US20010026868A1 - Si-SiC material and SiC fiber-reinforced Si-SiC composite material - Google Patents

Si-SiC material and SiC fiber-reinforced Si-SiC composite material Download PDF

Info

Publication number
US20010026868A1
US20010026868A1 US09/847,436 US84743601A US2001026868A1 US 20010026868 A1 US20010026868 A1 US 20010026868A1 US 84743601 A US84743601 A US 84743601A US 2001026868 A1 US2001026868 A1 US 2001026868A1
Authority
US
United States
Prior art keywords
sic
molded material
concentration
fiber
particles
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
US09/847,436
Other versions
US6444063B2 (en
Inventor
Shigeru Hanzawa
Masatoshi Futakawa
Saburo Shimizu
Kaoru Onuki
Ikuo Ioka
Ynte Stockmann
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
NGK Insulators Ltd
Original Assignee
NGK Insulators Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=16319449&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=US20010026868(A1) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by NGK Insulators Ltd filed Critical NGK Insulators Ltd
Priority to US09/847,436 priority Critical patent/US6444063B2/en
Publication of US20010026868A1 publication Critical patent/US20010026868A1/en
Application granted granted Critical
Publication of US6444063B2 publication Critical patent/US6444063B2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B18/00Layered products essentially comprising ceramics, e.g. refractory products
    • 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
    • C04B35/515Shaped 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
    • C04B35/573Shaped 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 obtained by reaction sintering or recrystallisation
    • 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
    • C04B35/622Forming processes; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
    • C04B35/62227Forming processes; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products obtaining fibres
    • C04B35/62272Forming processes; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products obtaining fibres based on non-oxide ceramics
    • C04B35/62277Fibres based on carbides
    • C04B35/62281Fibres based on carbides 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
    • C04B35/622Forming processes; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
    • C04B35/626Preparing or treating the powders individually or as batches ; preparing or treating macroscopic reinforcing agents for ceramic products, e.g. fibres; mechanical aspects section B
    • C04B35/62605Treating the starting powders individually or as mixtures
    • C04B35/62695Granulation or pelletising
    • 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
    • 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
    • C04B2235/00Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/02Composition of constituents of the starting material or of secondary phases of the final product
    • C04B2235/30Constituents and secondary phases not being of a fibrous nature
    • C04B2235/38Non-oxide ceramic constituents or additives
    • C04B2235/3817Carbides
    • C04B2235/3826Silicon carbides
    • 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
    • C04B2235/00Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/02Composition of constituents of the starting material or of secondary phases of the final product
    • C04B2235/30Constituents and secondary phases not being of a fibrous nature
    • C04B2235/38Non-oxide ceramic constituents or additives
    • C04B2235/3895Non-oxides with a defined oxygen content, e.g. SiOC, TiON
    • 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
    • C04B2235/00Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/02Composition of constituents of the starting material or of secondary phases of the final product
    • C04B2235/30Constituents and secondary phases not being of a fibrous nature
    • C04B2235/42Non metallic elements added as constituents or additives, e.g. sulfur, phosphor, selenium or tellurium
    • C04B2235/422Carbon
    • 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
    • C04B2235/00Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/02Composition of constituents of the starting material or of secondary phases of the final product
    • C04B2235/30Constituents and secondary phases not being of a fibrous nature
    • C04B2235/42Non metallic elements added as constituents or additives, e.g. sulfur, phosphor, selenium or tellurium
    • C04B2235/428Silicon
    • 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
    • C04B2235/00Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/02Composition of constituents of the starting material or of secondary phases of the final product
    • C04B2235/30Constituents and secondary phases not being of a fibrous nature
    • C04B2235/48Organic compounds becoming part of a ceramic after heat treatment, e.g. carbonising phenol resins
    • C04B2235/483Si-containing organic compounds, e.g. silicone resins, (poly)silanes, (poly)siloxanes or (poly)silazanes
    • 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
    • C04B2235/00Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/02Composition of constituents of the starting material or of secondary phases of the final product
    • C04B2235/50Constituents or additives of the starting mixture chosen for their shape or used because of their shape or their physical appearance
    • C04B2235/52Constituents or additives characterised by their shapes
    • C04B2235/5208Fibers
    • C04B2235/5216Inorganic
    • C04B2235/524Non-oxidic, e.g. borides, carbides, silicides or nitrides
    • C04B2235/5244Silicon 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
    • C04B2235/00Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/02Composition of constituents of the starting material or of secondary phases of the final product
    • C04B2235/50Constituents or additives of the starting mixture chosen for their shape or used because of their shape or their physical appearance
    • C04B2235/52Constituents or additives characterised by their shapes
    • C04B2235/5208Fibers
    • C04B2235/5252Fibers having a specific pre-form
    • C04B2235/5256Two-dimensional, e.g. woven structures
    • 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
    • C04B2235/00Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/02Composition of constituents of the starting material or of secondary phases of the final product
    • C04B2235/50Constituents or additives of the starting mixture chosen for their shape or used because of their shape or their physical appearance
    • C04B2235/54Particle size related information
    • C04B2235/5418Particle size related information expressed by the size of the particles or aggregates thereof
    • C04B2235/5427Particle size related information expressed by the size of the particles or aggregates thereof millimeter or submillimeter sized, i.e. larger than 0,1 mm
    • 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
    • C04B2235/00Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/02Composition of constituents of the starting material or of secondary phases of the final product
    • C04B2235/50Constituents or additives of the starting mixture chosen for their shape or used because of their shape or their physical appearance
    • C04B2235/54Particle size related information
    • C04B2235/5418Particle size related information expressed by the size of the particles or aggregates thereof
    • C04B2235/5436Particle size related information expressed by the size of the particles or aggregates thereof micrometer sized, i.e. from 1 to 100 micron
    • 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
    • C04B2235/00Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/02Composition of constituents of the starting material or of secondary phases of the final product
    • C04B2235/50Constituents or additives of the starting mixture chosen for their shape or used because of their shape or their physical appearance
    • C04B2235/54Particle size related information
    • C04B2235/5463Particle size distributions
    • C04B2235/5472Bimodal, multi-modal or multi-fraction
    • 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
    • C04B2235/00Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/60Aspects relating to the preparation, properties or mechanical treatment of green bodies or pre-forms
    • C04B2235/604Pressing at temperatures other than sintering temperatures
    • 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
    • C04B2235/00Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/65Aspects relating to heat treatments of ceramic bodies such as green ceramics or pre-sintered ceramics, e.g. burning, sintering or melting processes
    • C04B2235/656Aspects 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
    • 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
    • C04B2235/00Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/65Aspects relating to heat treatments of ceramic bodies such as green ceramics or pre-sintered ceramics, e.g. burning, sintering or melting processes
    • C04B2235/658Atmosphere during thermal treatment
    • 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
    • C04B2235/00Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/65Aspects relating to heat treatments of ceramic bodies such as green ceramics or pre-sintered ceramics, e.g. burning, sintering or melting processes
    • C04B2235/658Atmosphere during thermal treatment
    • C04B2235/6581Total pressure below 1 atmosphere, e.g. vacuum
    • 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
    • C04B2235/00Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/65Aspects relating to heat treatments of ceramic bodies such as green ceramics or pre-sintered ceramics, e.g. burning, sintering or melting processes
    • C04B2235/658Atmosphere during thermal treatment
    • C04B2235/6586Processes characterised by the flow of gas
    • 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
    • C04B2235/00Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/70Aspects relating to sintered or melt-casted ceramic products
    • C04B2235/74Physical characteristics
    • C04B2235/75Products with a concentration gradient
    • 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
    • C04B2235/00Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/70Aspects relating to sintered or melt-casted ceramic products
    • C04B2235/74Physical characteristics
    • C04B2235/77Density
    • 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
    • C04B2235/00Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/70Aspects relating to sintered or melt-casted ceramic products
    • C04B2235/96Properties of ceramic products, e.g. mechanical properties such as strength, toughness, wear resistance
    • 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
    • C04B2235/00Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/70Aspects relating to sintered or melt-casted ceramic products
    • C04B2235/96Properties of ceramic products, e.g. mechanical properties such as strength, toughness, wear resistance
    • C04B2235/9669Resistance against chemicals, e.g. against molten glass or molten salts
    • C04B2235/9684Oxidation resistance
    • 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
    • C04B2237/00Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
    • C04B2237/30Composition of layers of ceramic laminates or of ceramic or metallic articles to be joined by heating, e.g. Si substrates
    • C04B2237/32Ceramic
    • C04B2237/36Non-oxidic
    • C04B2237/365Silicon 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
    • C04B2237/00Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
    • C04B2237/30Composition of layers of ceramic laminates or of ceramic or metallic articles to be joined by heating, e.g. Si substrates
    • C04B2237/32Ceramic
    • C04B2237/38Fiber or whisker reinforced
    • 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
    • C04B2237/00Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
    • C04B2237/50Processing aspects relating to ceramic laminates or to the joining of ceramic articles with other articles by heating
    • C04B2237/58Forming a gradient in composition or in properties across the laminate or the joined articles
    • C04B2237/586Forming a gradient in composition or in properties across the laminate or the joined articles by joining layers or articles of the same composition but having different densities
    • 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
    • C04B2237/00Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
    • C04B2237/50Processing aspects relating to ceramic laminates or to the joining of ceramic articles with other articles by heating
    • C04B2237/58Forming a gradient in composition or in properties across the laminate or the joined articles
    • C04B2237/588Forming a gradient in composition or in properties across the laminate or the joined articles by joining layers or articles of the same composition but having different particle or grain sizes
    • 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
    • C04B2237/00Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
    • C04B2237/50Processing aspects relating to ceramic laminates or to the joining of ceramic articles with other articles by heating
    • C04B2237/61Joining two substrates of which at least one is porous by infiltrating the porous substrate with a liquid, such as a molten metal, causing bonding of the two substrates, e.g. joining two porous carbon substrates by infiltrating with molten silicon
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/24Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24942Structurally defined web or sheet [e.g., overall dimension, etc.] including components having same physical characteristic in differing degree
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/249921Web or sheet containing structurally defined element or component
    • Y10T428/249924Noninterengaged fiber-containing paper-free web or sheet which is not of specified porosity
    • Y10T428/249928Fiber embedded in a ceramic, glass, or carbon matrix
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/249921Web or sheet containing structurally defined element or component
    • Y10T428/249953Composite having voids in a component [e.g., porous, cellular, etc.]
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/249921Web or sheet containing structurally defined element or component
    • Y10T428/249953Composite having voids in a component [e.g., porous, cellular, etc.]
    • Y10T428/249961With gradual property change within a component
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/249921Web or sheet containing structurally defined element or component
    • Y10T428/249953Composite having voids in a component [e.g., porous, cellular, etc.]
    • Y10T428/249967Inorganic matrix in void-containing component
    • Y10T428/249969Of silicon-containing material [e.g., glass, etc.]
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/249921Web or sheet containing structurally defined element or component
    • Y10T428/249953Composite having voids in a component [e.g., porous, cellular, etc.]
    • Y10T428/249986Void-containing component contains also a solid fiber or solid particle
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/249921Web or sheet containing structurally defined element or component
    • Y10T428/249953Composite having voids in a component [e.g., porous, cellular, etc.]
    • Y10T428/249987With nonvoid component of specified composition
    • Y10T428/24999Inorganic

