WO2006068220A1 - サイアロン製インサート及びこれを備えた切削工具 - Google Patents
サイアロン製インサート及びこれを備えた切削工具 Download PDFInfo
- Publication number
- WO2006068220A1 WO2006068220A1 PCT/JP2005/023589 JP2005023589W WO2006068220A1 WO 2006068220 A1 WO2006068220 A1 WO 2006068220A1 JP 2005023589 W JP2005023589 W JP 2005023589W WO 2006068220 A1 WO2006068220 A1 WO 2006068220A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- sialon
- phase
- insert
- sintered body
- ratio
- Prior art date
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23B—TURNING; BORING
- B23B27/00—Tools for turning or boring machines; Tools of a similar kind in general; Accessories therefor
- B23B27/14—Cutting tools of which the bits or tips or cutting inserts are of special material
- B23B27/141—Specially shaped plate-like cutting inserts, i.e. length greater or equal to width, width greater than or equal to thickness
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B35/00—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
- C04B35/515—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics
- C04B35/58—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics based on borides, nitrides, i.e. nitrides, oxynitrides, carbonitrides or oxycarbonitrides or silicides
- C04B35/597—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics based on borides, nitrides, i.e. nitrides, oxynitrides, carbonitrides or oxycarbonitrides or silicides based on silicon oxynitride, e.g. SIALONS
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B35/00—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
- C04B35/622—Forming processes; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
- C04B35/626—Preparing or treating the powders individually or as batches ; preparing or treating macroscopic reinforcing agents for ceramic products, e.g. fibres; mechanical aspects section B
- C04B35/62605—Treating the starting powders individually or as mixtures
- C04B35/6261—Milling
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B35/00—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
- C04B35/622—Forming processes; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
- C04B35/626—Preparing or treating the powders individually or as batches ; preparing or treating macroscopic reinforcing agents for ceramic products, e.g. fibres; mechanical aspects section B
- C04B35/63—Preparing or treating the powders individually or as batches ; preparing or treating macroscopic reinforcing agents for ceramic products, e.g. fibres; mechanical aspects section B using additives specially adapted for forming the products, e.g.. binder binders
- C04B35/638—Removal thereof
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B35/00—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
- C04B35/622—Forming processes; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
- C04B35/64—Burning or sintering processes
- C04B35/645—Pressure sintering
- C04B35/6455—Hot isostatic pressing
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23B—TURNING; BORING
- B23B2200/00—Details of cutting inserts
- B23B2200/24—Cross section of the cutting edge
- B23B2200/242—Cross section of the cutting edge bevelled or chamfered
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23B—TURNING; BORING
- B23B2200/00—Details of cutting inserts
- B23B2200/28—Angles
- B23B2200/283—Negative cutting angles
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
- C04B2235/02—Composition of constituents of the starting material or of secondary phases of the final product
- C04B2235/30—Constituents and secondary phases not being of a fibrous nature
- C04B2235/32—Metal oxides, mixed metal oxides, or oxide-forming salts thereof, e.g. carbonates, nitrates, (oxy)hydroxides, chlorides
- C04B2235/3217—Aluminum oxide or oxide forming salts thereof, e.g. bauxite, alpha-alumina
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
- C04B2235/02—Composition of constituents of the starting material or of secondary phases of the final product
- C04B2235/30—Constituents and secondary phases not being of a fibrous nature
- C04B2235/32—Metal oxides, mixed metal oxides, or oxide-forming salts thereof, e.g. carbonates, nitrates, (oxy)hydroxides, chlorides
- C04B2235/3224—Rare earth oxide or oxide forming salts thereof, e.g. scandium oxide
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
- C04B2235/02—Composition of constituents of the starting material or of secondary phases of the final product
- C04B2235/30—Constituents and secondary phases not being of a fibrous nature
- C04B2235/32—Metal oxides, mixed metal oxides, or oxide-forming salts thereof, e.g. carbonates, nitrates, (oxy)hydroxides, chlorides
- C04B2235/3224—Rare earth oxide or oxide forming salts thereof, e.g. scandium oxide
- C04B2235/3225—Yttrium oxide or oxide-forming salts thereof
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
- C04B2235/02—Composition of constituents of the starting material or of secondary phases of the final product
- C04B2235/30—Constituents and secondary phases not being of a fibrous nature
- C04B2235/32—Metal oxides, mixed metal oxides, or oxide-forming salts thereof, e.g. carbonates, nitrates, (oxy)hydroxides, chlorides
- C04B2235/3224—Rare earth oxide or oxide forming salts thereof, e.g. scandium oxide
- C04B2235/3229—Cerium oxides or oxide-forming salts thereof
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
- C04B2235/02—Composition of constituents of the starting material or of secondary phases of the final product
- C04B2235/30—Constituents and secondary phases not being of a fibrous nature
- C04B2235/38—Non-oxide ceramic constituents or additives
- C04B2235/3817—Carbides
- C04B2235/3839—Refractory metal carbides
- C04B2235/3843—Titanium carbides
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
- C04B2235/02—Composition of constituents of the starting material or of secondary phases of the final product
- C04B2235/30—Constituents and secondary phases not being of a fibrous nature
- C04B2235/38—Non-oxide ceramic constituents or additives
- C04B2235/3852—Nitrides, e.g. oxynitrides, carbonitrides, oxycarbonitrides, lithium nitride, magnesium nitride
- C04B2235/3856—Carbonitrides, e.g. titanium carbonitride, zirconium carbonitride
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
- C04B2235/02—Composition of constituents of the starting material or of secondary phases of the final product
- C04B2235/30—Constituents and secondary phases not being of a fibrous nature
- C04B2235/38—Non-oxide ceramic constituents or additives
- C04B2235/3852—Nitrides, e.g. oxynitrides, carbonitrides, oxycarbonitrides, lithium nitride, magnesium nitride
- C04B2235/3865—Aluminium nitrides
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
- C04B2235/02—Composition of constituents of the starting material or of secondary phases of the final product
- C04B2235/30—Constituents and secondary phases not being of a fibrous nature
- C04B2235/38—Non-oxide ceramic constituents or additives
- C04B2235/3852—Nitrides, e.g. oxynitrides, carbonitrides, oxycarbonitrides, lithium nitride, magnesium nitride
- C04B2235/3873—Silicon nitrides, e.g. silicon carbonitride, silicon oxynitride
- C04B2235/3878—Alpha silicon nitrides
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
- C04B2235/02—Composition of constituents of the starting material or of secondary phases of the final product
- C04B2235/30—Constituents and secondary phases not being of a fibrous nature
- C04B2235/38—Non-oxide ceramic constituents or additives
- C04B2235/3852—Nitrides, e.g. oxynitrides, carbonitrides, oxycarbonitrides, lithium nitride, magnesium nitride
- C04B2235/3886—Refractory metal nitrides, e.g. vanadium nitride, tungsten nitride
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
- C04B2235/02—Composition of constituents of the starting material or of secondary phases of the final product
- C04B2235/50—Constituents or additives of the starting mixture chosen for their shape or used because of their shape or their physical appearance
- C04B2235/54—Particle size related information
- C04B2235/5418—Particle size related information expressed by the size of the particles or aggregates thereof
- C04B2235/5436—Particle size related information expressed by the size of the particles or aggregates thereof micrometer sized, i.e. from 1 to 100 micron
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
- C04B2235/02—Composition of constituents of the starting material or of secondary phases of the final product
- C04B2235/50—Constituents or additives of the starting mixture chosen for their shape or used because of their shape or their physical appearance
- C04B2235/54—Particle size related information
- C04B2235/5418—Particle size related information expressed by the size of the particles or aggregates thereof
- C04B2235/5445—Particle size related information expressed by the size of the particles or aggregates thereof submicron sized, i.e. from 0,1 to 1 micron
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
- C04B2235/65—Aspects relating to heat treatments of ceramic bodies such as green ceramics or pre-sintered ceramics, e.g. burning, sintering or melting processes
- C04B2235/656—Aspects relating to heat treatments of ceramic bodies such as green ceramics or pre-sintered ceramics, e.g. burning, sintering or melting processes characterised by specific heating conditions during heat treatment
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
- C04B2235/65—Aspects relating to heat treatments of ceramic bodies such as green ceramics or pre-sintered ceramics, e.g. burning, sintering or melting processes
- C04B2235/658—Atmosphere during thermal treatment
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
- C04B2235/65—Aspects relating to heat treatments of ceramic bodies such as green ceramics or pre-sintered ceramics, e.g. burning, sintering or melting processes
- C04B2235/66—Specific sintering techniques, e.g. centrifugal sintering
- C04B2235/661—Multi-step sintering
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
- C04B2235/70—Aspects relating to sintered or melt-casted ceramic products
- C04B2235/74—Physical characteristics
- C04B2235/76—Crystal structural characteristics, e.g. symmetry
- C04B2235/766—Trigonal symmetry, e.g. alpha-Si3N4 or alpha-Sialon
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
- C04B2235/70—Aspects relating to sintered or melt-casted ceramic products
- C04B2235/74—Physical characteristics
- C04B2235/76—Crystal structural characteristics, e.g. symmetry
- C04B2235/767—Hexagonal symmetry, e.g. beta-Si3N4, beta-Sialon, alpha-SiC or hexa-ferrites
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
- C04B2235/70—Aspects relating to sintered or melt-casted ceramic products
- C04B2235/80—Phases present in the sintered or melt-cast ceramic products other than the main phase
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
- C04B2235/70—Aspects relating to sintered or melt-casted ceramic products
- C04B2235/80—Phases present in the sintered or melt-cast ceramic products other than the main phase
- C04B2235/85—Intergranular or grain boundary phases
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
- C04B2235/70—Aspects relating to sintered or melt-casted ceramic products
- C04B2235/96—Properties of ceramic products, e.g. mechanical properties such as strength, toughness, wear resistance
- C04B2235/9607—Thermal properties, e.g. thermal expansion coefficient
Definitions
- the present invention relates to a sialon insert and a cutting tool provided with the same, and more particularly to a sialon insert having a long life and excellent in chipping resistance in which a cutting edge hardly wears and a cutting tool provided with the same.
