EP1751077A2 - Verfahren zur herstellung von rohteilen auf beta-sic-basis zur verwendung für aggressive medien - Google Patents

Verfahren zur herstellung von rohteilen auf beta-sic-basis zur verwendung für aggressive medien

Info

Publication number
EP1751077A2
EP1751077A2 EP05770958A EP05770958A EP1751077A2 EP 1751077 A2 EP1751077 A2 EP 1751077A2 EP 05770958 A EP05770958 A EP 05770958A EP 05770958 A EP05770958 A EP 05770958A EP 1751077 A2 EP1751077 A2 EP 1751077A2
Authority
EP
European Patent Office
Prior art keywords
sic
resin
receptacle
precursor
mixture
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.)
Withdrawn
Application number
EP05770958A
Other languages
English (en)
French (fr)
Inventor
Charlotte Pham
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.)
SICAT Societe Industrielle de Creations et d'Applications Textiles SARL
Original Assignee
SICAT Societe Industrielle de Creations et d'Applications Textiles SARL
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by SICAT Societe Industrielle de Creations et d'Applications Textiles SARL filed Critical SICAT Societe Industrielle de Creations et d'Applications Textiles SARL
Publication of EP1751077A2 publication Critical patent/EP1751077A2/de
Withdrawn legal-status Critical Current

Links

Classifications

    • C—CHEMISTRY; METALLURGY
    • C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B35/00—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
    • C04B35/515—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics
    • C04B35/56—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics based on carbides or oxycarbides
    • C04B35/565—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics based on carbides or oxycarbides based on silicon carbide
    • C04B35/571—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics based on carbides or oxycarbides based on silicon carbide obtained from Si-containing polymer precursors or organosilicon monomers
    • C—CHEMISTRY; METALLURGY
    • C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B35/00—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
    • C04B35/515—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics
    • C04B35/56—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics based on carbides or oxycarbides
    • C04B35/565—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics based on carbides or oxycarbides based on silicon carbide
    • C—CHEMISTRY; METALLURGY
    • C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B35/00—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
    • C04B35/515—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics
    • C04B35/56—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics based on carbides or oxycarbides
    • C04B35/565—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics based on carbides or oxycarbides based on silicon carbide
    • C04B35/573—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics based on carbides or oxycarbides based on silicon carbide obtained by reaction sintering or recrystallisation
    • C—CHEMISTRY; METALLURGY
    • C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B35/00—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
    • C04B35/71—Ceramic products containing macroscopic reinforcing agents
    • C04B35/78—Ceramic products containing macroscopic reinforcing agents containing non-metallic materials
    • C04B35/80—Fibres, filaments, whiskers, platelets, or the like
    • C—CHEMISTRY; METALLURGY
    • C25—ELECTROLYTIC OR ELECTROPHORETIC PROCESSES; APPARATUS THEREFOR
    • C25C—PROCESSES FOR THE ELECTROLYTIC PRODUCTION, RECOVERY OR REFINING OF METALS; APPARATUS THEREFOR
    • C25C3/00—Electrolytic production, recovery or refining of metals by electrolysis of melts
    • C25C3/06—Electrolytic production, recovery or refining of metals by electrolysis of melts of aluminium
    • C25C3/08—Cell construction, e.g. bottoms, walls, cathodes
    • C25C3/085—Cell construction, e.g. bottoms, walls, cathodes characterised by its non electrically conducting heat insulating parts
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23M—CASINGS, LININGS, WALLS OR DOORS SPECIALLY ADAPTED FOR COMBUSTION CHAMBERS, e.g. FIREBRIDGES; DEVICES FOR DEFLECTING AIR, FLAMES OR COMBUSTION PRODUCTS IN COMBUSTION CHAMBERS; SAFETY ARRANGEMENTS SPECIALLY ADAPTED FOR COMBUSTION APPARATUS; DETAILS OF COMBUSTION CHAMBERS, NOT OTHERWISE PROVIDED FOR