Definitions

  • the present invention relates to a Si—SiC material of Si concentration-gradient type and a SiC fiber-reinforced Si—SiC composite material of Si concentration-gradient type, both superior in properties such as weatherability, oxidation resistance, creeping resistance, strength, toughness and the like, as well as to processes for production of said materials.
  • CMC ceramic matrix material
  • CMC ceramic matrix composite
  • a fiber was mixed into a ceramic matrix, by making ceramic long fibers (ordinarily several hundreds to several thousands fibers) having a diameter of about 10 ⁇ m, into a fiber bundle (a yarn), arranging these fiber bundles two-dimensionally or three-dimensionally to form a unidirectional sheet or a cloth, or laminating a plurality of such sheets or such cloths to form a preliminary molded material (a fiber preform) having a desired shape, and forming, inside the preliminary molded material, a matrix by, for exampple, (a) chemical vapor infiltration or (b) inorganic polymer infiltration and sintering, or filling the inside of the preliminary molded material with a ceramic powder by casting and sintering the resulting material to form a matrix inside the preliminary molded material.
  • the conventional ceramic matrix material contains a SiC fiber inside, the thermal stress which the material receives during actual use, is caused by the difference in thermal expansion between SiC fiber and Si—SiC moiety; therefore, the material has had laminar peeling in some cases.
  • a Si—SiC material of Si concentration-gradient type and a SiC fiber-reinforced Si—SiC composite material of Si concentration-gradient type both significantly improved in corrosion resistance in highly oxidative and corrosive environment, strength, and healability of defects of surface layer and innermost layer, and
  • a SiC fiber-reinforced Si—SiC composite material of Si concentration-gradient type which has substantially no pore unlike ceramic matrix materials (CMC) having pores, such as SiC fiber-reinforced Si—SiC composite material obtained by CVD or infiltration of inorganic polymer and which is improved in toughness while having the features of Si—SiC sintered materials, such as high oxidation resistance, creeping resistance, and strength and toughness from ordinary temperature to high temperatures, and
  • CMC ceramic matrix materials
  • a Si—SiC material of Si concentration-gradient type obtained by melt-infiltrating Si into a molded material comprising SiC particles, which Si—SiC material has a porosity of 1.0% or less and in which Si—SiC material the Si concentration decreases gradually from the surface layer towards the innermost layer.
  • a process for producing a Si—SiC material of Si concentration-gradient type by melt-infiltrating Si into a molded material comprising SiC particles comprises preparing at least two kinds of mixtures each comprising SiC particles having a different tap density, laminating the mixtures to form a molded material, keeping the molded material and Si at a temperature of 1,100 to 1,400° C. in an inert gas atmosphere, and then increasing the temperature to 1,500 to 2,500° C. to melt-infiltrate Si into the molded material.
  • the molded material and Si are kept at a temperature of 1,100 to 1,400° C. at a pressure of 0.1 to 10 hPa for at least one hour with an inert gas being flown in an amount of 0.1 NL or more per kg of the total of the molded material and Si and then the temperature is increased to 1,500 to 2,500° C. to melt-infiltrate Si into the molded material.
  • the inert gas is preferably Ar.
  • SiC fiber-reinforced Si—SiC composite material of Si concentration-gradient type obtained by melt-infiltrating Si into a molded material comprising a SiC fiber and SiC particles, which composite material has a porosity of 1.0% or less and in which composite material the Si concentration decreases gradually from the surface layer towards the innermost layer.
  • the oxygen content of the SiC fiber is preferably 0.5 mass % or less and the SiC fiber may have a form of two-dimensional or three-dimensional cloth.
  • a process for producing a SiC fiber-reinforced Si—SiC composite material of Si concentration-gradient type obtained by melt-infiltrating Si into a molded material comprising a SiC fiber and SiC particles which process comprises preparing at least two kinds of mixtures each comprising SiC particles having a different tap density, mixing a SiC fiber into each mixture, laminating the resulting mixtures to form a molded material, keeping the molded material and Si at a temperature of 1,100 to 1,400° C. in an inert gas atmosphere, and then increasing the temperature to 1,500 to 2,500° C. to melt-infiltrate Si into the molded material.
  • the molded material and Si are kept at a temperature of 1,100 to 1,400° C. at a pressure of 0.1 to 10 hPa for at least one hour with an inert gas being flown in an amount of 0.1 NL or more per kg of the total of the molded material and Si and then the temperature is increased to 1,500 to 2,500° C. to melt-infiltrate Si into the molded material.
  • the inert gas is preferably Ar.
  • the porosity is almost zero (1.0% or less) and the Si concentration decreases gradually from the surface layer towards the innermost layer.
  • the present materials have excellent corrosion resistance in highly oxidative or corrosive environment and excellent strength, and are significantly improved in healability of defects of surface layer and innermost layer.
  • the Si—SiC material of Si concentration-gradient type of the present invention is obtained by melt-infiltrating Si into a molded material comprising SiC particles.
  • the properties of the Si—SiC material of Si concentration-gradient type differ depending upon the structure of the molded material into which Si is to be melt-infiltrated. Therefore, the production method of the molded material is very important and it is preferred to produce the molded material according to the following method.
  • the main raw material of the molded material is SiC granulated particles obtained by subjecting, to granulation by spray drying or the like, a mixture comprising SiC coarse particles having an average particle diameter of 50 to 100 ⁇ m, SiC fine particles having an average particle diameter of 0.1 to 10 ⁇ m and, desirably, a carbon powder having an average particle diameter of 0.1 to 30 ⁇ m.
  • SiC coarse particles having an average particle diameter of 50 to 100 ⁇ m
  • SiC fine particles having an average particle diameter of 0.1 to 10 ⁇ m
  • a carbon powder having an average particle diameter of 0.1 to 30 ⁇ m.
  • at least two kinds of SiC granulated particles different in tap density are appropriately selected and used.
  • tap density is a bulk specific gravity obtained when a powder is placed in a container and shaken or tapped for a given length of time for stabilization.
  • SiC granulated particles having a tap density of 0.7 to 0.85 are filled in a given mold and subjected to press molding or the like to prepare preliminary molded material 1.
  • preliminary molded material 2 comprising SiC granulated particles having a tap density of 0.85 to 1.00
  • preliminary molded material 3 comprising SiC granulated particles having a tap density of 1.00 to 1.3.
  • the tap densities of the SiC particles of the preliminary molded materials 1 to 3 are set so as to be “preliminary molded material 1 ⁇ preliminary molded material 2 ⁇ preliminary molded material 3”.
  • these preliminary molded materials are made into a molded material.
  • the preliminary molded material comprising SiC particles of the smallest tap density forms the surface layer of the molded material and that the innermost layer of the molded material is formed by at least one preliminary molded material comprising SiC particles having a tap density larger than that of the surface layer.
  • the preliminary molded materials are disposed so that the tap density of SiC particles increases gradually from the surface layer of the molded material towards the innermost layer.
  • the preliminary molded materials are disposed so as to form a sandwich structure of “preliminary molded material 1-preliminary molded material 2-preliminary molded material 1”or “preliminary molded material 1-preliminary molded material 3-preliminary molded material 1” or “preliminary molded material 1-preliminary molded material 2-preliminary molded material 3-preliminary molded material 2-preliminary molded material 1”; then, press molding is conducted to produce a laminated molded material.
  • slurries by adding an organic binder and water to a mixture comprising SiC coarse particles having an average particle diameter of 50 to 100 ⁇ m, SiC fine particles having an average particle diameter of 0.1 to 10 ⁇ m and, desirably, a carbon powder having an average particle diameter of 0.1 to 30 ⁇ m.
  • SiC coarse particles having an average particle diameter of 50 to 100 ⁇ m
  • SiC fine particles having an average particle diameter of 0.1 to 10 ⁇ m
  • a carbon powder having an average particle diameter of 0.1 to 30 ⁇ m.
  • few to several kinds of slurries different in the proportion (weight %) of the SiC coarse particles and the SiC fine particles are appropriately selected and used.
  • slurry A comprising the SiC coarse particles (20 to 40% by weight) and the SiC fine particles (80 to 60% by weight)
  • slurry B comprising the SiC coarse particles (40 to 60% by weight) and the SiC fine particles (60 to 40% by weight)
  • slurry C comprising the SiC coarse particles (60 to 80% by weight) and the SiC fine particles (40 to 20% by weight).
  • the total amount of SiC particles (the SiC coarse particles and the SiC fine particles) in each of slurries A to C is constant. Therefore, when the proportion (weight %) of the SiC coarse particles is high, the proportion (weight %) of the SiC fine particles is low; and when the proportion (weight %) of the SiC coarse particles is low, the proportion (weight %) of the SiC fine particles is high.
  • a molded material is produced using these slurries.
  • a slurry comprising the SiC coarse particles in the highest proportion (weight %) is disposed so as to form the surface layer of the molded material and that the innermost layer of the molded material is formed so as to comprise the SiC coarse particles in a proportion (weight %) smaller than that in the surface layer and the SiC fine particles in a proportion (weight %) larger than that in the surface layer.
  • the innermost layer of the molded material is formed so that in a position closer to the center of the molded material, the proportion (weight %) of the SiC coarse particles is smaller and the proportion (weight %) of the SiC fine particles is larger.
  • slurries A to C are cast into a given mold so as to form a sandwich structure of “slurry A-slurry B-slurry A” or “slurry A-slurry C-slurry A” or “slurry A-slurry B-slurry C-slurry B-slurry A”, whereby a laminated molded material is produced.
  • the concentration of Si infiltrated can be made smaller from the surface layer towards the innermost layer, that is, the Si concentration can have a gradient.
  • the ratio of the Si concentration of the innermost layer and the Si concentration of the surface layer can be allowed to be in a range of innermost layer/surface layer 0/100 to 90/100.
  • the laminated molded material produced as above is kept, together with Si, in a firing furnace at a temperature range of 1,100 to 1,400° C. at a pressure of 0.1 to 10 hPa for at least one hour with an inert gas being flown in an amount of 0.1 NL (normal liter) (corresponding to 5,065 liters of 1,200° C. and 0.1 hPa), whereby a molded material to be impregnated with Si is produced.
  • the molded material to be impregnated with Si is heated to a temperature of 1,500 to 2,500° C., preferably 1,700 to 1,800° C. to melt-infiltrate Si thereinto, to produce a Si—SiC material of Si concentration gradient-type according to the present invention.
  • the molded material and Si are kept in a firing furnace at a temperature of 1,100 to 1,400° C. at a pressure of 0.1 to 10 hPa for at least one hour with an inert gas being flown in an amount of 0.1 NL or more, preferably 1 NL or more, more preferably 10 NL or more per kg of the total of the molded material and Si.
  • the firing stage (a stage prior to Si melting and infiltration) in an inert gas current
  • the gas e.g. CO
  • the pollution of the firing atmosphere with external factor e.g. O 2 in air
  • the Si—SiC material of Si concentration-gradient type obtained by subsequent melt-infiltration of Si into molded material can have substantially zero porosity.
  • the atmosphere temperature is increased to 1,500 to 2,500° C., preferably 1,700 to 1,800° C.
  • the pressure inside the firing furnace is preferably 0.1 to 10 hPa.
  • the Si—SiC material of Si concentration-gradient type since the Si concentration is high in the innermost layer as compared with that in the surface layer, the microcracks appearing in the material can be healed. As a result, the material can retain oxidation resistance.
  • the surface layer is made of a protective film completely impregnated with Si. Therefore, the material has remarkably improved corrosion resistance in a highly oxidative and corrosive environment and the surface defects can be made smaller and removed. As a result, the material has even improved strength in a hihgly oxidative and corrosive environment.
  • the SiC fiber-reinforced Si—SiC composite material of Si concentration-gradient type of the present invention is obtained by melt-infiltrating Si into a molded material comprising a SiC fiber and SiC particles.
  • the properties of the SiC fiber-reinforced Si—SiC composite material of Si concentration-gradient type differ depending upon the structure of the molded material into which Si is to be melt-infiltrated. Therefore, the production method of the molded material is very important and it is preferred to produce the molded material according to the following method.
  • fine SiC fibers (ordinarily several hundreds to several thousands fibers) having a diameter of about 10 ⁇ m are made into a fiber bundle (a yarn); and these fiber bundles are arranged two-dimensionally or three-dimensionally to form a unidirectional sheet or a cloth, or such sheets or such cloths are laminated to form a fiber preform having a desired shape.
  • the main raw material of the molded material is SiC granulated particles obtained by subjecting, to granulation by spray drying or the like, a mixture comprising SiC coarse particles having an average particle diameter of 50 to 100 ⁇ m, SiC fine particles having an average particle diameter of 0.1 to 10 ⁇ m and, desirably, a carbon powder having an average particle diameter of 0.1 to 30 ⁇ m.
  • SiC coarse particles having an average particle diameter of 50 to 100 ⁇ m
  • SiC fine particles having an average particle diameter of 0.1 to 10 ⁇ m
  • a carbon powder having an average particle diameter of 0.1 to 30 ⁇ m.
  • at least two kinds of SiC granulated particles different in tap density are appropriately selected and used.
  • SiC granulated particles having a tap density of 0.7 to 0.85 are arranged in a layer with the above-obtained fiber preform being placed in the middle of the layer so as to form a sandwich structure, and subjected to press molding or the like to prepare preliminary molded material 1.
  • preliminary molded material 2 comprising SiC granulated particles having a tap density of 0.85 to 1.00
  • preliminary molded material 3 comprising SiC granulated particles having a tap density of 1.00 to 1.3.
  • the tap densities of the SiC particles of the preliminary molded materials 1 to 3 are set so as to be “preliminary molded material 1 ⁇ preliminary molded material 2 ⁇ preliminary molded material 3”.
  • these preliminary molded materials are made into a molded material.