- Cutting tools for example, outer diameter machining holder 2 shown in Fig. 2 and milling cutter 6 shown in Fig. 5, are inserts (throwers) that are disposable cutting edges at the tip of a support called a holder. Many structures are equipped with a wi-fi chip, also called a blade tip. Various materials are used for this insert depending on the type of work material, machining process and cutting speed. For example, cemented carbide, cermet, ceramic, CBN, and materials with coatings on these surfaces are used. Of these, silicon nitride ceramic inserts are suitable for rough machining of ordinary pig iron (abbreviated as FC) materials, especially for high speed forces.
- FC ordinary pig iron
- Sialon is recognized as a material having excellent hardness compared to silicon nitride, high strength from room temperature to high temperature, and high chemical stability. Therefore, it was often used as a structural material for hot steel rolling guide rolls and dies, aluminum die castings, machine sleeves, etc. that require heat resistance and chemical resistance. Furthermore, since it was recognized that the wear resistance was good, it was considered that it could also be used for cutting tools and bearings. However, in reality, sialon cutting tools are only used for rough cutting of difficult-to-cut heat-resistant alloys, etc., and wear resistance of the insert cutting edge that affects the surface roughness and dimensional accuracy of the work material. Sex was not considered much.
- This Z value is calculated from the difference between the a-axis lattice constant of ⁇ -sialon in the sintered sialon body measured by X-ray diffraction measurement and the a-axis lattice constant of ⁇ -silicon nitride (7.660442 A). (For example, see Patent Document 5 for the calculation method).
- Patent Document 1 US Pat. No. 4,323,323
- Patent Document 2 JP-A-10-36174
- Patent Document 3 Japanese Patent No. 2824701 (Japanese National Standard Heisei 8-510965)
- Patent Document 4 Japanese Patent No. 3266200 (Japanese Patent Laid-Open No. 2-2775763)
- Patent Document 5 Special Table 2004—paragraph number of 527434
- Patent Document 6 Patent Document 7, and Patent Document 8 disclose examples in which an FC compound is cut by coating a titanium compound such as titanium nitride and titanium carbide with an aluminum compound such as alumina.
- Patent Document 8 disclose examples in which titanium nitride is added to silicon nitride to suppress the chemical reactivity of the substrate itself. This titanium nitride exists in the structure as dispersed particles.
- Patent Document 2 Patent Document 3
- Patent Document 5 Patent Document 9
- Patent Document 10 a method of adding aluminum as aluminum nitride is known. Alumina dissolves in silicon nitride particles to form sialon particles, improving the chemical resistance of the silicon nitride particles themselves. It is disclosed in Patent Document 3, Patent Document 2, Patent Document 5, and the like.
- Patent Document 6 Japanese Patent No. 3107168
- Patent Document 7 Japanese Unexamined Patent Application Publication No. 2002-192404
- Patent Document 8 Japanese Patent Laid-Open No. 2002-284589
- Patent Document 9 Japanese Patent Laid-Open No. 11-335168
- Patent Document 10 Japanese Unexamined Patent Publication No. 2000-143351
- Patent Document 11 U.S. Pat.No. 5,525,134
- Patent Document 12 Japanese Unexamined Patent Application Publication No. 2002-192403
- the silicon nitride base material has low reactivity with iron and carbon, and a titanium compound or aluminum compound.
- a method of coating with a hard layer made of a material is known.
- Patent Document 11, Patent Document 8, Patent Document 12, and the like disclose cases where a silicon nitride base material is coated with titanium nitride or aluminum oxide, and ordinary pig iron and ductile pig iron are cut.
- titanium nitride or aluminum oxide leads to a decrease in high-temperature strength due to the difference in thermal expansion coefficient between titanium nitride and silicon nitride particles, or a decrease in strength of the particles themselves due to sialonization due to the addition of aluminum oxide. It was easy to control the performance balance. In particular, there was a difficulty in making a tool that had a sufficient life during high-speed cutting of difficult-to-cut materials such as ductile pig iron.
- stress is generated at the interface between the silicon nitride particles and the titanium nitride particles to cause the destruction of the insert itself.
- the aluminum compound does not form a solid solution in the silicon nitride particles, and remains as a crystal phase or a glass phase at the grain boundary, resulting in deterioration of high temperature characteristics and mechanical properties. Prone to wear damage.
- the aluminum compound does not dissolve sufficiently in the silicon nitride particles and remains at the grain boundaries, it becomes difficult to obtain a sufficient thermal shock resistance as a base material having a larger thermal expansion than silicon nitride. Les.
- Sialonii there is often a significant decrease in thermal conductivity.
- the present invention reduces wear caused by a chemical reaction between the work material and the insert without reducing the material strength, and abrasive mechanical wear, and has a long service life.
- the purpose is to provide inserts.
- the present invention solves the above-mentioned problems and has sufficient strength and excellent wear resistance not only for ordinary pig iron but also for high-speed cutting of difficult-to-cut materials such as ductile pig iron.
- Another object of the present invention is to provide a long-life sialon insert that does not cause damage to the cutting edge due to welding of the work material, and a cutting tool equipped with the insert. Means for solving the problem
- the present inventors have earnestly studied the mechanism of wear of the blade edge due to such a decomposition reaction of the insert material, and have found a means for solving the following problems.
- Means of the first invention for solving the above-mentioned problems are as follows.
- the component forming the grain boundary phase in the sialon sintered body is selected from the group consisting of specific elements derived from the sintering aid, that is, Sc, Y, Dy, Yb, and Lu.
- the total amount of this specific element in the sialon sintered body is limited to a ratio of 0.5 to 5 mol% in terms of oxide.
- the specific element contained in the sintering aid is contained in the sialon sintered body without substantially disappearing when the raw material powder for producing the sialon sintered body is sintered.
- Z value of sialon 0.2 to 0. A 7 average thermal expansion coefficients from room temperature of the sintered body to 1000 ° C is 3. 5 X 10- 6 / K or less, heat from room temperature to 1000 ° C
- Means of the second invention for solving the above-mentioned problems are as follows.
- the amount of the grain boundary phase contained in the sialon sintered body is limited by the area ratio of the grain boundary phase to the area of the cross section in the cross section inside the sialon sintered body.
- the area ratio which is the ratio of the area of the grain boundary phase to the cross-sectional area in the cross section of the sintered body, is 3 ⁇ 4 to 20%, and the ⁇ ratio indicating the ratio of ⁇ sialon in the sialon phase is 40%.
- the Z value of one sialon represented by Si Al ⁇ N is 0 ⁇ 2 ⁇ : ⁇ ⁇ 0
- One or more elements selected from Sc, Y, Ce, Er, Dy, Yb, and Lu are contained at a ratio of 0.5 to 10 mol% in terms of oxides with respect to the sintered body.
- the Sialon insert described in (4) The Sialon insert described in (4).
- the sintered body contains one or more selected from titanium carbide, nitride and carbonitride as a hard component in a proportion of 30 mol% or less (4) or (5) Sialon insert as described in.
- the Z value of the sialon phase is 0 ⁇ 2 to 1
- the ⁇ ratio indicating the proportion of ⁇ -sialon in the sialon phase is 10 to 40%
- Sc, Y, Dy, Yb, Lu force is selected in the sialon It is in a proportion of total 2-5 mole% in terms of oxide of one or more rare earth elements, made sialon present in 30 to 50 mole 0/0 Gahi sialon phase of the rare earth elements insert.