    • F23M5/00—Casings; Linings; Walls
    • C—CHEMISTRY; METALLURGY
    • C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/02—Composition of constituents of the starting material or of secondary phases of the final product
    • C04B2235/30—Constituents and secondary phases not being of a fibrous nature
    • C04B2235/32—Metal oxides, mixed metal oxides, or oxide-forming salts thereof, e.g. carbonates, nitrates, (oxy)hydroxides, chlorides
    • C04B2235/3217—Aluminum oxide or oxide forming salts thereof, e.g. bauxite, alpha-alumina
    • C—CHEMISTRY; METALLURGY
    • C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/02—Composition of constituents of the starting material or of secondary phases of the final product
    • C04B2235/30—Constituents and secondary phases not being of a fibrous nature
    • C04B2235/34—Non-metal oxides, non-metal mixed oxides, or salts thereof that form the non-metal oxides upon heating, e.g. carbonates, nitrates, (oxy)hydroxides, chlorides
    • C04B2235/3418—Silicon oxide, silicic acids, or oxide forming salts thereof, e.g. silica sol, fused silica, silica fume, cristobalite, quartz or flint
    • C—CHEMISTRY; METALLURGY
    • C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/02—Composition of constituents of the starting material or of secondary phases of the final product
    • C04B2235/30—Constituents and secondary phases not being of a fibrous nature
    • C04B2235/38—Non-oxide ceramic constituents or additives
    • C04B2235/3817—Carbides
    • C04B2235/3826—Silicon carbides
    • C04B2235/383—Alpha silicon carbide
    • C—CHEMISTRY; METALLURGY
    • C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/02—Composition of constituents of the starting material or of secondary phases of the final product
    • C04B2235/30—Constituents and secondary phases not being of a fibrous nature
    • C04B2235/38—Non-oxide ceramic constituents or additives
    • C04B2235/3817—Carbides
    • C04B2235/3826—Silicon carbides
    • C04B2235/3834—Beta silicon carbide
    • C—CHEMISTRY; METALLURGY
    • C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/02—Composition of constituents of the starting material or of secondary phases of the final product
    • C04B2235/30—Constituents and secondary phases not being of a fibrous nature
    • C04B2235/38—Non-oxide ceramic constituents or additives
    • C04B2235/3852—Nitrides, e.g. oxynitrides, carbonitrides, oxycarbonitrides, lithium nitride, magnesium nitride
    • C04B2235/3873—Silicon nitrides, e.g. silicon carbonitride, silicon oxynitride
    • C—CHEMISTRY; METALLURGY
    • C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/02—Composition of constituents of the starting material or of secondary phases of the final product
    • C04B2235/30—Constituents and secondary phases not being of a fibrous nature
    • C04B2235/38—Non-oxide ceramic constituents or additives
    • C04B2235/3852—Nitrides, e.g. oxynitrides, carbonitrides, oxycarbonitrides, lithium nitride, magnesium nitride
    • C04B2235/3886—Refractory metal nitrides, e.g. vanadium nitride, tungsten nitride
    • C—CHEMISTRY; METALLURGY
    • C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/02—Composition of constituents of the starting material or of secondary phases of the final product
    • C04B2235/30—Constituents and secondary phases not being of a fibrous nature
    • C04B2235/42—Non metallic elements added as constituents or additives, e.g. sulfur, phosphor, selenium or tellurium
    • C04B2235/422—Carbon
    • C04B2235/424—Carbon black
    • C—CHEMISTRY; METALLURGY
    • C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/02—Composition of constituents of the starting material or of secondary phases of the final product
    • C04B2235/30—Constituents and secondary phases not being of a fibrous nature
    • C04B2235/42—Non metallic elements added as constituents or additives, e.g. sulfur, phosphor, selenium or tellurium
    • C04B2235/428—Silicon
    • C—CHEMISTRY; METALLURGY
    • C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/02—Composition of constituents of the starting material or of secondary phases of the final product
    • C04B2235/30—Constituents and secondary phases not being of a fibrous nature
