WO2018062051A1 - Corps fritté en composite de carbure de silicium et procédé pour sa fabrication - Google Patents

Corps fritté en composite de carbure de silicium et procédé pour sa fabrication Download PDF

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WO2018062051A1
WO2018062051A1 PCT/JP2017/034371 JP2017034371W WO2018062051A1 WO 2018062051 A1 WO2018062051 A1 WO 2018062051A1 JP 2017034371 W JP2017034371 W JP 2017034371W WO 2018062051 A1 WO2018062051 A1 WO 2018062051A1
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carbon
less
silicon carbide
sintered body
composite sintered
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PCT/JP2017/034371
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English (en)
Japanese (ja)
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友 山内
池田 吉紀
淳史 添田
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帝人株式会社
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Priority to JP2018542524A priority Critical patent/JP6695436B2/ja
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    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B35/00Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
    • C04B35/515Shaped 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
    • C04B35/56Shaped 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 carbides or oxycarbides
    • C04B35/565Shaped 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 carbides or oxycarbides based on silicon carbide
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B35/00Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
    • C04B35/71Ceramic products containing macroscopic reinforcing agents
    • C04B35/78Ceramic products containing macroscopic reinforcing agents containing non-metallic materials
    • C04B35/80Fibres, filaments, whiskers, platelets, or the like
    • HELECTRICITY
    • H05ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05KPRINTED CIRCUITS; CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS
    • H05K9/00Screening of apparatus or components against electric or magnetic fields

Definitions

  • the present invention relates to a silicon carbide composite sintered body and a method for producing the same.
  • the present invention relates to a silicon carbide composite sintered body useful as an electromagnetic wave absorber that absorbs high frequencies in the gigahertz (GHz) region and a method for manufacturing the same.
  • GHz gigahertz
  • noise generated from digital electronic devices, automobiles, marine aircraft, etc. is also becoming higher in the GHz band. Such noise causes problems such as malfunction of electronic devices, information leakage, and radio interference.
  • the electromagnetic wave absorber is required to have weather resistance, heat resistance, impact resistance, wear resistance, and the like in order to be installed in various devices, moving bodies, buildings, and the like.
  • Patent Document 1 discloses an electromagnetic wave absorber including a resin and graphite. Such an electromagnetic wave absorber may not have sufficient hardness and heat resistance.
  • Silicon carbide is known as an electromagnetic wave absorber having hardness and heat resistance.
  • Patent Document 2 discloses an electromagnetic wave absorber that is a silicon carbide sintered body obtained by sintering silicon carbide powder.
  • silicon carbide is used as a starting material, and it is expensive to produce a large-area electromagnetic wave absorber.
  • Patent Document 3 discloses an electromagnetic wave absorber in which silicon carbide powder is dispersed in a resin matrix. This electromagnetic wave absorber may not have sufficient hardness and heat resistance.
  • Patent Document 4 discloses that a silicon carbide powder including a step of heating a particle comprising silica and carbon in an Atchison furnace to obtain a silicon carbide powder, and a step of sintering the silicon carbide powder.
  • a method for producing a knot is disclosed.
  • Patent Document 5 discloses a method of directly reacting silicon powder and carbon powder.
  • An object of the present invention is to provide a novel silicon carbide composite sintered body useful as an electromagnetic wave absorber and a method for producing the same.
  • ⁇ Aspect 1 A silicon carbide composite sintered body containing carbon fibers as a first carbon-based material.
  • ⁇ Aspect 2 The silicon carbide composite sintered body according to aspect 1, wherein the first carbon-based material is in the form of dispersed short fibers, or in the form of a woven fabric or a non-woven fabric.
  • ⁇ Aspect 3 Aspect 1 or 2 in which the real part of the complex relative permittivity is 5 or more and 200 or less and the imaginary part of the complex relative permittivity is 1 or more and 150 or less at at least one frequency in the frequency region of 1 GHz or more and 150 GHz or less. 2.
  • ⁇ Aspect 4 The silicon carbide composite-fired according to any one of aspects 1 to 3, wherein the volume resistivity of the first carbon-based material is 1 ⁇ 10 ⁇ 6 ⁇ ⁇ cm or more and 1 ⁇ 10 3 ⁇ ⁇ cm or less. Union.
  • ⁇ Aspect 5 An electromagnetic wave absorber comprising the silicon carbide composite sintered body according to any one of embodiments 1 to 4.
  • ⁇ Aspect 6 In any one of aspects 1 to 4, the method includes sintering the carbon fiber that is the first carbon-based material and the sintering composition containing at least the silicon nanoparticles and the second carbon-based material. The manufacturing method of the silicon carbide compound sintered compact of description.
  • ⁇ Aspect 7 The manufacturing method according to aspect 6, wherein the sintering is performed while pressure-molding the composition for sintering and the first carbon-based material.
  • ⁇ Aspect 8 The manufacturing method according to aspect 6 or 7, wherein the sintering is performed at 1400 ° C or higher.
  • ⁇ Aspect 9 The production method according to any one of Embodiments 6 to 8, wherein the silicon nanoparticles have an average particle size of less than 200 nm.
  • ⁇ Aspect 10 >> The production method according to any one of aspects 6 to 9, wherein the second carbon-based material is a carbon nanofiber having a diameter of 100 nm to 900 nm.
  • ⁇ Aspect 11 The production method according to any one of embodiments 6 to 10, wherein the one carbon-based material is a carbon fiber in the form of a short fiber, or a carbon fiber in the form of a woven fabric or a non-woven fabric.
  • FIG. 1A shows high-frequency reflection characteristics and transmission characteristics of the composite sintered body of Example 1, and FIG. 1B shows reflection transmission attenuation.
