coated cutting tools are significantly improved, and have decline compared with embodiment 6.
Embodiment 8
By physical gas-phase deposite method (referring to：Correlation between arc evaporationof Ti-
Al-N coatings and corresponding Ti0.50Al0.50target types, Surface＆Coatings
Technology, 275 (2015) 309-315) deposition, the Cr that deposition thickness is 200 nanometers on tool matrix 10.32Al68N mistakes
Layer is crossed, then in Cr0.32Al68Deposition deposition " Cr on N transition zones0.32Al68N layers are arrived Cr0.60Zr0.40N layers to ZrN layers are arrived
Cr0.60Zr0.40N layers " cyclically-varying trend Cr0.32Al68N/Cr0.60Zr0.40N/ZrN/Cr0.60Zr0.40N MULTILAYER COMPOSITEs apply
Layer, wherein Cr0.32Al68N layers, Cr0.60Zr0.40N layers, ZrN layers, Cr0.60Zr0.40N layers of thickness be followed successively by 2nm, 2nm, 2nm,
2nm, by 375 periods until the overall thickness of coating is 3.0 μm.Cr prepared by the present invention0.32Al68N/Cr0.60Zr0.40N/
ZrN/Cr0.60Zr0.40N multi-layer composite coatings be single phase cubic, by nano impress method measure the coating hardness be~
40.6GPa, and the Cr prepared0.48Al52The hardness of N signal layer coatings is only~45.1GPa.
Compared with Example 6, each layer of thickness and the number of modulation period are changed only in periodical coating,
Other to remain unchanged, the structure of coating is still single phase cubic, and hardness improves.
Reference substance be equally using above-mentioned standard milling cutter as tool matrix, by common physical gas-phase deposite method (referring to：
Correlation between arc evaporation of Ti-A1-Ncoatings and corresponding
Ti0.50Al0.50target types, Surface＆Coatings Technology, 275 (2015) 309-315) it sinks respectively
The ingredient of the common CrAlN coatings of product, TiAlN coatings is Ti0.50Al0.50N。
Above-mentioned coating is deposited on the carbide blade base of model TNMG120408, then uses the present embodiment 8
Composite coating layer cutter and reference substance obtained carry out the contrast experiment of continuous turning stainless steel, cutting parameter：Vc=120m/min,
F=0.3mm/r, ap=1.0mm.Wherein the working durability of CrAlN coated chips is 8 minutes, the cutting of coated chip of the present invention
Service life is 24 minutes.Service life of the coated cutting tool of the composite coating of the present invention in turning stainless steel is than under the prior art
CrAlN coated cutting tools are significantly improved, and are improved compared with embodiment 6.
Embodiment 9
By physical gas-phase deposite method (referring to：Correlation between arc evaporation of Ti-
Al-N coatings and corresponding Ti0.50Al0.50target types, Surface＆Coatings
Technology, 275 (2015) 309-315) deposition, the Cr that deposition thickness is 200 nanometers on tool matrix 10.32Al68N mistakes
Layer is crossed, then in Cr0.32Al68Deposition deposition " Cr on N transition zones0.32Al68N layers are arrived Cr0.60Zr0.40N layers to ZrN layers are arrived
Cr0.60Zr0.40N layers " cyclically-varying trend Cr0.32Al68N/Cr0.60Zr0.40N/ZrN/Cr0.60Zr0.40N MULTILAYER COMPOSITEs apply
Layer, wherein Cr0.32Al68N layers, Cr0.60Zr0.40N layers, ZrN layers, Cr0.60Zr0.40N layers of thickness be followed successively by 10nm, 10nm,
10nm, 10nm, by 75 periods until the overall thickness of coating is 3.0 μm.Cr prepared by the present invention0.32Al68N/
Cr0.60Zr0.40N/ZrN/Cr0.60Zr0.40N multi-layer composite coatings are single phase cubic, and the painting is measured by nano impress method
The hardness of layer is~40.6GPa, and the Cr prepared0.48Al52The hardness of N signal layer coatings is only~35.8GPa.
Compared with Example 8, each layer of thickness and periodical number are changed only in periodical coating, other
It remains unchanged, the structure of coating is still single phase cubic, and hardness declines.
