WO2022210604A1 - 刃物 - Google Patents

刃物 Download PDF

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Publication number
WO2022210604A1
WO2022210604A1 PCT/JP2022/015188 JP2022015188W WO2022210604A1 WO 2022210604 A1 WO2022210604 A1 WO 2022210604A1 JP 2022015188 W JP2022015188 W JP 2022015188W WO 2022210604 A1 WO2022210604 A1 WO 2022210604A1
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WO
WIPO (PCT)
Prior art keywords
hard particles
metal
cutting edge
base portion
edge portion
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Ceased
Application number
PCT/JP2022/015188
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English (en)
French (fr)
Japanese (ja)
Inventor
康二 櫻井
孝典 西原
圭輔 土屋
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Kyocera Corp
Original Assignee
Kyocera Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Kyocera Corp filed Critical Kyocera Corp
Priority to JP2023511303A priority Critical patent/JPWO2022210604A1/ja
Priority to US18/553,421 priority patent/US20240190029A1/en
Publication of WO2022210604A1 publication Critical patent/WO2022210604A1/ja
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B26—HAND CUTTING TOOLS; CUTTING; SEVERING
    • B26B—HAND-HELD CUTTING TOOLS NOT OTHERWISE PROVIDED FOR
    • B26B9/00—Blades for hand knives
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K26/00—Working by laser beam, e.g. welding, cutting or boring
    • B23K26/34—Laser welding for purposes other than joining
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B24—GRINDING; POLISHING
    • B24B—MACHINES, DEVICES, OR PROCESSES FOR GRINDING OR POLISHING; DRESSING OR CONDITIONING OF ABRADING SURFACES; FEEDING OF GRINDING, POLISHING, OR LAPPING AGENTS
    • B24B3/00—Sharpening cutting edges, e.g. of tools; Accessories therefor, e.g. for holding the tools
    • B24B3/36—Sharpening cutting edges, e.g. of tools; Accessories therefor, e.g. for holding the tools of cutting blades
    • B24B3/54—Sharpening cutting edges, e.g. of tools; Accessories therefor, e.g. for holding the tools of cutting blades of hand or table knives

Definitions

  • the present disclosure relates to a blade with excellent wear resistance.
  • the blade of the present disclosure includes a blade having a base portion and a cutting edge portion connected to an end portion of the base portion.
  • the base portion includes a first metal
  • the cutting edge portion includes a second metal and hard particles having higher hardness than the second metal.
  • the hard particles include first hard particles having a particle size of 20 ⁇ m or more and 50 ⁇ m or less and having an angular polyhedral shape.
  • Another blade of the present disclosure includes a blade having a base portion and a cutting edge portion connected to an end of the base portion.
  • the base includes a first metal
  • the cutting edge includes a second metal and hard particles having higher hardness than the second metal.
  • An interface portion having a larger crystal grain size than that of the cutting edge portion is provided between the base portion and the cutting edge portion.
  • FIG. 1 is a plan view of a blade according to an embodiment of the present disclosure
  • FIG. FIG. 2 is a view of the cutting tool in FIG. 1 as seen from the cutting edge side
  • 3 is an enlarged cross-sectional view of the Zm region of FIG. 2
  • FIG. FIG. 4 is an explanatory diagram showing a build-up process for forming a cutting edge portion on a base portion of a cutting tool
  • 4B is a front view of the base portion shown in FIG. 4A
  • FIG. 1 is a scanning electron microscope (hereinafter referred to as SEM) photograph (magnification: 100 times) of tungsten carbide (WC) powder used as a raw material for hard particles.
  • SEM scanning electron microscope
  • FIG. 5 is an SEM photograph showing a state in which a built-up portion for forming a cutting edge portion is formed on the end portion of the base portion by the method shown in FIG. 4; It is a SEM photograph which shows the cutting edge part after sharpening. It is a SEM photograph (magnification: 40 times) which shows the edge part after sharpening.