  • 2A shows high-frequency reflection characteristics and transmission characteristics of the composite sintered body of Comparative Example 1, and FIG. 2B shows reflection transmission attenuation.
  • the silicon carbide composite sintered body of the present invention includes carbon fibers that are first carbon-based materials.
  • the silicon carbide composite sintered body of the present invention may include a carbon fiber layer in which carbon fibers are present in layers. Further, the carbon fibers may be dispersed throughout the sintered body, and in this case, the carbon fibers may be in the form of short fibers.
  • the carbon fiber layer may be sandwiched between silicon carbides, or may exist in a form in which silicon carbide enters between the fibers in the carbon fiber layer. Good.
  • the carbon fibers are present in the form of a woven fabric or a non-woven fabric rather than being dispersed in the silicon carbide.
  • carbon fibers when carbon fibers are dispersed throughout the sintered body, there may be a plurality of layers having different abundance ratios of carbon fibers, and the ratio of carbon fibers in the sintered body It may be different depending on the position.
  • the silicon carbide composite sintered body of the present invention can be obtained by a relatively easy manufacturing method and is very useful as an electromagnetic wave absorber.
  • the silicon carbide composite sintered body of the present invention can have high electromagnetic wave absorption characteristics, and can also have weather resistance, heat resistance, impact resistance, wear resistance, and the like. Therefore, the silicon carbide composite sintered body of the present invention is useful as an electromagnetic wave absorber. Therefore, this invention relates also to the use or usage method of such a silicon carbide sintered body in an electromagnetic wave absorber.
  • the silicon carbide composite sintered body of the present invention can have a high complex relative dielectric constant particularly in a high frequency region.
  • a thin and lightweight electromagnetic wave absorber can be designed.
  • an imaginary part with a high complex dielectric constant high electromagnetic wave absorption characteristics can be imparted to the silicon carbide composite sintered body due to high dielectric loss.
  • the real part of the complex relative dielectric constant may be 5 or more, 10 or more, or 15 or more in the high frequency region. 200 or less, 150 or less, 100 or less, 80 or less, 60 or less, 50 or less, or 40 or less, and the imaginary part of the complex dielectric constant is 1 or more, 1.5 or more, 2 or more, or 3 It may be 150 or less, 100 or less, 80 or less, 50 or less, 40 or less, 30 or less, or 10 or less.
  • the high frequency region in which the silicon carbide composite sintered body of the present invention satisfies the above dielectric constant may be 1 GHz or more, 3 GHz or more, 5 GHz or more, or 10 GHz or more, 150 GHz or less, 120 GHz or less, 100 GHz.
  • it may be 90 GHz or less, 80 GHz or less, 50 GHz or less, 30 GHz or less, 20 GHz or less, 10 GHz or less, or 5 GHz or less.
  • the dielectric loss tangent (tan ⁇ ) of the silicon carbide composite sintered body of the present invention may be 0.01 or more, 0.02 or more, 0.05 or more, 0.1 or more, or 0.2 or more, or 10 or less. It may be 5 or less, 1 or less, or 0.5 or less.
  • the complex dielectric constant is measured by the coaxial tube method in the present invention.
  • the thermal conductivity at room temperature of the silicon carbide composite sintered body of the present invention can have a high thermal conductivity, for example, 20 W / (m ⁇ K) or more, 30 W / (m ⁇ K) or more, 50 W / ( m ⁇ K) or more, 80 W / (m ⁇ K) or more, 100 W / (m ⁇ K) or more, 200 W / (m ⁇ K) or more, or 300 W / (m ⁇ K) or more, and 1000 W / It may be (m ⁇ K) or less, 500 W / (m ⁇ K) or less, 300 W / (m ⁇ K) or less, 200 W / (m ⁇ K) or less, or 100 W / (m ⁇ K) or less.
  • the silicon carbide composite sintered body of the present invention can have high electromagnetic wave absorption characteristics particularly in a high frequency region.
  • a high frequency region may be 1 GHz or more, 3 GHz or more, 5 GHz or more, or 10 GHz or more, and may be 100 GHz or less, 90 GHz or less, 80 GHz or less, 50 GHz or less, 30 GHz or less, or 20 GHz or less. .
  • the silicon carbide composite sintered body of the present invention has an electromagnetic wave absorptivity of 10 dB or more at at least one point in the frequency region described above.
  • the electromagnetic wave absorption rate is measured by a microstrip line method.
  • the silicon carbide composite sintered body of the present invention can contain one or more silicon carbides having different crystal structures.
  • Examples of such a crystal structure may be, for example, ⁇ -type silicon carbide (2H, 4H, 6H, 16H, etc.) or ⁇ -type (3C) silicon carbide.
  • the silicon carbide contained in the silicon carbide composite sintered body may be composed of a single crystal structure or may be composed of a plurality of different crystal structures.
  • the silicon carbide composite sintered body of the present invention may be porous or dense.
  • the silicon carbide composite sintered body is porous, it is possible to provide an electromagnetic wave absorber that is lightweight and has good workability while having sufficient strength.
  • an electromagnetic wave absorber having high strength and high thermal conductivity can be provided.
  • the porosity of the silicon carbide composite sintered body of the present invention may be 1% or less, 3% or less, 5 %% or less, 10% or less, 30% or less, 50% or less, or 70% or less. % Or more, 1% or more, 3% or more, 5% or more, 10% or more, 20% or more, or 30% or more. In this case, the porosity is calculated on the basis of the formula “(1 ⁇ actual density / theoretical density when completely dense) ⁇ 100 (%)”.
  • Examples of the carbon fiber that is the first carbon-based material include polyacrylonitrile-based carbon fibers obtained by heating and carbonizing polyacrylonitrile fibers at a high temperature in a nitrogen atmosphere, and pitch-based carbon fibers. Can do. Among these, it is particularly preferable to use pitch-based carbon fibers.
