TECHNICAL FIELD
[0001] The present invention relates to a hard coating for a cutting tool to be coated onto
an end mill, drill, or other cutting tool.
BACKGROUND ART
[0002] There are examples of AlCrN coatings with excellent abrasion resistance as hard coatings
for coating metal cutting tools (see Patent Document 1), but there are also known
AlCrVBN coatings having greater abrasion resistance than AlCrN due to the addition
V and B to AlCrN (see Patent Document 2).
[0003] Patent Document 2 furthermore discloses that adding V to CrN improves lubricity.
In Patent Document 2, coating a CrVN coating on the surface layer of an AlCrVBN coating
is intended to improve seizing resistance (lubricity), but seizing resistance is insufficient
when stainless steel is worked and there is a need for further improvement in seizing
resistance.
[0004] In other words, stainless steel (in particular, SUS304 and other austenitic stainless
steels) has high viscosity and machining hardenability, and accordingly, there is
need for both hardness and toughness in a coating for a tool for machining. Also,
since the thermal conductivity is low, high heat generated during cutting and machining
does not readily dissipate, and the tool blade tip readily seizes. Consequently, there
is not only a need for abrasion resistance, but also seizing resistance.
[0005] When the tool blade tip has seized, machining surface roughness is worsened due to
wear between seized material and the material being cut, and when machining is further
continued, the seized material is more firmly deposited on the tool blade tip and
a "built-up" blade tip is formed. It is known that when cutting and machining is further
continued in a state in which a built-up blade tip has been formed, the built-up blade
tip repeatedly grows and falls away. In such a case, the tool blade tip becomes chipped
when the built-up blade tip falls away, whereby the hard coating falls off. Therefore,
not only does this lead to further abrasion and degraded machining surface roughness,
but also to reduced service life of the tool.
[0006] Owing to the above reasons, a tool covered with a hard coating for machining stainless
steel requires not only abrasion resistance, but also seizing resistance so that chipping
does not occur due to a built-up blade tip, and as described above, sufficient seizing
resistance has currently not yet been obtained with a conventional hard coating.
[Prior Art Documents]
[Patent Documents]
[0008] JP 2003 136305 A discloses a surface coated cemented carbide cutting tool having hard coating layer
exerting excellent ware resistance in high-speed cutting.
DISCLOSURE OF THE INVENTION
Problem the Invention is to Solve
[0011] In view of the above-described current situation, an object of the present invention
is to provide an extremely practical hard coating for a cutting tool that is a further
improvement of the hard coating according to Patent Document 2, and in which good
abrasion resistance and seizing resistance is demonstrated against austenitic stainless
steels, and longer service life of a cutting tool is realized.
Means for Solving the Problem
[0012] The above object is achieved by a cutting tool in accordance with claim 1. Further
developments of the invention are recited in the dependent claims.
Effect of the Invention
[0013] The present invention, being configured as described above, is an extremely practical
cutting tool in which excellent abrasion resistance and seizing resistance additionally
against austenitic stainless steel are demonstrated, and with which a longer service
life of a cutting tool can be realized.
BRIEF DESCRIPTION OF THE DRAWINGS
[0014]
FIG. 1 is an overall descriptive view of the external periphery abrasion width;
FIG. 2 is an overall descriptive view of the maximum seizing width;
FIG. 3 is an X-ray diffraction pattern of experiment example 2 (measurement range:
0° ≤ 2θ ≤ 80°);
FIG. 4 is an X-ray diffraction pattern of experiment example 10 (measurement range:
0° ≤ 2θ ≤ 80°);
FIG. 5 is an X-ray diffraction pattern of conventional example 2 (measurement range:
0° ≤ 2θ ≤ 80°); and
FIG. 6 is a comparative view of the X-ray diffraction patterns of experiment 2 and
the substrate alone (measurement range: 0° ≤ 2θ ≤ 80°).
BEST MODE FOR CARRYING OUT THE INVENTION
[0015] Embodiments of the present invention considered to be advantageous are briefly described
with indications the effects of the present invention.