  • the preliminary molded material comprising SiC particles of the smallest tap density forms the surface layer of the molded material and that the innermost layer of the molded material is formed by at least one preliminary molded material comprising SiC particles having a tap density larger than that of the surface layer.
  • the preliminary molded materials are disposed so that the tap density of SiC particles increases gradually from the surface layer of the molded material towards the innermost layer.
  • the preliminary molded materials are disposed so as to form a sandwich structure of “preliminary molded material 1-preliminary molded material 2-preliminary molded material 1” or “preliminary molded material 1-preliminary molded material 3-preliminary molded material” or “preliminary molded material 1-preliminary molded material 2-preliminary molded material 3-preliminary molded material 2-preliminary molded material 1”; then, press molding is conducted to produce a molded material.
  • fine SiC fibers (ordinarily several hundreds to several thousands fibers) having a diameter of about 10 ⁇ m are made into a fiber bundle (a yarn); and these fiber bundles are arranged two-dimensionally or three-dimensionally to form a unidirectional sheet or a cloth, or such sheets or such cloths are laminated to form a fiber preform having a desired shape.
  • main materials of the molded material there are prepared slurries by adding an organic binder and water to a mixture comprising SiC coarse particles having an average particle diameter of 50 to 100 ⁇ m, SiC fine particles having an average particle diameter of 0.1 to 10 ⁇ m and, desirably, a carbon powder having an average particle diameter of 0.1 to 30 ⁇ m.
  • SiC coarse particles having an average particle diameter of 50 to 100 ⁇ m
  • SiC fine particles having an average particle diameter of 0.1 to 10 ⁇ m
  • a carbon powder having an average particle diameter of 0.1 to 30 ⁇ m.
  • few to several kinds of slurries different in the proportion (weight %) of the SiC coarse particles and the SiC fine particles are appropriately selected and used.
  • Slurry A comprising the SiC coarse particles (20 to 40% by weight) and the SiC fine particles (80 to 60% by weight) is cast into a given mold in which the above-obtained fiber preform has been placed, to impregnate the fiber preform with the slurry, whereby preliminary molded material A is produced.
  • preliminary molded material B by using slurry B comprising the SiC coarse particles (60 to 40% by weight) and the SiC fine particles (40 to 60% by weight)
  • preliminary molded material C by using slurry C comprising the SiC coarse particles (60 to 80% by weight) and the SiC fine particles (40 to 20% by weight).
  • the total amount of SiC particles (the SiC coarse particles and the SiC fine particles) is constant. Therefore, when the proportion (weight %) of the SiC coarse particles is high, the proportion (weight %) of the SiC fine particles is low; and when the proportion (weight %) of the SiC coarse particles is low, the proportion (weight %) of the SiC fine particles is high.
  • a molded material is produced using these preliminary molded materials.
  • a preliminary molded material comprising the SiC coarse particles in the highest proportion (weight %) is disposed so as to form the surface layer of the molded material and that the innermost layer of the molded material is formed with a preliminary molded material comprising the SiC coarse particles in a proportion (weight %) smaller than that in the surface layer and the SiC fine particles in a proportion (weight %) larger than that in the surface layer.
  • the innermost layer of the molded material is formed so that in a position closer to the center of the molded material, the proportion (weight %) of the SiC coarse particles is smaller and the proportion (weight %) of the SiC fine particles is larger.
  • the preliminary molded materials are disposed so as to form a sandwich structure of “preliminary molded material A-preliminary molded material B-preliminary molded material A” or “preliminary molded material A-preliminary molded material C-preliminary molded material A” or “preliminary molded material A-preliminary molded material B-preliminary molded material C-preliminary molded material B-preliminary molded material A”; then, press molding is conducted to produce a molded material.
  • the concentration of Si infiltrated can be made smaller from the surface layer towards the innermost layer, that is, the Si concentration can have a gradient.
  • the molded material produced as above is kept, together with Si, in a firing furnace at a temperature range of 1,100 to 1,400° C. at a pressure of 0.1 to 10 hPa for at least one hour with an inert gas being flown in an amount of 0.1 NL (normal liter) (corresponding to 5,065 liters of 1,200° C. and 0.1 hPa), whereby a molded material to be impregnated with Si is produced.
  • the molded material to be impregnated with Si is heated to a temperature of 1,500 to 2,500° C., preferably 1,700 to 1,800° C. to melt-infiltrate Si thereinto, to produce a SiC fiber-reinforced Si—SiC composite material of Si concentration gradient-type according to the present invention wherein a SiC fiber and a Si—SiC sintered material have been made into a composite material.
  • the molded material and Si are kept in a firing furnace at a temperature of 1,100 to 1,400° C. at a pressure of 0.1 to 10 hPa for at least one hour with an inert gas being flown in an amount of 0.1 NL or more, preferably 1 NL or more, more preferably 10 NL or more per kg of the total of the molded material and Si.
  • the firing stage (a stage prior to Si melting and infiltration) in an inert gas current
  • the gas e.g. CO
  • the pollution of the firing atmosphere with external factor e.g. O 2 in air
  • the SiC fiber-reinforced Si—SiC composite material of Si concentration-gradient type obtained by subsequent melt-infiltration of Si into molded material can have substantially zero porosity.
  • the atmosphere temperature is increased to 1,500 to 2,500° C., preferably 1,700 to 1,800° C.
  • the pressure inside the firing furnace is preferably 0.1 to 10 hPa.
  • the SiC fiber-reinforced Si—SiC composite material of Si concentration-gradient type according to the present invention is substantially free from pores which are present in conventional ceramic matrix materials (CMC) (e.g. SiC fiber-reinforced Si—SiC composite materials) produced by CVD or inorganic fiber infiltration; therefore, the present composite material, as compared with conventional ceramic matrix materials (CMC), is dense and moreover retains excellent features of Si—SiC sintered material, such as oxidation resistance, creeping resistance, strength from ordinary temperature to high temperatures and toughness. Further, in obtaining a bonded ceramic material from a plurality of non-oxide ceramic members (e.g.
  • Si-based ceramics containing an excessive amount of an element participating in bonding, by allowing a metal to be present between said members to be bonded and heating them in a non-oxidizing atmosphere to form a compound of (1) said element participating in bonding and (2) said metal at the portion where said bonding is to be made, according to a procedure as described in Japanese Patent Application Kokai (Laid-Open) No. 128046/1994, the SiC fiber-reinforced Si—SiC composite material of Si concentration-gradient type of the present invention, since having a Si-rich layer at the surface, can enable ceramic-to-ceramic bonding easily.
  • the present composite material can be used in an article such as crucible for chemical liquid, or the like.
  • the surface of the present composite material is used as the inside of the crucible which comes in contact with the liquid, and the innermost layer of the present composite material is used as the outside of the crucible which makes no contact with the liquid.
  • W 1 is a dry weight obtained by drying a sample in an oven of 100° C. for 1 hour, followed by weighing.
  • W 2 is an in-water weight obtained by boiling a sample in water to infiltrate water completely into the pores, followed by weighing in water.
  • W 3 is a water-saturated weight obtained by infiltrating water completely into the pores of a sample, followed by weighing in air.
  • test piece of 60 mm ⁇ 60 mm ⁇ 5 mm was prepared by cutting; it was allowed to stand in a furnace of 1,150° C. in an O 2 gas current containing saturated steam of 90° C., to give rise to the oxidation of the test piece; and the per-hour weight increase of the test piece by oxidation was measured.
  • test sample was subjected to a four-point bending strength test at ordinary temperature according to JIS R 1601 “Test Method for Bending Strength of Fine Ceramics”, using the plane of the test sample at the half thickness (the plane is the central plane of the test sample) as a tensile plane.
  • Material A obtained above was cast into a gypsum mold of 100 mm ⁇ 100 mm ⁇ 30 mm (height) at a thickness of 5 mm; thereon was cast material B at a thickness of 5 mm; thereon was cast material A at a thickness of 5 mm to produce a molded material (molded material 1) of 100 mm ⁇ 100 mm ⁇ 15 mm.
  • Molded material 1 was vertically placed in a carbon crucible filled with a Si powder having a purity of 99.8% and an average particle diameter of 1 mm. The carbon crucible was transferred into a firing furnace.
  • the temperature inside the firing furnace was kept at 1,100 to 1,400° C. and the crucible contents were subjected to a firing treatment under the conditions of inert gas flow rate, in-furnace pressure and treatment time, shown in Table 1. Then, while the in-furnace pressure was kept at the same level, the in-furnace temperature was increased to the maximum temperature shown in Table 1 to infiltrate Si into molded material 1, whereby a Si—SiC material of Si concentration-gradient type was produced.
  • Material C was placed in a mold of 100 mm ⁇ 100 mm. Thereon was placed a SiC fiber cloth. Thereon was placed material C (the SiC fiber cloth was between the two material C layers). The resulting material was subjected to press molding at a pressure of 500 kgf/cm 2 to obtain a molded material (preliminary molded material C) of 100 mm ⁇ 100 mm ⁇ 5 mm.
  • a molded material (preliminary molded material D) of 100 mm ⁇ 100 mm ⁇ 5 mm was produced in the same manner as above.
  • SiC fiber cloth was used Nicalon (a product of Nippon Carbon Co., Ltd.) or Hinicalon (also a product of Nippon Carbon Co., Ltd.). Molded material 2 using Nicalon was named as molded material 2-1, and molded material 2 using Hinicalon was named as molded material 2-2.
  • Molded material 2-1 or 2-2 was vertically placed in a carbon crucible filled with a Si powder having a purity of 99.8% and an average particle diameter of 1 mm. The carbon crucible was transferred into a firing furnace.
  • the temperature inside the firing furnace was kept at 1,100 to 1,400° C. and the crucible contents were subjected to a firing treatment under the conditions of inert gas flow rate, in-furnace pressure and treatment time, shown in Table 1. Then, while the in-furnace pressure was kept at the same level, the in-furnace temperature was increased to the maximum temperature shown in Table 1 to infiltrate Si into molded material 2-1 or 2-2, whereby a SiC fiber-reinforced Si—SiC composite material of Si concentration-gradient type was produced.
  • Oxidation resistance was measured on the SiC fiber-reinforced Si—SiC composite materials of Examples 10 and 11, obtained in Examples 8 and 9; a Si—SiC sintered material [NEWSIC (trade name), a product of NGK Insulators, Ltd.] of Comparative Example 1; and a Si—SiC sintered material (a product of CESIWID Co., Germany) of Comparative Example 2.
  • the results are shown in Table 2. TABLE 2 Oxidation resistance Weight increase (%) After 100 hours After 500 hours Example 10 0.01 0.02 Example 11 0.008 0.015 Comparative 0.01 0.02 Example 1 Comparative 0.01 0.34 Example 2
  • the SiC fiber-reinforced Si—SiC composite materials of Si concentration-gradient type according to the present invention can have a porosity of 0.2% or less and, as compared with commercial Si—SiC sintered materials of Comparative Examples 1 (3 ?) to 4, have about the same oxidation resistance and bending strength and can have higher fracture toughens.
  • the SiC fiber-reinforced Si—SiC composite material of Si concentration-gradient type of the present invention obtained by using Nicalon [a SiC fiber cloth (a fiber preform) made of a Si—C—O type silicon carbide fiber] has improved strength at high temperatures and is significantly improved in fragility inherently possessed by ceramics.
  • SiC fiber-reinforced Si—SiC composite material of Si concentration-gradient type of the present invention obtained by using Hinicalon [a SiC fiber cloth (a fiber preform) made of a Si—C—O type silicon carbide fiber], as compared with the above composite material obtained using Nicalon, had higher oxidation resistance and creeping resistance.
  • Nicalon and Hinicalon are produced as follows.
  • Nicalon which is a Si—C—O type silicon carbide fiber having a ⁇ -SiC structure, is produced by melt-spinning an organic silicic acid polymer (a polycarbosilane) to obtain a continuous fiber, heating the fiber in air to give rise to crosslinking of Si—O—Si and infusibilization, and firing the resulting material in an inert gas atmosphere at 1,200 to 1,500° C.
  • organic silicic acid polymer a polycarbosilane
  • a silicon carbide fiber organic silicic acid polymer a polycarbosilane
  • the Si—SiC materials of Si concentration-gradient type of Examples 13 to 15 and SiC fiber-reinforced Si—SiC composite materials of Si concentration-gradient type of Examples 16 to 18, all according to the present invention are superior in healability of microcracks, as compared with conventional Si—SiC sintered materials.
  • the Si concentration in the surface layer is relatively higher than the Si concentration in the innermost layer; therefore, the formed microcracks are oxidized by heating and simultaneously healed; as a result, the sizes of defects in material become smaller and the properties of material are retained.
  • Si concentrations in surface layer and innermost layer were measured for the Si—SiC materials of Si concentration-gradient type obtained in Examples 1 to 3, the SiC fiber-reinforced Si—SiC composite materials of SiC concentration-gradient type obtained in Examples 4, 8 and 9, the commercial Si—SiC sintered material [NEWSIC (trade name), a product of NGK Insulators, Ltd.] of Comparative Example 1, and the commercial Si—SiC sintered material (a product of CESIWID Co, Germany) of Comparative Example 2.
  • the Si concentration is higher in the surface layer and lower in the innermost layer and has a gradient. Meanwhile, in the commercial products, the Si concentration is almost the same in the surface layer and the innermost layer.
  • the Si—SiC material of Si concentration-gradient type and SiC fiber-reinforced Si—SiC composite material of Si concentration-gradient type produced by the present processes are superior in corrosion resistance in highly oxidative and corrosive environment as well as in strength, and is significantly improved in healability of defects of surface layer and innermost layer.
  • the SiC fiber-reinforced Si—SiC composite material of Si concentration-gradient type according to the present invention is substantially free from pores which are present in conventional ceramic matrix materials (CMC) (e.g. SiC fiber-reinforced Si—SiC composite materials) produced by CVD or inorganic polymer infiltration; therefore, the present composite material, as compared with conventional ceramic matrix composites (CMC), is dense and moreover retains excellent features of Si—SiC sintered material, such as oxidation resistance, creeping resistance, strength from ordinary temperature to high temperatures and toughness.
  • CMC ceramic matrix materials