  • the carbon fiber that is the first carbon-based material may be a single carbon fiber or a combination of a plurality of different carbon fibers.
  • the diameter of the carbon fiber may be 1 ⁇ m or more, 2 ⁇ m or more, 3 ⁇ m or more, 5 ⁇ m or more, or 10 ⁇ m or more, or 30 ⁇ m or less, 20 ⁇ m or less, 10 ⁇ m or less, 5 ⁇ m or less, or 3 ⁇ m or less.
  • the length of the carbon fiber may be 1 ⁇ m or more, 2 ⁇ m or more, 5 ⁇ m or more, 10 ⁇ m or more, 20 ⁇ m or more, or 50 ⁇ m or more, 50 mm or less, 30 mm or less, 20 mm or less, 15 mm or less, 50 mm or less, or 10 mm or less. It may be.
  • the volume resistivity of the carbon fiber may be 1 ⁇ 10 ⁇ 9 ⁇ ⁇ cm or more, 1 ⁇ 10 ⁇ 7 ⁇ ⁇ cm or more, or 1 ⁇ 10 ⁇ 6 ⁇ ⁇ cm or more, and 1 ⁇ 10 3 ⁇ It may be cm or less, 1 ⁇ ⁇ cm or less, 0.1 ⁇ ⁇ cm or less, or 0.01 ⁇ ⁇ cm or less.
  • the thermal conductivity of the carbon fiber at room temperature is, for example, 50 W / (m ⁇ K) or more, 80 W / (m ⁇ K) or more, 100 W / (m ⁇ K) or more, or 200 W / (m ⁇ K) or more. 1000 W / (m ⁇ K) or less, 500 W / (m ⁇ K) or less, 300 W / (m ⁇ K) or less, 200 W / (m ⁇ K) or less, or 100 W / (m ⁇ K) It may be the following.
  • the thickness may be 0.05 mm or more, 0.10 mm or more, or 0.20 m or more, and 3.0 mm or less. 1.0 mm or less, or 0.50 mm or less.
  • the first carbon-based material is carbon fiber in the form of a woven or non-woven fabric, only one or a plurality of woven or non-woven fabrics may be used.
  • the silicon carbide composite sintered body of the present invention may be used alone as an electromagnetic wave absorber, or may be used in a form in which a plurality of silicon carbide composite sintered bodies having different complex relative dielectric constants are laminated. .
  • the silicon carbide composite sintered body can be used for a wide high frequency band electromagnetic wave, a wide range of incident angle electromagnetic waves, and / or a wide range of polarization characteristics. It can have high electromagnetic wave absorption performance with respect to the characteristic electromagnetic waves.
  • the silicon carbide composite sintered body of the present invention may be used as a radio wave shielding structure having not only electromagnetic wave absorptivity but also electromagnetic wave shielding properties when used together with a conductive base material.
  • a radio wave shielding structure having not only electromagnetic wave absorptivity but also electromagnetic wave shielding properties when used together with a conductive base material.
  • the base material etc. which have electroconductive materials, such as a metal base material, a conductive polymer base material, and carbon, can be mentioned.
  • the silicon carbide composite sintered body of the present invention may have a shape other than a plane on the incident surface side of the electromagnetic wave for the purpose of matching with the characteristic impedance of air.
  • a shape is not particularly limited, and examples thereof include a wedge type, a pyramid type, a swell type, a honeycomb type, and a multilayer core type structure.
  • the silicon carbide composite sintered body of the present invention may be used as a laminate having a matching layer for matching with the characteristic impedance of air on the electromagnetic wave incident surface side.
  • the complex relative permittivity of the matching layer is smaller in the real part and / or the imaginary part in the frequency band region intended for electromagnetic wave absorption than the silicon carbide composite sintered body of the present invention.
  • a material having a value can be preferably used.
  • the material of the matching layer is not particularly limited, and examples thereof include a resin containing a conductive material, a foamed resin, a silicon carbide composite sintered body, a porous silicon carbide composite sintered body, and the like.
  • the shape of the interface of the matching layer with air may have a shape other than a plane for the purpose of matching with the characteristic impedance of the air.
  • a shape is not particularly limited, and examples thereof include a wedge type, a pyramid type, a swell type, a honeycomb type, and a multilayer core type.
  • the method for producing a silicon carbide composite sintered body of the present invention includes carbon fibers that are first carbon-based materials, silicon nanoparticles having an average particle size of less than 200 nm, and second carbon-based materials.
  • a silicon carbide composite sintered body is obtained by sintering a sintering composition containing at least a certain carbon-based material.
  • the method for producing a silicon carbide composite sintered body of the present invention is to prepare a sintering composition containing at least silicon nanoparticles having an average particle size of less than 200 nm and a carbon-based material that is a second carbon-based material.
  • the silicon carbide composite sintered body as described above may be obtained by sintering the sintering composition and the carbon fiber that is the first carbon-based material.
  • both the first carbon-based material and the second carbon-based material may be carbon fibers; even if the first carbon-based material is carbon fiber and the second carbon-based material is not used.
  • the second carbon-based material may be a carbon-based material other than carbon fiber.
  • the carbon fibers of the first carbon-based material may be in the form of short fibers.
  • the production method of the present invention includes sintering the sintering composition and the first carbon-based material.
  • the third component other than the sintering composition and the first carbon-based material may be sintered together.
  • the carbon fiber as the first carbon-based material may be preliminarily dispersed in the sintering composition in the form of short fibers or the like;
  • the carbon-based material may be impregnated with, for example, woven or non-woven carbon fiber, and the sintering composition may be present between the first carbon-based materials;
  • the carbonaceous material may be in the form of a sandwich, or the sintering composition may be present on the paste or powder on the first carbonaceous material.