[0016] The first coating layer has a predetermined composition and does not include V and
B; therefore, hardness is not excessively high, hardness and toughness are both achieved,
and good abrasion resistance against stainless steel is demonstrated. Also, seizing
resistance can be ensured by the second coating layer, which has excellent lubricity.
[0017] Therefore, it is possible to improve the abrasion resistance and seizing resistance
of a cutting tool against stainless steel (in particular, austenitic stainless steel),
and to inhibit chipping to the extent possible and ensure a longer service life of
a cutting tool.
Examples
[0018] Specific examples of the present disclosure are described with reference to the diagrams.
[0019] The present example is a hard coating for a cutting tool that is formed on a substrate,
the hard coating for a cutting tool comprising:
a first coating layer consisting of

where 25 ≤ X ≤ 35
with the metal component content expressed in units of at%,
N as a non-metal element, and inevitable impurities; and
a second coating layer consisting of

where 15 ≤ α ≤ 50
with the metal component content expressed in units of at%,
N as a non-metal element, and inevitable impurities,
the second coating layer being disposed on the topmost surface.
[0020] Each part will be described in detail.
[0021] The substrate is made of a super hard metal alloy containing WC (tungsten carbide)
and Co (cobalt). Specifically, the average particle diameter of the WC particles is
set to be 0.1 µm or more and 2.0 µm or less, and the Co content is set to be 5 mass%
or more and 15 mass% or less. The substrate is specifically an end mill, or a drill
or other cutting tool, and the first coating layer and the second coating layer are
sequentially provided in a layered state on the surface of the cutting tool.
[0022] The ratio of the thickness T1 of the first coating layer and the thickness T2 of
the second coating layer is set to 0.1 ≤ T2/T1 ≤ 0.5, and set so that the sum of the
thickness T1 and the thickness T2 will be 2.0 µm or more and 5.0 µm or less.
[0023] The present example includes a NaCl crystal structure and the diffraction intensity
of the (111) plane measured by X-ray diffractometry is greater than the diffraction
intensity of the (200) plane.
[0024] Specifically, the following expression holds, where I(111) is the diffraction intensity
of the (111) plane and I(200) is the diffraction intensity of the (200) plane.

[0025] The term α is preferably set to 15 or more and 25 or less.
[0026] In the present example, an undercoat layer is provided between the substrate and
the first coating layer. The undercoat layer comprises a Ti nitride or carbonitride,
and the thickness of the undercoat layer is set to 0.20 µm or more and 1.0 µm or less.
[0027] In other words, the present example is composed of an undercoat layer disposed directly
on the cutting tool, a first coating layer disposed on the undercoat layer, and a
second coating layer disposed on the first coating layer.
[0028] The reasons for the above-stated configuration and the effects obtained by the configuration
are described below.
[0029] First, the reasons for the above-described configuration will be stated in terms
of the composition and thickness of the first coating layer and the second coating
layer.
[0030] Stainless steel, which is a hard-to-cut material, has high viscosity and machining
hardenability; accordingly, there is need for both hardness and toughness in a tool
for machining stainless steel. The AlCrVBN coating of Patent Document 2, in which
V and B have been added to an AlCrN coating, has inferior toughness ostensibly because
hardness is excessively high, and chipping is observed even in the initial stage of
machining when stainless steel is machined (see conventional examples 1 to 3 in Table
1 of the later-described experiment examples). Chipping in the initial stage of machining
was not observed in (Al
70Cr
30)N to which V and B have not been added, but abrasion resistance was inferior (Conventional
example 4 of Table 1).