  • FIG. 8B is a SEM photograph (magnification: 2000 times) showing an enlarged portion A of FIG. 8A. It is an SEM photograph (magnification: 9000 times) which shows the B section of FIG. 8B expanded.
  • FIG. 4 is an SEM photograph showing a boundary region between a base portion and a build-up portion; It is a SEM photograph which shows an enlarged interface part interposed between a base part and a build-up part. It is a SEM photograph which shows the continuous measurement direction of Vickers hardness. 4 is a graph showing measurement results of Vickers hardness distribution. It is a SEM photograph (magnification: 3000 times) which shows the enlarged cross section of the cutting edge part which formed the indentation for Vickers hardness measurement. 14 is a SEM photograph (magnification: 8000 times) showing an enlarged portion A of FIG. 13.
  • FIG. 4 is a SEM photograph (magnification: 1800 times) showing a state in which an indentation for Vickers hardness measurement is formed on nickel (Ni) used as a second metal.
  • the blade 1 of the present disclosure includes a blade 1a and a handle 1b connected to the blade 1a.
  • the blade 1a is set to have a shape and size suitable for the use of the blade 1.
  • the shape of the blade 1a includes, for example, the shape of a Japanese kitchen knife such as a Deba knife or a Santoku knife, a Western knife such as a beef knife, or a Chinese knife.
  • the blade 1 is used for a knife, surgical instrument, or other application other than kitchen knives, it may have any shape as long as it is suitable for the application.
  • the handle 1b connected to the blade 1a is to be gripped by a person when using the blade 1, and is set to a shape and size suitable for the use of the blade 1, similar to the blade 1a.
  • the blade 1a and the handle 1b may be formed integrally or separately. Further, the blade 1 is not limited to having the handle 1b, and may be composed only of the blade 1a. In this embodiment, the blade 1a and the handle 1b are formed separately, and a portion of the blade 1a is inserted into the handle 1b and fixed to the handle 1b at the insertion portion. A part of the blade 1a may be welded to the metal handle 1b.
  • the handle 1b includes wood, resin, ceramics or metal material.
  • a rust-resistant material such as a titanium-based or stainless steel-based material may be used.
  • the resin for example, ABS resin (a copolymer of acrylonitrile, butadiene and styrene) or polypropylene resin may be used.
  • the blade 1 a has a base portion 3 and a cutting edge portion 2 connected to the base portion 3 .
  • the base portion 3 contains a first metal.
  • the first metal for example, steel, synthetic steel, stainless steel, titanium alloy, etc. may be used. Synthetic steels may use materials including, for example, chromium, molybdenum, vanadium, tungsten, cobalt, copper, combinations thereof, and the like. Any of chromium-nickel-based and chromium-based stainless steels may be used.
  • As the titanium alloy for example, a so-called 64 titanium alloy containing 6% aluminum (Al) and 4% vanadium (V) may be used. When the first metal is stainless steel, the corrosion resistance of the base portion 3 against rust can be improved.
  • the first metal is the main component of the base portion 3.
  • the main component means a component exceeding 70% by mass out of 100% by mass of all components constituting the base portion 3 .
  • the base portion 3 has an exposed portion 30 exposed from the handle 1b and a core 3E inserted inside the handle 1b.
  • the exposed portion 30 has an end portion 3C and a back portion 3A extending along its length direction (x-axis direction), and the width of the exposed portion 30 is narrowed near the tip of the exposed portion 30 in the length direction.
  • the end portion 3C and the back portion 3A are connected at the tip of the exposed portion 30.
  • the edge portion 2 is connected to the end portion 3C of the exposed portion 30 along the end portion 3C.
  • the core 3E is narrower in the width direction (y-axis direction) than the exposed portion 30, and is inserted inside the handle 1b.
  • the core 3E in this embodiment has one or more holes 3Ea, and the blade 1a and the handle 1b are firmly fixed by inserting a part of the handle 1b into the holes 3Ea.
  • the base portion 3 and the handle 1b may be integrated by welding.
  • the cutting edge portion 2 includes a second metal 2a and a plurality of hard particles 4.