    • C04B2235/48—Organic compounds becoming part of a ceramic after heat treatment, e.g. carbonising phenol resins
    • C—CHEMISTRY; METALLURGY
    • C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/02—Composition of constituents of the starting material or of secondary phases of the final product
    • C04B2235/50—Constituents or additives of the starting mixture chosen for their shape or used because of their shape or their physical appearance
    • C04B2235/52—Constituents or additives characterised by their shapes
    • C04B2235/5208—Fibers
    • C04B2235/5216—Inorganic
    • C04B2235/524—Non-oxidic, e.g. borides, carbides, silicides or nitrides
    • C04B2235/5244—Silicon carbide
    • C—CHEMISTRY; METALLURGY
    • C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/02—Composition of constituents of the starting material or of secondary phases of the final product
    • C04B2235/50—Constituents or additives of the starting mixture chosen for their shape or used because of their shape or their physical appearance
    • C04B2235/52—Constituents or additives characterised by their shapes
    • C04B2235/5208—Fibers
    • C04B2235/526—Fibers characterised by the length of the fibers
    • C—CHEMISTRY; METALLURGY
    • C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/02—Composition of constituents of the starting material or of secondary phases of the final product
    • C04B2235/50—Constituents or additives of the starting mixture chosen for their shape or used because of their shape or their physical appearance
    • C04B2235/54—Particle size related information
    • C04B2235/5418—Particle size related information expressed by the size of the particles or aggregates thereof
    • C04B2235/5427—Particle size related information expressed by the size of the particles or aggregates thereof millimeter or submillimeter sized, i.e. larger than 0,1 mm
    • C—CHEMISTRY; METALLURGY
    • C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/02—Composition of constituents of the starting material or of secondary phases of the final product
    • C04B2235/50—Constituents or additives of the starting mixture chosen for their shape or used because of their shape or their physical appearance
    • C04B2235/54—Particle size related information
    • C04B2235/5418—Particle size related information expressed by the size of the particles or aggregates thereof
    • C04B2235/5436—Particle size related information expressed by the size of the particles or aggregates thereof micrometer sized, i.e. from 1 to 100 micron
    • C—CHEMISTRY; METALLURGY
    • C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/60—Aspects relating to the preparation, properties or mechanical treatment of green bodies or pre-forms
    • C04B2235/602—Making the green bodies or pre-forms by moulding
    • C04B2235/6021—Extrusion moulding
    • C—CHEMISTRY; METALLURGY
    • C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/65—Aspects relating to heat treatments of ceramic bodies such as green ceramics or pre-sintered ceramics, e.g. burning, sintering or melting processes
    • C04B2235/658—Atmosphere during thermal treatment
    • C—CHEMISTRY; METALLURGY
    • C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/65—Aspects relating to heat treatments of ceramic bodies such as green ceramics or pre-sintered ceramics, e.g. burning, sintering or melting processes
    • C04B2235/658—Atmosphere during thermal treatment
    • C04B2235/6587—Influencing the atmosphere by vaporising a solid material, e.g. by using a burying of sacrificial powder
    • C—CHEMISTRY; METALLURGY
    • C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/70—Aspects relating to sintered or melt-casted ceramic products
    • C04B2235/74—Physical characteristics
    • C04B2235/76—Crystal structural characteristics, e.g. symmetry
    • C04B2235/762—Cubic symmetry, e.g. beta-SiC
    • C—CHEMISTRY; METALLURGY
    • C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/70—Aspects relating to sintered or melt-casted ceramic products
    • C04B2235/74—Physical characteristics
    • C04B2235/76—Crystal structural characteristics, e.g. symmetry
    • C04B2235/767—Hexagonal symmetry, e.g. beta-Si3N4, beta-Sialon, alpha-SiC or hexa-ferrites
    • C—CHEMISTRY; METALLURGY