[0031] In view of the above and as a result of attempts to develop a coating (first coating
layer) provided with both chipping resistance and abrasion resistance, and repeated
variations of experiments and investigations, it was found that a coating, in which
the composition is (Al
(100-x)Cr
(x))N (where 25 ≤ x ≤ 35) and contains a NaCl crystal structure, and the diffraction
intensity of the (111) plane measured by X-ray diffractometry is greater than the
diffraction intensity of the (200) plane (a coating in which the maximum intensity
peak plane index is (111), where the measurement range 0° ≤ 2θ ≤ 80°), does not undergo
chipping in the initial stage of machining and has excellent abrasion resistance (Comparative
examples 1 to 3 of Table 1). Cases excluded from the above-stated composition undergo
considerable abrasion (Comparative examples 4 to 6 of Table 1). Cases in which the
maximum intensity peak plane index is not (111) also undergo considerable abrasion
(Comparative examples 7 to 9 of Table 1). This is presumably because, when the composition
is (Al
(100-x)Cr
(x))N (where 25 ≤ x ≤ 35), the hardness is highest, and the density is high because the
closest-packed plane is the (111) plane of a NaCl crystal, which is the structure
of AlCrN, and the abrasion resistance and chipping resistance are excellent. On the
other hand, seizing resistance is inadequate (Comparative examples 1 to 3 of Table
1).
[0032] Machining surface roughness degrades when the tool seizes. When machining is further
continued with seizing unresolved, a built-up blade tip is formed, the built-up blade
tip repeatedly grows and falls away, and chipping and abrasion are accelerated, leading
to shorter tool service life.
[0033] The surface of the first coating layer is coated with a second coating layer (Cr
(100-α)V
(α)N in order to improve the seizing resistance of the first coating layer against stainless
steel. A CrN coating is known as a coating having excellent lubricity, and V, which
has excellent lubricating performance against steel materials, is dissolved as a solid
solution in CrN with the intention of improving lubricity. Coating hardness is reduced
when the V content is excessively high, and therefore, the experimentation was carried
by varying the V content. It was found that seizing resistance is excellent when the
composition is (Cr
(100-α)V
(α))N (where 15 ≤ α ≤ 50) (see Experiment examples 1-18 of Table 2). In other words,
when α < 15, lubricity is inadequate and seizing increases (Comparative examples 10,
11 of Table 1). Seizing increases when α > 50 as well (Comparative example 12 of Table
1). This is presumably because with the V content being excessive, the film becomes
soft, the CrVN film is worn away in the initial stage of machining, and the seizing
resistance effect disappears.
[0034] In view of the above, it was found that when the composition of the second coating
layer is (Cr
(100-α)V
(α))N (where 15 ≤ α ≤ 50), a balance between lubricity and hardness can be achieved.
In particular, it was found that the effect of α being in the range of 15 ≤ α ≤ 25
is considerable (Experiment examples 1 to 5, 8 to 10, and 13 to 18 of Table 2).
[0035] The thickness ratio of the thicknesses T1 and T2 is preferably 0.1 ≤ T2/T1 ≤ 0.5,
where T1 is the thickness of the first coating layer and T2 is the thickness of the
second coating layer. When T2/T1 is less than 0.1, the effect of seizing resistance
is low (comparative example 13 of Table 1), and when T2/T1 exceeds 0.5, the ratio
of the second coating layer with low hardness is increased and abrasion resistance
is reduced (Comparative examples 14, 15 of Table 1). The total thickness (T1 + T2)
of the first coating layer and the second coating layer is preferably 2.0 µm or more
and 5.0 µm or less. When the total thickness is too low, the abrasion resistance effect
is reduced (Comparative example 16 of Table 1), and when the thickness is greater
than 5.0 µm, the abrasion resistance effect can be maintained (Comparative example
17 of Table 1), but the film formation time is extended in commensurate fashion to
the greater thickness. Also, a greater amount of the target material is consumed,
resulting in a high-cost cutting tool. It has already been confirmed that the rake
face peels away when the total thickness (T1 + T2) exceeds 11 µm.
[0036] Next, the reasons for using the above-described configuration in terms of the composition
and thickness of the undercoat layer will be described.