  • the second metal 2a may be made of a material different from that of the first metal, or may be made of the same material.
  • the second metal 2a is made of a material different from that of the first metal.
  • a metal material suitable for the cutting edge portion 2 can be selected without being restricted by the material of the base portion 3 .
  • the material of the second metal 2a for example, stainless steel, nickel, titanium, a nickel alloy, a titanium alloy, or the like can be used, and furthermore, an alloy of nickel, chromium, and iron (for example, Inconel (registered trademark)), nickel, and silicon. and boron alloys (eg Colmonoy®), or alloys of titanium, aluminum and vanadium may also be used.
  • the corrosion resistance is relatively high, and the thermal stress remaining in the cutting edge 2 can be reduced when a laser is used in the manufacturing method.
  • the second metal 2a is made of Ni-based colmonoy, it is possible to suppress deterioration in strength due to quenching and annealing of the blade edge during manufacture of the blade 1.
  • the Ni-based colmonoy contains 0.06% by mass or less of carbon, 0.8% by mass or less of iron, 2.4-3.0% by mass of silicon, and 1.6-2.00% by mass of boron with respect to the total amount of the Ni-based colmonoy. %, oxygen not more than 0.08% by mass, and the balance being nickel.
  • the second metal 2a forms a metal matrix as a main component of the cutting edge 2, and hard particles are present in this matrix.
  • the main component means a component exceeding 50% by mass out of 100% by mass of all components constituting the cutting edge portion 2 . Since the second metal 2a is the main component of the cutting edge portion 2, the durability of the cutting edge portion 2 can be further improved.
  • the plurality of hard particles 4 contained in the cutting edge portion 2 have higher Vickers hardness than the second metal 2a contained in the cutting edge portion 2 . Therefore, the hardness of the entire cutting edge portion 2 can be increased, and the wear resistance of the cutting edge portion 2 can be improved.
  • the hard particles 4 are made of a material harder than the second metal 2a, the hard particles 4 come into contact with the object when the blade 1 is used, thereby improving the sharpness of the cutting edge 2 with respect to the object.
  • the hard particles 4 are made of a material that is not only harder than the second metal 2a, but also harder than the first metal.
  • the hard particles 4 may have a Vickers hardness of, for example, 1000 Hv or more and 4000 Hv or less.
  • the Vickers hardness of the hard particles 4, the first metal and the second metal 2a can be measured using a method according to JIS Z 2244 (ISO6507-2, hereinafter the same).
  • the hard particles 4 are preferably exposed on the surface of the cutting edge portion 2. Furthermore, in order to make it easier for the hard particles 4 to be exposed on the surface of the cutting edge portion 2 even when the cutting edge portion 2 is polished, the hard particles 4 are distributed inside the cutting edge portion 2 in the length direction (x-axis direction) of the base portion 3. And it is preferable that they are dispersed not only in the width direction (y-axis direction) but also in the thickness direction (z-axis direction) of the base portion 3 .
  • the hard particles 4 include cemented carbide containing tungsten carbide (WC), cermet containing titanium carbide (TiC), titanium nitride (TiN), tantalum carbide (TaC), vanadium carbide (VC), and the like. Moreover, as the hard particles 4, a mixture of a plurality of types such as tungsten carbide and titanium carbide may be used.
  • the hard particles 4 preferably contain first hard particles 41 having an angular polyhedral shape (see FIG. 8B), which can improve the wear resistance of the cutting edge 2 .
  • the shape of the hard particles 4 includes polygonal shapes such as a triangular shape, a square shape, and a trapezoidal shape in a cross-sectional view. Any shape can also be used.
  • FIG. 5 shows the raw material powder shape of the hard particles 4 .
  • the first hard particles 41 having an angular polyhedral shape and having a particle size of 20 ⁇ m or more and 50 ⁇ m or less are contained in the matrix of the second metal 2a in an area ratio of the cross section of 3% or more.