  • the sintering temperature may be 1900 ° C or higher, 2000 ° C or higher, 2100 ° C or higher, or 2200 ° C or higher, 2500 ° C or lower, 2300 ° C or lower, or 2100 ° C or lower. May be.
  • the sintering temperature may be 1300 ° C. or higher, 1350 ° C. or higher, 1400 ° C. or higher, or 1500 ° C. or higher, 1800 ° C. or lower, 1600 ° C. or lower, 1500 ° C. or lower. Or 1400 ° C. or lower.
  • the sintering atmosphere is preferably performed in an inert atmosphere such as argon gas or nitrogen gas in order to sufficiently react the raw material silicon nanoparticles with the second carbon-based material.
  • an inert atmosphere such as argon gas or nitrogen gas
  • the sintering time is preferably a time until the silicon nanoparticles as a raw material and the carbon-based material sufficiently react.
  • the sintering time may be 10 minutes or more, 30 minutes or more, 1 hour or more, or 2 hours or more. It may be 1 day or less, 12 hours or less, 6 hours or less, 3 hours or less, 2 hours or less, or 1 hour or less.
  • the production method of the present invention may further include a step of pressure-molding the sintering composition and the first carbon-based material into a predetermined shape.
  • the pressure forming means the sinter composition and the first carbon-based material are put into a mold, and the uniaxial pressure forming method, the hot press method, the cold isostatic pressing method (CIP) in which the pressure is formed. Law).
  • the molding temperature can be appropriately selected depending on the molding means, but it may be performed at room temperature, may be heated, or may be performed simultaneously with the following sintering step.
  • the molding pressure may be, for example, 10 MPa or more, 30 MPa or more, 50 MPa or more, 100 MPa or more, or 200 MPa or more, or 900 MPa or less, 800 MPa or less, 600 MPa or less, 400 MPa or less, or 200 MPa or less.
  • mold According to the use to which the silicon carbide compound sintered body obtained is applied, it can process into arbitrary shapes.
  • the sintering step under pressure.
  • pressure molding is performed by the CIP method, and then 200 MPa or less by a hot isostatic pressing method (HIP method) or the like. It is preferable to perform the baking under the pressure condition in (1). It is also preferable to add the sintering composition and the first carbon-based material to the mold and perform firing under a pressurized condition by a hot press method.
  • the composition for sintering contains at least silicon nanoparticles and a second carbon-based material.
  • This composition for sintering may be in the form of a powder of silicon nanoparticles and the second carbon-carbon material, in the form of a paste, or in the form of a dispersion.
  • this composition may contain a solvent, and the type of the solvent is not particularly limited as long as the silicon nanoparticles and the carbon-based material can be dispersed.
  • the solvent include an aqueous solvent and an organic solvent.
  • examples of the aqueous solvent include water or alcohol solvents such as methanol, ethanol, isopropyl alcohol, and butanol.
  • examples of the organic solvent include hydrocarbon solvents such as toluene, xylene, hexane, cyclohexane, mesitylene, and tetralin.
  • ester solvents such as ethyl acetate, butyl acetate, methyl 3-methoxypropionate and the like
  • ketone solvents such as methyl ethyl ketone and methyl isobutyl ketone.
  • amine solvents such as N, N-dimethylformamide, N, N-dimethylacetamide, N-methyl-2-pyrrolidone and the like
  • acetate solvents such as propylene glycol monomethyl ether acetate
  • other polar solvents such as dimethyl A sulfoxide etc.
  • This composition may include a third component other than the silicon nanoparticles and the second carbon-carbon material.
  • the ratio of the number of moles of carbon of the second carbonaceous material to the number of moles of silicon contained in the composition may be about 1.0, whereby the first after sintering. Silicon carbide may be obtained while substantially leaving the carbon-based material. As long as the first carbon-based material can remain, this molar ratio is 0.10 or more, 0.30 or more, 0.50 or more, 0.80 or more, 1.0 or more, 1.5 or more, or 2. It may be 0 or more, and may be 10.0 or less, 5.0 or less, 3.0 or less, 2.0 or less, 1.5 or less, 1.0 or less, 0.80 or less, or 0.50 or less. May be.
  • silicon nanoparticles By using silicon nanoparticles, a silicon carbide sintered body can be obtained at a relatively low sintering temperature. Without being limited by theory, the reason why silicon carbide can be obtained at a low sintering temperature is that the number of reaction sites with the second carbon-based material using silicon nanoparticles having a small average particle diameter is increased, and thus the reaction proceeds. It is thought to be easy.
  • the average particle diameter of the silicon nanoparticles used in the present invention can be less than 200 nm, 150 nm or less, 100 nm or less, 50 nm or less, 20 nm or less, or 5 nm or less.
  • the average primary particle size of the semiconductor particles used in the present invention may be 1 nm or more, 3 nm or more, 5 nm or more, or 10 nm or more.
  • the average particle diameter of the particles and the average diameter of the fibers are directly projected based on the photographed image by observation with a scanning electron microscope (SEM), a transmission electron microscope (TEM), or the like.
  • SEM scanning electron microscope
  • TEM transmission electron microscope
  • silicon nanoparticles examples include silicon nanoparticles that are preferably obtained by a laser pyrolysis method.
  • silicon nanoparticles for example, particles described in JP-T-2010-514585 can be used. This document is incorporated herein by reference.
  • a characteristic of silicon nanoparticles obtained by laser pyrolysis is the high degree of circularity of primary particles.
  • the circularity may be 0.80 or more, 0.90 or more, 0.93 or more, 0.95 or more, 0.97 or more, 0.98 or more, or 0.99 or more.