Abstract

A Si—SiC material of Si concentration-gradient type is obtained by melt-infiltrating Si into a molded material comprising SiC particles. The Si—SiC material has a porosity of 1.0% or less and in the Si—SiC material the Si concentration decreases gradually from the surface layer towards the innermost layer. A SiC fiber-reinforced Si—SiC composite material of Si concentration-gradient type is obtained by melt-infiltrating Si into a molded material comprising a SiC fiber and SiC particles. The composite material has a porosity of 1.0% or less and in the composite material the Si concentration decreases gradually from the surface layer towards the innermost layer. These materials are significantly improved in corrosion resistance in highly oxidative and corrosive environment, strength, and healability of defects of surface layer and innermost layer.

Description

    BACKGROUND OF THE INVENTION
  • (1) Field of the Invention [0001]
  • The present invention relates to a Si—SiC material of Si concentration-gradient type and a SiC fiber-reinforced Si—SiC composite material of Si concentration-gradient type, both superior in properties such as weatherability, oxidation resistance, creeping resistance, strength, toughness and the like, as well as to processes for production of said materials. [0002]
  • (2) Description of Related Art [0003]
  • In the midst of rapid progress of technological innovation, big projects are being planned and carried out in various parts of the world for development of state-of-the-art technologies such as space shuttle and space plane (in the field of space development), high-temperature combustion gas turbine (in the field of energy) and high-temperature gas furnace and nuclear fusion reactor (in the field of atomic energy). [0004]
  • Also, utilization of hydrogen energy is being studied in order to use it as an energy other than nuclear energy and solar energy. In this connection, expensive metal or fine ceramic is being investigated to use it as a reactor material. These structural materials must have high strength at intermediate to high temperatures (200 to 2,000° C.), high reliabilities in toughness and impact resistance, and resistances to environment (e.g. corrosion resistance, oxidation resistance and radiation resistance). [0005]
  • Currently, as a ceramic superior in heat resistance, there are newly developed ceramics, i.e. silicon nitride and silicon carbide both having high strength. They, however, are inherently fragile and are very fragile even when there have small flaws, and further have low resistance to thermal or mechanical impact. [0006]
  • In order to overcome these drawbacks of the above ceramics, there was developed a ceramic matrix material (CMC) wherein a continuous ceramic fiber is mixed with a ceramic. This material, having high strength and high toughness even at high temperatures, excellent impact resistance and excellent resistances to environment, is under active study as a structural material having an ultrahigh resistance to heat, in Europe, U.S.A., etc. [0007]
  • For example, there was developed a ceramic matrix composite (CMC) wherein a fiber was mixed into a ceramic matrix, by making ceramic long fibers (ordinarily several hundreds to several thousands fibers) having a diameter of about 10 μm, into a fiber bundle (a yarn), arranging these fiber bundles two-dimensionally or three-dimensionally to form a unidirectional sheet or a cloth, or laminating a plurality of such sheets or such cloths to form a preliminary molded material (a fiber preform) having a desired shape, and forming, inside the preliminary molded material, a matrix by, for exampple, (a) chemical vapor infiltration or (b) inorganic polymer infiltration and sintering, or filling the inside of the preliminary molded material with a ceramic powder by casting and sintering the resulting material to form a matrix inside the preliminary molded material. [0008]
  • In the sintering (firing) used in production of conventional ceramic matrix material, however, no attention was paid to the CO gas generated in the process, and it was conducted only to introduce an inert gas by a slight pressure control mainly for prevention of Si vaporization. [0009]
  • Consequently, the CO gas produced during firing in association with the conversion of organic polymer into ceramic, by the reaction of free carbon (present in firing atmosphere) and O[0010] 2 and the reaction of free carbon and SiO2, is liberated to form defects; these defects and the growth of β-SiC crystals bring about significant deterioration of strength; further, the pores in produced ceramic matrix material cannot be reduced to zero and their size is as large as about 1 mm, inviting deterioration of weatherability and oxidation resistance.
  • Further, although the conventional ceramic matrix material contains a SiC fiber inside, the thermal stress which the material receives during actual use, is caused by the difference in thermal expansion between SiC fiber and Si—SiC moiety; therefore, the material has had laminar peeling in some cases. [0011]
  • SUMMARY OF THE INVENTION
  • In view of the above-mentioned problems of the prior art, the present invention has been completed with objects of providing: [0012]
  • a Si—SiC material of Si concentration-gradient type and a SiC fiber-reinforced Si—SiC composite material of Si concentration-gradient type, both significantly improved in corrosion resistance in highly oxidative and corrosive environment, strength, and healability of defects of surface layer and innermost layer, and [0013]
  • processes for production of the above materials. [0014]
  • The further objects of the present invention are to provide: [0015]
  • a SiC fiber-reinforced Si—SiC composite material of Si concentration-gradient type, which has substantially no pore unlike ceramic matrix materials (CMC) having pores, such as SiC fiber-reinforced Si—SiC composite material obtained by CVD or infiltration of inorganic polymer and which is improved in toughness while having the features of Si—SiC sintered materials, such as high oxidation resistance, creeping resistance, and strength and toughness from ordinary temperature to high temperatures, and [0016]
  • a process for production of the above material. [0017]
  • According to the present invention, there is provided a Si—SiC material of Si concentration-gradient type obtained by melt-infiltrating Si into a molded material comprising SiC particles, which Si—SiC material has a porosity of 1.0% or less and in which Si—SiC material the Si concentration decreases gradually from the surface layer towards the innermost layer. [0018]
  • In the above Si—SiC material of Si concentration-gradient type, it is preferred that the ratio of the Si concentration of the surface layer and the Si concentration of the innermost layer is in a range of innermost layer/surface layer=0/100 to 90/100. [0019]
  • According to the present invention, there is also provided a process for producing a Si—SiC material of Si concentration-gradient type by melt-infiltrating Si into a molded material comprising SiC particles, which process comprises preparing at least two kinds of mixtures each comprising SiC particles having a different tap density, laminating the mixtures to form a molded material, keeping the molded material and Si at a temperature of 1,100 to 1,400° C. in an inert gas atmosphere, and then increasing the temperature to 1,500 to 2,500° C. to melt-infiltrate Si into the molded material. [0020]
  • In the above process, it is preferred that the molded material and Si are kept at a temperature of 1,100 to 1,400° C. at a pressure of 0.1 to 10 hPa for at least one hour with an inert gas being flown in an amount of 0.1 NL or more per kg of the total of the molded material and Si and then the temperature is increased to 1,500 to 2,500° C. to melt-infiltrate Si into the molded material. The inert gas is preferably Ar. [0021]
  • According to the present invention, there is also provided a SiC fiber-reinforced Si—SiC composite material of Si concentration-gradient type obtained by melt-infiltrating Si into a molded material comprising a SiC fiber and SiC particles, which composite material has a porosity of 1.0% or less and in which composite material the Si concentration decreases gradually from the surface layer towards the innermost layer. [0022]
  • In the above SiC fiber-reinforced Si—SiC composite material of Si concentration-gradient type, it is preferred that the ratio of the Si concentration of the surface layer and the Si concentration of the innermost layer is in a range of innermost layer/surface layer=0/100 to 90/100. [0023]
  • Also in the above SiC fiber-reinforced Si—SiC composite material of Si concentration-gradient type, the oxygen content of the SiC fiber is preferably 0.5 mass % or less and the SiC fiber may have a form of two-dimensional or three-dimensional cloth. [0024]
  • According to the present invention, there is also provided a process for producing a SiC fiber-reinforced Si—SiC composite material of Si concentration-gradient type obtained by melt-infiltrating Si into a molded material comprising a SiC fiber and SiC particles, which process comprises preparing at least two kinds of mixtures each comprising SiC particles having a different tap density, mixing a SiC fiber into each mixture, laminating the resulting mixtures to form a molded material, keeping the molded material and Si at a temperature of 1,100 to 1,400° C. in an inert gas atmosphere, and then increasing the temperature to 1,500 to 2,500° C. to melt-infiltrate Si into the molded material. [0025]
  • In the above process for producing a SiC fiber-reinforced Si—SiC composite material of Si concentration-gradient type, it is preferred that the molded material and Si are kept at a temperature of 1,100 to 1,400° C. at a pressure of 0.1 to 10 hPa for at least one hour with an inert gas being flown in an amount of 0.1 NL or more per kg of the total of the molded material and Si and then the temperature is increased to 1,500 to 2,500° C. to melt-infiltrate Si into the molded material. The inert gas is preferably Ar. [0026]
  • DETAILED DESCRIPTION OF THE INVENTION
  • In the Si—SiC material of Si concentration-gradient type and the SiC fiber-reinforced Si—SiC composite material of Si concentration-gradient type both of the present invention, the porosity is almost zero (1.0% or less) and the Si concentration decreases gradually from the surface layer towards the innermost layer. [0027]
  • Thereby, the present materials have excellent corrosion resistance in highly oxidative or corrosive environment and excellent strength, and are significantly improved in healability of defects of surface layer and innermost layer. [0028]
  • Description is first made on the process for production of the present Si—SiC material of Si concentration-gradient type. [0029]
  • The Si—SiC material of Si concentration-gradient type of the present invention is obtained by melt-infiltrating Si into a molded material comprising SiC particles. [0030]
  • The properties of the Si—SiC material of Si concentration-gradient type differ depending upon the structure of the molded material into which Si is to be melt-infiltrated. Therefore, the production method of the molded material is very important and it is preferred to produce the molded material according to the following method. [0031]
  • Compaction molding as one example of the production method of the molded material used in the present process is described below. [0032]
  • The main raw material of the molded material is SiC granulated particles obtained by subjecting, to granulation by spray drying or the like, a mixture comprising SiC coarse particles having an average particle diameter of 50 to 100 μm, SiC fine particles having an average particle diameter of 0.1 to 10 μm and, desirably, a carbon powder having an average particle diameter of 0.1 to 30 μm. Preferably, at least two kinds of SiC granulated particles different in tap density are appropriately selected and used. [0033]
  • Incidentally, “tap density” is a bulk specific gravity obtained when a powder is placed in a container and shaken or tapped for a given length of time for stabilization. [0034]
  • SiC granulated particles having a tap density of 0.7 to 0.85 are filled in a given mold and subjected to press molding or the like to prepare preliminary molded material 1. [0035]
  • In the same manner are prepared preliminary molded material 2 comprising SiC granulated particles having a tap density of 0.85 to 1.00 and preliminary molded material 3 comprising SiC granulated particles having a tap density of 1.00 to 1.3. [0036]
  • As shown above, the tap densities of the SiC particles of the preliminary molded materials 1 to 3 are set so as to be “preliminary molded material 1<preliminary molded material 2<preliminary molded material 3”. [0037]
  • Then, these preliminary molded materials are made into a molded material. In that case, it is important that the preliminary molded material comprising SiC particles of the smallest tap density forms the surface layer of the molded material and that the innermost layer of the molded material is formed by at least one preliminary molded material comprising SiC particles having a tap density larger than that of the surface layer. Also, it is preferred that the preliminary molded materials are disposed so that the tap density of SiC particles increases gradually from the surface layer of the molded material towards the innermost layer. [0038]
  • For example, the preliminary molded materials are disposed so as to form a sandwich structure of “preliminary molded material 1-preliminary molded material 2-preliminary molded material 1”or “preliminary molded material 1-preliminary molded material 3-preliminary molded material 1” or “preliminary molded material 1-preliminary molded material 2-preliminary molded material 3-preliminary molded material 2-preliminary molded material 1”; then, press molding is conducted to produce a laminated molded material. [0039]
  • Further, cast molding as other example of the production method of the molded material used in the present process is described below. [0040]
  • First, as main materials of the molded material, there are prepared slurries by adding an organic binder and water to a mixture comprising SiC coarse particles having an average particle diameter of 50 to 100 μm, SiC fine particles having an average particle diameter of 0.1 to 10 μm and, desirably, a carbon powder having an average particle diameter of 0.1 to 30 μm. Preferably, few to several kinds of slurries different in the proportion (weight %) of the SiC coarse particles and the SiC fine particles (these two kinds of SiC particles are main materials of each slurry) are appropriately selected and used. [0041]
  • Specifically, there are prepared slurry A comprising the SiC coarse particles (20 to 40% by weight) and the SiC fine particles (80 to 60% by weight), slurry B comprising the SiC coarse particles (40 to 60% by weight) and the SiC fine particles (60 to 40% by weight), and slurry C comprising the SiC coarse particles (60 to 80% by weight) and the SiC fine particles (40 to 20% by weight). [0042]
  • The total amount of SiC particles (the SiC coarse particles and the SiC fine particles) in each of slurries A to C is constant. Therefore, when the proportion (weight %) of the SiC coarse particles is high, the proportion (weight %) of the SiC fine particles is low; and when the proportion (weight %) of the SiC coarse particles is low, the proportion (weight %) of the SiC fine particles is high. [0043]
  • Next, a molded material is produced using these slurries. In that case, it is necessary that a slurry comprising the SiC coarse particles in the highest proportion (weight %) is disposed so as to form the surface layer of the molded material and that the innermost layer of the molded material is formed so as to comprise the SiC coarse particles in a proportion (weight %) smaller than that in the surface layer and the SiC fine particles in a proportion (weight %) larger than that in the surface layer. Preferably, the innermost layer of the molded material is formed so that in a position closer to the center of the molded material, the proportion (weight %) of the SiC coarse particles is smaller and the proportion (weight %) of the SiC fine particles is larger. [0044]