  • the first hard particles 41 having such a relatively large particle size are easily cracked, but in the present disclosure, since the first hard particles 41 exist in the matrix of the second metal 2a, cracking can be blocked by the matrix, it has become possible to use hard particles 4 having a relatively large particle size.
  • wear resistance is improved by setting the particle size of the first hard particles 41 to 20 ⁇ m or more.
  • the particle size of the first hard particles 41 As described above, for example, a sieve may be used to select particles with a particle size of less than 20 ⁇ m and particles with a particle size of more than 50 ⁇ m. The percentage of particles in the area ratio of the cross section is measured by calculating the area of hard particles using software "Image J".
  • the hard particles 4 preferably contain particles (first hard particles 41) having a particle size (average particle size, hereinafter the same) of 20 ⁇ m or more and 50 ⁇ m or less.
  • first hard particles 41 having a particle size (average particle size, hereinafter the same) of 20 ⁇ m or more and 50 ⁇ m or less.
  • the hard particles 4 may contain particles (second hard particles 42 to be described later) having a particle size of 2 ⁇ m or more and 10 ⁇ m or less. By dispersing such fine hard particles 42 in the cutting edge portion, the strength of the cutting edge portion is improved, and the wear resistance is also improved.
  • the hard particles 4 may contain particles (third hard particles 43 to be described later) crystallized in a dendrite form from the matrix of the second metal 2a. The shedding of the hard particles 43 can be prevented by the anchoring effect of such dendritic particles.
  • the hard particles 4 may be contained in the cutting edge portion 2 in an amount of 10% by mass or more. At that time, the hard particles 4 having a particle size outside the range of 20 ⁇ m or more and 50 ⁇ m or less may be included, but the hard particles 4 having a particle size of 20 ⁇ m or more and 50 ⁇ m or less are 3% in terms of the area ratio of the cross section as described above. It is preferable that the above is included. As a result, sharpness and wear resistance of the cutting edge portion 2 can be further improved. Further, the hard particles 4 may be contained in the cutting edge portion 2 in an amount of 50% by mass or less. In this case, high productivity of the cutting edge portion 2 can be maintained.
  • the content of the hard particles 4 having a particle size of 20 ⁇ m or more and 50 ⁇ m or less is preferably 32% or less in terms of area ratio of the cross section.
  • the content of the hard particles 4 is obtained by observing the cross section of the cutting edge 2 (cross section parallel to the yz plane) using an SEM, and from the photograph of the observed image, the total amount of the hard particles 4 with respect to the entire area of the cutting edge 2. can be obtained as area %.
  • the cutting edge portion 2 has a cutting edge 2A and a pair of side surfaces 2c arranged on both sides of the cutting edge 2A and connected to the cutting edge 2A. At least one of the plurality of hard particles 4 is exposed from the side surface 2 c of the cutting edge portion 2 .
  • the hard grains 4 come into contact with the object.
  • the sharpness of the cutting edge portion 2 is improved, and the wear resistance of the cutting edge portion 2 can be improved.
  • at least one of the hard particles 4 is preferably exposed from the cutting edge 2A. Therefore, when the blade 1 is used to cut an object, the hard particles 4 exposed from the blade edge 2A come into contact with the object, and the sharpness of the blade edge 2A can be improved.
  • the cutting tool 1 includes a step of preparing the base portion 3 containing the first metal, a step of preparing the metal powder 2a1 and the hard particles 4 constituting the second metal, and a step of applying the metal to the end 3C of the base portion 3.
  • a step of preparing the base portion 3 containing the first metal By firing the metal powder 2a1 while injecting the powder 2a1 and the hard particles 4, a built-up portion 6 for forming the cutting edge portion 2 containing the second metal as a main component and a plurality of hard particles 4 is formed. and a step of polishing the build-up portion 6 or the build-up portion 6 and the base portion 3 .
  • Each step will be described in order below.
  • the base portion 3 containing the first metal is prepared.
  • the base portion 3 has a shape as shown in FIGS. 4A and 4B.