- sialon insert according to (6) wherein the sialon contains one or more selected from a carbide, nitride and carbonitride of titanium as a hard component in a proportion of 30 mol% or less. .
- the insert according to the first invention and the cutting tool according to the fourth invention using the insert are made of Sialon, and the chemical reaction between the work material and the tool base material with only high strength of the cutting blade. Decomposition and wear due to In addition, mechanical damage typified by abrasive wear that tends to occur when using sialon as a cutting tool can be suppressed, and tool life can be greatly improved.
- the sialon inserts and cutting tools of the first invention are difficult-to-cut materials as well as ordinary pig iron.For example, when machining ductile pig iron, heat-resistant alloys, etc. Tool life with low defect rate is long. Even when used as a rough cutting tool, the tool edge has excellent wear resistance that affects the surface roughness and dimensional accuracy of the work material, and cutting with good surface roughness and dimensional accuracy can be continued for a long time.
- the insert of the second invention and the cutting tool of the fourth invention using this insert are made of sialon, and are decomposed by a chemical reaction between the work material and the tool base, which is not only high in strength of the cutting blade. Can suppress wear. Also, defining the solid solution ratio of aluminum can suppress mechanical damage typified by abrasive wear when using sialon as a cutting tool, and can greatly improve the tool life.
- the sialon insert and cutting tool of the second invention are most suitable for cutting FC materials and the like, and even when used as a rough cutting tool, the resistance of the tool edge that affects the surface roughness and dimensional accuracy of the work material is affected. Abrasion Excellent machining with excellent surface roughness and dimensional accuracy can be continued for a long time.
- the insert of the third invention and the cutting tool of the fourth invention using the insert are sialon inserts having a controlled composition and a sintered body structure, and have high temperature strength, hardness, and wear resistance. In addition, it has fracture resistance due to welding damage, and has a very long life not only for ordinary cutting materials but also for high-speed cutting of difficult-to-cut materials. As a result, difficult-to-machine ductile pig iron and heat-resistant alloys can be processed at high speed, which contributes to reduction in processing costs and improvement in processing efficiency.
- FIG. 1 is a perspective view showing an example of an insert of the present invention.
- FIG. 2 is a side view showing an example of a cutting tool for outer diameter machining in which an insert which is an example of the present invention is attached to a holder.
- FIG. 3 is a perspective view of an example of the insert of the present invention.
- FIG. 4 is a front view showing chamfering of the insert of FIG.
- FIG. 5 is a plan view of a cutting tool in which an insert as an example of the present invention is attached to a milling cutter holder.
- the sialon inserts of the first to third inventions are formed of a sintered body whose main phase is ⁇ -sialon and a sialon phase having one sialon force.
- sialon insert according to the first invention is produced by adding a sintering aid to a raw material powder containing constituent elements such as silicon nitride, alumina, aluminum nitride, and silica such as Si, Al, ⁇ , and N.
- a sintering aid such as silicon nitride, alumina, aluminum nitride, and silica such as Si, Al, ⁇ , and N.
- sialon particles have the composition formula SiAlO N (0 ⁇ Z ⁇ 4.
- ⁇ -Sialon has a high toughness because it has a structure in which needle-like structures are entangled like silicon nitride, and H-Sialon has an equiaxed particle shape, so it has low toughness compared to ⁇ -Sialon. However, it has a feature of high hardness.
- the grain boundary phase between sialon particles includes a glass phase and a crystal phase.
- the sintering aid became a liquid phase along with silicon nitride and silica components contained as impurities in silicon nitride, and contributed to the generation of sialon particles, redistribution of sialon particles ij, grain growth, and densification. Thereafter, it solidifies upon cooling to produce a grain boundary phase at the sialon grain boundary as a glass phase or a crystalline phase.
- this grain boundary phase Since this grain boundary phase has a low melting point, low toughness, and low hardness compared to sialon particles, it must be controlled to an appropriate amount in order to improve the heat resistance, toughness, and hardness of the sialon sintered body. There is. To control the sialon grains and grain boundary phase, it must force s to adjust the sintering aid.
- the sialon insert according to the first invention is a rare earth element used as a sintering aid, preferably at least one selected from the group consisting of Sc, Y, Dy, Yb, and Lu.
- the element is contained in the sialon sintered body in an amount of 0.5 to 5 mol% in terms of oxide.
- the raw material powder for obtaining a sialon sintered body when producing a sialon insert contains the rare earth element oxide in a proportion of 0.5 to 5 mol%.
- the sialon sintered body can be controlled to a suitable sialon structure by defining the type and content of the above elements that contribute to acicularization of the sialon structure.
- the sialon structure will not be sufficiently needle-like, which will cause the strength of the sialon sintered body to be reduced, and in some cases, densification itself will be difficult.
- it exceeds 5 mol% the heat resistance, toughness and hardness of the sintered sialon itself will decrease.
- Sialon inserts are not preferred because they reach the end of their lives due to mechanical wear damage such as abrasive wear.
- the molecular weight is determined by regarding each of the above elements as a compound such as an oxide or nitride.
- Si is calculated as SiN, A1 as Al ⁇ , Y as Y ⁇ , and so on.
- the ratio indicating the ratio of one sialon in the sialon particles is 10 to 40%.
- Hsialon is a solid solution of the specific rare earth element derived from the specific rare earth oxide added as a sintering aid at the time of its formation, reducing the amount of crystal phase or glass phase at the sialon grain boundary, Mechanical wear damage can be suppressed.
- the ⁇ rate which is the ratio of ⁇ -sialon in sialon, is the (101) plane peak intensity of i3-sialon in X-ray diffraction, (210) plane peak intensity of 2, and (102) of ⁇ sialon.
- the plane peak intensity is al and the (210) plane peak intensity is ⁇ 2, it is calculated using the formula ⁇ (al + ⁇ 2) / (; 3 1 +; 3 2 + ⁇ 1 + ⁇ 2) ⁇ ⁇ 100 Is done.
- the ⁇ ratio is less than 10%, a lot of grain boundary phases remain and the wear resistance and thermal shock resistance are not sufficient.
- the ratio exceeds 40%, the number of equiaxed sialon particles having low toughness increases, so that the fracture resistance is inferior.
- the Z value of one sialon represented by N is 0.2 to 0 ⁇ 7.
- ⁇ -Sialon's threshold is
- the sialon insert is less likely to cause a chemical reaction with the work material and the strength reduction due to sialon is less than silicon nitride. sand In other words, if it is less than 0.2, the effect of suppressing the chemical reaction between the sialon insert and the work material is not sufficient. If it is greater than 0.7, the strength of the sialon insert is significantly reduced.
- This Z value can be measured by measuring the a-axis lattice constant of ⁇ -sialon in a sintered sialon body by X-ray diffraction measurement and the a-axis lattice constant of j3-nitride (7. 60442 A). It is calculated from the difference by a normal method (refer to Patent Document 5 for the calculation method).
- the average thermal expansion coefficients from room temperature to 1000 ° C is 3. is 5 X 10- 6 ZK below.
- inserts repeatedly undergo thermal expansion and contraction due to heat generated during cutting.
- the insert may crack due to repeated expansion and contraction.
- Reduction of the coefficient of thermal expansion is important in order to suppress the expansion and contraction of the insert due to heat, to suppress the generation and growth of cracks, and to prevent defects.
- the thermal expansion coefficient can be reduced when the grain boundary phase amount is reduced.
- the sintered body in the sialon insert of the first invention has a thermal conductivity of 10 W / m'K or more from room temperature to 1000 ° C.
- thermal conductivity a higher value from room temperature to higher temperature is easier to dissipate heat and can reduce heating of the insert, which is more effective in reducing thermal shock.
- the thermal conductivity is lOWZm'K or more, the loss of sialon inserts due to the generation and growth of thermal cracks can be remarkably suppressed.
- Sialon inserts can suppress cracks significantly during high-speed cutting, where high temperatures are likely to occur.
- the three-point bending strength at room temperature (sometimes abbreviated as "room temperature strength") is lOOOMPa or more.
- Sialon sintered body is preferred.
- the sialon insert of the present invention is used as a cutting tool, the greater the strength of the sialon sintered body, the better the thermal shock resistance that is achieved by simple strength alone, and stable processing becomes possible.
- Sialon inserts with a three-point bending strength are particularly suitable.
- the sialon insert of the present invention having a room temperature strength of lOOOMPa or higher enables stable processing.
- sialon sintered bodies constituting the sialon insert of the first invention a sialon sintered body having a three-point bending strength at 1000 ° C. of 900 MPa or more is preferable.