  • In an example, slurries A to C are cast into a given mold so as to form a sandwich structure of “slurry A-slurry B-slurry A” or “slurry A-slurry C-slurry A” or “slurry A-slurry B-slurry C-slurry B-slurry A”, whereby a laminated molded material is produced. [0045]
  • In melt-infiltrating Si into the molded material produced by any of the above two processes, since the molded material is produced so that the innermost layer has a smaller porosity (Si is later infiltrated into these pores) than the surface layer has, the concentration of Si infiltrated can be made smaller from the surface layer towards the innermost layer, that is, the Si concentration can have a gradient. The ratio of the Si concentration of the innermost layer and the Si concentration of the surface layer can be allowed to be in a range of innermost layer/surface layer 0/100 to 90/100. [0046]
  • The laminated molded material produced as above is kept, together with Si, in a firing furnace at a temperature range of 1,100 to 1,400° C. at a pressure of 0.1 to 10 hPa for at least one hour with an inert gas being flown in an amount of 0.1 NL (normal liter) (corresponding to 5,065 liters of 1,200° C. and 0.1 hPa), whereby a molded material to be impregnated with Si is produced. [0047]
  • Next, the molded material to be impregnated with Si is heated to a temperature of 1,500 to 2,500° C., preferably 1,700 to 1,800° C. to melt-infiltrate Si thereinto, to produce a Si—SiC material of Si concentration gradient-type according to the present invention. [0048]
  • In the present process for production of Si—SiC molded material of Si concentration-gradient type, it is desirable that the molded material and Si are kept in a firing furnace at a temperature of 1,100 to 1,400° C. at a pressure of 0.1 to 10 hPa for at least one hour with an inert gas being flown in an amount of 0.1 NL or more, preferably 1 NL or more, more preferably 10 NL or more per kg of the total of the molded material and Si. [0049]
  • Thus, by conducting the firing stage (a stage prior to Si melting and infiltration) in an inert gas current, the gas (e.g. CO) generated in conversion of inorganic polymer or inorganic substance into ceramic is removed from the firing atmosphere and, moreover, the pollution of the firing atmosphere with external factor (e.g. O[0050] 2 in air) is prevented; as a result, the Si—SiC material of Si concentration-gradient type obtained by subsequent melt-infiltration of Si into molded material can have substantially zero porosity.
  • In melt-infiltration of Si into the fired molded material, the atmosphere temperature is increased to 1,500 to 2,500° C., preferably 1,700 to 1,800° C. In this case, the pressure inside the firing furnace is preferably 0.1 to 10 hPa. [0051]
  • As stated above, in the Si—SiC material of Si concentration-gradient type, since the Si concentration is high in the innermost layer as compared with that in the surface layer, the microcracks appearing in the material can be healed. As a result, the material can retain oxidation resistance. [0052]
  • Further, in the Si—SiC material of Si concentration-gradient type, the surface layer is made of a protective film completely impregnated with Si. Therefore, the material has remarkably improved corrosion resistance in a highly oxidative and corrosive environment and the surface defects can be made smaller and removed. As a result, the material has even improved strength in a hihgly oxidative and corrosive environment. [0053]
  • Description is then made on the process for production of the present SiC fiber-reinforced Si—SiC composite material of Si concentration-gradient type. [0054]
  • The SiC fiber-reinforced Si—SiC composite material of Si concentration-gradient type of the present invention is obtained by melt-infiltrating Si into a molded material comprising a SiC fiber and SiC particles. [0055]
  • The properties of the SiC fiber-reinforced Si—SiC composite material of Si concentration-gradient type differ depending upon the structure of the molded material into which Si is to be melt-infiltrated. Therefore, the production method of the molded material is very important and it is preferred to produce the molded material according to the following method. [0056]
  • Compaction molding as one example of the production method of the molded material used in the present process is described below. [0057]
  • First, fine SiC fibers (ordinarily several hundreds to several thousands fibers) having a diameter of about 10 μm are made into a fiber bundle (a yarn); and these fiber bundles are arranged two-dimensionally or three-dimensionally to form a unidirectional sheet or a cloth, or such sheets or such cloths are laminated to form a fiber preform having a desired shape. [0058]
  • The main raw material of the molded material is SiC granulated particles obtained by subjecting, to granulation by spray drying or the like, a mixture comprising SiC coarse particles having an average particle diameter of 50 to 100 μm, SiC fine particles having an average particle diameter of 0.1 to 10 μm and, desirably, a carbon powder having an average particle diameter of 0.1 to 30 μm. Preferably, at least two kinds of SiC granulated particles different in tap density are appropriately selected and used. [0059]
  • SiC granulated particles having a tap density of 0.7 to 0.85 are arranged in a layer with the above-obtained fiber preform being placed in the middle of the layer so as to form a sandwich structure, and subjected to press molding or the like to prepare preliminary molded material 1. [0060]
  • In the same manner are prepared preliminary molded material 2 comprising SiC granulated particles having a tap density of 0.85 to 1.00 and preliminary molded material 3 comprising SiC granulated particles having a tap density of 1.00 to 1.3. [0061]
  • As shown above, the tap densities of the SiC particles of the preliminary molded materials 1 to 3 are set so as to be “preliminary molded material 1<preliminary molded material 2<preliminary molded material 3”. [0062]
  • Then, these preliminary molded materials are made into a molded material. In that case, it is important that the preliminary molded material comprising SiC particles of the smallest tap density forms the surface layer of the molded material and that the innermost layer of the molded material is formed by at least one preliminary molded material comprising SiC particles having a tap density larger than that of the surface layer. Also, it is preferred that the preliminary molded materials are disposed so that the tap density of SiC particles increases gradually from the surface layer of the molded material towards the innermost layer. [0063]
  • For example, the preliminary molded materials are disposed so as to form a sandwich structure of “preliminary molded material 1-preliminary molded material 2-preliminary molded material 1” or “preliminary molded material 1-preliminary molded material 3-preliminary molded material” or “preliminary molded material 1-preliminary molded material 2-preliminary molded material 3-preliminary molded material 2-preliminary molded material 1”; then, press molding is conducted to produce a molded material. [0064]
  • Further, cast molding as other example of the production method of the molded material is described below. [0065]
  • First, fine SiC fibers (ordinarily several hundreds to several thousands fibers) having a diameter of about 10 μm are made into a fiber bundle (a yarn); and these fiber bundles are arranged two-dimensionally or three-dimensionally to form a unidirectional sheet or a cloth, or such sheets or such cloths are laminated to form a fiber preform having a desired shape. [0066]
  • Then, as main materials of the molded material, there are prepared slurries by adding an organic binder and water to a mixture comprising SiC coarse particles having an average particle diameter of 50 to 100 μm, SiC fine particles having an average particle diameter of 0.1 to 10 μm and, desirably, a carbon powder having an average particle diameter of 0.1 to 30 μm. Preferably, few to several kinds of slurries different in the proportion (weight %) of the SiC coarse particles and the SiC fine particles (these two kinds of SiC particles are main materials of each slurry) are appropriately selected and used. [0067]
  • Slurry A comprising the SiC coarse particles (20 to 40% by weight) and the SiC fine particles (80 to 60% by weight) is cast into a given mold in which the above-obtained fiber preform has been placed, to impregnate the fiber preform with the slurry, whereby preliminary molded material A is produced. [0068]
  • In the same manner, there are produced preliminary molded material B by using slurry B comprising the SiC coarse particles (60 to 40% by weight) and the SiC fine particles (40 to 60% by weight), and preliminary molded material C by using slurry C comprising the SiC coarse particles (60 to 80% by weight) and the SiC fine particles (40 to 20% by weight). [0069]
  • In the slurries A to C of the preliminary molded materials A to C, the total amount of SiC particles (the SiC coarse particles and the SiC fine particles) is constant. Therefore, when the proportion (weight %) of the SiC coarse particles is high, the proportion (weight %) of the SiC fine particles is low; and when the proportion (weight %) of the SiC coarse particles is low, the proportion (weight %) of the SiC fine particles is high. [0070]
  • Next, a molded material is produced using these preliminary molded materials. In that case, it is necessary that a preliminary molded material comprising the SiC coarse particles in the highest proportion (weight %) is disposed so as to form the surface layer of the molded material and that the innermost layer of the molded material is formed with a preliminary molded material comprising the SiC coarse particles in a proportion (weight %) smaller than that in the surface layer and the SiC fine particles in a proportion (weight %) larger than that in the surface layer. Preferably, the innermost layer of the molded material is formed so that in a position closer to the center of the molded material, the proportion (weight %) of the SiC coarse particles is smaller and the proportion (weight %) of the SiC fine particles is larger. [0071]
  • For example, the preliminary molded materials are disposed so as to form a sandwich structure of “preliminary molded material A-preliminary molded material B-preliminary molded material A” or “preliminary molded material A-preliminary molded material C-preliminary molded material A” or “preliminary molded material A-preliminary molded material B-preliminary molded material C-preliminary molded material B-preliminary molded material A”; then, press molding is conducted to produce a molded material. [0072]
  • In melt-infiltrating Si into the molded material produced by any of the above two processes, since the molded material is produced so that the innermost layer has a smaller porosity (Si is later infiltrated into the pores) than the surface layer has, the concentration of Si infiltrated can be made smaller from the surface layer towards the innermost layer, that is, the Si concentration can have a gradient. The ratio of the Si concentration of the innermost layer and the Si concentration of the surface layer can be allowed to be in a range of innermost layer/surface layer=0/100 to 90/100. [0073]
  • The molded material produced as above is kept, together with Si, in a firing furnace at a temperature range of 1,100 to 1,400° C. at a pressure of 0.1 to 10 hPa for at least one hour with an inert gas being flown in an amount of 0.1 NL (normal liter) (corresponding to 5,065 liters of 1,200° C. and 0.1 hPa), whereby a molded material to be impregnated with Si is produced. [0074]
  • Next, the molded material to be impregnated with Si is heated to a temperature of 1,500 to 2,500° C., preferably 1,700 to 1,800° C. to melt-infiltrate Si thereinto, to produce a SiC fiber-reinforced Si—SiC composite material of Si concentration gradient-type according to the present invention wherein a SiC fiber and a Si—SiC sintered material have been made into a composite material. [0075]
  • In the present process for production of SiC fiber-reinforced Si—SiC composite material of Si concentration-gradient type, it is desirable that the molded material and Si are kept in a firing furnace at a temperature of 1,100 to 1,400° C. at a pressure of 0.1 to 10 hPa for at least one hour with an inert gas being flown in an amount of 0.1 NL or more, preferably 1 NL or more, more preferably 10 NL or more per kg of the total of the molded material and Si. [0076]
  • Thus, by conducting the firing stage (a stage prior to Si melting and infiltration) in an inert gas current, the gas (e.g. CO) generated in conversion of inorganic polymer or inorganic substance into ceramic is removed from the firing atmosphere and, moreover, the pollution of the firing atmosphere with external factor (e.g. O[0077] 2 in air) is prevented; as a result, the SiC fiber-reinforced Si—SiC composite material of Si concentration-gradient type obtained by subsequent melt-infiltration of Si into molded material can have substantially zero porosity.
  • In melt-infiltration of Si into the fired molded material, the atmosphere temperature is increased to 1,500 to 2,500° C., preferably 1,700 to 1,800° C. In this case, the pressure inside the firing furnace is preferably 0.1 to 10 hPa. [0078]
  • As described above, the SiC fiber-reinforced Si—SiC composite material of Si concentration-gradient type according to the present invention is substantially free from pores which are present in conventional ceramic matrix materials (CMC) (e.g. SiC fiber-reinforced Si—SiC composite materials) produced by CVD or inorganic fiber infiltration; therefore, the present composite material, as compared with conventional ceramic matrix materials (CMC), is dense and moreover retains excellent features of Si—SiC sintered material, such as oxidation resistance, creeping resistance, strength from ordinary temperature to high temperatures and toughness. Further, in obtaining a bonded ceramic material from a plurality of non-oxide ceramic members (e.g. Si-based ceramics) containing an excessive amount of an element participating in bonding, by allowing a metal to be present between said members to be bonded and heating them in a non-oxidizing atmosphere to form a compound of (1) said element participating in bonding and (2) said metal at the portion where said bonding is to be made, according to a procedure as described in Japanese Patent Application Kokai (Laid-Open) No. 128046/1994, the SiC fiber-reinforced Si—SiC composite material of Si concentration-gradient type of the present invention, since having a Si-rich layer at the surface, can enable ceramic-to-ceramic bonding easily. [0079]
  • Furthermore, the present composite material can be used in an article such as crucible for chemical liquid, or the like. In that case, the surface of the present composite material is used as the inside of the crucible which comes in contact with the liquid, and the innermost layer of the present composite material is used as the outside of the crucible which makes no contact with the liquid. [0080]
  • The present invention is described in more detail below by way of Examples. However, the present invention is not restricted to these Examples. [0081]
  • The properties of the materials and composite materials obtained in Examples were measured according to the following methods. [0082]
  • (Porosity) [0083]
  • Was measured by the Archimedes method. [0084]
  • Porosity (%)=[(W 3 −W 1)/(W 3 −W 2)]×100
  • W[0085] 1 is a dry weight obtained by drying a sample in an oven of 100° C. for 1 hour, followed by weighing.
  • W[0086] 2 is an in-water weight obtained by boiling a sample in water to infiltrate water completely into the pores, followed by weighing in water.