[0037] It was found that abrasion resistance and seizing resistance are further improved
by disposing a compound comprising a Ti nitride or carbonitride as an undercoat layer
between the substrate for a cutting tool and the first coating layer, and by optimizing
adhesion between the substrate and the first coating layer (Experiment examples 1
to 10, 13 to 18 of Table 2, Experiment examples 19 to 27 of Table 3). It was also
found that the thickness of the undercoat layer is preferably 0.20 µm or more and
1.0 um or less (Experiment examples 1 to 10, 13 to 18 of Table 2, Experiment examples
18 to 21 of Table 3). When the thickness of the undercoat layer is less than 0.2 µm,
the adhesion improvement effect is low, and when the thickness is exceeds 1 µm, the
ratio of undercoat layer having low hardness is increased and abrasion resistance
is reduced.
[0038] In the present example having the above-described configuration, the first coating
layer has both hardness and toughness without excessively high hardness, and demonstrates
good abrasion resistance against stainless steel. Also, seizing resistance can be
ensured due to the second coating layer, which has excellent lubricity. Therefore,
the abrasion resistance and seizing resistance of a cutting tool against stainless
steel (in particular, austenitic stainless steel) is improved, and the occurrence
of chipping can be inhibited to the extent possible to ensure longer service life
of a cutting tool.
[0039] Hence, the present example demonstrates good abrasion resistance and seizing resistance
against austenitic stainless steel as well, and is extremely practical in that longer
service life of a cutting tool can be realized.
[0040] Experiment examples that support the effect of the present example will be described.
[0041] An arc-discharge ion-plating device was used as a film formation device, targets
having various compositions were mounted in the film formation device as evaporation
sources having metal and metalloid components, N
2 gas as a reaction gas was introduced into the film formation device, and a predetermined
coating was formed on a four-blade square end mill (outside diameter: 6 mm) made of
a super hard metal alloy as a film formation substrate. The super hard metal alloy
substrate that was used was composed of hard particles having WC as a main component
and a binding material having Co as a main component, the average particle diameter
of the WC particles being 0.5 µm and the Co content being 10 mass%. The films were
formed on the above-described substrate end mill so that the undercoat layer, the
first coating layer, and the second coating layer reached various thicknesses.
[0042] A cutting test was carried out by using SUS304 as a workpiece, and cutting a side
surface under wet machining conditions using water-soluble cutting oil. The test was
carried out using an end mill having an outside diameter of 6 mm at a rotating speed
of 12,000 min
-1, a feed speed of 650 mm/min, a cutting distance of 0.3 mm in the diameter direction,
and a cutting distance of 2.0 mm in the axial direction. In the machining test for
Tables 1 and 2, comparative evaluations were made for a machining time of 60 minutes
(initial stage of machining).
[0043] In the machining tests of Table 3, the machining test was further extended to 180
minutes and a comparative evaluation was made in order to manifest the effect of improving
the adhesion of the hard coating by the provision of an undercoat layer.
[0044] In other words, the hard coatings (experiment examples) pertaining to the configuration
of the present example, conventional hard coatings, and the hard coatings (comparative
examples) outside the range of the present invention were each coated on an end mill
using the above-described means, and a cutting test was carried out using the end
mills. The test results are shown in Tables 1 to 3.
[0045] The external periphery abrasion width was obtained by measuring the abrasion width
at the external periphery of the blade in a right-angle direction to the blade from
the distal end of the end mill at a position 2 mm of cutting distance in the axial
direction (see FIG. 1). The maximum seizing width was obtained by measuring the maximum
seizing width (rake face side) of the seized material seized to the external peripheral
blade in the right-angle direction to the blade from the distal end of the end mill
in an area within 2.0 mm of cutting distance in the axial direction (see FIG. 2).