- the sialon insert of the present invention When the sialon insert of the present invention is used as a cutting tool, the tool becomes hot due to friction with the work material. Therefore, the higher the strength of the sialon sintered body in the present invention, particularly at a high temperature, the more stable force can be obtained in the high-speed casing.
- the cutting tool of the present invention includes the sialon insert of the present invention and a holder for mounting the insert as a throw-away chip, and is used as a high-performance cutting tool.
- the sialon insert and cutting tool of the present invention are not only ordinary pig iron but also difficult-to-cut materials, such as ductile pig iron, heat-resistant alloys, etc. Long tool life. Even if it is used as a rough cutting tool, it has excellent tool edge wear resistance that affects the surface roughness and dimensional accuracy of the work material, and cutting with good surface roughness and dimensional accuracy can be continued for a long time.
- the cutting tool of the present invention is a cutting tool in a broad sense, and refers to all tools that perform turning, milling and the like.
- sialon insert of the first invention A preferred method for producing the sialon insert of the first invention will be described below. Contains sialon constituent elements such as Si N powder, Al O powder, A1N powder, etc.
- the mixture is used as a raw material powder.
- a powder having an average particle size of 10 zm or less, preferably 5 zm or less, more preferably 3 zm or less is used as the raw material powder.
- the ratio of these raw material powders may be determined in consideration of the composition of the insert after sintering.
- Si N silicon
- the sintering aid may be 0.5 to 5 mol%.
- the prepared raw material powder is mixed with a grinder such as a ball mill, for example, ethanol powder using a Si N pot equipped with Si N balls. A liquid that does not substantially dissolve the powder is collected and mixed for 1 to 300 hours to produce a slurry. At this time, if the particle size of the raw material powder is large, the pulverization time is lengthened to ensure sufficient pulverization.
- the slurry is passed through a sieve of about 200 to 500 mesh to remove the coarse particles.
- an organic binder such as micro wax is added to the raw material powder:! ⁇ 30% by mass, and granulated and dried by spray drying or the like.
- the obtained granulated powder is pressed into a desired shape assuming the shape of the sintered body after firing.
- injection molding, extrusion molding, squeeze molding, etc. can be applied.
- Degrease the compact after molding Usually, degreasing is performed in an inert gas atmosphere such as nitrogen in a heating apparatus. Degreasing is completed in about 30 to 120 minutes at 400 to 800 ° C.
- the degreased shaped body is sintered at 1500 to 1900 ° C, preferably 1650 to 1800 ° C.
- Sintering is preferably performed in two stages.
- Primary sintering is preferably performed in a chamber formed of silicon carbide, boron nitride, silicon nitride, etc., preferably in an Ar atmosphere at 1500 to 1600 ° C.
- the molded body is held for ⁇ 4 hours, and then heated to 1650 ⁇ : 1800 ° C. in a nitrogen or Ar atmosphere of 1 to 9 atm, and held at this temperature for 1 to 5 hours.
- Secondary sintering may be performed by hot isostatic pressing (HIP). For example, heating is performed at 1650 to 1800 ° C for 1 to 5 hours in a nitrogen atmosphere of 100 to 5000 atmospheres. In this way, a sialon sintered body is obtained.
- HIP hot isostatic pressing
- the sialon insert according to the second invention has a sialon phase consisting of ⁇ sialon and ⁇ sialon or a sialon phase consisting of i3-sialon as the main phase.
- This is a sintered body obtained by adding a sintering aid and sintering.
- the sialon insert according to the second invention is an area ratio that is a ratio of the area of the grain boundary phase to the cross-sectional area in the cross section of the sialon sintered body.
- sialon adds a sintering aid or the like to a raw material powder containing constituent elements such as Si, Al, O, and N such as silicon nitride, alumina, aluminum nitride, and silica. Sintered.
- the sialon usually has a composition formula Si
- M is an interstitial solid solution element such as Mg, Ca, Sc, Y, Dy, Er, Yb, Lu
- sialon indicated by is mixed in the sialon sintered body.
- ⁇ -sialon has a high toughness because it has a structure in which needle-like structures are entangled like silicon nitride, and since sialon has an equiaxed particle shape, it has low toughness, but Compared with Aaron, it has a high hardness and features.
- the grain boundary phase between the sialon particles is such that the sintering aid, silicon nitride and silica components contained as impurities in the silicon nitride become a liquid phase during the sintering, thereby generating sialon particles and rearranging the sialon particles. After contributing to grain growth, it solidifies upon cooling and forms as a glass phase or a crystalline phase. Since this grain boundary phase has a low melting point, low toughness, and low hardness compared to sialon particles, it must be controlled to an appropriate amount in order to improve the heat resistance, toughness, and hardness of the sialon sintered body. There is.
- the grain boundary glass phase and the grain boundary crystal phase are reduced, for example, by reducing the amount of sintering aid, the force S can be reduced, and if the proportion of the grain boundary phase is reduced to less than 5%, sialon sintering Causes the strength of the body to decrease.
- the proportion of the grain boundary phase is increased from 20%, as described above, the grain boundary phase is a component that is inferior in melting point, toughness, and hardness as compared to sialon particles, so the heat resistance, toughness, Hardness will decrease.
- the life is shortened due to mechanical damage represented by abrasive wear. That is, in the second invention, the grain boundary phase composed of the grain boundary crystal phase and / or the grain boundary glass phase needs to be 5 to 20%.
- the area ratio (%) which is the ratio of the area of the grain boundary phase to the cross-sectional area in the cross section of the sialon sintered body, was measured using a scanning electron microscope (SEM) at an observation magnification of 5000 times. After taking a photograph of a cross section inside lmm or more from the sintered skin of the sintered body, the area ratio of the grain boundary phase part in a certain area of the photograph is measured by image processing software, so that the grain for the whole certain area is measured. It is obtained as a ratio (%) of the area of the field phase part.
- SEM scanning electron microscope
- the constant region in the SEM photograph is the entire field of view observed at the observation magnification of 5000 times, and is an area region of 15 zm x 12 zm in terms of actual size.
- the image processing software calculates the area ratio of the grain boundary phase other than sialon particles observed in this observation field. Measured with When the area of the cross section of the sialon sintered body is much larger than the visual field, the area ratio may vary depending on the observation site in the cross section of the sialon sintered body. The variation in the area ratio is the average value
- the hard component particles are not the grain boundary phase part.
- the sialon insert according to the second invention has good toughness due to its high toughness when the sialon particles are ⁇ -sialon, but even if some of them are single sialon. There is no decline in cutting performance. Good cutting performance can be obtained up to a ratio of 40%, which is the ratio of one sialon. If the ratio exceeds 40%, equiaxed sialon crystal grains with low toughness increase, so that the fracture resistance is inferior. That is, as described above, when the ratio is 40% or less, it is preferable because sufficient cutting performance (abrasion resistance and chipping resistance) is obtained.
- the insert of the second invention is represented by the composition formula Si Al O N -Z value of sialon
- the insert of the second invention Since the insert of the second invention has a Z value (actually measured Z value) in the range of 0.2 to:! ⁇ 0, it is less susceptible to decomposition due to chemical reaction with the work material than silicon nitride. There is little decrease in strength. Further, the sialon insert according to the second invention has a solid solution ratio of A1 of 70% or more. As a result, mechanical damage represented by abrasive wear with the work material with a small residual amount of aluminum component in the grain boundary phase is suppressed.
- the measured Z-value is the a-axis lattice constant of i3—sialon and the a-axis lattice constant of silicon nitride (7.6044), which is measured by X-ray diffractometry. 2 Calculate by the difference of A) (refer to, for example, WO02Z44104, page 28).
- A1 represents 8% by weight and Si represents 31% by weight.
- the insert of the second invention has a measured Z value Z theory
- the work material with a small residual amount of aluminum component at the grain boundary due to the A1 solid solution ratio represented by the Z value being 70% or more.
- Abrasive wear The mechanical damage represented by is suppressed.
- the solid solution ratio of A1 is controlled by adjusting the firing temperature, temperature rise time, firing atmosphere, etc. during firing of the sintered body and / or changing the ratio of nitrogen and oxygen in the sintered body. It is possible.
- a sintering aid used for sintering the sialon insert one or more selected from the rare earth elements Sc, Y, Ce, Er, Dy, Yb, and Lu are converted into oxides for the sintered body. It is preferable to use at a ratio of 0.5 to 10 mol%.
- the sialon structure can be controlled appropriately. If it is less than 0.5 mol%, the sialon structure is not sufficiently needle-like, which causes a decrease in the strength of the sialon substrate.
- At least one selected from carbide, nitride and carbonitride of titanium as a hard component is 30 mol% or less, preferably 0.1 to 25 mol%, Preferably it is contained in a proportion of 1 to 20 mol%.
- a hard component is dispersed alone in the sialon sintered body.