  • W[0087] 3 is a water-saturated weight obtained by infiltrating water completely into the pores of a sample, followed by weighing in air.
  • (Oxidation Resistance) [0088]
  • A test piece of 60 mm×60 mm×5 mm (thickness) was prepared by cutting; it was allowed to stand in a furnace of 1,150° C. in an O[0089] 2 gas current containing saturated steam of 90° C., to give rise to the oxidation of the test piece; and the per-hour weight increase of the test piece by oxidation was measured.
  • (Bending Strength) [0090]
  • A test sample was subjected to a four-point bending strength test at ordinary temperature according to JIS R 1601 “Test Method for Bending Strength of Fine Ceramics”, using the plane of the test sample at the half thickness (the plane is the central plane of the test sample) as a tensile plane. [0091]
  • (Si Concentration) [0092]
  • From a test sample having a thickness of 10 mm were cut out a surface layer having a thickness of 0.5 mm and an innermost layer having a thickness of 0.5 mm. The two layers were measured for Si content by fluorescent X-ray analysis.[0093]
  • EXAMPLES 1 TO 3
  • There were mixed 70% by weight of SiC coarse particles having an average particle diameter of 100 μm, 30% by weight of SiC fine particles having an average particle diameter of 5 μm and 10% by weight, based on 100% by weight of the total Sic particles, of a C powder having an average particle diameter of 2 μm. To 100% by weight of the resulting mixture were added 2% by weight of an organic binder and 10% by weight of water to obtain a slurry mixture (material A). [0094]
  • There were mixed 50% by weight of SiC coarse particles having an average particle diameter of 100 μm, 50% by weight of SiC fine particles having an average particle diameter of 5 μm and 5% by weight, based on 100% by weight of the total SiC particles, of a C powder having an average particle diameter of 2 μm. To 100% by weight of the resulting mixture were added 1.5% by weight of an organic binder and 14% by weight of water to obtain a slurry mixture (material B). [0095]
  • Material A obtained above was cast into a gypsum mold of 100 mm×100 mm×30 mm (height) at a thickness of 5 mm; thereon was cast material B at a thickness of 5 mm; thereon was cast material A at a thickness of 5 mm to produce a molded material (molded material 1) of 100 mm×100 mm×15 mm. [0096]
  • Molded material 1 was vertically placed in a carbon crucible filled with a Si powder having a purity of 99.8% and an average particle diameter of 1 mm. The carbon crucible was transferred into a firing furnace. [0097]
  • The temperature inside the firing furnace was kept at 1,100 to 1,400° C. and the crucible contents were subjected to a firing treatment under the conditions of inert gas flow rate, in-furnace pressure and treatment time, shown in Table 1. Then, while the in-furnace pressure was kept at the same level, the in-furnace temperature was increased to the maximum temperature shown in Table 1 to infiltrate Si into molded material 1, whereby a Si—SiC material of Si concentration-gradient type was produced. [0098]
  • The porosity and Si concentration of the Si—SiC material are shown in Table 1. [0099]
  • EXAMPLES 4 TO 9
  • There were mixed 70% by weight of SiC coarse particles having an average particle diameter of 100 μm, 30% by weight of SiC fine particles having an average particle diameter of 5 μm and 10% by weight, based on 100% by weight of the total SiC particles, of a C powder having an average particle diameter of 2 μm. To 100% by weight of the resulting mixture were added 5% by weight of an organic binder and an appropriate amount of water to obtain a slurry mixture. This slurry mixture was subjected to granulation by the use of a spray dryer to produce granulated particles having an average particle diameter of 120 μm (material C). [0100]
  • There were mixed 50% by weight of SiC coarse particles having an average particle diameter of 100 μm, 50% by weight of SiC fine particles having an average particle diameter of 5 μm and 5% by weight, based on 100% by weight of the total SiC particles, of a C powder having an average particle diameter of 2 μm. To 100% by weight of the resulting mixture were added 5% by weight of an organic binder and an appropriate amount of water to obtain a slurry mixture. This slurry mixture was subjected to granulation by the use of a spray dryer to produce granulated particles having an average particle diameter of 120 μm (material D). [0101]
  • Material C was placed in a mold of 100 mm×100 mm. Thereon was placed a SiC fiber cloth. Thereon was placed material C (the SiC fiber cloth was between the two material C layers). The resulting material was subjected to press molding at a pressure of 500 kgf/cm[0102] 2 to obtain a molded material (preliminary molded material C) of 100 mm×100 mm×5 mm.
  • Using material D, a molded material (preliminary molded material D) of 100 mm×100 mm×5 mm was produced in the same manner as above. [0103]
  • The above two kinds of molded materials were piled in the order of “preliminary molded material C-preliminary molded material D-preliminary molded material C”. The resulting material was subjected to press molding to obtain a molded material (molded material 2) of 100 mm×100 mm×15 mm. [0104]
  • Incidentally, as the SiC fiber cloth was used Nicalon (a product of Nippon Carbon Co., Ltd.) or Hinicalon (also a product of Nippon Carbon Co., Ltd.). Molded material 2 using Nicalon was named as molded material 2-1, and molded material 2 using Hinicalon was named as molded material 2-2. [0105]
  • Molded material 2-1 or 2-2 was vertically placed in a carbon crucible filled with a Si powder having a purity of 99.8% and an average particle diameter of 1 mm. The carbon crucible was transferred into a firing furnace. [0106]
  • The temperature inside the firing furnace was kept at 1,100 to 1,400° C. and the crucible contents were subjected to a firing treatment under the conditions of inert gas flow rate, in-furnace pressure and treatment time, shown in Table 1. Then, while the in-furnace pressure was kept at the same level, the in-furnace temperature was increased to the maximum temperature shown in Table 1 to infiltrate Si into molded material 2-1 or 2-2, whereby a SiC fiber-reinforced Si—SiC composite material of Si concentration-gradient type was produced. [0107]
  • The porosity and Si concentration of the composite material are shown in Table 1. [0108]
    TABLE 1
    Flow rate Kind of Maximum
    Temperature 1100˜1400° C. of Ar molded temperature Time Porosity
    Pressure (hPa) Time (Hr) (NL/min) material (° C.) (Hr) (%)
    Example 1 0.1 5 0.1 1 1800 1 0.15
    Example 2 10.0  8 1.0 1 1700 2 0.10
    Example 3 1.0 10  10.0  1 1750 1 0.05
    Example 4 0.1 5 0.1 2-1 1800 1 0.90
    Example 5 0.1 5 0.1 2-2 1800 1 0.50
    Example 6 10.0  8 1.0 2-1 1700 2 0.60
    Example 7 10.0  8 1.0 2-2 1700 2 0.30
    Example 8 1.0 10  10.0  2-1 1750 1 0.10
    Example 9 1.0 10  10.0  2-2 1750 1 0.05
  • As shown in Table 1, there was a general tendency that at a temperature range of 1,100 to 1,400° C., the porosities of the present materials decreased with the gradual increase of Ar (inert gas) flow rate, in-furnace pressure and firing time. Pores, even when present, were very fine and about 10 μm or less in diameter. [0109]
  • For reducing pores, the interaction of in-furnace pressure with firing time and Ar flow rate was a very important factor. [0110]
  • EXAMPLES 10 TO 11 AND COMPARATIVE EXAMPLES 1 TO 2
  • Oxidation resistance was measured on the SiC fiber-reinforced Si—SiC composite materials of Examples 10 and 11, obtained in Examples 8 and 9; a Si—SiC sintered material [NEWSIC (trade name), a product of NGK Insulators, Ltd.] of Comparative Example 1; and a Si—SiC sintered material (a product of CESIWID Co., Germany) of Comparative Example 2. The results are shown in Table 2. [0111]
    TABLE 2
    Oxidation resistance
    Weight increase (%)
    After 100 hours After 500 hours
    Example 10 0.01 0.02
    Example 11 0.008 0.015
    Comparative 0.01 0.02
    Example 1
    Comparative 0.01 0.34
    Example 2
  • EXAMPLE 12 AND COMPARATIVE EXAMPLES 3 TO 4
  • Porosity and bending strength were measured on four kinds (sample Nos. 1 to 4) of SiC fiber-reinforced Si—SiC composite materials of Examples 12, obtained in Examples 6 to 9; four kinds of Si—SiC sintered materials [NEWSIC (trade name), products of NGK Insulators, Ltd.] of Comparative Example 3; and four kinds of Si—SiC sintered materials (products of CESIWID Co., Germany) of Comparative Example 4. [0112]
  • The results are shown in Tables 3 and 4. [0113]
    TABLE 3
    Porosity (%)
    Samples
    No. 1 No. 2 No. 3 No. 4
    Example 12 0.1 0.1 0.2 0.2
    Comparative 0.1 0.1 0.2 0.2
    Example 3
    Comparative 0.8 0.9 0.9 1.0
    Example 4
  • [0114]
    TABLE 4
    Bending strength (MPa) at ordinary temperature
    Samples
    No. 1 No. 2 No. 3 No. 4
    Example 12 320 325 315 327
    Comparative 265 268 273 275
    Example 3
    Comparative 189 210 218 224
    Example 4
  • As shown in Tables 2 to 4, the SiC fiber-reinforced Si—SiC composite materials of Si concentration-gradient type according to the present invention (Examples 10 to 12) can have a porosity of 0.2% or less and, as compared with commercial Si—SiC sintered materials of Comparative Examples 1 (3 ?) to 4, have about the same oxidation resistance and bending strength and can have higher fracture toughens. [0115]
  • The SiC fiber-reinforced Si—SiC composite material of Si concentration-gradient type of the present invention, obtained by using Nicalon [a SiC fiber cloth (a fiber preform) made of a Si—C—O type silicon carbide fiber] has improved strength at high temperatures and is significantly improved in fragility inherently possessed by ceramics. [0116]
  • The SiC fiber-reinforced Si—SiC composite material of Si concentration-gradient type of the present invention, obtained by using Hinicalon [a SiC fiber cloth (a fiber preform) made of a Si—C—O type silicon carbide fiber], as compared with the above composite material obtained using Nicalon, had higher oxidation resistance and creeping resistance. [0117]
  • Incidentally, Nicalon and Hinicalon are produced as follows. [0118]
  • Nicalon, which is a Si—C—O type silicon carbide fiber having a β-SiC structure, is produced by melt-spinning an organic silicic acid polymer (a polycarbosilane) to obtain a continuous fiber, heating the fiber in air to give rise to crosslinking of Si—O—Si and infusibilization, and firing the resulting material in an inert gas atmosphere at 1,200 to 1,500° C. [0119]
  • Hinicalon, which is a Si—C—O type silicon carbide fiber of very low oxygen content (oxygen content=0.5 mass % or less), is produced by melt-spinning a silicon carbide fiber organic silicic acid polymer (a polycarbosilane) to obtain a continuous fiber, irradiating the fiber with an electron beam in a non-oxygen atmosphere to give rise to self-crosslinking and infusibilization of polycarbosilane in the absence of oxygen, and firing the resulting material in an inert gas atmosphere at a temperature of 1,000° C. or higher. [0120]
  • EXAMPLES 13 TO 18 AND COMPARATIVE EXAMPLES 5 TO 6
  • Ten test pieces (3 mm×4 mm×40 mm) as described in JIS R 1601 were cut out from each of the Si—SiC materials of Si concentration-gradient type of Examples 13 to 15 obtained in Examples 1 to 3, the SiC fiber-reinforced Si—SiC composite materials of Si concentration-gradient type of Examples 16 to 18 obtained in Examples 7 to 9, a Si—SiC sintered material [NEWSIC (trade name), a product of NGK Insulators, Ltd.] of Comparative Example 5, and a Si—SiC sintered material (a product of CESIWID Co., Germany) of Comparative Example 6. Microcracks were forcibly formed in each test piece by microindentation. Five of the test pieces with microcracks were measured for bending strength as they were. The remaining five test samples were kept in air at 1,300° C. for 500 hours for surface healing, and then measured for bending strength. [0121]
  • The bending strengths before and after surface healing, of test pieces are shown in Table 5. [0122]
  • Table 5
  • Ordinary-temperature bending strengths (MPa) before and after healing, of test pieces with microcracks forcibly formed by microindentation [0123]
    Ordinary-temperature bending strength (MPa)
    Before healing After healing Improvement (%)
    Example 13 118 150 27
    Example 14 135 178 32
    Example 15 133 162 22
    Example 16 153 190 20
    Example 17 138 186 35
    Example 18 145 181 25
    Comparative 124 146 18
    Example 5
    Comparative 102 121 19
    Example 6
  • As shown in Table 5, the Si—SiC materials of Si concentration-gradient type of Examples 13 to 15 and SiC fiber-reinforced Si—SiC composite materials of Si concentration-gradient type of Examples 16 to 18, all according to the present invention are superior in healability of microcracks, as compared with conventional Si—SiC sintered materials. [0124]
  • The reason is as follows. In the materials of the present invention, the Si concentration in the surface layer is relatively higher than the Si concentration in the innermost layer; therefore, the formed microcracks are oxidized by heating and simultaneously healed; as a result, the sizes of defects in material become smaller and the properties of material are retained. [0125]
  • In the SiC fiber-reinforced Si—SiC composite materials of Si concentration-gradient-type of Examples 16 to 18, a smaller amount of the microcracks formed by microindentation gives a higher healability in strength, toughness and fragility of ceramic. [0126]
  • [Confirmation and Evaluation of Si Concentration Gradient][0127]
  • Si concentrations in surface layer and innermost layer were measured for the Si—SiC materials of Si concentration-gradient type obtained in Examples 1 to 3, the SiC fiber-reinforced Si—SiC composite materials of SiC concentration-gradient type obtained in Examples 4, 8 and 9, the commercial Si—SiC sintered material [NEWSIC (trade name), a product of NGK Insulators, Ltd.] of Comparative Example 1, and the commercial Si—SiC sintered material (a product of CESIWID Co, Germany) of Comparative Example 2. [0128]
  • The results are shown in Table 6. [0129]
    TABLE 6
    Si concentration (wt. %)
    Surface layer Innermost layer Ratio
    (a) (b) (b)/(a)
    Example 1 27 13.5 50/100
    Example 2 32 11.0 34/100
    Example 3 20 14.0 70/100
    Example 4 22.0 19.5 89/100
    Example 8 35 0.5  1/100
    Example 9 25 5.5 22/100
    Comparative 18.5 18.5 100/100 
    Example 1
    Comparative 21.0 20.5 98/100
    Example 2
  • As is clear from Table 6, in the Si—SiC materials of Si concentration-gradient type and the SiC fiber-reinforced Si—SiC composite materials of SiC concentration-gradient type all according to the present invention, the Si concentration is higher in the surface layer and lower in the innermost layer and has a gradient. Meanwhile, in the commercial products, the Si concentration is almost the same in the surface layer and the innermost layer. [0130]
  • As described above, the Si—SiC material of Si concentration-gradient type and SiC fiber-reinforced Si—SiC composite material of Si concentration-gradient type produced by the present processes are superior in corrosion resistance in highly oxidative and corrosive environment as well as in strength, and is significantly improved in healability of defects of surface layer and innermost layer. [0131]
  • Further, the SiC fiber-reinforced Si—SiC composite material of Si concentration-gradient type according to the present invention is substantially free from pores which are present in conventional ceramic matrix materials (CMC) (e.g. SiC fiber-reinforced Si—SiC composite materials) produced by CVD or inorganic polymer infiltration; therefore, the present composite material, as compared with conventional ceramic matrix composites (CMC), is dense and moreover retains excellent features of Si—SiC sintered material, such as oxidation resistance, creeping resistance, strength from ordinary temperature to high temperatures and toughness. [0132]