  • the circularity is measured by measuring the projected area (S) of the particle and the perimeter (l) of the particle from an image taken by observation with a scanning electron microscope (SEM), a transmission electron microscope (TEM), etc. using image processing software or the like. Then, (4 ⁇ S) / l2 can be calculated and obtained. In this case, the circularity can be obtained as an average value of 100 or more particle groups.
  • silicon nanoparticles having a circularity of 0.80 or more, 0.90 or more, 0.93 or more, 0.95 or more, 0.97 or more, 0.98 or more, or 0.99 or more are preferable. Can be used. By using silicon nanoparticles having a high degree of circularity, it is considered that the reaction with the carbon-based material further proceeds.
  • the inside of the particle is in a crystalline state and the particle surface is in an amorphous state. This can give unique physical properties to various articles in which silicon nanoparticles are used.
  • the silicon nanoparticles used in the present invention are preferably pre-doped with boron.
  • the present inventors have found that the silicon nanoparticle is doped with boron, whereby the crystal grain size of the resulting silicon carbide is increased. Without being limited to theory, it is believed that this is because boron functions as a sintering aid and promotes crystal growth.
  • the dopant concentration may be 10 17 atoms / cm 3 or more, 10 18 atoms / cm 3 or more, 10 19 atoms / cm 3 or more, or 1 ⁇ 10 20 atoms / cm 3 or more in silicon nanoparticles. It may be 1 ⁇ 10 22 atom / cm 3 or less, 1 ⁇ 10 21 atom / cm 3 or less, 1 ⁇ 10 20 atom / cm 3 or less, or 1 ⁇ 10 19 atom / cm 3 or less.
  • impurities of silicon nanoparticles such as aluminum, calcium, chromium, copper, iron, lead, zinc, magnesium, manganese, molybdenum, potassium, sodium, and titanium, are each or in total, 100 ppm or less, 50 ppm or less, or 10 ppm or less. Preferably there is. Such impurities may affect properties such as the thermal conductivity of the sintered body.
  • the composition for sintering includes a second carbon-based material for the purpose of generating silicon carbide by reacting with silicon derived from silicon nanoparticles in the sintering process.
  • the second carbon-based material is not particularly limited as long as it is a material that reacts with silicon to produce silicon carbide by being sintered.
  • Examples of such a second carbon-based material include organic polymers, carbon black, graphene, activated carbon, graphite, acetylene black, and carbon fibers.
  • carbon fibers, carbon nanotubes, and carbon nanofibers can be particularly mentioned.
  • Examples of the carbon nanofiber include fibers described in JP 2010-013742 A. This document is incorporated herein by reference.
  • the diameter of the carbon nanofiber may be 10 nm or more, 20 nm or more, 30 nm or more, 50 nm or more, 100 nm or more, 200 nm or more, 300 nm or more, or 500 nm or more, 30 ⁇ m or less, 20 ⁇ m or less, 10 ⁇ m or less, 5 ⁇ m or less, or It may be 1 ⁇ m or less.
  • carbon nanofibers having a diameter of more than 900 nm and not more than 30 ⁇ m are useful, and carbon nanofibers having a diameter of not less than 100 nm and not more than 900 nm are particularly useful.
  • the carbon fiber may be used with a diameter of 1 micrometer or more and 30 micrometers or less as a 2nd carbonaceous material.
  • the carbon fiber is preferably in the form of a short fiber, and may be the same as the first carbon fiber.
  • the length is not particularly limited, but may be 1 ⁇ m or more, 2 ⁇ m or more, 5 ⁇ m or more, 10 ⁇ m or more, 20 ⁇ m or more, or 50 ⁇ m or more, or 50 mm or less. 30 mm or less, 20 mm or less, 15 mm or less, 50 mm or less, or 10 mm or less.
  • the length is appropriate, mixing with silicon nanoparticles, sintering, and the like are facilitated.
  • Impurities of the second carbon-based material such as aluminum, calcium, chromium, copper, iron, lead, zinc, magnesium, manganese, molybdenum, potassium, sodium, and titanium, respectively, or in total, 100 ppm or less, 50 ppm or less, or 10 ppm or less It is preferable that Such impurities may affect properties such as the thermal conductivity of the sintered body.
  • the second carbon-based material used in the sintering composition a single carbon-based material may be used, or a plurality of different carbon-based materials may be used.
  • characteristics of the carbon fiber that is the first carbon-based material sintered together with the sintering composition refer to the characteristics of the carbon fiber that is the first carbon-based material described for the silicon carbide composite sintered body. can do.
  • the composition for sintering composed of silicon nanoparticles and the second carbon-based material, and the solid content contained in the mixture of carbon fibers in the form of short fibers as the first carbon-based material
  • the weight ratio of the carbon fibers in the form of short fibers as the first carbon-based material is 0.1% by weight or more, 0.2% by weight or more, 0.5% by weight or more, 1% by weight or more, 2% by weight or more.
  • the carbon fiber in the form of a short fiber which is the first carbon-based material with respect to 100 parts by mass of the solid content of the composition for sintering composed of the silicon nanoparticles and the second carbon-based material is 0.1 Parts by weight, 0.2 parts by weight, 0.5 parts by weight, 1 part by weight, 2 parts by weight, 5 parts by weight, 10 parts by weight, 20 parts by weight, 30 parts by weight, or 50 parts by weight 95 parts by weight, 90 parts by weight, 80 parts by weight, 70 parts by weight, 60 parts by weight, 50 parts by weight, 40 parts by weight, 30 parts by weight, 20 parts by weight,
  • the amount can be not more than parts by weight, or not more than 15 parts by weight.
  • the composition for sintering can contain a third component other than the first carbon-based material for the purpose of imparting desired physical properties to the silicon carbide composite sintered body of the present invention.
  • a third component a single material may be selected and used, or a plurality of two or more materials may be selected and used.
