Technical Field
Background Art
[0002] WC-based cemented carbides are used, for example, in the substrates of cutting tools
and surface-coated cutting tools (hereinafter referred to as coated tools). Coated
tools have coating layers, such as Al
2O
3 or TiCN layers, deposited on substrates and are used in cutting of carbon steel,
cast iron, alloy steel, and other materials.
[0003] In cutting processes of stainless steel where the cutting edges are subject to high
temperatures, the cutting edges of the coated tool may undergo plastic deformation,
leading to early tool life. If the hardness of the substrate is increased to suppress
this plastic deformation, the chipping resistance is reduced. Accordingly, there is
a need for a substrate made of WC-based cemented carbides that satisfy compatibility
of plastic deformation resistance and chipping resistance. Such cemented carbides
have been proposed, for example, as described as follows:
[0004] Patent Literature 1 discloses a cemented carbide comprising a hard phase containing
tungsten carbide grains and a binder phase mainly composed of iron group elements
such as cobalt, wherein the relation: B/A ≤ 0.05 is satisfied where A is the number
of grains of tungsten carbide and B is the number of grains of tungsten carbide having
one or less contact points with other tungsten carbide grains. This WC-based cemented
carbide has excellent plastic deformation resistance.
[0005] Patent Literature 2 discloses a WC-based cemented carbide that contains 10 to 13
mass% Co, 2 to 8 mass% Cr relative to Co, and 0.2 to 0.5 mass% of at least one of
TaC and NbC, the balance being WC, and has a hardness of 88.6 to 89.5 HRA, where the
ratio D
80/D
20 of the WC number cumulative 80% grain size D
80 to the number cumulative 20% grain size D
20 satisfies the relation: 2.0 ≤ D80/D20 ≤ 4.0, the grain size D
80 is 4.0 to 4.86 µm, and degree c of the WC adhesion satisfies the relation 0.36 ≤
c ≤ 0.43. This WC-based cemented carbide has excellent chipping resistance.
Citation List
Patent Literature
Summary of Invention
Technical Problem
[0007] An object of the present invention, which has been accomplished in view of the aforementioned
circumstances and proposals, is to provide a cemented carbide that exhibits high plastic
deformation resistance and high chipping resistance, in use as cutting tools and coated
tools.
Solution to Problem
[0008] A WC-based cemented carbide in accordance with an embodiment of the present invention
comprises: 6.0 to 10.0 mass% Co, 0.08 to 0.90 mass% Cr (provided that the Cr content
(mass%)/Co content (mass%) is 10% or less), 0.0 to 3.8 mass% M (where M is at least
one element selected from the group consisting of V, Ta, Nb, Ti and Zr), 4.5 to 7.5
mass% C, the balance being W and inevitable impurities, wherein
the cemented carbide comprises binder phases, hard phases, and γ phases,
the binder phases are mainly composed of Co, the hard phases are mainly composed of
W carbide, and the γ phases are mainly composed of M carbide,
in the crystal grains constituting the hard phases, the number cumulative 99% grain
size C99 is 3.30 µm or less, and the ratio C99/C50 of the number cumulative 99% grain
size C99 (µm) to the number cumulative 50% grain size C50 (µm) ranges from 4.80 to
6.50, and
the proportion (L) of the interfacial length of crystal grains constituting the hard
phases in contact with crystal grains constituting the binder phases to the total
interfacial length of crystal grains constituting the hard phases is 35% or more.
[0009] The WC-based cemented carbide may satisfy the condition (1):
- (1) The Rockwell hardness (HRA) is in the range of 88.8 to 90.6.
Advantageous Effects of Invention
[0010] A substrate for a cutting or coated tool made of WC-based cemented carbide of the
above embodiment exhibits excellent plastic deformation resistance and chipping resistance.
Description of Embodiments
[0011] The inventor has made a diligent study of cemented carbides that provide excellent
plastic deformation resistance and chipping resistance when used as substrates of
coated tools, and has found the following matters (1) and (2) for the WC-based cemented
carbides described in Patent Literatures 1 and 2.
- (1) The WC-based cemented carbide described in Patent Literature 1 reaches the end
of tool life early when being used in intermittent cutting; and
- (2) The WC-based cemented carbide described in Patent Literature 2 lacks plastic deformation
resistance when being used in high-speed high-feed cutting.
[0012] The inventor has made further diligent investigations. As a result, the inventor
has reached the following findings to derive the present invention.
- (a) The plastic deformation resistance of WC-based cemented carbides depends on the
grain size of the crystal grains constituting the hard phases. In detail, as the grain
diameter decreases, the plastic deformation resistance of the WC-based cemented carbide
improves. Thus, the plastic deformation resistance of WC-based cemented carbide improves
in the case that a larger number of crystal grains with smaller grain size constituting
the hard phases is present in the WC-based cemented carbide than before.
- (b) The crystal grains constituting the hard phase are appropriately distributed in
the WC-based cemented carbide to suppress contact between crystal grains in the hard
phase, thereby suppressing stress concentration at contact points and thus improving
the chipping resistance.
[0013] The WC-based cemented carbide in the embodiment of the present invention will now
be described in detail.
[0014] Throughout the specification and the claims, a numerical range expressed as "A to
B" (A and B are both numerical values) includes the upper limit (B) and the lower
limit (A). In the case that units are stated only for the upper limit (B), the units
for the upper limit (B) and the lower limit (A) should be the same.