Claims (10)

What is claimed is:
1. A Si—SiC material of Si concentration-gradient type obtained by melt-infiltrating Si into a molded material comprising SiC particles, which Si—SiC material has a porosity of 1.0% or less and in which Si—SiC material the Si concentration decreases gradually from the surface layer towards the innermost layer.
2. A Si—SiC material of Si concentration-gradient type according to
claim 1
, wherein the ratio of the Si concentration of the surface layer and the Si concentration of the innermost layer is in a range of innermost layer/surface layer =0/100 to 90/100.
3. A process for producing a Si—SiC material of Si concentration-gradient type by melt-infiltrating Si into a molded material comprising SiC particles, which process comprises preparing at least two kinds of mixtures each comprising SiC particles having a different tap density, laminating the mixtures to form a molded material, keeping the molded material and Si at a temperature of 1,100 to 1,400° C. in an inert gas atmosphere, and then increasing the temperature to 1,500 to 2,500° C. to melt-infiltrate Si into the molded material.
4. A process according to
claim 3
, wherein the molded material and Si are kept at a temperature of 1,100 to 1,400° C. at a pressure of 0.1 to 10 hPa for at least one hour with an inert gas being flown in an amount of 0.1 NL or more per kg of the total of the molded material and Si, and then the temperature is increased to 1,500 to 2,500° C. to melt-infiltrate Si into the molded material.
5. A SiC fiber-reinforced Si—SiC composite material of Si concentration-gradient type obtained by melt-infiltrating Si into a molded material comprising a SiC fiber and SiC particles, which composite material has a porosity of 1.0% or less and in which composite material the Si concentration decreases gradually from the surface layer towards the innermost layer.
6. A SiC fiber-reinforced Si—SiC composite material of Si concentration-gradient type according to
claim 5
, wherein the ratio of the Si concentration of the surface layer and the Si concentration of the innermost layer is in a range of innermost layer/surface layer=0/100 to 90/100.
7. A SiC fiber-reinforced Si—SiC composite material of Si concentration-gradient type according to
claim 5
, wherein the oxygen content in the SiC fiber used in the composite material is 0.5 mass % or less.
8. A SiC fiber-reinforced Si—SiC composite material of Si concentration-gradient type according to
claim 6
, wherein the oxygen content in the SiC fiber used in the composite material is 0.5 mass % or less.
9. A process for producing a SiC fiber-reinforced Si—SiC composite material of Si concentration-gradient type obtained by melt-infiltrating Si into a molded material comprising a SiC fiber and SiC particles, which process comprises preparing at least two kinds of mixtures each comprising SiC particles having a different tap density, mixing a SiC fiber into each mixture, laminating the resulting mixtures to form a molded material, keeping the molded material and Si at a temperature of 1,100 to 1,400° C. in an inert gas atmosphere, and then increasing the temperature to 1,500 to 2,500° C. to melt-infiltrate Si into the molded material.
10. A process according to
claim 9
, wherein the molded material and Si are kept at a temperature of 1,100 to 1,400° C. at a pressure of 0.1 to 10 hPa for at least one hour with an inert gas being flown in an amount of 0.1 NL or more per kg of the total of the molded material and Si, and then the temperature is increased to 1,500 to 2,500° C. to melt-infiltrate Si into the molded material.
US09/847,436 1997-07-18 2001-05-03 Si-SiC material and SiC fiber-reinforced Si-SiC composite material Expired - Lifetime US6444063B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US09/847,436 US6444063B2 (en) 1997-07-18 2001-05-03 Si-SiC material and SiC fiber-reinforced Si-SiC composite material

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
JP9-194132 1997-07-18
JP19413297A JP4014254B2 (en) 1997-07-18 1997-07-18 Si concentration step-variable Si-SiC material, Si concentration step change-type SiC fiber reinforced Si-SiC composite material, and production method thereof
US09/114,260 US6254974B1 (en) 1997-07-18 1998-07-13 Si-SiC material and SiC fiber-reinforced Si-SiC composite material
US09/847,436 US6444063B2 (en) 1997-07-18 2001-05-03 Si-SiC material and SiC fiber-reinforced Si-SiC composite material

Related Parent Applications (1)

Application Number Title Priority Date Filing Date
US09/114,260 Division US6254974B1 (en) 1997-07-18 1998-07-13 Si-SiC material and SiC fiber-reinforced Si-SiC composite material

Publications (2)

Publication Number Publication Date
US20010026868A1 true US20010026868A1 (en) 2001-10-04
US6444063B2 US6444063B2 (en) 2002-09-03

Family

ID=16319449

Family Applications (2)

Application Number Title Priority Date Filing Date
US09/114,260 Expired - Lifetime US6254974B1 (en) 1997-07-18 1998-07-13 Si-SiC material and SiC fiber-reinforced Si-SiC composite material
US09/847,436 Expired - Lifetime US6444063B2 (en) 1997-07-18 2001-05-03 Si-SiC material and SiC fiber-reinforced Si-SiC composite material

Family Applications Before (1)

Application Number Title Priority Date Filing Date
US09/114,260 Expired - Lifetime US6254974B1 (en) 1997-07-18 1998-07-13 Si-SiC material and SiC fiber-reinforced Si-SiC composite material

Country Status (4)

Country Link
US (2) US6254974B1 (en)
EP (1) EP0891956B2 (en)
JP (1) JP4014254B2 (en)
DE (1) DE69802748T3 (en)