  • the hardness of the base body 3 can be increased by performing quenching after stamping a plate material such as stainless steel and punching out a mold for a predetermined cutting tool.
  • FIG. 5 shows the shape of tungsten carbide (WC) powder as an example of raw material powder forming the hard particles 4 .
  • the raw material powder of the hard particles 4 preferably contains pulverized particles having a particle size of 20 ⁇ m or more and 50 ⁇ m or less and having an angular surface.
  • the metal powder 2a1 is sprayed onto the end portion 3C. burn. Thereby, the build-up portion 6 for forming the cutting edge portion 2 including the second metal 2a and the plurality of hard particles 4 is formed.
  • the metal powder 2a1 is preferably melted by a laser and baked. That is, it is preferable to use a cladding technique using a laser. Specifically, as shown in FIG. 4A, while irradiating the vicinity of the end portion 3C of the base portion 3 with a laser beam 7 indicated by an arrow, the powder mixture 5 (cladding material) containing the metal powder 2a1 is applied to the end portion. Feed on part 3C. In this state, the base portion 3 is relatively moved along its length direction (x direction shown in FIG. 1) with respect to the irradiation position of the laser beam 7 .
  • the mixed powdery-granular material 5 is irradiated with the laser beam 7 (two lasers in this embodiment) to melt the mixed powdery-granular material 5, thereby forming the build-up portion 6 at the end portion 3C of the base portion 3. Therefore, the base portion 3 is difficult to dissolve, and the mole pool is suppressed. Further, it is preferable to blow an inert gas from the outside of the mixed granular material 5 to the end portion 3C. This makes it easier for the mixed granular material 5 to hit the laser beam 7 . Examples of inert gas include argon gas. As shown in FIG. 4B, the end portion 3C of the base portion 3 preferably has a width W of 0.3 mm or more and 1.0 mm or less. not to be
  • the mixed granular material 5 When the mixed granular material 5 is irradiated with the laser beam 7, the mixed granular material 5 other than the hard particles 4 is melted and adheres to the end portion 3C. On the other hand, since the hard particles 4 have a high melting point, they are difficult to be melted by the laser beam 7 . Therefore, when the mixed powder 5 is dissolved, it is possible to obtain the build-up portion 6 in which the plurality of hard particles 4 are dispersed in the cutting edge portion 2 . As will be described later, some of the hard particles 4 are solid-dissolved in the matrix during the build-up process, and the hard particles 4 are crystallized from the supersaturated solid-solution matrix.
  • FIG. 6 is a SEM photograph showing an example of the built-up portion 6 formed on the end portion 3C of the base portion 3 as described above.
  • part of the build-up portion 6 is ground. Only the build-up portion 6 may be polished, or not only the build-up portion 6 but also a part of the base portion 3 may be polished. Polishing can be performed using, for example, a polishing stone whose surface is coated with aluminum oxide (Al 2 O 3 ), silicon carbide (SiC) or diamond, mixed particles of silicon carbide (SiC) or diamond, or the like. Further, the polishing may be performed in multiple steps.
  • FIG. 7 is an SEM photograph showing the cutting edge 2A portion of the cutting edge portion 2 thus created. As is clear from the figure, the hard particles 4 are exposed at the tip and both side surfaces of the cutting edge 2A. 2 sharpness is improved.
  • FIGS. 6 and 7 Materials used in FIGS. 6 and 7 are as follows.
  • Base portion 3 stainless steel
  • Composition Ceramics mainly composed of tungsten carbide Mesh particle size: 45 ⁇ m Content in build-up portion 6: 30% by mass
  • FIG. 8A is an SEM photograph showing the build-up portion 6 formed in the same manner as the build-up portion 6 shown in FIG. 6, and FIG. 8B is an enlarged SEM photograph of the portion A in FIG. 8A.
  • FIG. 9 is an enlarged SEM photograph of the B portion in FIG. 8B. 8B and 9 show that three types of first, second and third hard particles 41, 42 and 43 having different shapes are present in the buildup portion 6.