  • a material intended to impart desired physical properties to the silicon carbide composite sintered body of the present invention can be selected. Therefore, examples of the third component include a conductive material, an insulating material, and a binder.
  • the weight ratio of the third component in the solid content contained in the sintering composition is not particularly limited.
  • the third component can be added to the dispersion for sintering at an arbitrary weight ratio.
  • the weight ratio of the third component in the solid content contained in the sintering composition is 0.1% by weight or more, 0.2% by weight or more, 0.5% by weight or more, 1% by weight or more, and 2% by weight. 5 wt% or more, 10 wt% or more, 20 wt% or more, 30 wt% or more, or 50 wt% or more, 95 wt% or less, 90 wt% or less, 80 wt% or less, 70 wt% % Or less, 60% or less, 50% or less, 40% or less, or 30% or less.
  • the third component materials in the form of particles, fibers, long fibers, short fibers, scales and the like can be preferably used from the viewpoint of ensuring good dispersibility in the dispersion for a sintered body.
  • the third component may be in the form of ink, slurry, or the like previously dispersed in a solvent or the like in order to facilitate mixing with the silicon nanoparticles. With such a form, mixing with silicon nanoparticles, sintering, and the like are facilitated.
  • a conductive material can be used to adjust the complex relative dielectric constant of the silicon carbide composite sintered body.
  • a conductive material include silicon, silicon carbide, metal, and the like.
  • the volume resistivity of the conductive material used as the conductive material is 1 ⁇ 10 ⁇ 9 ⁇ ⁇ cm or more, 1 ⁇ 10 ⁇ 6 ⁇ ⁇ cm or more, 1 ⁇ It may be 10 ⁇ 5 ⁇ ⁇ cm or more, or 1 ⁇ 10 ⁇ 4 ⁇ ⁇ cm or more, 1 ⁇ 10 3 ⁇ ⁇ cm or less, 1 ⁇ ⁇ cm or less, 0.1 ⁇ ⁇ cm or less, or 0.01 ⁇ ⁇ cm It may be cm or less.
  • the conductive material used as the third component contained in the sintering composition is 400 ° C, 600 ° C, 800 ° C, 1000 ° C or higher, 1200 ° C or higher, 1400 ° C or higher, 1600 ° C or higher, 1800 ° C or higher, 2000 It is possible to select a material having a melting point of not lower than ° C, or not lower than 2200 ° C, or not having a melting point under atmospheric pressure. By using a material having a melting point in this range or having no melting point under atmospheric pressure, the third component, which is a conductive material, can be stably used in the sintering process of the silicon carbide composite sintered body of the present invention. It can be present in the silicon carbide composite sintered body, and desired physical properties can be imparted to the silicon carbide composite sintered body of the present invention.
  • the semiconductor material may be previously doped with an arbitrary dopant for the purpose of obtaining a desired resistance value.
  • a doping concentration is 10 17 atoms / cm 3 or more, 10 18 atoms / cm 3 or more, 10 19 atoms / cm 3 or more, or 1 ⁇ 10 20 atoms / cm 3 or more among semiconductor materials. It may be 1 ⁇ 10 22 atom / cm 3 or less, 1 ⁇ 10 21 atom / cm 3 or less, 1 ⁇ 10 20 atom / cm 3 or less, or 1 ⁇ 10 19 atom / cm 3 or less.
  • an insulating material can be used for improving the insulating property of the silicon carbide composite sintered body and / or adjusting the complex relative dielectric constant.
  • an insulating material include alumina, silicon nitride, mica, silica, and the like.
  • a dielectric material can be used to adjust the complex relative dielectric constant of the silicon carbide composite sintered body.
  • examples of such an insulating material include alumina, silicon nitride, mica, silica, titanium oxide, zirconium oxide, silicon carbide and the like.
  • the carbon nanofibers used here were produced according to the method described in JP 2010-013742 A, had a fiber diameter of 200 to 500 nm, and had almost no fiber aggregate in which the fibers were fused. It was very dispersible.
  • the above first mixture was stirred at 2000 rpm for 20 minutes and defoamed at 2200 rpm for 5 minutes with a planetary mixer (Awatori Netaro, Shinki Co., Ltd.) to obtain a Si / CNF mixed paste.
  • the solvent in the Si / CNF mixed paste was distilled off to obtain a sintering composition composed of Si / CNF powder.
  • the above Si / CNF powder is filled into a mold of a hot press machine (HP-10X10-CC-23 type, Nemus Co., Ltd.), and a carbon fiber nonwoven fabric (manufactured by Toho Tenax Co., Ltd.) as the first carbon-based material is filled thereon BP-1030A-ES, thickness 1 mm, volume resistivity of carbon fiber 1.6 ⁇ 10 ⁇ 3 ⁇ ⁇ cm, diameter 7 ⁇ m), and Si / CNF powder is further filled thereon, 40 MPa, 2000 The resulting silicon carbide composite sintered body was held for 1 hour at a degree, and the carbon fiber nonwoven fabric remained substantially.
  • Example 1 A silicon carbide composite sintered body was obtained in the same manner as in Example 1 except that the non-woven fabric of carbon fiber as the first carbon-based material was not used.
  • Example 2 Example except that the carbon nanofiber as the second carbon-based material was changed to carbon fiber (manufactured by Toho Tenax, fiber length 6 mm, volume resistivity 1.6 ⁇ 10 ⁇ 3 ⁇ ⁇ cm, diameter 7 ⁇ m) In the same manner as in No. 1, a composite sintered body of silicon carbide was obtained.