- the above titanium compound has a low reactivity with iron and carbon, which are the main components of the work material, as compared with silicon nitride, as well as alumina. Therefore, it reacts with the work material by being present in the sintered body. It is possible to suppress sex.
- the titanium compound is not dispersed in the sintered body but dispersed alone.
- the titanium compound content exceeds the above upper limit, no reduction in cutting performance is observed, but it is a component with a larger coefficient of thermal expansion than sialon, so it is affected by the heat generated during cutting and generates heat. It is not preferable because the tool edge may be lost due to cracks. Whether or not the titanium compound is dispersed alone can be confirmed with an optical microscope or an electron microscope.
- the method for calculating mol% is the same as the method for calculating mol% of the oxide equivalent content of the rare earth element.
- the sialon insert of the second invention is a holder as a throwaway tip. It is used as a high-performance cutting tool by mounting it on the die. It is particularly suitable as a long-life insert that performs high-speed roughing such as pig iron with high accuracy.
- the powder is rare earth element oxide powder as sintering aid, SC O powder, Y O powder, Ce
- any of hard component TiN powder, TiC powder, or TiCN powder is added to obtain a raw material powder.
- the raw material powder may be a powder having an average particle size of 5 xm or less, preferably 3 zm or less, more preferably 2 zm or less. These raw material powders should be determined in proportion to the composition of the insert after sintering. Usually 95 to 30 mol Si N powder 0/0, A1
- Hard component may be 0-30 mol%.
- a slurry is produced from the prepared raw material powder in the same manner as in the method for producing a sialon insert in the first invention.
- a granulated powder is obtained from this slurry, a press-molded body having a desired shape is produced from this granulated powder, this press-molded body is degreased, and then sintered.
- a sialon insert can be produced.
- the sintered body thus obtained is a sialon sintered body, which can be polished into a shape as shown in FIG. 1 to obtain the insert 1 for a cutting tool according to the second invention.
- a cutting tool can be obtained by attaching it to a holder as shown in FIG.
- the sialon insert according to the third invention has a sialon phase consisting of a hyaluronic phase and a ⁇ sialon phase obtained by sialonizing an aluminum compound into silicon nitride.
- the main phase is formed of a sialon sintered body bonded with a sintering aid.
- the ⁇ sialon phase in the sintered sialon is a structure in which fine needle-like particles similar to silicon nitride are intertwined, and the strength of the particles themselves is higher than that of alumina used in conventional tools. Defects are unlikely to occur and have a long life.
- the amount of the aluminum compound is too high, the strength of the sialon phase will be reduced and the tool edge will be damaged. It will be easy. It is necessary to adjust the amount of aluminum compound added to such an extent that the reactivity with the work material is suppressed and the adverse effect of reducing the strength does not occur. Even if the aluminum compound is dissolved in silicon nitride and does not sialonize, it exists in the grain boundary phase, so that it also has an effect of contributing to suppression of the reaction with the work material. Compared to silicon nitride, the sialon phase is chemically stable and does not easily react with iron or carbon, which are the main components of the work material, even at high temperatures, so strength and chemicals can be maintained by maintaining an appropriate amount of aluminum compound. The ability to satisfy both stability requirements is important.
- the specific amount of aluminum compound added is that the Z value of the / 3 sialon phase expressed by SiAlO N in the sialon sintered body is 0.2 or more and 1 or less.
- the Z value is less than 0.2, a welding reaction with the work material occurs, and a sufficient life extension effect cannot be obtained immediately. If the Z value exceeds 1, the aluminum component increases and sialonization occurs. As a result, the strength of the tool edge decreases and wear and chipping become noticeable.
- the method for measuring the Z value is as described above.
- aSialon phase is represented by the composition formula M (Si, Al) (O, N).
- M is Mg, Ca, Sc, Y, Dy, Er, Yb, Lu x 12 16
- X represents the value of 0 ⁇ X ⁇ 2. Since the ⁇ sialon phase has an equiaxed particle shape, the ⁇ sialon phase is characterized by low toughness and high strength and strength compared to the ⁇ sialon phase. In this way, a predetermined amount of high-hardness ⁇ -sialon phase is generated, and at the same time, the elements to be dissolved in the ⁇ -sialon phase and the amount of the solid solution are optimized, compared with the sialon-sintered sialon sintered body alone. It becomes possible to increase the reaction resistance and wear resistance with the work material.
- aSialon is obtained by setting the total amount of rare earth elements Sc, Y, Dy, Yb, and Lu dissolved in the sialon phase to 30 to 50 mol% of the total amount of the rare earth elements contained in the entire sialon sintered body.
- the chemical stability of the sintered body is increased, and the reaction between the sialon and the work material can be suppressed.
- the sialon sintered body contains at least one of the rare earth elements in a ratio of 2 to 5 mol% in total, and the sialon sintered body is dissolved in the sialon phase by dissolving the above ratio in the sialon phase.
- the grain boundary phase can be reduced while ensuring the sinterability of It also works effectively for suppressing mechanical wear damage.
- the sialon insert according to the third invention has an ⁇ ratio of 10 to 40% and is at least one rare selected from the group consisting of Sc, Y, Dy, Yb, and Lu contained in sialon.
- the earth element is 2 to 5 mol% in terms of oxide, and 30 to 50 mol% of the rare earth element is present in the hyalonic phase. If the ratio is less than 10% and the amount of the rare earth element dissolved in the sialon phase is less than 30 mol%, the formation of sialon phase with excellent reaction resistance with the work material will be insufficient. The reaction resistance of the sialon sintered body is reduced, and welding damage due to the chemical reaction between the work material and the tool edge tends to occur.
- the solid solution amount of the rare earth element in the sialon phase is 50 mol of the whole rare earth element.
- the reaction resistance of the sialon sintered body to the work material is sufficient, but a strength of the sialon particles themselves is lowered, which is not preferable.
- the grain boundary phase between sialon particles is a liquid phase during sintering, such as a sintering aid, silicon nitride, and a silicon component contained as an impurity in silicon nitride, and generation, rearrangement, and grain growth of sialon particles. Then, it is solidified upon cooling to form a glass phase or a crystalline phase. Since this grain boundary phase has a lower melting point, lower toughness and lower hardness than sialon particles, it is better to reduce the grain boundary phase in order to improve the heat resistance, toughness and hardness of the sialon sintered body.
- the grain boundary phase can be reduced, for example, by reducing the sintering aid, but if the sintering aid is reduced too much, the sialon phase cannot be completely sintered and the strength of the sialon sintered body is reduced. It becomes.
- the mol% of the oxide conversion content of the rare earth element in the sialon sintered body can be calculated by the method described above.
- At least one selected from carbide, nitride and carbonitride of titanium as a hard component is 30 mol% or less, preferably 0.:! To 25 monolayers. 0/0, it is desirable that more preferably contains 1 to 20 mol 0/0.
- a hard component is dispersed in a single particle in the sintered body.
- the titanium compound has a lower reactivity with iron and carbon, which are the main components of the work material, as compared with silicon nitride, as well as alumina. Reactivity can be suppressed. When the titanium compound content exceeds the upper limit, the titanium compound is sialon.
- the tool edge is likely to be damaged due to thermal cracks that occur due to the effect of heat during cutting.
- the titanium compound is dispersed alone can be confirmed with an optical microscope or an electron microscope.
- the method for calculating the mol% of the titanium compound is the same as the method for calculating the mol% of the oxide equivalent content of the rare earth element.
- the sialon insert according to the third invention is mounted on a holder for a cutting tool and used as a high-performance cutting tool.
- the It is particularly suitable for long-life cutting tools that perform high-speed coarse forces such as ductile pig iron with high accuracy.
- the cutting tool according to the fourth invention formed using the first to third sialon inserts is a broad-cutting tool, such as roughing and finishing such as turning, milling, and grooving. Say the general tool to do.
- a preferred method for producing a sialon insert according to the third invention is basically the same as the method for producing a sialon insert according to the first and second inventions.
- a sialon sintered body is produced in the same manner as in the first invention.
- the sintered body thus obtained is a sialon sintered body, which is polished into the shape of inserts 1 and 1 'as shown in FIGS. 1 and 3, and used for the cutting tool of the third invention. It can be a Sialon insert.
- the outer diameter force holder can be mounted on a milling cutter holder 6 to obtain an outer diameter cutting tool as a frying cutter cutting tool.
- a raw material powder was prepared by blending the A1N powder of 3 ⁇ m in the proportion shown in Table 1 so as to have the composition shown in Table 1. Next, the raw material powder is mixed with a Si N pot and Si N
- ethanol was added and mixed for 96 hours to prepare a slurry.
- coarse particles were removed with a 325 mesh sieve, and 5.0% by mass of a microwax organic binder dissolved in ethanol was added, followed by spray drying to produce granules.