[0015] The composition not expressed using a formula of the compound is not limited to stoichiometric
compositions, but includes all known compositions with any atomic ratio.
1. Composition
[0016] The WC-based cemented carbide comprises: 6.0 to 10.0 mass% Co, 0.08 to 0.90 mass%
Cr (provided that the Cr content (mass%)/Co content (mass%) is 10 percent or less),
0.0 to 3.8 mass% M (where M is at least one element selected from the group consisting
of V, Ta, Nb, Ti and Zr), 4.5 to 7.5 mass% C, the balance being W and inevitable impurities.
[0017] Individual components will now be described.
(1) Co
[0018] In the case of a Co content of 6.0 to 10.0 mass%, the WC-based cemented carbide has
excellent plastic deformation resistance when used as coated tools and substrates
of coated tools.
[0019] Co is primarily present in the binder phases and is the main component of the binder
phases (accounting for at least 50 atomic% of all components in the binder phases).
The binder phases are composed of crystal grains with fcc and hcp structures.
[0020] The Co content is more preferably in a range of 7.0 to 9.6 mass%.
(2) Cr
[0021] Cr is present in the form of solid solution in Co, which is the main component of
the binder phase, and contributes to suppression of the growth of W carbide grains
in in the hard phases, making crystal grains of W carbide finer or smaller. This function
is insufficient at a Cr content of less than 0.08 mass%. A Cr content exceeding 10%
of the Co content causes composite carbides of Cr and W to be precipitated and the
toughness of the WC-based cemented carbide to decrease. Since the composite carbides
work as the starting points of defect generation, the Cr content (mass %)/Co content
(mass %) should be 10% or less. Since the upper limit of the Co content is 10.0 mass
%, the upper limit of Cr content should be 0.90 mass % to allow for a margin of error.
(3) M (at least one element selected from V, Ta, Nb, Ti, and Zr)
[0022] M is an optional component (the content may be 0.0 mass%). M however is present in
the form of solid solution in Co, which is the main component of the binder phases,
and can increase the hardness of WC-based cemented carbide. M also forms carbide (not
limited to the stoichiometric composition) and is present as the main component of
the γ-phases (M accounts for more than at least 50 atomic% of all the components in
the γ-phases). The upper limit of M content is set at 3.8 mass% because an M content
exceeding 3.8 mass% leads to the toughness of WC-based cemented carbides to decrease
and generation of the starting points of defects.
(4) C
[0023] C is contained to form carbides primarily in the hard phases and γ phases. A C content
of 4.5 to 7.5 mass% causes an appropriate amount of carbides to be formed in the hard
phase and γ phases.
(5) W
[0024] W is the main component of the hard phases. In detail, W accounts for at least 50
atom% of all the components in the hard phases. W is primarily present in the hard
phases in the form of carbides (mostly WC, also including W carbides with non-stoichiometric
composition).
(6) Inevitable impurities
[0025] Raw materials may contain unintended impurities, which may be incorporated during
the manufacturing process. These impurities are called inevitable impurities. The
content of inevitable impurities should preferably be 0.3 mass% or less in internal
number when the entire WC-base cemented carbide is set as 100 mass%.
2. Microstructure
[0026] The WC-based cemented carbide ally includes binder phases, hard phases, and γ phases.
The cemented carbide may unintentionally contain other phases, such as free carbon
phases and η phases. The following description, however, proceeds under the assumption
that only the binder phases, hard phases and γ phases exist. In the claims and the
description, the binder phases, hard phases, and γ phases are composed of crystal
grains and their sizes are expressed as crystal grain sizes, where the crystal grain
size refers to the circle equivalent diameter.
(1) Binder phase
[0027] The binder phases are composed of crystal grains that are primarily composed of Co
and can contain W and C, which are components of the hard phases, M and Cr in the
γ phases, and inevitable impurities. These components other than Co are considered
to be present in the form of solid solution in the crystal grains constituting the
binder phases. The crystal grains have fcc and hcp structures. The method of differentiating
these crystalline grains constituting the binder phases will be described below.
(2) Hard phase
[0028] The hard phases consist of crystal grains that are mainly composed of W carbides
and may contain components of the binder phases and γ phases, and Cr and inevitable
impurities. These crystal grains have an hcp structure. The method of identification
of these crystal grains constituting the hard phases will be described below.
[0029] In the hard phases, it is preferable that the ratio C99/C50 of the number cumulative
99% grain size C99 (µm) to the number cumulative 50% grain size C50 (µm) be within
a range from 4.80 to 6.50, for the following reasons: A ratio C99/C50 less than 4.80
leads to an insufficient number of fine crystal grains constituting the hard phases
and a decrease in plastic deformation resistance, whereas a ratio C99/C50 exceeding
6.50 leads to a large difference in grain size (difference in grain diameter) between
the coarse crystal grains and fine crystal grains constituting the hard phases, and
thus formation of large crystal grains constituting the hard phases, resulting in
a reduction in plastic deformation resistance of WC-based cemented carbide. The ratio
C99/C50 is more preferably in the range of 5.30 to 6.30.