Table 1
| No. |
Undercoat layer |
First coating layer |
Second coating layer |
Total thk (T1+T2) (µm) |
Thk ratio (T2/T1) |
(Max. intensity peak plane) |
(Ext. periph. abras. width) (mm) |
Max. seizing width (mm) |
Chipping |
Assessment |
| Comp. |
Thk (µm) |
Comp. |
Thk T1 (µm) |
Comp. |
Thk T2 (µm) |
Abrasion resist. |
Seizing resist. |
Overall determ. |
| Conv. ex. 1 |
TiN |
0.3 |
(Al50Cr30V10B10) N |
3 |
- |
- |
3 |
- |
(200) |
0.016 |
0.069 |
Yes |
○ |
× |
Δ |
| Conv. ex. 2 |
- |
- |
(Al60Cr32V3B5)N |
4 |
- |
- |
4 |
- |
(200) |
0.018 |
0.065 |
Yes |
○ |
× |
Δ |
| Conv. ex. 3 |
- |
- |
(Al57Cr30V3B10)N |
1.8 |
(Cr80V20)N |
0.4 |
2.2 |
0.22 |
(200) |
0.016 |
0.032 |
Yes |
○ |
○ |
○ |
| Conv. ex. 4 |
TiN |
0.3 |
(Al70Cr30)N |
3 |
- |
- |
3 |
- |
(200) |
0.022 |
0.069 |
No |
× |
× |
× |
| Comp. ex. 1 |
TiN |
0.5 |
(A175Cr25)N |
3 |
- |
- |
3 |
- |
(111) |
0.018 |
0.056 |
No |
○ |
× |
Δ |
| Comp. ex. 2 |
TiN |
0.3 |
(Al65Cr35)N |
3 |
- |
- |
3 |
- |
(111) |
0.019 |
0.088 |
No |
○ |
× |
Δ |
| Comp. ex. 3 |
TiN |
0.5 |
(Al70Cr30)N |
3 |
- |
- |
3 |
- |
(111) |
0.018 |
0.081 |
No |
○ |
× |
Δ |
| Comp. ex. 4 |
TiN |
0.8 |
(Al80Cr20)N |
3 |
- |
- |
3 |
- |
(111) |
0.024 |
0.089 |
No |
× |
× |
× |
| Comp. ex. 5 |
TiN |
0.3 |
(Al50Cr50)N |
3 |
- |
- |
3 |
- |
(111) |
0.022 |
0.051 |
No |
× |
× |
× |
| Comp ex. 6 |
TiN |
0.3 |
(Al20Cr80)N |
3 |
- |
- |
3 |
- |
(111) |
0.029 |
0.050 |
No |
× |
× |
× |
| Comp ex. 7 |
TiN |
0.3 |
(Al70Cr30)N |
3 |
- |
- |
3 |
- |
(200) |
0.022 |
0.050 |
No |
× |
× |
× |
| Comp. ex. 8 |
TiN |
0.8 |
(Al75Cr25)N |
3 |
- |
- |
3 |
- |
(200) |
0.024 |
0.053 |
No |
× |
× |
× |
| Comp. ex. 9 |
TiN |
0.3 |
(Al65Cr35)N |
3 |
- |
- |
3 |
- |
(200) |
0.024 |
0.044 |
No |
× |
× |
× |
| Comp. ex. 10 |
TiN |
0.3 |
(Al70Cr30)N |
3 |
(Cr100)N |
0.6 |
3.6 |
0.20 |
(111) |
0.017 |
0.044 |
No |
○ |
× |
× |
| Comp. ex. 11 |
TiN |
0.8 |
(Al70Cr30)N |
3 |
(Cr90V10)N |
0.6 |
3.6 |
0.20 |
(111) |
0.016 |
0.069 |
No |
○ |
× |
× |
| Comp. ex. 12 |
TiN |
0.3 |
(Al70Cr30)N |
3 |
(Cr45V55)N |
0.6 |
3.6 |
0.20 |
(111) |
0.016 |
0.056 |
No |
○ |
× |
× |
| Comp. ex. 13 |
TiN |
0.3 |
(Al70Cr30)N |
3 |
(Cr80v20)N |
0.2 |
3.2 |
0.07 |
(111) |
0.016 |
0.057 |
No |
○ |
× |
× |
| Comp. ex. 14 |
TiN |
0.8 |
(Al70Cr30)N |
2 |
(Cr80V20)N |
1.2 |
3.2 |
0.60 |
(111) |
0.024 |
0.050 |
No |
× |
× |
× |
| Comp. ex. 15 |
TiN |
0.3 |
(Al70Cr30)N |
1 |