  • FIG. 8A is an SEM photograph showing the build-up portion 6 formed in the same manner as the build-up portion 6 shown in FIG. 6, and FIG. 8B is an enlarged SEM photograph of the portion A in FIG. 8A.
  • FIG. 9 is an enlarged SEM photograph of the B portion in FIG. 8B. 8B and 9 show that three types of first, second and third hard particles 41, 42 and 43 having different shapes are present in the buildup portion 6.
  • FIG. 8A is an SEM photograph showing the build-up portion 6 formed in the same manner as the build-up portion 6 shown in FIG.
  • the first hard particles 41 have a particle size of 20 ⁇ m or more and 50 ⁇ m or less and have an angular polyhedral shape.
  • the first hard particles 41 retain the shape of the raw material powder of the hard particles (WC) to some extent.
  • the presence of such coarse first hard particles 41 improves the wear resistance of the cutting edge 2 .
  • a large number of acicular hard particles 411 are precipitated from around the first hard particles 41, whereby the hard particles in the matrix of the second metal 2a It has a higher concentration (ie, a larger surface area).
  • the presence of such needle-like hard particles 411 functions as an anchor effect of the coarse first hard particles 41, which can prevent shedding of the hard particles 41 and enable long-term use.
  • the first hard particles 41 are formed by the raw material powder-sized hard particles 4 not being dissolved during processing and being present in the build-up as they are.
  • the second hard particles 42 are fine hard particles with a particle size of 2 ⁇ m or more and 3 ⁇ m or less. By dispersing such fine second hard particles 42 in the matrix of the second metal 2a, the strength of the cutting edge 2 is improved and the wear resistance is improved. It is presumed that the second hard particles 42 are obtained by pulverizing the raw material powder, making it finer and dispersing it. The second hard particles 42 are formed by grinding raw powder-sized hard particles during processing.
  • the third hard particles 43 are shown in FIG. 9, which is an enlarged view of part B of FIG. 8B. That is, the third hard particles 43 are obtained by crystallizing a part of the hard particles 4 in a dendrite form from the matrix of the second metal 2a. It is presumed that part of the raw material powder of the hard particles 4 solid-dissolves in the matrix of the second metal 2a during the build-up process, and crystallizes in the form of dendrites due to cooling of the supersaturated solid-solution matrix. .
  • the dendritic crystallization of the third hard particles 43 can be expected to have an anchor effect, and the shedding of the third hard particles 43 can be prevented.
  • the first, second and third hard particles 41 , 42 , 43 are present in the buildup portion 6 . It is presumed that this is because the raw material powder of the hard particles 4 has a particle size that is relatively large, the hard particles are easily pulverized, and the energy during processing locally has enough energy to dissolve the hard particles. Moreover, all three kinds of hard particles 41, 42, 43 do not need to be present in one built-up portion 6, and at least one kind of hard particles 41, 42, 43 may be present.
  • FIG. 10 is an SEM photograph (magnification: 2,000 times) for showing in detail the structure of the boundary region between the base portion 3 and the build-up portion 6, and the SEM photograph P2 is an enlarged portion A of the SEM photograph P1. , and is shown by stitching together a plurality of SEM photographs (magnification: 2,000 times).
  • an interface portion 8 having a larger crystal grain size than that of the cutting edge portion 2 is formed between the base portion 3 and the build-up portion 6 .
  • the crystal grains of the interface portion 8 have an average crystal grain size of 1.2 times or more and an area ratio of the crystal grains of 2 times or more that of the crystal grains of the cutting edge portion 2 .
  • the crystal grain size can be calculated by using image analysis software. In the analysis, the area per crystal was calculated by dividing the total area of the crystals by the number of crystals, and the diameter was calculated from the area per crystal assuming that the crystals were circular. is the grain size.
  • the reason why the crystal grains are coarsened in the interface portion 8 is that the base portion 3 is heated by the irradiation of the laser beam 7, so that after building up, the crystal grains are closer to the boundary between the base portion 3 and the buildup portion 6. It is presumed that this is because the cooling rate becomes smaller than the inside of the built-up portion 6 as the temperature increases.