[0030] The grain size C50 should preferably be 0.68 µm or less, more preferably be 0.60
µm or less. The lower limit of the number cumulative 50% grain size C50 (µm) may have
any value within the range of a ratio C99/C50 between 4.80 and 6.50 µm. In the case
that the product is manufactured according to one example of the methods described
below, the lower limit is about 0.38 µm. In other words, the number cumulative 50%
grain size C50 (µm) is preferably in the range of 0.38 to 0.68 µm, more preferably
0.38 to 0.60 µm.
[0031] The number cumulative 99% grain size C99 (µm) should preferably be 3.30 µm or less;
a grain size exceeding 3.30 µm leads to a reduction in plastic deformation resistance
of the WC-based cemented carbide. The number cumulative 99% grain size C99 (µm) should
more preferably be 3.20 µm or less. The number cumulative 99% grain size C99 (µm)
may have any lower limit within the range of a ratio C99/C50 between 4.80 µm and 6.50
µm. In the case that the product is manufactured according to one example of the methods
described below, the lower limit of the number cumulative 99% grain size C99 (µm)
is about 2.50 µm. In other words, the number cumulative 99% grain size C99 (µm) is
preferably in the range of 2.50 to 3.30 µm, more preferably 2.50 to 3.20 µm.
[0032] The crystal grains constituting the hard phases are in contact with the crystal grains
constituting the binder phases, the γ-phases, and other hard phases. It is preferred
that the proportion L of the interfacial length in contact with the crystal grains
constituting the binder phases in the total interfacial length of the crystal grains
constituting the hard phases be 35% or more. A proportion of less than 35% leads to
an increase in opportunity of contact between crystal grains constituting the hard
phases and thus ready stress concentration, which results in a decrease in the chipping
resistance of the WC-based cemented carbide. The proportion L is more preferably 40%
or more. The proportion L may have any upper limit. In the case that the product is
manufactured in accordance with one example of the methods described below, the upper
limit of the proportion L is about 55%. In other words, the proportion L is in the
range of preferably 35 to 55%, more preferably 40 to 55%.
[0033] There are no restrictions on the proportion of the crystal grains constituting the
hard phases in contact with the crystal grains constituting the γ phases and the crystal
grains constituting the phases, such as free carbon phases and η phases, unintentionally
generated in the manufacturing process, with the proviso that the proportion of the
interfacial length in contact with the crystal grains constituting the binder phases
in the total interfacial length of the crystal grains constituting the hard phases
is 35% or more.
(3) γ phase
[0034] The γ-phases consist mainly of M carbides (not limited to stoichiometric composition)
and may contain the components of the binder phases, the components of the hard phases,
Cr and inevitable impurities. The γ-phases are composed of crystal grains with an
fcc structure. The method of differentiating crystal grains constituting the γ-phases
will be described below.
3. Rockwell hardness
[0036] The WC-based cemented carbide should preferably have a Rockwell hardness (HRA) in
the range of 88.8 to 90.4. In a Rockwell hardness within this range, the cemented
carbide exhibits more reliable improvements in plastic deformation resistance and
chipping resistance. The Rockwell hardness (HRA) is measured in accordance with ISO
3738-1:1982 and ISO 3738-2:1988.
4. Method of differentiating the binder, hard, and γ phases and crystal grains in
these phases, and measurement of the grain size and the cumulative number of grains
[0037] The binder phases, hard phases, and γ phases, and the crystal grains constituting
these phases are differentiated and the grain size and the cumulative number of grains
are measured as follows.
- (1) Any surface or cross-section of the cemented carbide is smoothed by milling to
remove minute irregularities that interfere with the EBSD measurement. To measure
the size of the crystal grains in each phase, several fields of view (e.g., two fields
of view) are determined on the smoothed surface, each field of view being 90 µm (length)
by 120 µm (width) in size. Each field of view is observed with a field emission scanning
electron microscope (SEM) equipped with an energy dispersive X-ray spectrometer (EDS)
and an electron backscatter diffractometer (EBSD (e.g., OIM Data Collection by AMETEK))
at an acceleration voltage of 15kV with a measuring point interval of 0.1 µm. The
EBSD pattern and EDS data are simultaneously captured.
The milling of the surface or cross-section is performed with, for example, a focused
ion beam (FIB) system.
- (2) The observed results of EBSD measurement are analyzed with software, e.g., OIM
Analysis ver. 7.3.1 by EDAX/TSL. The EDS count values corresponding to elements captured
from all the measuring points inside individual crystal grains are averaged into an
observed EDS value of each element in each crystal grain. The composition of each
crystal grain is then determined from the observed value.
- (3) The phase to which each crystal grain belongs is identified in accordance with
the definition of crystal grains, as described above. In detail, the hard phases are
each defined by an aggregate of crystal grains identified from the EBSD pattern as
having a hcp crystal structure and in which W carbides account for at least 50 atomic%.
The binder phases are each identified as an aggregate of crystal grains with a hcp
or fcc crystal structure. The γ phases are also each identified as an aggregate of
crystal grains with an fcc crystal structure; hence, EBSD measurements alone cannot
differentiate between the binder phases and the γ phases. Thus, the aggregates of
crystal grains having EDS count values of M (V, Ti, Nb, Ta, or Zr) observed by EDS
measurement are determined to be γ phases, and the remaining aggregates of crystal
grains identified as aggregates of crystal grains with an fcc crystal structure are
determined to be binder phases.