Reference substance be equally using above-mentioned standard milling cutter as tool matrix, by common physical gas-phase deposite method (referring to：
Correlation between arc evaporation of Ti-Al-N coatings and corresponding
Ti0.50Al0.50target types, Surface＆Coatings Technology, 275 (2015) 309-315) it sinks respectively
The ingredient of the common CrAlN coatings of product, TiAlN coatings is Ti0.50Al0.50N。
Above-mentioned coating is deposited on the carbide blade base of model TNMG120408, then uses the present embodiment 9
Composite coating layer cutter and reference substance obtained carry out the contrast experiment of continuous turning stainless steel, cutting parameter：Vc=120m/min,
F=0.3mm/r, ap=1.0mm.Wherein the working durability of CrAlN coated chips is 8 minutes, the cutting of coated chip of the present invention
Service life is 18 minutes.Service life of the coated cutting tool of the composite coating of the present invention in turning stainless steel is than under the prior art
CrAlN coated cutting tools are significantly improved, and are reduced compared with embodiment 8.
What has been described above is only a preferred embodiment of the present invention, it is noted that for those of ordinary skill in the art
For, without departing from the concept of the premise of the invention, various modifications and improvements can be made, these belong to the present invention
Protection domain.
Claims (8)
1. a kind of multi-layer composite coatings for cutter, which is characterized in that multiple coated elements including periodical alternating deposit,
The coated elements include the Cr for the alternating deposit being sequentially depositing1-xAlxN layers, Cr1-yZryN layers, ZrN layers and Cr1-yZryN layers；Its
In, 0≤x≤0.70,0.30≤y≤0.70；
The Cr1-xAlxN layers, Cr1-yZryN layers, ZrN layers of thickness in monolayer be 2~10nm.
2. the multi-layer composite coatings according to claim 1 for cutter, which is characterized in that the multi-layer composite coatings
Overall thickness is 1 μm~12.0 μm.
3. the multi-layer composite coatings according to claim 2 for cutter, which is characterized in that the multi-layer composite coatings
Overall thickness is 1 μm~6.0 μm.
4. the multi-layer composite coatings according to any one of claim 1 to 3 for cutter, which is characterized in that described
Cr1-xAlxN layers, Cr1-yZryN layers and ZrN layers are face-centred cubic structure.
5. a kind of cutter, which is characterized in that further include knife including multi-layer composite coatings any one of Claims 1-4
Has matrix, the multi-layer composite coatings are located on the tool matrix.
6. the preparation method of cutter according to claim 5, the method uses the more target alternating deposits of physical vapour deposition (PVD)
Method, pass through CrAl targets, CrZr targets, Zr targets and CrZr target alternating deposits Cr respectively on cutter body1-xAlxN layers, Cr1- yZryN layers, ZrN layers and Cr1-yZryN layers, obtain into the Cr of periodical alternating deposit1-xAlxN/Cr1-yZryN/ZrN/Cr1-yZryN
Multi-layer composite coatings.
7. the preparation method of cutter according to claim 6, which is characterized in that deposit MULTILAYER COMPOSITE on cutter body and apply
Further include the CrAl targets deposition Cr on matrix before layer1-xAlxThe step of N transition zones.
8. the preparation method of cutter according to claim 7, which is characterized in that the Cr1-xAlxThe thickness of N transition zones is
50nm~1000nm.
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| CN107287565B (en) * | 2017-07-10 | 2020-01-07 | 台州学院 | ZrCrN/ZrMoN laminated cutter coating and preparation method thereof |
| JPWO2019044714A1 (en) * | 2017-08-29 | 2020-09-17 | 京セラ株式会社 | Covering tool and cutting tool equipped with it |
| JPWO2019044715A1 (en) * | 2017-08-29 | 2020-09-17 | 京セラ株式会社 | Covering tool and cutting tool equipped with it |
| CN111041481A (en) * | 2019-11-20 | 2020-04-21 | 中南大学 | Coating cutter containing gradient and nano multilayer structure and preparation method |
| CN111304612B (en) * | 2020-03-30 | 2022-02-08 | 天津职业技术师范大学(中国职业培训指导教师进修中心) | CrAlN/AlN nano multilayer coating with high hardness and high oxidation resistance and preparation method thereof |
| CN112962060B (en) * | 2021-01-23 | 2021-12-28 | 西安交通大学 | Cr (chromium)3Al/Zr multilayer film and preparation method thereof |
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| CN102242338B (en) * | 2011-06-28 | 2013-04-10 | 株洲钻石切削刀具股份有限公司 | Composite coated cutting tool containing periodic coating and preparation method thereof |
| DE102012109254A1 (en) * | 2012-09-28 | 2014-04-03 | Walter Ag | Tool with TiAlCrSiN PVD coating |
| RU2538060C1 (en) * | 2013-07-23 | 2015-01-10 | Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования "Ульяновский государственный технический университет" | Method for obtaining multi-layered coating for cutting tool |
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