- the resulting granules were press-molded into the SNGN 120412 insert shape according to the ISO standard shown in Fig. 1, and then degreased at 600 ° C in a nitrogen atmosphere at 1 atm for 60 minutes in a heating device.
- the primary sintering of the degreased compact is set in a silicon nitride sheath, held in the set state at 1600 ° C for 60 to 240 minutes, then:!
- sialon sintered body was polished and processed into an SNGN120412 shape according to ISO standards to obtain an insert for a cutting tool.
- Table 1 shows the composition and properties of the inserts of Examples and Comparative Examples along with the results of cutting performance evaluation.
- “*” in the “Example” column is a comparative example.
- the composition of the sialon sintered body is expressed in mol% by the above method.
- the percentage of sialon particles and the value of ⁇ -sialon were determined by the method described above.
- the thermal expansion coefficient was determined by polishing the above-mentioned sialon sintered body to a length of 5 mm x width 5 mm x length 10 mm, and using JIS R1618 method, the average thermal expansion coefficient up to 1000 ° C at room temperature in a nitrogen atmosphere. It was measured.
- the fabricated sintered body was polished into a disk shape with a diameter of 10 mm and a thickness of 2 mm, and from room temperature to 1000 ° C by the JIS R161 1 method (this is commonly referred to as the laser flash method). The value of was measured and the lowest value was shown.
- the density of the obtained sintered body was measured by the Archimedes method, and the theoretical density ratio was calculated by dividing by the theoretical density.
- the sampnore was densified with no micropores remaining in the sintered body having a sufficiently high theoretical density ratio.
- the chamfering edge is machined to a chamfering width of 0.3 mm and a chamfering angle of 25 degrees, as shown in Fig. 4. It was set in a single tooth milling cutter holder and cut under the processing conditions shown below. The number of workpieces that could be machined until the wear amount (VB) of the insert blade edge reached 0.3 mm was evaluated as the life, and if the blade edge was lost before VB became 0.3 mm At the time, it was determined to be a lifetime.
- VB wear amount
- 'Cutter used ⁇ 100, machined with a single blade.
- the cutting tips of Examples A to U which are examples, have a large number of workable workpieces until the wear amount (VB) of the tool edge reaches 0.3 mm. The tool blade tip is not damaged.
- the inserts of comparative examples * 1, * 3, * 7 to * 11 are clearly less in number of cuts and have poor chipping resistance and are inferior to the inserts of the examples.
- Example 3 where the Z value is less than 0.2 and the result of Example are compared
- the chemical reaction between the work material and the tool base material It can be seen that the decomposition-wear caused by is suppressed.
- Example * 9 where the a ratio is less than 10% and the results of Examples
- the sialon insert according to the present invention mechanical damage represented by abrasive wear is suppressed. I understand that.
- the sialon insert according to the present invention has excellent tool edge wear resistance that affects the surface roughness and dimensional accuracy of the work material even when used as a rough cutting tool, and the surface roughness and dimensions. Cutting with good accuracy can be performed for a long time.
- the average particle size is 1. as an ⁇ — Si N powder with an average particle size of 0.5 / im and a sintering aid.
- the raw material powder was prepared by blending at the ratio shown in 2. Next, this raw material powder was press-molded into the shape of the insert shown in FIG. 1 in the same manner as in “Preparation of Insert” in the embodiment of the first invention, and then nitrogen at 1 atm in the heating device. Degreasing was performed in an atmosphere at 600 ° C for 60 minutes. The primary sintering of the degreased compact was set in a silicon nitride sheath, and was heated from 1700 to 1800 ° C.
- Insert shape SNGN120408, chamfer 0.2 mm
- work material pig iron (FC200)
- cutting speed 500 mm / min
- cutting depth 0.3 mm
- feed rate 0.3 mm / min
- after cutting under dry conditions before The cutting distance was calculated when the maximum VB wear (VBmax) on the flank surface reached 0.3 mm.
- Insert shape SNGN120408, chamfer 0.2 mm
- work material pig iron (FC200) with dredged sand on the side
- cutting speed 300 mmZmin
- depth of cut 1.5 mm
- feed rate 0.2 mmZ
- the maximum amount of flank wear was measured by using the boundary wear amount (unit: mm).
- Insert shape SNGN120408, chamfer 0. 085 mm
- work material pig iron (FC20 0)
- cutting speed 150 mm / min
- cutting depth 2.0 mm
- feed rate 0.6 mm From Zrev
- the evaluation method was started and increased by 0.05 mm / rev for each processing pass, and the evaluation was made based on the feed rate leading to the defect under dry conditions.
- the insert according to the embodiment of the second invention has a long cutting distance of the tool blade edge and is excellent in fracture resistance with a small amount of boundary wear.
- the insert of the comparative example is not preferable because any one of the cutting distance, the boundary wear amount and the fracture resistance is inferior.
- O powder, and A10 powder with an average particle size of 0. Average particle size is 1.3 ⁇ m
- A1N powder and TiN powder having an average particle size of 1.5 zm were blended in the proportions shown in Table 3 to prepare raw material powder. Next, these raw material powders are placed in a Si N
- a method for measuring the characteristics of the throw-away tip will be described.
- the density of the obtained throwaway chips of Examples and Comparative Examples was measured by the Archimedes method, and the theoretical density ratio was calculated by dividing by the theoretical density. Except for the sample of Comparative Example 8, the theoretical density ratio was sufficiently high, and the micropores did not remain in the sintered body and were densified, so the properties were measured.
- the measurement and calculation of the Z value and the probability were based on the method described above.
- the solid solution amount of Sc, Ce, Y, Dy, Er, Yb, and Lu in the Hsialon particles was measured by observing the structure with a transmission electron microscope and analyzing the composition of Hysialon with the attached EDX analyzer. .
- Cutter used ⁇ 100, processed with a single blade.
- the throwaway inserts of the present invention of Examples 24-41 have a wear amount (VB) of the tool edge of 0.
- the number of workpieces that can be machined up to 3 mm was as large as 9 or more, and there was no defect in the tool edge.
- only five of the throw-away tips of comparative examples that did not satisfy the requirements of the present invention could be cut.