- (4) In the case that adjacent measuring points are determined to be in the same phase,
the boundary (midpoint) between those two measuring points is defined as the interface
of the crystal grains if the difference in orientation observed from the measuring
points is at least 5 degrees.
- (5) The crystal grains identified as those constituting the hard phases, the γ phases,
and the binder phases in paragraph (3) are again subjected to EDS measurement to confirm
that the crystal grains identified as constituting the hard phases contain W carbides
in at least 50 atomic%; that the crystal grains identified as constituting the γ phases
contain M carbides in at least 50 atomic%; and that the crystal grains identified
constituting the binder phases contain at least 50 atomic% Co.
- (6) Based on the result of paragraph (5), a graph is created where the size of the
crystal grains constituting the hard phases is taken on the horizontal axis, and the
proportions of the cumulative number of crystal grains constituting the hard phases
corresponding to each grain size on the vertical axis (cumulative number of crystal
grains constituting the hard phases up to each grain size)/(total number of crystal
grains constituting the hard phase) × 100) is taken on the vertical axis.
[0038] The number cumulative 50% grain size C50 (µm), at which the number of cumulative
grains has reached 50%, and the number cumulative 99% grain size C99 (µm), at which
the cumulative count percentage has reached 99%, are determined for each observation
field, and the ratio C99/C50 is calculated by arithmetic averaging of the results.
5. Differentiation of the binder, hard, and γ phases and the crystal grains constituting
them, measurement of the interfacial length, and calculation of proportion of interfacial
length
[0039] The binder, hard, and γ phases and their constituent crystal grains are differentiated,
and the interfacial lengths of the crystal grains constituting each phase are measured
as follows:
- (1) Any surface or cross-section of the cemented carbide is smoothed by milling to
remove minute irregularities that interfere with EBSD measurement. In measurement
of the size of the crystal grains in each phase, several fields of view (e.g., 4 or
5 fields of view) are determined on the smoothed surface, each field of view being,
for example, 37 µm (length) by 47 µm (width) in size. Each field of view is observed
with a field emission scanning electron microscope (SEM) equipped with an energy dispersive
X-ray spectrometer (EDS) and an electron backscatter diffractometer (EBSD (e.g., OIM
Data Collection by AMETEK)) at an acceleration voltage of 15kV with a measuring point
interval of 0.1 µm. The EBSD pattern and EDS data are simultaneously captured.
- (2) The observed results of the EBSD measurement are analyzed with software, e.g.,
OIM Analysis ver. 7.3.1 by EDAX/TSL. The EDS count values corresponding to elements
in individual crystal grains, obtained from all the measuring points inside these
crystal grains are averaged into an observed EDS value of each element in each crystal
grain. The composition of each crystal grain is then derived from the observed value.
- (3) The phase to which each crystal grain belongs is identified in accordance with
the definition of crystal grains, as described above. In detail, the hard phases are
each defined by an aggregate of crystal grains identified from the EBSD pattern as
having a hcp crystal structure and in which W carbides account for at least 50 atomic%.
The binder phases are each identified as an aggregate of crystal grains with an hcp
or fcc crystal structure. The γ phases are also each identified as an aggregate of
crystal grains with an fcc crystal structure; hence, EBSD measurements alone cannot
differentiate between the binder phases and the γ phases. Thus, the aggregates of
crystal grains having EDS count values of M (V, Ti, Nb, Ta, or Zr) observed by EDS
measurement are determined to be γ phases, and the remaining aggregates of crystal
grains identified as aggregates of crystal grains with an fcc crystal structure are
determined to be binder phases.
- (4) In the case that adjacent measuring points are determined to be in the same phase,
the boundary (midpoint) between those two measuring points is defined as the interface
of the crystal grains if the difference in orientation observed from the measuring
points is at least 5 degrees.
- (5) Based on the results of paragraph (3), the total interfacial length of the crystal
grains constituting the hard phases and the interfacial length where the crystal grains
constituting the hard phases are in contact with the crystal grains constituting the
binder phases are calculated in each of the several views, as described above. The
interfacial length is calculated with the aforementioned software, such as OIM Analysis
ver. 7.3.1 from EDAX/TSL, for analysis of the results of the EBSD measurement.
[0040] Finally, the proportion of the interfacial length between the crystal grains constituting
the hard phases and the crystal grains constituting the binder phases to the total
interfacial length of the crystal grains constituting the hard phases is calculated
by arithmetically averaging the observed values obtained for each field of measurement.
6. Measurement of composition
[0042] The contents of W, Co, Cr, M (V, Ta, Nb, Ti, Zr), and C are measured with an electron
beam microanalyzer. Any surface or cross section of the WC-based cemented carbide
is mirror-finished to remove minute irregularities that interfere with measurements
by an electron beam microanalyzer. The sample is then placed into the electron beam
microanalyzer and irradiated with electron beams. For example, three observation fields
of view with a size of 100 µm (length) by 100 µm (width) are selected, and the components
and their contents are determined from the characteristic X-rays emitted from each
observation field, and the results are averaged.
7. Production
[0044] An exemplary method of production will now be described.
[0045] The method involves, preparing predetermined raw powders, and then (1) mixing step,
(2) molding step, (3) sintering step, (4) finishing step, and optional (5) coating
step, in sequence. These processes will be described below.