  • Example 3 ⁇ -SiC particles (Yakushima Electric Co., Ltd., OY-12) were further added to the first mixture of Example 1, and the proportion of ⁇ -SiC particles in the solid content of the sintering composition was 80 wt. The 2nd mixture was obtained so that it might become%. In the same manner as in Example 1, stirring, defoaming, and evaporation of the solvent were performed to prepare a sintering composition, and this was sintered to sinter the silicon carbide composite firing of Example 3. A ligature was obtained.
  • Example 4 11.1 parts by mass of carbon fiber in the form of short fibers (manufactured by Toho Tenax, fiber length 6 mm) with respect to 100 parts by mass of the solid content of the first mixture of Example 1 is part of the first carbon-based material As a second mixture.
  • stirring, defoaming, and evaporation of the solvent were performed to prepare a sintering composition, and this was sintered to sinter the silicon carbide composite firing of Example 4. A ligature was obtained.
  • Example 5 A composite sintered body of silicon carbide was obtained in the same manner as in Example 4 except that no carbon fiber nonwoven fabric was used, that is, only carbon fibers in the form of short fibers were used as the first carbon-based material. .
  • Carbon nanofibers which are the second carbon-based material, are made of carbon fiber (manufactured by Nippon Graphite Fiber Co., Ltd., XN100-2M, fiber length 250 ⁇ m, thermal conductivity 900 W / (m ⁇ K), volume resistivity 1.5 ⁇ 10.
  • a composite sintered body of silicon carbide was obtained in the same manner as in Example 5 except that it was changed to ⁇ 6 ⁇ ⁇ cm and a diameter of 10 ⁇ m.
  • Example 7 ⁇ -SiC particles (Yakushima Electric Co., Ltd., OY-12) were added to the first mixture of Example 1, and the proportion of ⁇ -SiC particles in the solid content of the sintering composition was 80% by weight. Thus, a sintering composition was obtained. Furthermore, 11.1 parts by mass of carbon fiber (XN100-2M, manufactured by Nippon Graphite Fiber Co., Ltd., fiber length 200 ⁇ m) in the form of a short fiber is added to 100 parts by mass of the solid content of the first mixture of Example 1. As a first carbon-based material, a second mixture was obtained. In the same manner as in Example 1, stirring, defoaming, and evaporation of the solvent were performed to prepare a sintering composition, and this was sintered to sinter the silicon carbide composite firing of Example 7. A ligature was obtained.
  • carbon fiber XN100-2M, manufactured by Nippon Graphite Fiber Co., Ltd., fiber length 200 ⁇ m
  • Example 8 is the same as Example 7 except that 25.0 parts by mass of carbon fiber is added as the first carbon-based material to 100 parts by mass of the solid content of the first mixture of Example 1. A composite sintered body of silicon carbide was obtained.
  • Example 9 is the same as Example 7 except that 42.9 parts by mass of carbon fiber is added as the first carbon-based material to 100 parts by mass of the solid content of the first mixture of Example 1. A composite sintered body of silicon carbide was obtained.
  • the silicon carbide composite sintered bodies of Examples 1 to 9 have relatively high values of the real part and the imaginary part of the complex relative dielectric constant
  • the silicon carbide composite sintered bodies of Comparative Examples 1 and 2 have a complex relative dielectric constant of Since the values of the real part and the imaginary part are relatively low, it can be understood that the silicon carbide composite sintered body can be suitably used as an electromagnetic wave absorber in a high frequency region by including carbon fibers.
  • a silicon carbide composite sintered material that can be suitably used as an electromagnetic wave absorber in either case of using CNF or carbon fiber as a carbon source for forming SiC. It can be understood that the body is obtained.
  • Examples 1 and 2 and Examples 5 and 6 as a carbon source for forming SiC, it is suitable as an electromagnetic wave absorber in both cases of using CNF and carbon fiber. It can be understood that a silicon carbide composite sintered body having a complex dielectric constant can be obtained.
  • Examples 1-4 When Examples 1-4 are compared with Examples 5-9, the imaginary part of the complex relative dielectric constant becomes large in Examples 1-4 including carbon fibers as the first carbon-based material in layers. It can be seen that the dielectric loss can be increased.
  • the composite sintered bodies of Examples 1 to 9 have relatively high values of the real part and the imaginary part of the complex relative dielectric constant and can be suitably used as an electromagnetic wave absorber in a high frequency region.
  • Example 1 and Example 2 exhibited a transmission attenuation of 10 dB or more over at least 2.5 GHz to 6 GHz, and were confirmed to have high electromagnetic wave absorption characteristics.
  • Comparative Example 1 did not show much transmission attenuation in the region from 2.5 GHz to 6 GHz and had a high-frequency electromagnetic wave absorption characteristic, but was lower than Examples 1 and 2.
  • FIG. 1A shows high-frequency reflection characteristics and transmission characteristics of the composite sintered body of Example 1, and FIG. 1B shows reflection transmission attenuation.
  • 2A shows high-frequency reflection characteristics and transmission characteristics of the composite sintered body of Comparative Example 1
  • FIG. 2B shows reflection transmission attenuation.
  • Example 1 the reflectance was suppressed and transmission attenuation was observed. Therefore, the silicon carbide composite sintered body showed high electromagnetic wave absorption characteristics.
  • Comparative Example 1 the reflectance varies greatly depending on the frequency, and the transmittance decreases even at a frequency where the reflectance is low. Since transmission attenuation of 10 dB or less is observed, electromagnetic wave absorption is obtained, but it is inferior to Example 1.
  • SiC was manufactured using silicon (Si) nanoparticles and carbon black (CB).
  • Si nanoparticles ink containing Nanogram TM Si nanoparticles (no dopant, average particle size 20 nm, product number: nSol-3002) was used.
  • carbon black manufactured by Denki Black, Denka Black 75% press product
  • Si / CB mixed ink is added. Obtained.