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Ceramic Engineering (AREA)
- Manufacturing & Machinery (AREA)
- Materials Engineering (AREA)
- Structural Engineering (AREA)
- Organic Chemistry (AREA)
- Inorganic Chemistry (AREA)
- Mechanical Engineering (AREA)
- Ceramic Products (AREA)
- Cutting Tools, Boring Holders, And Turrets (AREA)
Abstract
Description
Claims
Priority Applications (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US11/793,500 US20080119349A1 (en) | 2004-12-22 | 2005-12-22 | Sialon Insert and Cutting Tool Equipped Therewith |
EP05820104A EP1837105A4 (en) | 2004-12-22 | 2005-12-22 | SIALON INSERT AND CUTTING TOOL EQUIPPED WITH SIALON |
CN2005800445856A CN101087670B (zh) | 2004-12-22 | 2005-12-22 | 赛纶陶瓷刀片以及装备这种刀片的切削工具 |
EP11180944.8A EP2402098B2 (en) | 2004-12-22 | 2005-12-22 | Sialon insert and cutting tool equipped therewith |
Applications Claiming Priority (8)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2004-372004 | 2004-12-22 | ||
JP2004-372005 | 2004-12-22 | ||
JP2004372004A JP4434938B2 (ja) | 2004-12-22 | 2004-12-22 | サイアロン製インサートの製造方法 |
JP2004372005 | 2004-12-22 | ||
JP2005134157A JP2006305708A (ja) | 2005-05-02 | 2005-05-02 | サイアロン製スローアウェイチップおよび切削工具 |
JP2005-134157 | 2005-05-02 | ||
JP2005-324180 | 2005-11-08 | ||
JP2005324180A JP2006198761A (ja) | 2004-12-22 | 2005-11-08 | サイアロン製インサート及びこれを備えた切削工具 |
Publications (1)
Publication Number | Publication Date |
---|---|
WO2006068220A1 true WO2006068220A1 (ja) | 2006-06-29 |
Family
ID=36601817
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/JP2005/023589 WO2006068220A1 (ja) | 2004-12-22 | 2005-12-22 | サイアロン製インサート及びこれを備えた切削工具 |
Country Status (4)
Country | Link |
---|---|
US (1) | US20080119349A1 (ja) |
EP (2) | EP1837105A4 (ja) |
CN (1) | CN101087670B (ja) |
WO (1) | WO2006068220A1 (ja) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1939155A3 (en) * | 2006-12-27 | 2011-04-13 | Sandvik Intellectual Property AB | Ceramic material and cutting tools made thereof for toughness demanding operations |
EP1939154A3 (en) * | 2006-12-27 | 2011-04-20 | Sandvik Intellectual Property AB | Ceramic material and cutting tools made thereof for applications demanding good notch wear resistance |
Families Citing this family (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102008022758A1 (de) | 2007-05-09 | 2008-12-18 | Michael Bader | Mittels Verbundguss hergestellte Umform- und Trennwerkzeuge |
JP5685523B2 (ja) | 2009-03-13 | 2015-03-18 | 日本特殊陶業株式会社 | サイアロン焼結体および切削インサート |
EP2648475B1 (en) * | 2010-12-02 | 2018-10-17 | NGK Sparkplug Co., Ltd. | Ceramic heater element, ceramic heater, and glow plug |
US20130298474A1 (en) | 2010-12-22 | 2013-11-14 | Sandvik Intellectual Property Ab | Cutting tool made of sialon based material |
CN103787663B (zh) * | 2014-02-25 | 2015-03-11 | 丽水桉阳生物科技有限公司 | 多相高强度、导热性好的氮化硅陶瓷刀具材料及刀具 |
KR102328802B1 (ko) * | 2015-04-24 | 2021-11-18 | 대구텍 유한책임회사 | SiAlON 복합 재료 및 이 SiAlON 복합 재료로 만들어진 절삭 공구 |
CN105057717A (zh) * | 2015-08-07 | 2015-11-18 | 江苏塞维斯数控科技有限公司 | 机床切割用尖状双面刃具 |
CN108610057A (zh) * | 2018-04-09 | 2018-10-02 | 中国科学院兰州化学物理研究所 | 一种宽温域减摩抗磨兼具高韧的赛隆基复合材料及其制备方法 |
KR102500926B1 (ko) * | 2018-07-11 | 2023-02-17 | 니뽄 도쿠슈 도교 가부시키가이샤 | 광파장 변환 부재 및 발광 장치 |
EP4079429A4 (en) * | 2019-12-20 | 2024-01-24 | Ntk Cutting Tools Co., Ltd. | CUTTING TOOL |
Citations (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS63260869A (ja) * | 1986-08-18 | 1988-10-27 | 日本特殊陶業株式会社 | 炭化珪素ウイスカ−強化複合材料 |
JPH0446062A (ja) * | 1990-06-11 | 1992-02-17 | Hitachi Metals Ltd | サイアロン焼結体およびその製造方法ならびにこれを用いたガスタービン翼 |
JPH04321562A (ja) * | 1991-04-22 | 1992-11-11 | Sumitomo Electric Ind Ltd | 窒化珪素系焼結体およびその製造方法 |
JPH06100306A (ja) * | 1992-09-22 | 1994-04-12 | Toray Ind Inc | サイアロン結晶粒子および複合セラミックス焼結体 |
JPH06305840A (ja) * | 1993-04-27 | 1994-11-01 | Kyocera Corp | 窒化珪素質焼結体及びその製造方法 |
JPH09155415A (ja) * | 1995-12-08 | 1997-06-17 | Hitachi Metals Ltd | セラミックスローラ |
JPH1029868A (ja) * | 1996-07-15 | 1998-02-03 | Honda Motor Co Ltd | 窒化珪素複合焼結体及びその製造方法 |
JP2002263915A (ja) * | 2001-03-05 | 2002-09-17 | Ngk Spark Plug Co Ltd | 窒化珪素質切削工具 |
JP2002307208A (ja) * | 2001-04-06 | 2002-10-23 | Ngk Spark Plug Co Ltd | 窒化珪素質焼結体製切削工具 |
JP2003267787A (ja) * | 2002-03-12 | 2003-09-25 | Toshiba Tungaloy Co Ltd | β´−サイアロン基セラミックス工具およびその製造方法 |
JP2004527434A (ja) * | 2000-11-28 | 2004-09-09 | ケンナメタル インコーポレイテッド | イッテルビウムを含有するSiAlON及びその生成方法 |
Family Cites Families (40)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1600602A (en) | 1977-03-17 | 1981-10-21 | Lucas Industries Ltd | Tool tip for a machine tool |
US4323232A (en) * | 1977-09-26 | 1982-04-06 | Acro Matic, Inc. | Exercising method |
US4563433A (en) * | 1982-02-22 | 1986-01-07 | Kennametal Inc. | Ceramic material and method of manufacture |
JPS6011288A (ja) † | 1983-06-30 | 1985-01-21 | 三菱マテリアル株式会社 | 表面被覆サイアロン基セラミツクス工具部材 |
DE8321120U1 (de) † | 1983-07-22 | 1983-12-29 | Wilhelm Link GmbH & Co KG Stahlrohrmöbel, 7475 Meßstetten | Gasdruckfeder mit sicherungsvorrichtung |
SE451581B (sv) * | 1984-04-06 | 1987-10-19 | Sandvik Ab | Keramiskt material huvudsakligen baserat pa kiselnitrid, aluminiumnitrid och aluminiumoxid |
US4946807A (en) * | 1986-08-18 | 1990-08-07 | Ngk Spark Plug Co., Ltd. | Composite ceramic material reinforced with silicon carbide whiskers |
US4880755A (en) † | 1987-05-19 | 1989-11-14 | Kennametal Inc. | Sialon cutting tool composition |
US4826791A (en) † | 1987-05-29 | 1989-05-02 | Kennametal Inc. | Silicon carbide-alpha prime sialon beta prime sialon |
JP2719941B2 (ja) † | 1988-11-24 | 1998-02-25 | 日本特殊陶業株式会社 | 窒化珪素焼結体 |
US5316856A (en) * | 1988-12-03 | 1994-05-31 | Ngk Spark Plug Co., Ltd. | Silicon nitride base sintered body |
JP3266200B2 (ja) | 1989-01-12 | 2002-03-18 | 日本特殊陶業株式会社 | 窒化珪素基焼結体 |
JPH0383865A (ja) † | 1989-08-25 | 1991-04-09 | Toyota Central Res & Dev Lab Inc | 窒化珪素質焼結体およびその製造方法 |
GB2243364B (en) † | 1990-04-06 | 1994-06-15 | Ube Industries | Sialon-based sintered body and process for producing same |
DE4119391A1 (de) | 1991-06-12 | 1992-12-17 | Knorr Bremse Ag | Klotzbremseinheit fuer schienenfahrzeuge |
JP3107168B2 (ja) | 1991-08-06 | 2000-11-06 | 東芝タンガロイ株式会社 | 工具用被覆窒化ケイ素焼結体 |
US5227346A (en) * | 1992-03-06 | 1993-07-13 | The Dow Chemical Company | Sialon composites and method of preparing the same |
JP3198662B2 (ja) * | 1992-09-21 | 2001-08-13 | 住友電気工業株式会社 | 窒化ケイ素系焼結体及びその製造方法 |
US5370716A (en) | 1992-11-30 | 1994-12-06 | Kennamental Inc. | High Z sialon and cutting tools made therefrom and method of using |
US5382273A (en) * | 1993-01-15 | 1995-01-17 | Kennametal Inc. | Silicon nitride ceramic and cutting tool made thereof |
US5424256A (en) * | 1993-03-17 | 1995-06-13 | Sumitomo Electric Industries, Ltd. | Silicon nitride sintered body |
SE506151C2 (sv) | 1996-03-18 | 1997-11-17 | Sandvik Ab | Sintrat keramiskt material omfattande sialonkorn samt metod för dess framställning |