(1) Mixing step
[0046] In order to produce a WC-based cemented carbide of the embodiment it is desirable
to add WC powder that has been ground and processed into fine particles, and to sinter
the WC particles at relatively low sintering temperature, which suppresses growth
of WC particles, accelerates distribution of Co around WC particles, and thus well
disperse WC particles. Accordingly, it is recommended to perform the following two-stage
mixing:
1) Primary mixing stage
[0047] The primary mixing stage involves pre-grinding a portion of the raw WC powder into
finely ground WC powder. In the primary mixing stage, 20 to 50 mass% of the WC powder
to be used is agitated in a known device, such as an atomizer or ball mill. For example,
mixing conditions using an atomizer preferably includes a rotation speed of 40 to
90 min
-1, a total load of superhard balls of 100 to 300 kg, and a mixing time of 70 to 240
min.
[0048] To yield a WC-based cemented carbide having a more preferred Rockwell hardness in
the range of 88.8 to 90.4, the mixing time should be adjusted within the range of
120 to 240 min.
2) Secondary mixing stage
[0049] In the secondary mixing stage, the remaining WC powder, powder for binder phases,
and powder for γ-phases are added to the ground powder from the primary mixing stage
to produce the composition of the WC-based cemented carbide to be manufactured. These
are mixed in a known device, such as an atomizer or ball mill. Preferred mixing conditions
using an atomizer includes a rotation speed of 40 to 90 min
-1, a total load of cemented carbide balls of 200 to 500 kg, and a mixing time of 70
to 420 min.
[0050] To yield a WC-based cemented carbide having a more preferred Rockwell hardness in
the range of 88.8 to 90.4, the mixing time should be adjusted within the range of
240 to 420 min.
[0051] The raw powder for WC-based cemented carbide that has undergone these two-stage mixing
steps contains a large amount of fine-grained WC powder, which contributes to improved
resistance to plastic deformation. As a result, for the crystal grains constituting
the hard phase, the number cumulative 50% grain size C50 decreases, and the ratio
C99/C50 of the number cumulative 99% grain size C99 to the number cumulative 50% grain
size C50 can be controlled to be within a range of 4.80 to 6.50.
[0052] The two-stage mixing step promotes formation of fresh surfaces on the WC particles,
concentration of Co around the surfaces, and an improvement in sintering ability.
Despite the upper limit of the sintering temperature described later is set to a relatively
low temperature of 1430°C, which suppresses the growth of the hard phases, Co readily
diffuses around the hard phases, forming a WC-based cemented carbide with dispersed
crystal grains constituting the hard phases. For these crystal grains, the number
cumulative 99% grain size C99 can be controlled to 3.30 µm or less and the length
L to 35% or more.
(2) Molding step
[0053] The raw powder material that has undergone the mixing step is shaped into a substrate
with a predetermined shape (e.g., an insert shape conforming to specification CNMG120408).
Molding can be performed, for example, by press molding under a pressure of 100 MPa.
(3) Sintering step
[0054] This process involves sintering the formed raw material. To prevent excess growth
of the crystal grains constituting the hard phases, the maximum holding temperature
is set to 1350 to 1430°C, and the material is held for 50 to 120 minutes under a vacuum
atmosphere of 10
-1 Pa or less. While any cooling rate is available, more preferred is cooling from the
maximum holding temperature to 1100°C to 1200°C at a rate of 35°C/min. A cooling rate
slower than this rate may accelerate growth of the crystal grains forming the hard
phases during the cooling process, potentially leading to coarsening of grains. Thus,
adequate cooling reduces the occurrence of coarse-grained WC caused by abnormal grain
growth of the crystal grains.
[0055] The upper limit for the cooling rate was determined based on the constraints of the
equipment available at the time of filing.
(4) Finishing step
[0056] The sintered compact is ground into the specified shape, for example, the CNMG120408
insert shape defined in ISO Standard 1832:2017. It is noted that the sintered compact
can be ground into any other shape for drills, milling cutters, or end mills.
(5) Coating step
[0057] A predetermined coating layer is formed by any known method.
[0058] The WC-based cemented carbide of this embodiment can be machined into a substrate
with a predetermined shape and used as a cutting tool as it is. Alternately, the cemented
carbide may be coated with a hard layer by any known method to serve as a surface-coated
cutting tool.
The above description is summarized in the following Appendices:
(Appendix 1)
A WC-based cemented carbide comprising: 6.0 to 10.0 mass% Co, 0.08 to 0.90 mass% Cr
(provided that the Cr content (mass%)/Co content (mass%) is 10% or less), 0.0 to 3.8
mass% M (where M is at least one element selected from the group consisting of V,
Ta, Nb, Ti and Zr), 4.5 to 7.5 mass% C, the balance being W and inevitable impurities,
wherein
the cemented carbide comprises binder phases, hard phases, and γ phases,
the binder phases are mainly composed of Co, the hard phases are mainly composed of
W carbide, and the γ phases are mainly composed of M carbide,
in the crystal grains constituting the hard phases, the number cumulative 99% grain
size C99 is 3.30 µm or less, and the ratio C99/C50 of the number cumulative 99% grain
size C99 (µm) to the number cumulative 50% grain size C50 (µm) ranges from 4.80 to
6.50, and
the proportion (L) of the interfacial length of crystal grains constituting the hard
phases in contact with crystal grains constituting the binder phases to the total
interfacial length of crystal grains constituting the hard phases is 35% or more.