(Cr80V20)N |
1.2 |
2.2 |
1.20 |
(111) |
0.030 |
0.060 |
No |
× |
× |
× |
| Comp, ex. 16 |
TiN |
0.3 |
(Al70Cr30)N |
0.6 |
(Cr80V20)N |
0.2 |
0.8 |
0.33 |
(111) |
0.024 |
0.033 |
No |
× |
○ |
Δ |
| Comp. ex. 17 |
TiN |
0.3 |
(Al70Cr30)N |
5 |
(Cr80V20)N |
1.8 |
6.8 |
0.36 |
(111) |
0.016 |
0.028 |
No |
○ |
○ |
Δ |
Table 2
| No. |
Undercoat layer |
First coating layer |
Second coating layer |
Total thk (T1+T2) (µm) |
Thk ratio (T2/T1) |
(Max. intensity peak plane) |
(Ext. periph. abras. width) (mm) |
Max. seizing width (mm) |
Chipping |
Assessment |
| Comp. |
Thk (µm) |
Comp. |
Thk T1 (µm) |
Comp. |
Thk T2 (µm) |
Abrasion resist. |
Seizing resist. |
Overall determ. |
| Exp ex. 1 |
TiN |
0.3 |
(Al75Cr25)N |
3 |
(Cr80V20)N |
0.6 |
3.6 |
0.20 |
(111) |
0.012 |
0.025 |
No |
⊚ |
⊚ |
⊚ |
| Exp ex. 2 |
TiN |
0.5 |
(Al70Cr30)N |
2.8 |
(Cr80V20)N |
0.6 |
3.4 |
0.21 |
(111) |
0.013 |
0.026 |
No |
⊚ |
⊚ |
⊚ |
| Exp ex. 3 |
TiN |
0.3 |
(Al63Cr35)N |
3 |
(Cr80V20)N |
0.6 |
3.6 |
0.20 |
(111) |
0.015 |
0.024 |
No |
⊚ |
⊚ |
⊚ |
| Exp ex. 4 |
TiN |
0.5 |
(Al70Cr30)N |
3 |
(Cr85V15)N |
0.6 |
3.6 |
0.20 |
(111) |
0.015 |
0.028 |
No |
⊚ |
⊚ |
⊚ |
| Exp ex. 5 |
TiN |
0.7 |
(Al70Cr30)N |
2.6 |
(Cr75V25)N |
0.6 |
3.2 |
0.23 |
(111) |
0.015 |
0.028 |
No |
⊚ |
⊚ |
⊚ |
| Exp ex. 6 |
TiN |
0.5 |
(Al70Cr30)N |
3 |
(Cr65V35)N |
0.6 |
3.6 |
0.20 |
(111) |
0.019 |
0.030 |
No |
○ |
○ |
○ |
| Exp ex. 7 |
TiN |
0.3 |
(Al70Cr30)N |
3 |
(Cr50V50)N |
0.6 |
3.6 |
0.20 |
(111) |
0.018 |
0.038 |
No |
○ |
○ |
○ |
| Exp ex. 8 |
TiN |
0.5 |
(Al70Cr30)N |
3.5 |
(Cr80V20)N |
1.5 |
5 |
0.43 |
(111) |
0.012 |
0.026 |
No |
⊚ |
⊚ |
⊚ |
| Exp ex. 9 |
TiN |
0.3 |
(Al70Cr30)N |
2 |
(Cr80V20)N |
1.0 |
3 |
0.50 |
(111) |
0.016 |
0.028 |
No |
⊚ |
⊚ |
⊚ |
| Exp ex.10 |
TiN |
0.5 |
(Al70Cr30)N |
2 |
(Cr80V20)N |
0.2 |
2.2 |
0.10 |
(111) |
0.015 |
0.025 |
No |
⊚ |
⊚ |
⊚ |
| Exp ex. 11 |
- |
- |
(Al70Cr30)N |
3 |
(Cr80V20)N |
0.6 |
3.6 |
0.20 |
(111) |
0.019 |
0.030 |
No |
○ |
○ |
○ |
| Exp ex. 12 |
- |
- |
(Al70Cr30)N |
3 |
(Cr80V20)N |
0.6 |
3.6 |
0.20 |
(111) |
0.02 |
0.035 |
No |
○ |
○ |
○ |
| Exp ex. 13 |
TiN |
0.2 |
(Al70Cr30)N |
3 |
(Cr80V20)N |
0.6 |
3.6 |
0.20 |
(111) |
0.012 |
0.027 |
No |
⊚ |
⊚ |
⊚ |
| Exp ex. 14 |
TiN |
0.5 |
(Al70Cr30)N |
3 |
(Cr80V20)N |
0.6 |
3.6 |
0.20 |
(111) |
0.015 |
0.023 |
No |
⊚ |
⊚ |
⊚ |
| Exp ex. 15 |
TiN |
1.0 |
(Al70Cr30)N |
3 |
(Cr80V20)N |
0.6 |