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1657227A1 (en) * 2004-11-15 2006-05-17 Deutsches Zentrum für Luft- und Raumfahrt e.V. Process of manufacture of a carbide ceramic material with a defined graded phase distribution profile, carbide ceramic material and structural member.
US7179532B2 (en) 2002-03-22 2007-02-20 Schunk Kohlenstofftechnik Gmbh Composite ceramic body and method for producing the same
US20070196693A1 (en) * 2006-02-22 2007-08-23 General Electric Company Manufacture of CMC articles having small complex features
WO2015055264A3 (en) * 2013-10-16 2015-06-25 Schunk Ingenieurkeramik Gmbh Method for the production of molded bodies from reaction-bonded, silicon-infiltrated silicon carbide and/or boron carbide and thus produced molded body
US9446989B2 (en) 2012-12-28 2016-09-20 United Technologies Corporation Carbon fiber-reinforced article and method therefor
CN106830968A (en) * 2017-02-24 2017-06-13 中南大学 A kind of modified C/C composites of compound interface layer and its preparation method and application
EP2982661A4 (en) * 2013-04-05 2017-06-28 In-Ho Park Method for manufacturing exothermic ceramics for microwave oven and exothermic ceramics for microwaves
CN109534834A (en) * 2018-08-08 2019-03-29 中国科学院化学研究所 One kind can ceramic phenolic resin and its preparation method and application
CN110981516A (en) * 2019-12-13 2020-04-10 苏州纳迪微电子有限公司 Composite bulletproof plate and preparation method thereof
EP3712122A1 (en) * 2019-03-21 2020-09-23 United Technologies Corporation Systems and methods for additively manufactured ceramic composites
FR3130272A1 (en) * 2021-12-13 2023-06-16 Safran Ceramics Manufacturing process of a CMC part

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6541134B1 (en) * 2000-06-22 2003-04-01 The United States Of America As Represented By The Secretary Of The Air Force Abradable thermal barrier coating for CMC structures
US6630029B2 (en) * 2000-12-04 2003-10-07 General Electric Company Fiber coating method and reactor
JP4454191B2 (en) * 2001-07-30 2010-04-21 日本特殊陶業株式会社 Manufacturing method of ceramic heater
DE10231278A1 (en) * 2002-07-10 2004-02-05 Sgl Carbon Ag Ceramic composite body
US7255924B2 (en) * 2004-01-13 2007-08-14 The United States Of America As Represented By The Secretary Of The Navy Carbon nanoarchitectures with ultrathin, conformal polymer coatings for electrochemical capacitors
US7279230B1 (en) * 2004-02-23 2007-10-09 United States Of America As Represented By The Secretary Of The Air Force Hybrid composite materials
US7846546B2 (en) * 2005-09-20 2010-12-07 Ube Industries, Ltd. Electrically conducting-inorganic substance-containing silicon carbide-based fine particles, electromagnetic wave absorbing material and electromagnetic wave absorber
DE102006009388B4 (en) * 2006-03-01 2009-02-26 Audi Ag Apparatus for siliconising carbonaceous materials and method practicable therein
US20090001219A1 (en) * 2006-12-07 2009-01-01 Honeywell International, Inc. Fiber polymer matrix composites having silicon-containing inorganic-organic matrices and methods of making the same
JP5379059B2 (en) * 2010-03-31 2013-12-25 太平洋セメント株式会社 Method for producing SiC / Si composite material
WO2012063923A1 (en) 2010-11-11 2012-05-18 国立大学法人京都大学 Sic ceramic material and sic ceramic structure, and production method for same
JP2014108896A (en) * 2012-11-30 2014-06-12 Nihon Ceratec Co Ltd SiC/Si COMPOSITE MATERIAL BODY AND METHOD OF PRODUCING THE SAME
US9644158B2 (en) 2014-01-13 2017-05-09 General Electric Company Feed injector for a gasification system
US9931818B1 (en) * 2017-04-05 2018-04-03 General Electric Company Method for forming CMC article
JP7085388B2 (en) * 2018-03-30 2022-06-16 イビデン株式会社 Method for manufacturing SiC fiber reinforced SiC composite material
FR3098513B1 (en) * 2019-07-09 2021-06-11 Safran Ceram Manufacturing process of a composite material part with a silicon carbide matrix

Family Cites Families (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1180918A (en) * 1966-06-10 1970-02-11 Atomic Energy Authority Uk Improvements in or relating to the Manufacture of Dense Bodies of Silicon Carbide.
US4795673A (en) * 1978-01-09 1989-01-03 Stemcor Corporation Composite material of discontinuous silicon carbide particles and continuous silicon matrix and method of producing same
US4294788A (en) * 1979-12-05 1981-10-13 General Electric Company Method of making a shaped silicon carbide-silicon matrix composite and articles made thereby
JPS56114871A (en) * 1980-02-18 1981-09-09 Shinetsu Chemical Co Manufacture of high strength silicon carbide molded body
US4923832A (en) * 1986-05-08 1990-05-08 Lanxide Technology Company, Lp Method of making shaped ceramic composites with the use of a barrier
JPH04224198A (en) * 1990-12-26 1992-08-13 Tokai Carbon Co Ltd Production of mmc preform
US5240672A (en) * 1991-04-29 1993-08-31 Lanxide Technology Company, Lp Method for making graded composite bodies produced thereby
EP0519641A1 (en) * 1991-06-17 1992-12-23 General Electric Company Silicon carbide composite with coated fiber reinforcement and method of forming
JPH0551268A (en) * 1991-08-21 1993-03-02 Sumitomo Electric Ind Ltd Fiber-reinforced functionally gradient material
US5503122A (en) * 1992-09-17 1996-04-02 Golden Technologies Company Engine components including ceramic-metal composites
US5735332A (en) * 1992-09-17 1998-04-07 Coors Ceramics Company Method for making a ceramic metal composite
DE4243868C2 (en) * 1992-12-23 1996-01-25 Bosch Siemens Hausgeraete Method for operating a dishwasher
US5455000A (en) * 1994-07-01 1995-10-03 Massachusetts Institute Of Technology Method for preparation of a functionally gradient material
DE4429825C1 (en) * 1994-08-23 1995-11-09 Heraeus Quarzglas Coated component made of quartz glass
US5628938A (en) * 1994-11-18 1997-05-13 General Electric Company Method of making a ceramic composite by infiltration of a ceramic preform
JPH0945467A (en) 1995-07-31 1997-02-14 Sumitomo Osaka Cement Co Ltd Carbon heater and manufacture thereof
US5952100A (en) * 1997-05-21 1999-09-14 General Electric Company Silicon-doped boron nitride coated fibers in silicon melt infiltrated composites

Cited By (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7179532B2 (en) 2002-03-22 2007-02-20 Schunk Kohlenstofftechnik Gmbh Composite ceramic body and method for producing the same
EP1657227A1 (en) * 2004-11-15 2006-05-17 Deutsches Zentrum für Luft- und Raumfahrt e.V. Process of manufacture of a carbide ceramic material with a defined graded phase distribution profile, carbide ceramic material and structural member.
US20070196693A1 (en) * 2006-02-22 2007-08-23 General Electric Company Manufacture of CMC articles having small complex features
US7507466B2 (en) 2006-02-22 2009-03-24 General Electric Company Manufacture of CMC articles having small complex features
US20090261508A1 (en) * 2006-02-22 2009-10-22 General Electric Company Manufacture of cmc articles having small complex features
US9446989B2 (en) 2012-12-28 2016-09-20 United Technologies Corporation Carbon fiber-reinforced article and method therefor
EP2982661A4 (en) * 2013-04-05 2017-06-28 In-Ho Park Method for manufacturing exothermic ceramics for microwave oven and exothermic ceramics for microwaves
WO2015055264A3 (en) * 2013-10-16 2015-06-25 Schunk Ingenieurkeramik Gmbh Method for the production of molded bodies from reaction-bonded, silicon-infiltrated silicon carbide and/or boron carbide and thus produced molded body
US9695089B2 (en) 2013-10-16 2017-07-04 Schunk Ingenieurkeramik Gmbh Method for the production of shaped articles from reaction-bonded, silicon-infiltrated silicon carbide and/or boron carbide and thus produced shaped body
EP3800169A1 (en) * 2013-10-16 2021-04-07 Schunk Ingenieurkeramik GmbH Method for the production of moulds from reaction-bonded silicon carbide and / or boron carbide infiltrated with silicon
EP3984980A1 (en) * 2013-10-16 2022-04-20 Schunk Ingenieurkeramik GmbH Moulded body of reaction-bonded silicon infiltrated silicon carbide
CN106830968A (en) * 2017-02-24 2017-06-13 中南大学 A kind of modified C/C composites of compound interface layer and its preparation method and application
CN109534834A (en) * 2018-08-08 2019-03-29 中国科学院化学研究所 One kind can ceramic phenolic resin and its preparation method and application
EP3712122A1 (en) * 2019-03-21 2020-09-23 United Technologies Corporation Systems and methods for additively manufactured ceramic composites
US11414355B2 (en) 2019-03-21 2022-08-16 Raytheon Technologies Corporation Systems and methods for additively manufactured ceramic composites
CN110981516A (en) * 2019-12-13 2020-04-10 苏州纳迪微电子有限公司 Composite bulletproof plate and preparation method thereof
FR3130272A1 (en) * 2021-12-13 2023-06-16 Safran Ceramics Manufacturing process of a CMC part

Also Published As

Publication number Publication date
EP0891956B1 (en) 2001-12-05
DE69802748T3 (en) 2006-07-06
JPH1135376A (en) 1999-02-09
EP0891956A2 (en) 1999-01-20
DE69802748T2 (en) 2002-09-26
US6444063B2 (en) 2002-09-03
DE69802748D1 (en) 2002-01-17
EP0891956A3 (en) 1999-06-30
US6254974B1 (en) 2001-07-03
JP4014254B2 (en) 2007-11-28
EP0891956B2 (en) 2005-10-12

Similar Documents

Publication Publication Date Title
US6444063B2 (en) Si-SiC material and SiC fiber-reinforced Si-SiC composite material
US6576076B1 (en) Process for producing fiber-reinforced silicon carbide composites
US9353013B2 (en) SiC ceramic material, SiC ceramic structure, and their fabrication methods
US5338576A (en) Silicon carbide sintered article and method
Yano et al. Fabrication of silicon carbide fiber-reinforced silicon carbide composite by hot-pressing
JP3491902B2 (en) Fiber composite material and method for producing the same
EP1013626B1 (en) Ceramic matrix composite and method for changing the dielectric properties of a ceramic matrix composite
Kim et al. Nicalon-fibre-reinforced silicon-carbide composites via polymer solution infiltration and chemical vapour infiltration
JP2765543B2 (en) Reaction sintered ceramics and method for producing the same
JPH0157075B2 (en)
JP2879675B1 (en) Method for producing two-dimensional fiber reinforced silicon carbide / carbon composite ceramics
US5296417A (en) Self-supporting bodies
JPH10167831A (en) Sic fiber reinforced si-sic composite material and its production
US5034356A (en) Ceramic matrix composite
US5180697A (en) Process for preparing self-supporting bodies and products produced thereby
Sieber et al. Light weight ceramic composites from laminated paper structures
JP3574583B2 (en) Heat radiating material and method of manufacturing the same
IE921081A1 (en) Process for the preparation of non-oxide monolithic ceramics
Chawla et al. Processing of ceramic matrix composites
JPH08169761A (en) Production of silicon carbide-based fiber composite material
JPH07315932A (en) Production of carbon fiber reinforced carbon composite material converted into silicon carbide
SHIN et al. Fabrication and mechanical properties of reaction-bonded carbon fiber/Si/SiC composites
Nakano et al. Microstructures and Mechanical Properties of Hi‐Nicalon Fiber Reinforced Si3N4 Matrix Composites
Mohr et al. Polyorganosilazane preceramic binder development for reaction bonded silicon nitride composites
JPH06287062A (en) Reinforced sic-based ceramic member

Legal Events

Date Code Title Description
STCF Information on status: patent grant

Free format text: PATENTED CASE

FPAY Fee payment

Year of fee payment: 4

FPAY Fee payment

Year of fee payment: 8

FEPP Fee payment procedure

Free format text: PAYOR NUMBER ASSIGNED (ORIGINAL EVENT CODE: ASPN); ENTITY STATUS OF PATENT OWNER: LARGE ENTITY

FPAY Fee payment

Year of fee payment: 12