(Appendix 2)
The WC-based cemented carbide described in Appendix 1, having a Rockwell hardness
(HRA) in a range of 88.8 and 90.6.
(Appendix 3)
The WC-based cemented carbide described in Appendix 1 or 2, wherein the crystal grains
constituting the hard phases have a number cumulative 50% grain size C50 (µm) of 0.68
or less.
(Appendix 4)
The WC-based cemented carbide described in any one of Appendices 1 to 3, wherein the
proportion (L) of the interfacial length of crystal grains constituting the hard phases
in contact with crystal grains constituting the binder phases to the total interfacial
length of crystal grains constituting the hard phases is 40% or more.
Examples
[0059] The present invention will now be described in more detail with reference to examples
where the cemented carbide of the present invention is used as a cutting tool substrate;
however, the examples should not be construed to limit the present invention.
1. Production of inserts of Examples
(1) Raw Material Powder
[0060] The following raw material powders were prepared:
WC powder with an average particle size as listed in Table 1,
Co powder with an average particle size of 1.0 µm,
Cr3C2 powder with an average particle size of 1.6 µm,
TiC powder with an average particle size of 1.0 µm,
TaC powder with an average particle size of 1.9 µm,
NbC powder with an average particle size of 1.1 µm,
ZrC powder with an average particle size of 1.2 µm, and
VC powder with an average particle size of 1.7 µm.
These powders were blended according to the formulation A to G and A' to E' shown
in Table 1.
[0061] The average particle size of each raw material powder is the Fischer size measured
by an air permeation method with a Fischer sub-sieve classifier.
(2) Mixing step, molding step, sintering step, and finishing step
[0062] As described above, the mixing step, molding step, sintering step, and finishing
step were performed in sequence.
[0063] In the primary mixing stage, the WC powder was mixed and ground according to the
formulation (mass %) and mixing times shown in Tables 2 and 3, based on the average
particle size of the WC powder listed in Table 1 to yield finely ground WC powder.
In the secondary mixing stage the WC powder after the primary mixing stage was mixed
with the remaining WC powder not processed in the primary mixing stage (100 - the
mass% of WC powder consumed in the primary mixing stage), raw material powder for
the hard phase, and raw material powder for the binder phase for the mixing time specified
in Tables 2 and 3. The raw powder after the secondary mixing stage was press-molded
into green compacts with a shape of CNMG120408 insert under a pressure of 100 MPa.
In the subsequent sintering step, the green compacts were sintered at holding temperatures
and times shown in Tables 2 and 3 (some of the examples were cooled at cooling rates
shown in Table 3). In the finishing step, the sintered compacts were ground to produce
inserts with the specified CNMG120408 shape. The inserts were analyzed by the method
described above. The results are shown in Table 4.
2. Production of inserts of Comparative Examples
[0064] For comparison, raw powders were prepared according to the formulations A to E, G,
and B' shown in Table 1. The mixtures were then subjected to the mixing step, molding
step, sintering step, and finishing step in sequence.
[0065] In the mixing step, WC powder at the proportion shown in Tables 2 and 3 was mixed
in the primary mixing stage (in Table 2, Comparative Examples where the primary mixing
stage is indicated as "-" had no primary mixing stage and only a secondary mixing
stage). After the mixing step, the raw powder was press-molded into green compacts
with an insert shape of CNMG120408 under a pressure of 100 MPa. The green compacts
were then sintered at holding temperatures and time shown in Tables 2 and 3 (some
of the Comparative Examples were cooled at cooling rates shown in Table 3). In the
finishing step, the sintered compacts were grounded to produce inserts with a specified
shape of CNMG120408. The inserts were analyzed by the method described above. The
results are shown in Table 5.
3. Formation of Coating Layer
[0066] On the surface of each insert of Examples and Comparative Examples, a TiN layer (average
thickness 0.2 µm), a TiCN layer (average thickness 3.5 µm), an Al
2O
3 layer (average thickness 2.5 µm), and a TiN (average thickness 0.2 µm) were formed
in sequence by chemical vapor deposition into a coating layer.
[Table 1]
| Row powder |
Formulation (mass%) |
WC mean grain size (µm) |
| Co |
Cr3C2 |
VC |
TaC |
NbC |
TiC |
ZrC |
WC |
| A |
9.2 |
0.4 |
- |
1.4 |
- |
- |
0.1 |
Balance |
2.5 |
| B |
8.4 |
0.6 |
- |
- |
0.9 |
0.4 |
- |
Balance |
2.5 |
| C |
7.6 |
0.2 |
0.2 |
- |
0.7 |
- |
- |
Balance |
2.5 |
| D |
6.9 |
0.4 |
- |
0.6 |
- |
0.1 |
- |
Balance |
2.5 |
| E |
9.8 |
0.5 |
- |
1.2 |
0.8 |
- |
- |
Balance |
2.5 |
| F |
9.3 |
0.3 |
0.3 |
1.1 |
0.7 |
0.6 |
0.1 |
Balance |
2.5 |
| G |
9.0 |
- |
- |
1.3 |
- |
- |
0.1 |
Balance |
2.5 |
| A' |
9.2 |
0.4 |
- |
1.4 |
- |
- |
0.1 |
Balance |
4.5 |
| B' |
8.4 |
0.6 |
- |
- |
0.9 |
0.4 |
- |
Balance |
4.5 |
| C' |
7.6 |
0.2 |
0.2 |
- |
0.7 |
- |
- |
Balance |
4.5 |
| D' |
6.9 |
0.4 |
- |
0.6 |
- |
0.1 |
- |
Balance |
4.5 |
| E' |
9.8 |
0.5 |
- |
1.2 |
0.8 |
- |
- |
Balance |
4.5 |
[0067] In Table 1, the symbol "-" indicates that the component was not included in the formulation.