3.6 |
0.20 |
(111) |
0.015 |
0.024 |
No |
⊚ |
⊚ |
⊚ |
| Exp ex.16 |
TiCN |
0.2 |
(Al70Cr30)N |
3 |
(Cr80V20)N |
0.6 |
3.6 |
0.20 |
(111) |
0.016 |
0.028 |
No |
⊚ |
⊚ |
⊚ |
| Exp ex. 17 |
TiCN |
0.5 |
(Al70Cr30)N |
3 |
(Cr80V20)N |
0.6 |
3.6 |
0.20 |
(111) |
0.012 |
0.024 |
No |
○ |
⊚ |
⊚ |
| Exp ex. 18 |
TiCN |
1.0 |
(Al70Cr30)N |
3 |
(Cr80V20)N |
0.6 |
3.6 |
0.20 |
(111) |
0.017 |
0.028 |
No |
⊚ |
⊚ |
⊚ |
Table 3
| No. |
Undercoat layer |
First coating layer |
Second coating layer |
Total thk (T1+T2) (µm) |
Thk ratio (T2/T1) |
(Max. intensity peak plane) |
(Ext. periph. abras. width) (mm) |
Max. seizing width (mm) |
Chipping |
Assessment |
Remarks |
| Comp. |
Thk (µm) |
Comp. |
Thk T1 (µm) |
Comp. |
Thk T2 (µm) |
Adhesion |
| Exp ex. 19 |
TiN |
0.3 |
(Al70Cr30)N |
3 |
(Cr80V20)N |
1 |
4 |
0.33 |
(111) |
0.025 |
0.028 |
No |
⊚ |
|
| Exp ex. 20 |
TiN |
0.5 |
(Al70Cr30)N |
2.5 |
(Cr80V20)N |
0.4 |
2.9 |
0.16 |
(111) |
0.030 |
0.029 |
No |
⊚ |
|
| Exp ex. 21 |
TiN |
0.3 |
(Al70Cr30)N |
4 |
(Cr80V20)N |
0.4 |
4.4 |
0.10 |
(111) |
0.035 |
0.026 |
No |
⊚ |
|
| Exp ex. 22 |
TiN |
0.2 |
(Al70Cr30)N |
3.1 |
(Cr80V20)N |
1 |
4.1 |
0.32 |
(111) |
0.033 |
0.030 |
No |
⊚ |
|
| Exp ex. 23 |
TiN |
0.5 |
(Al70Cr30)N |
3.3 |
(Cr80V20)N |
0.8 |
4.1 |
0.24 |
(111) |
0.035 |
0.030 |
No |
© |
|
| Exp ex. 24 |
TiN |
1.0 |
(Al70Cr30)N |
3 |
(Cr80V20)N |
0.6 |
3.6 |
0.20 |
(111) |
0.040 |
0.027 |
No |
⊚ |
|
| Exp ex.25 |
TiCN |
0.2 |
(Al70Cr30)N |
3.1 |
(Cr80V20)N |
0.6 |
3.7 |
0.19 |
(111) |
0.039 |
0.030 |
No |
⊚ |
|
| Exp ex.26 |
TiCN |
0.5 |
(Al70Cr30)N |
3.3 |
(Cr80v20)N |
0.8 |
4.1 |
0.24 |
(111) |
0.028 |
0.027 |
No |
⊚ |
|
| Exp ex.27 |
TiCN |
1.0 |
(Al70Cr30)N |
3 |
(Cr80V20)N |
0.6 |
3.6 |
0.20 |
(111) |
0.035 |
0.028 |
No |
⊚ |
|
| Exp ex. 28 |
- |
- |
(Al70Cr30)N |
4 |
(Cr80V20)N |
0.8 |
4.8 |
0.20 |
(111) |
0.044 |
0.044 |
No |
× |
Rake face peeling |
| Exp ex. 29 |
- |
- |
(Al70Cr30)N |
3 |
(Cr80V20)N |
1 |
4 |
0.33 |
(111) |
0.045 |
0.045 |
No |
× |
Rake face peeling |
| Comp. ex. 18 |
TiN |
0.1 |
(Al70Cr30)N |
3 |
(Cr80V20)N |
0.8 |
3.8 |
0.27 |
(111) |
0.063 |
0.045 |
No |
× |
Rake face peeling |
| Comp. ex. 19 |
TiN |
1.2 |
(Al70Cr30)N |
3 |
(Cr80V20)N |
1 |
4 |
0.33 |
(111) |
0.071 |
0.055 |
No |
Δ |
Abrasion resistance × |
| Comp. ex. 20 |
TiCN |
0.1 |
(Al70Cr30)N |
3 |
(Cr80V20)N |
1.2 |
4.2 |
0.40 |
(111) |
0.068 |
0.065 |
No |