    • C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/70—Aspects relating to sintered or melt-casted ceramic products
    • C04B2235/74—Physical characteristics
    • C04B2235/77—Density
    • C—CHEMISTRY; METALLURGY
    • C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/70—Aspects relating to sintered or melt-casted ceramic products
    • C04B2235/80—Phases present in the sintered or melt-cast ceramic products other than the main phase
    • C—CHEMISTRY; METALLURGY
    • C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/70—Aspects relating to sintered or melt-casted ceramic products
    • C04B2235/94—Products characterised by their shape
    • C—CHEMISTRY; METALLURGY
    • C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/70—Aspects relating to sintered or melt-casted ceramic products
    • C04B2235/95—Products characterised by their size, e.g. microceramics
    • C—CHEMISTRY; METALLURGY
    • C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/70—Aspects relating to sintered or melt-casted ceramic products
    • C04B2235/96—Properties of ceramic products, e.g. mechanical properties such as strength, toughness, wear resistance
    • C04B2235/9669—Resistance against chemicals, e.g. against molten glass or molten salts
    • C04B2235/9692—Acid, alkali or halogen resistance
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23M—CASINGS, LININGS, WALLS OR DOORS SPECIALLY ADAPTED FOR COMBUSTION CHAMBERS, e.g. FIREBRIDGES; DEVICES FOR DEFLECTING AIR, FLAMES OR COMBUSTION PRODUCTS IN COMBUSTION CHAMBERS; SAFETY ARRANGEMENTS SPECIALLY ADAPTED FOR COMBUSTION APPARATUS; DETAILS OF COMBUSTION CHAMBERS, NOT OTHERWISE PROVIDED FOR
    • F23M2900/00—Special features of, or arrangements for combustion chambers
    • F23M2900/05004—Special materials for walls or lining

Definitions

  • the present invention relates to ceramic materials based on ⁇ -SiC for use in aggressive media, such as they arise in particular in chemical and electrometallurgical engineering, and more particularly refractory pieces or bricks used in incineration furnaces or electrolysis tanks. It relates more particularly to a simplified manufacturing process for such parts or bricks.
  • EP 0 356 800 (Shin-Etsu Chemical Co) describes a binder composition for silicon carbide, comprising fine powders of silicon carbide, silicon and carbon and carbon resins. This composition is compressed between two pieces of SiC and the assembly is heated to 1500 ° C. to react the components of the binder and obtain a solid interface between the two pieces.
  • the heat treatment is preferably carried out under inert gas or under vacuum. An example produced by heating the parts in air shows that the mechanical resistance of the interface is less good than when the treatment is carried out under argon.
  • the methods according to the prior art require heat treatment under an atmosphere of inert gas, typically nitrogen or argon , or under vacuum, because the chemical resistance of the parts obtained in air is not satisfactory. This results in additional investment and operating costs, which is linked to the management of vacuum or inert gases, the consumption of inert gases and the maintenance of vacuum pumps. It would be desirable to have a process for manufacturing these parts in air and at normal pressure, without sacrificing the functional performance of the parts obtained.
  • inert gas typically nitrogen or argon
  • the problem is solved according to the present invention by confining the intermediate parts to be treated in a box, typically made of ceramic material, making it possible to isolate them from the atmosphere of the furnace.
  • the method according to the invention comprises (a) the preparation of a so-called “precursor mixture” comprising at least one ⁇ -SiC precursor with at least one carbonaceous resin, preferably thermosetting, (b) the shaping of said mixture precursor, in particular in granules, plates, tubes or bricks, to form an intermediate piece; (c) polymerizing the resin; (d) introducing said intermediate parts into a receptacle; (e) closing said receptacle by a closing means allowing a gas overpressure to escape; (f) the heat treatment of said intermediate parts at a temperature between 1100 and 1500 ° C to remove the organic constituents from the resin and form ⁇ -SiC in the final part.