[0068] In Table 2, the symbol "-" indicates that the primary mixing stage was not performed.
[Table 3]
| Step |
Raw powder |
Primary mixing stage |
Secondary mixing stage |
Sintering conditions (Main sintering) |
| WC powder content (mass%) |
Mixing time (min) |
Mixing time (min) |
Holding temp. (°C) |
Holding time (min) |
Cooling rate (°C/min) |
| Step of Example |
11 |
F |
35 |
120 |
120 |
1380 |
80 |
40 |
| 12 |
A' |
40 |
180 |
360 |
1380 |
60 |
50 |
| 13 |
B' |
35 |
150 |
270 |
1410 |
75 |
40 |
| 14 |
C' |
30 |
240 |
360 |
1410 |
90 |
45 |
| 15 |
D' |
25 |
120 |
240 |
1430 |
60 |
35 |
| 16 |
E' |
45 |
150 |
300 |
1360 |
90 |
30 |
| Step of Comparative Example |
9' |
B' |
10 |
120 |
240 |
1420 |
90 |
30 |
[Table 4]
| Example |
Raw Powder |
Formulation (mass%) |
Cr content/Co content (%) |
C50 (µm) |
C99 (µm) |
C99/C50 |
L (%) |
Rockwell hardness (HRA) |
| Co |
Cr |
V |
Ta |
Nb |
Ti |
Zr |
C |
W |
| 1 |
A |
9.2 |
0.35 |
- |
1.3 |
- |
- |
0.1 |
4.9 |
Balance |
4 |
0.49 |
2.79 |
5.69 |
48.3 |
89.5 |
| 2 |
B |
8.4 |
0.52 |
- |
- |
0.8 |
0.3 |
- |
5.4 |
Balance |
6 |
0.51 |
2.76 |
5.41 |
44.2 |
89.7 |
| 3 |
C |
7.6 |
0.17 |
0.2 |
- |
0.6 |
- |
- |
5.7 |
Balance |
2 |
0.5 |
2.72 |
5.44 |
41.9 |
89.9 |
| 4 |
D |
6.8 |
0.35 |
- |
0.6 |
0.6 |
0.1 |
- |
6.7 |
Balance |
5 |
0.47 |
2.67 |
5.68 |
38.2 |
90.3 |
| 5 |
E |
9.8 |
0.43 |
- |
1.1 |
0.7 |
- |
- |
4.7 |
Balance |
4 |
0.58 |
3.04 |
5.24 |
51.8 |
88.9 |
| 6 |
A |
9.2 |
0.35 |
- |
1.3 |
- |
- |
0.1 |
4.8 |
Balance |
4 |
0.58 |
2.82 |
4.86 |
47.8 |
89.4 |
| 7 |
B |
8.4 |
0.52 |
- |
- |
0.8 |
0.3 |
- |
5.5 |
Balance |
6 |
0.54 |
2.73 |
5.06 |
42.9 |
89.8 |
| 8 |
C |
7.6 |
0.17 |
0.2 |
- |
0.6 |
- |
- |
5.7 |
Balance |
2 |
0.52 |
2.74 |
5.27 |
43.8 |
89.8 |
| 9 |
D |
6.8 |
0.35 |
- |
0.6 |
0.6 |
0.1 |
- |
6.6 |
Balance |
5 |
0.47 |
2.62 |
5.57 |
35.9 |
90.9 |
| 10 |
E |
9.8 |
0.43 |
- |
1.1 |
0.7 |
- |
- |
4.8 |
Balance |
4 |
0.58 |
3.16 |
5.45 |
51.6 |
88.5 |
| 11 |
G |
9.3 |
0.29 |
0.2 |
1.0 |
0.7 |
0.5 |
0.1 |
5.6 |
Balance |
3 |
0.54 |
3.21 |
5.94 |
52.4 |
89.6 |
| 12 |
A' |
9.2 |
0.35 |
- |
1.3 |
- |
- |
0.1 |
4.9 |
Balance |
4 |
0.5 |
2.96 |
5.92 |
49.4 |
89.5 |
| 13 |
B' |
8.4 |
0.52 |
- |
- |
0.8 |
0.3 |
- |
5.4 |
Balance |
6 |
0.48 |
3.08 |
6.42 |
48.6 |
89.7 |
| 14 |
C' |
7.6 |
0.17 |
0.2 |
- |
0.6 |
- |
- |
5.7 |
Balance |
2 |
0.47 |
2.82 |
6.00 |
44.2 |
90.1 |
| 15 |
D' |
6.8 |
0.35 |
- |
0.6 |
0.6 |
0.1 |
- |
6.7 |
Balance |
5 |
0.51 |
3.14 |
6.16 |
42.1 |
90.4 |
| 16 |
E' |
9.8 |
0.43 |
- |
1.1 |
0.7 |
- |
- |
4.7 |
Balance |
4 |
0.53 |
3.02 |
5.70 |
49.8 |
89.3 |
[0069]
[Table 5]
| Compartive Example |
Raw powder |
Formulation (mass%) |
Cr content/Co content (%) |
C50 (µm) |
C99 (µm) |
C99/C50 |
L (%) |
Rockwell hardness (HRA) |
| Co |
Cr |
v |
Ta |
Nb |
Ti |
Zr |
C |
W |
| 1' |
A |
9.2 |
0.35 |
- |
1.3 |
- |
- |
0.1 |
5.6 |
Balance |
4 |
0.84 |
3.21 |
3.82 |
39.2 |
88.9 |
| 2' |
B |
8.4 |
0.52 |
- |
- |
0.8 |
0.3 |
- |
5.8 |
Balance |
6 |
0.73 |
3.08 |
4.22 |
38.1 |
89.3 |
| 3' |
C |
7.6 |
0.17 |
0.2 |
- |
0.6 |
- |
- |
5.7 |
Balance |
2 |
0.69 |
2.92 |
4.23 |
34.6 |
89.7 |
| 4' |
D |
6.8 |
0.35 |
- |
0.6 |
0.6 |
0.1 |
- |