US5965471A (en) † | 1997-03-17 | 1999-10-12 | Sandvik Ab | Wear and thermal shock resistant SiAION cutting tool material |
JPH09295869A (ja) * | 1996-04-26 | 1997-11-18 | Nippon Cement Co Ltd | 耐衝撃性に優れたサイアロンセラミックス及びその製 造方法 |
KR100235203B1 (ko) † | 1997-03-15 | 1999-12-15 | 배문한 | 표면이 개질된 사이알론 복합체 및 그것의 제조 방법 |
JPH11335168A (ja) | 1998-05-27 | 1999-12-07 | Kyocera Corp | 高靱性セラミック質焼結体 |
US6471734B1 (en) * | 1998-07-09 | 2002-10-29 | Kennametal Pc Inc. | Ceramic and process for the continuous sintering thereof |
JP2000143351A (ja) | 1998-10-30 | 2000-05-23 | Kyocera Corp | 高靭性窒化珪素質焼結体 |
US7072888B1 (en) * | 1999-06-16 | 2006-07-04 | Triogo, Inc. | Process for improving search engine efficiency using feedback |
JP4070417B2 (ja) | 2000-03-31 | 2008-04-02 | 日本特殊陶業株式会社 | 窒化珪素質部材及びその製造方法並びに切削工具 |
CA2422179C (en) * | 2000-10-02 | 2008-07-08 | Indexable Cutting Tools Of Canada Limited | Siaion material and cutting tools made thereof |
US20020076284A1 (en) * | 2000-10-19 | 2002-06-20 | Ngk Spark Plug Co., Ltd. | Cutting tool |
JP2002192404A (ja) | 2000-10-19 | 2002-07-10 | Ngk Spark Plug Co Ltd | 切削工具 |
US7099860B1 (en) * | 2000-10-30 | 2006-08-29 | Microsoft Corporation | Image retrieval systems and methods with semantic and feature based relevance feedback |
US7049256B2 (en) * | 2000-11-28 | 2006-05-23 | Kennametal Inc. | SiAlON containing ytterbium and method of making |
US7094717B2 (en) * | 2000-11-28 | 2006-08-22 | Kennametal Inc. | SiAlON containing ytterbium and method of making |
JP2002192403A (ja) | 2000-12-27 | 2002-07-10 | Hitachi Tool Engineering Ltd | 多層被覆工具 |
JP4003468B2 (ja) * | 2002-02-05 | 2007-11-07 | 株式会社日立製作所 | 適合性フィードバックによる類似データ検索方法および装置 |
KR20030096057A (ko) † | 2002-06-13 | 2003-12-24 | 니혼도꾸슈도교 가부시키가이샤 | 질화규소 소결체, 절삭 팁, 내마모성 부재, 절삭공구 및질화규소 소결체의 제조방법 |
WO2005016847A1 (de) † | 2003-08-07 | 2005-02-24 | Ceramtec Ag Innovative Ceramic Engineering | Werkstoff auf basis von sialonen |
-
2005
- 2005-12-22 CN CN2005800445856A patent/CN101087670B/zh active Active
- 2005-12-22 EP EP05820104A patent/EP1837105A4/en not_active Withdrawn
- 2005-12-22 US US11/793,500 patent/US20080119349A1/en not_active Abandoned
- 2005-12-22 WO PCT/JP2005/023589 patent/WO2006068220A1/ja active Application Filing
- 2005-12-22 EP EP11180944.8A patent/EP2402098B2/en active Active
Patent Citations (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS63260869A (ja) * | 1986-08-18 | 1988-10-27 | 日本特殊陶業株式会社 | 炭化珪素ウイスカ−強化複合材料 |
JPH0446062A (ja) * | 1990-06-11 | 1992-02-17 | Hitachi Metals Ltd | サイアロン焼結体およびその製造方法ならびにこれを用いたガスタービン翼 |
JPH04321562A (ja) * | 1991-04-22 | 1992-11-11 | Sumitomo Electric Ind Ltd | 窒化珪素系焼結体およびその製造方法 |
JPH06100306A (ja) * | 1992-09-22 | 1994-04-12 | Toray Ind Inc | サイアロン結晶粒子および複合セラミックス焼結体 |
JPH06305840A (ja) * | 1993-04-27 | 1994-11-01 | Kyocera Corp | 窒化珪素質焼結体及びその製造方法 |
JPH09155415A (ja) * | 1995-12-08 | 1997-06-17 | Hitachi Metals Ltd | セラミックスローラ |
JPH1029868A (ja) * | 1996-07-15 | 1998-02-03 | Honda Motor Co Ltd | 窒化珪素複合焼結体及びその製造方法 |
JP2004527434A (ja) * | 2000-11-28 | 2004-09-09 | ケンナメタル インコーポレイテッド | イッテルビウムを含有するSiAlON及びその生成方法 |
JP2002263915A (ja) * | 2001-03-05 | 2002-09-17 | Ngk Spark Plug Co Ltd | 窒化珪素質切削工具 |
JP2002307208A (ja) * | 2001-04-06 | 2002-10-23 | Ngk Spark Plug Co Ltd | 窒化珪素質焼結体製切削工具 |
JP2003267787A (ja) * | 2002-03-12 | 2003-09-25 | Toshiba Tungaloy Co Ltd | β´−サイアロン基セラミックス工具およびその製造方法 |
Non-Patent Citations (1)
Title |
---|
See also references of EP1837105A4 * |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1939155A3 (en) * | 2006-12-27 | 2011-04-13 | Sandvik Intellectual Property AB | Ceramic material and cutting tools made thereof for toughness demanding operations |
EP1939154A3 (en) * | 2006-12-27 | 2011-04-20 | Sandvik Intellectual Property AB | Ceramic material and cutting tools made thereof for applications demanding good notch wear resistance |
Also Published As
Publication number | Publication date |
---|---|
CN101087670A (zh) | 2007-12-12 |
EP1837105A1 (en) | 2007-09-26 |
US20080119349A1 (en) | 2008-05-22 |
EP2402098B2 (en) | 2021-03-03 |
CN101087670B (zh) | 2011-07-20 |
EP2402098B1 (en) | 2014-04-30 |
EP2402098A1 (en) | 2012-01-04 |
EP1837105A4 (en) | 2011-03-16 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
WO2006068220A1 (ja) | サイアロン製インサート及びこれを備えた切削工具 | |
JP5428118B2 (ja) | cBN焼結体及びcBN焼結体工具 | |
CA2577615A1 (en) | Cbn sintered body for high surface integrity machining and cbn sintered body cutting tool | |
KR101609090B1 (ko) | 사이알론 소결체 및 절삭 인서트 | |
EP2957368B1 (en) | Cutting tool | |
JP4716855B2 (ja) | サイアロン製切削工具及びこれを備えた工具 | |
JPWO2008026641A1 (ja) | 酸化アルミニウム基複合焼結体及び切削インサート | |
KR20170122103A (ko) | 소결체 및 절삭 공구 | |
JP6161830B2 (ja) | サイアロン焼結体及び切削インサート | |
JP2006305708A (ja) | サイアロン製スローアウェイチップおよび切削工具 | |
JP2004026555A (ja) | 立方晶窒化ホウ素含有焼結体およびその製造方法 | |
JP4434938B2 (ja) | サイアロン製インサートの製造方法 | |
JP4342975B2 (ja) | サイアロン質工具、切削インサート、及び切削工具 | |
JP2006198761A (ja) | サイアロン製インサート及びこれを備えた切削工具 | |
KR19990063395A (ko) | 세라믹 절삭 공구 | |
JP2015009327A (ja) | 切削インサート | |
JP6938227B2 (ja) | 窒化珪素質複合焼結体、切削工具、及び摩擦攪拌接合用工具 | |
WO2019065372A1 (ja) | セラミックス焼結体、インサート、切削工具、及び摩擦攪拌接合用工具 | |
JP2006193353A (ja) | アルミナ焼結体、切削インサートおよび切削工具 | |
JP7451350B2 (ja) | エンドミル及び摩擦攪拌接合用工具 | |
JP3560629B2 (ja) | 工具用高靱性硬質焼結体の製造法 | |
JP2002192405A (ja) | 切削工具 | |
JP2007130699A (ja) | サイアロン切削工具及び工具 | |
JP2001253767A (ja) | アルミナ基複合焼結体及び耐摩耗部材並びにアルミナ基複合焼結体の製造方法 | |
JPH08112705A (ja) | 窒化ケイ素質焼結体製切削工具およびその製造方法 |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
AK | Designated states |
Kind code of ref document: A1 Designated state(s): AE AG AL AM AT AU AZ BA BB BG BR BW BY BZ CA CH CN CO CR CU CZ DE DK DM DZ EC EE EG ES FI GB GD GE GH GM HR HU ID IL IN IS KE KG KM KN KP KR KZ LC LK LR LS LT LU LV LY MA MD MG MK MN MW MX MZ NA NG NI NO NZ OM PG PH PL PT RO RU SC SD SE SG SK SL SM SY TJ TM TN TR TT TZ UA UG US UZ VC VN YU ZA ZM ZW |
|
AL | Designated countries for regional patents |
Kind code of ref document: A1 Designated state(s): BW GH GM KE LS MW MZ NA SD SL SZ TZ UG ZM ZW AM AZ BY KG KZ MD RU TJ TM AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IS IT LT LU LV MC NL PL PT RO SE SI SK TR BF BJ CF CG CI CM GA GN GQ GW ML MR NE SN TD TG |
|
121 | Ep: the epo has been informed by wipo that ep was designated in this application | ||
WWE | Wipo information: entry into national phase |
Ref document number: 11793500 Country of ref document: US |
|
WWE | Wipo information: entry into national phase |
Ref document number: 200580044585.6 Country of ref document: CN |
|
NENP | Non-entry into the national phase |
Ref country code: DE |
|
WWE | Wipo information: entry into national phase |
Ref document number: 2005820104 Country of ref document: EP |
|
WWP | Wipo information: published in national office |
Ref document number: 2005820104 Country of ref document: EP |
|
WWP | Wipo information: published in national office |
Ref document number: 11793500 Country of ref document: US |