× |
Rake face peeling |
| Comp. ex. 21 |
TiCN |
1.2 |
(Al70Cr30)N |
3 |
(Cr80V20)N |
1.4 |
4.4 |
0.47 |
(111) |
0.069 |
0.070 |
No |
Δ |
Abrasion resistance × |
[0046] The experiment examples are observed from Tables 1 and 2 to have reduced external
periphery abrasion width of the end mill and improved seizing resistance in comparison
with the conventional examples and comparative examples.
[0047] FIGS. 3 and 4 are X-ray diffraction patterns of experiment examples 2 and 10, respectively,
of Table 2. It can be confirmed that the diffraction intensity of the (111) plane
is greater than the diffraction intensity of the (200) plane. FIG. 5 is an X-ray diffraction
pattern of conventional example 2, and FIG. 6 is a comparative view of X-ray diffraction
patterns of experiment example 2 and the substrate alone.
[0048] When film is formed using an arc-discharge ion-plating device, the crystal alignment
of the coating can be controlled using film formation conditions, regardless of targets
having identical compositions, and in the present example, excellent abrasion resistance
is realized by ensuring that the diffraction intensity of the (111) plane having a
NaCl crystal structure is greater than the diffraction intensity of the (200) plane.
In particular, the ratio between the diffraction intensity of the (111) plane and
the diffraction intensity of the (200) plane is preferably I(111)/I(200) ≥ 1.5. Although
not shown in the table, it had been confirmed that I(111)/I(200) ≥ 1.5 in each of
the experiment examples.
[0049] It was also confirmed from Table 3 that adhesion is improved by the provision of
an undercoat layer, and that even greater abrasion resistance and seizing resistance
are demonstrated.
[0050] It is explicitly stated that all features disclosed in the description and/or the
claims are intended to be disclosed separately and independently from each other for
the purpose of original disclosure as well as for the purpose of restricting the claimed
invention independent of the composition of the features in the embodiments and/or
the claims. It is explicitly stated that all value ranges or indications of groups
of entities disclose every possible intermediate value or intermediate entity for
the purpose of original disclosure as well as for the purpose of restricting the claimed
invention, in particular as limits of value ranges.