5.8 |
Balance |
5 |
0.62 |
2.62 |
4.23 |
31.8 |
90.2 |
| 5' |
E |
9.8 |
0.43 |
- |
1.1 |
0.7 |
- |
- |
5.6 |
Balance |
4 |
0.86 |
2.93 |
3.41 |
37.2 |
88.7 |
| 6' |
G |
9.1 |
- |
- |
1.2 |
0.5 |
- |
0.1 |
5.6 |
Balance |
0 |
0.53 |
2.62 |
4.94 |
30.2 |
89.5 |
| 7' |
A |
9.2 |
0.35 |
- |
1.3 |
- |
- |
0.1 |
5.6 |
Balance |
4 |
0.47 |
2.38 |
5.06 |
32.9 |
90.7 |
| 8' |
B |
8.4 |
0.52 |
- |
- |
0.8 |
0.3 |
- |
5.8 |
Balance |
6 |
0.59 |
2.79 |
4.73 |
37.1 |
88.9 |
| 9' |
B' |
8.4 |
0.50 |
- |
- |
0.8 |
0.4 |
- |
5.9 |
Balance |
6 |
0.64 |
3.48 |
5.44 |
42.5 |
88.7 |
[0070] In Tables 4 and 5, the symbol "-" indicates that the component was not formulated.
The contents of inevitable impurities in all Examples and Comparative Examples were
0.3 mass% or less, calculated as a percentage in the entire WC-based cemented carbide
(100 mass%).
[0071] Cutting tests were then conducted for 15 minutes each on Examples 1 to 16 and Comparative
Examples 1' to 9' under the cutting conditions 1 to 4 below. Every minute after the
start of the cutting test, each sample was visually observed for checking of chipping
and detachment due to plastic deformation and for measurement of the width of the
flank wear. For samples where the width of the flank wear exceeded 0.2 mm, the elapsed
time since the start of testing (measuring time) corresponding to the wear width exceeding
0.2 mm was determined by fitting a straight line between that wear width and the wear
width measured at the immediately preceding measuring time. This yielded the elapsed
time since the start of testing (time to end of service life) corresponding to a 0.2
mm width of the flank wear. The results are shown in Tables 6 to 9.
Cutting Condition 1 (High-Speed, High-Feed Cutting)
[0072]
Workpiece Material: stainless steel SUS304 round bar, outer diameter 100 mm
Cutting Speed: 150 m/s
Depth of Cut: 1.5 mm
Feed Per Revolution: 0.3 mm
Wet Cutting
Cutting Condition 2
[0073]
Workpiece Material: stainless steel SUS316 round bar, outer diameter 100 mm
Cutting Speed: 150 m/s
Depth of Cut: 2.0 mm
Feed Per Revolution: 0.2 mm
Wet Cutting
Cutting Condition 3
[0074]
Workpiece Material: stainless steel SUS630 round bar, outer diameter 100 mm
Cutting Speed: 120 m/s
Depth of Cut: 2.0 mm
Feed Per Revolution: 0.15 mm
Wet Cutting
Cutting Condition 4 (intermittent cutting)
[0076] Tables 6 to 9 evidentially demonstrate that all Examples exhibit low flank wear,
no chipping or detachment due to plastic deformation, and thus excellent cutting performance
even during interrupted cutting or high-speed, high-feed machining.
In contrast, all Comparative Examples exhibit either chipping or detachment due to plastic
deformation before the end of the cutting test time (15 minutes) and a width of the
flank wear of 0.2 mm, resulting in the end of the service life.
[0077] The above-disclosed embodiments are merely illustrative in all respects and are not
restrictive. The scope of the present invention is defined by the claims, not by the
above-disclosed embodiments, and is intended to include meanings equivalent to the
claims and all modifications within the scope of the claims.