  • ⁇ -SiC precursor is used here to mean a compound which forms under the conditions of the heat treatment (step (e)) with the constituents of the ⁇ -SiC resin.
  • precursor of ⁇ -SiC silicon is preferred, and more particularly in the form of a powder.
  • This silicon powder can be a commercial powder, of known particle size and purity.
  • the particle size of the silicon powder is preferably between 0.1 and 20 ⁇ m, preferably between 2 and 20 ⁇ m and more especially between 5 and 20 ⁇ m.
  • Said precursors can also be used in the form of grains or fibers.
  • carbon resin is used here to mean any resin containing carbon atoms. It is neither necessary nor useful for it to contain silicon atoms. It is advantageous that the silicon is provided only by the precursor of ⁇ -SiC.
  • the resin is advantageously selected from thermosetting resins containing carbon, and in particular from phenolic, acrylic or furfuryl resins. A phenolic type resin is preferred.
  • the respective amounts of resin and ⁇ -SiC precursor are adjusted so as to transform the ⁇ -SiC precursor quantitatively into ⁇ -SiC. To this end, the quantity of carbon contained in the resin is calculated.
  • Part of the carbon can also be provided by direct addition of a carbon powder into the mixture of carbon resin and the precursor of ⁇ -SiC.
  • This carbon powder can be a commercial powder, for example carbon black, of known particle size and purity. For reasons of homogeneity of the mixture, a particle size of less than 50 ⁇ m is preferred.
  • the choice of the composition of the mixture results from a compromise between the viscosity, the cost of the raw materials and the desired final porosity.
  • a slight excess of carbon is preferred in the precursor mixture. This excess carbon can then be burned in air. However, the excess carbon should not be too high so as not to generate too large a porosity inside the material after combustion of the residual carbon, thus inducing embrittlement in the mechanical strength of the final part.
  • the precursor mixture can be shaped by any known process such as molding, extrusion, rolling or pressing between at least two surfaces, to obtain three-dimensional shapes such as granules, tubes, bricks, plates, or tiles.
  • the method chosen will be adapted to the viscosity of the precursor mixture, itself a function of the viscosity of the resin and of the composition of the precursor mixture.
  • You can also make bricks with dimensions from a few centimeters to a few decimeters or more. Parts of more complex shapes can also be obtained, in particular by molding. To make bricks, pressing is preferred.
  • Said precursor mixture is then heated in air to a temperature between 100 ° C and 300 ° C, preferably between 150 ° C and 300 ° C, more preferably between 150 ° C and 250 ° C, and even more preferably between 150 ° C and 210 ° C.
  • the duration of this treatment, during which the polymerization of the resin takes place and the hardening of the part, is typically between 0.5 hours and 10 hours at the temperature level, preferably between 1 h and 5 h, and even more preferably between 2 and 3 hours.
  • the material gives off volatile organic compounds which create a variable residual porosity as a function of the level of carbon present in the composition of the precursor mixture and of the conditions applied during the polymerization.
  • An intermediate part is thus obtained which has a certain mechanical strength and which can therefore be easily handled.
  • Said intermediate piece thus obtained is introduced into a receptacle, as will be explained below, and heated to a temperature between 1100 ° C and 1500 ° C for a period ranging from 1 to 10 hours, preferably between 1 and 5 hours and especially between 1 and 3 hours.
  • the optimum temperature range is preferably between 1200 ° C and 1500 ° C, more especially between 1250 ° C and 1450 ° C.
  • the most preferred range is between 1250 ° C and 1400 ° C.
  • the SiC formed from the carbon originating from the resin and from the precursor of ⁇ -SiC is ⁇ -SiC.
  • the temperature of the parts gradually rises and causes the carbonaceous resin to decompose.
  • This decomposition is accompanied by the generation of volatile organic compounds which effectively expel the air initially present between the parts, and in their possible porosity.