  • This Si / CB mixed ink was added to an alumina crucible for thermogravimetry-differential thermal analyzer (TG-DTA, specification made by NETZSCH: STA 449F1 Jupiter), and the solvent was dried to obtain Si / CB powder.
  • TG-DTA thermogravimetry-differential thermal analyzer
  • This Si / CB powder was subjected to a TG-DTA measuring apparatus and heated to 1550 ° C. at 20 ° C./min in an Ar atmosphere to obtain silicon carbide (SiC).
  • the carbon nanofibers used here were produced according to the method described in JP 2010-013742 A, had a fiber diameter of 200 to 500 nm, and had almost no fiber aggregate in which the fibers were fused. It was very dispersible.
  • the above mixture was stirred at 2000 rpm for 20 minutes and defoamed at 2200 rpm for 3 minutes with a planetary mixer (Awatori Netaro, Shinki Co., Ltd.) to obtain a Si / CNF mixed paste.
  • the solvent in the Si / CNF mixed paste was distilled off to obtain Si / CNF powder.
  • the powder was loaded into a forming jig and uniaxially pressed under vacuum at about 700 MPa for 2 hours to obtain a Si / ⁇ of 13 mm in diameter and 2.2 mm in thickness.
  • a CNF compact was obtained.
  • the obtained molded body was sintered at 1500 ° C. for 1 hour under an Ar stream.
  • ⁇ -SiC was obtained in the same manner as in Reference Example 2 except that the molar ratio of Si: C was changed to 25:75.
  • ⁇ -SiC was obtained in the same manner as in Reference Example 2, except that the carbon nanofiber was changed to carbon black (Denka Black 75% press product manufactured by Denki Kagaku Kogyo).
  • ⁇ -SiC was obtained in the same manner as in Reference Example 3, except that the carbon nanofiber was changed to carbon black (Denka Black 75% press product manufactured by Denki Kagaku Kogyo).
  • ⁇ -SiC was obtained in the same manner as in Reference Example 4 except that the carbon nanofiber was changed to carbon black (manufactured by Denki Kagaku, Denka Black 75% pressed product).
  • Comparison of Reference Example 2 and Reference Example 8 revealed that the presence of boron doping increases the SiC crystal size. Further, comparing Reference Examples 2 to 4 and Reference Examples 5 to 7, it was found that the SiC crystal size was larger when carbon nanofibers were used than when carbon black was used.

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Abstract

L'objectif de la présente invention concerne un nouveau corps fritté en composite de carbure de silicium qui est utile en tant qu'absorbeur d'ondes électromagnétiques et un procédé pour sa fabrication. La présente invention concerne un corps fritté en composite de carbure de silicium comprenant des fibres de carbone en tant que premier matériau carboné. La présente invention concerne également un procédé de fabrication du corps fritté en composite de carbure de silicium, ledit procédé comprenant le frittage d'une composition à fritter qui comprend au moins des nanograins de silicium et un matériau carboné contenant des fibres de carbone.
PCT/JP2017/034371 2016-09-30 2017-09-22 Corps fritté en composite de carbure de silicium et procédé pour sa fabrication WO2018062051A1 (fr)

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR20220027453A (ko) * 2020-08-27 2022-03-08 국방과학연구소 전파 흡수체 제조 방법 및 흡수 복합체
WO2024127795A1 (fr) * 2022-12-12 2024-06-20 株式会社リケン Feuille d'absorption d'ondes radio

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2006089340A (ja) * 2004-09-24 2006-04-06 Toyota Motor Corp 炭素複合材料、炭素複合材料からなるブレーキ材料、および炭素複合材料の製造方法
JP2006290670A (ja) * 2005-04-08 2006-10-26 Mitsubishi Electric Corp 繊維強化炭化ケイ素複合材料及びその製造方法
JP2010254541A (ja) * 2009-04-02 2010-11-11 Covalent Materials Corp 炭素繊維強化シリコン含浸炭化ケイ素セラミックスの製造方法及びこの製造方法によって製造されたセラミックス
WO2015140937A1 (fr) * 2014-03-18 2015-09-24 株式会社 東芝 Électrode pour batterie à électrolyte non aqueux, batterie secondaire à électrolyte non aqueux et bloc-batterie

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2005011878A (ja) * 2003-06-17 2005-01-13 Inoac Corp 電磁波吸収体
EP2960361B1 (fr) * 2013-02-19 2018-05-30 Ocean University of China Fibre de carbone à base de polyacrylonitrile co-dopée à l'oxygène et à l'azote et son procédé de préparation

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2006089340A (ja) * 2004-09-24 2006-04-06 Toyota Motor Corp 炭素複合材料、炭素複合材料からなるブレーキ材料、および炭素複合材料の製造方法
JP2006290670A (ja) * 2005-04-08 2006-10-26 Mitsubishi Electric Corp 繊維強化炭化ケイ素複合材料及びその製造方法
JP2010254541A (ja) * 2009-04-02 2010-11-11 Covalent Materials Corp 炭素繊維強化シリコン含浸炭化ケイ素セラミックスの製造方法及びこの製造方法によって製造されたセラミックス
WO2015140937A1 (fr) * 2014-03-18 2015-09-24 株式会社 東芝 Électrode pour batterie à électrolyte non aqueux, batterie secondaire à électrolyte non aqueux et bloc-batterie

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR20220027453A (ko) * 2020-08-27 2022-03-08 국방과학연구소 전파 흡수체 제조 방법 및 흡수 복합체
KR102381408B1 (ko) * 2020-08-27 2022-03-31 국방과학연구소 전파 흡수체 제조 방법 및 흡수 복합체
WO2024127795A1 (fr) * 2022-12-12 2024-06-20 株式会社リケン Feuille d'absorption d'ondes radio

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