  • the length L of the interface portion 8 is preferably approximately 10 ⁇ m or more and 200 ⁇ m or less with respect to the total length of the buildup portion 6 .
  • FIG. 11 is an SEM photograph showing an enlarged view of the interface portion 8.
  • SEM energy dispersive X-ray spectroscopy
  • Table 1 shows the results. From Table 1, it can be seen that in the region (2) of the interface portion 8, the iron (Fe) element mainly diffuses from the base portion 3 to form a Ni—Fe alloy phase.
  • heat treatment such as annealing of the cutting edge, which is performed in the normal manufacturing process of blades, is not performed, or that the heat treatment be moderate. .
  • heat treatment such as annealing is preferably performed before the build-up portion 6 is formed by the laser beam 7 .
  • the Vickers hardness distribution from the built-up portion 6 to the base portion 3 was measured. Specifically, first, the base portion 3 and the build-up portion 6 were cut in a direction perpendicular to the x-axis direction shown in FIG. 1 and parallel to the blade edge direction (y-axis direction) of the blade edge portion 2 . Next, the Vickers hardness was measured from the tip of the built-up portion 6 toward the base portion 3 in the section of the cut portion. The measurement was performed according to JIS Z 2244. Measurement conditions are as follows. Test force: 5kg Measurement pitch: 200 ⁇ m
  • Fig. 12B shows the measurement results of the Vickers hardness distribution.
  • an arrow S indicates the position of the interface portion 8 near the boundary between the build-up portion 6 and the base portion 3.
  • the Vickers hardness at the position of this arrow S was 412 HV, which was the lowest hardness.
  • the length L (see FIG. 10) of the interface portion 8 in this example was 70 ⁇ m.
  • the hardness of the interface portion 8 is thus low, the toughness of the boundary region between the cutting edge portion and the base portion 3 of the cutting tool 1 is increased.
  • the interface part 8 serves as a cushioning material against the impact applied to the cutting tool 1, and the cutting edge part 2 can be prevented from being cracked or damaged. , there is an advantage that the life of the cutting tool 1 is extended.
  • the Vickers hardness of the interface portion 8 is 400 HV or more and 450 HV or less.
  • FIG. 13 is an enlarged SEM photograph showing the surface of the cutting edge portion 2, in which hard particles 4 having angular surfaces are present in the matrix within the second metal 2a.
  • FIG. 13 shows a state in which an indentation P for Vickers hardness measurement is formed on the surface of such a cutting edge portion 2 .
  • the indentation P for Vickers hardness measurement refers to a depression obtained by pressing a diamond rigid body (indenter) (not shown) into the surface of the target portion (here, the cutting edge portion 2). Since the indenter has the shape of an inverted square pyramid, the formed indentation P is substantially square.
  • the test force which is the load for pressing the indenter, was 5 kg.
  • FIG. 14 is an enlarged SEM photograph showing part A of FIG.
  • the crack 9 grows from the edge of the indentation P and is stopped by the matrix of the second metal 2a. It is presumed that this is because the second metal 2a has low hardness and high toughness.
  • FIG. 15 even when an indenter for Vickers hardness measurement was pressed against nickel (Ni) as the second metal 2a to form an indentation P', no crack was observed.

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  • Forests & Forestry (AREA)
  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Knives (AREA)
  • Powder Metallurgy (AREA)
PCT/JP2022/015188 2021-03-31 2022-03-28 刃物 Ceased WO2022210604A1 (ja)

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US18/553,421 US20240190029A1 (en) 2021-03-31 2022-03-28 Cutting implement

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Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH11207488A (ja) * 1998-01-23 1999-08-03 Daido Steel Co Ltd 耐食耐摩耗複合部材
WO2016190343A1 (ja) * 2015-05-25 2016-12-01 京セラ株式会社 セラミック刃物
JP2018008074A (ja) * 2015-06-22 2018-01-18 京セラ株式会社 刃物

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