  • the gassing that accompanies the decomposition of the carbonaceous resin is complete at around 800 ° C.
  • the essential step of the present invention is the introduction of the intermediate parts into a receptacle, which is then closed by a closure means allowing a gas overpressure to escape.
  • the receptacle is preferably made of inert ceramic material, for example refractory bricks.
  • said receptacle is filled in a fairly compact manner, while minimizing the unoccupied volume. If the load is too low, it can be supplemented by filling the volume of the receptacle which is not occupied by said intermediate parts to be treated with an inert solid, preferably easily separable and recoverable.
  • They can be, for example, bricks made of ⁇ -SiC or ⁇ -SiC, or grains of ⁇ -SiC.
  • the volume occupied by the gas inside the receptacle is not more than more than 50% to the external volume of the intermediate parts, preferably not more than 20% and even more preferably not more than 10%.
  • the term “external volume” is understood here to mean the volume calculated from the external dimensions of the intermediate parts to be treated, without taking into account their internal surface linked to the porosity. It is moreover preferable for the gas evolution generated by the intermediate parts between the ambient temperature and 800 ° C. to be at least equal to twice the volume occupied by the gas inside the receptacle, preferably at least five times, and even more preferably at least ten times.
  • volume occupied by the gas inside the receptacle means here the difference between the internal volume of the receptacle and the sum of the external volume of the intermediate parts to be treated and the volume of any inert solids added.
  • the receptacle must then be closed by an appropriate closing means, for example by a cover or plug of ceramic material.
  • an appropriate closing means for example by a cover or plug of ceramic material.
  • the Applicant has discovered that it is not only unnecessary for this closure to be waterproof, but even annoying. In fact, it is necessary for the closure means to escape the gas overpressure (carbon monoxide, volatile organic compounds, etc.) which forms during cooking. In most cases, and in particular when the edges of the receptacle and of the cover are of fairly flat and smooth shape, it is sufficient to simply place the cover visually tight on the opening of the receptacle. It is also possible to provide a sealed closure means provided with a valve.
  • the gas overpressure can escape, and at the same time, the ambient air does not appreciably access the products, or in any case not during cooking at high temperature.
  • the pressure inside the receptacle drops; the Applicant has found that it is no longer annoying that the air can access the products, since the temperature will be low enough for the ambient air
  • the method according to the invention allows the production of refractory bricks or plates based on ⁇ -SiC without binder, with a density greater than 1.5 g / cm and a thickness of at least 1 mm, preferably at least at least 3 mm, and even more preferably at least 5 mm.
  • the smallest section of said plates is advantageously at least 15 mm, and preferably at least 50 mm, with a ratio of length or width to thickness of at least 10 and preferably at least 15.
  • bricks are made.
  • the smallest dimension of said bricks is advantageously at least 10 mm, and preferably at least 50 mm or even 100 mm.
  • the smallest section of said bricks is advantageously at least 20 cm 2 , preferably at least 75 cm 2 and even more advantageously at least 150 cm 2 , with a ratio of length or width to thickness of at least 3
  • the density of the material can reach 2.8 g / cm 3 .
  • a density of at least 2.4 g / cm 3 is preferred.
  • the most preferred density for this use is between 2.45 and 2.75 g / cm 3 .
  • inclusions are added to the precursor mixture, at least part of which consists of ⁇ -SiC. In this case, step (a) indicated above is replaced by step (aa):
  • ⁇ -SiC ⁇ -SiC
  • ⁇ -SiC ⁇ -SiC
  • ⁇ -SiC with a variable particle size ranging from 0.01 to a few millimeters is used as inclusions.
  • a grain size of between a few tens of ⁇ m and 3 mm is suitable.
  • This silicon carbide can consist of any of the silicon carbides known to date.
  • Part of the ⁇ -SiC can be replaced by alumina, silica, TiN, Si 3 N 4 or other inorganic solids which do not decompose and do not sublimate at the synthesis temperature of the final composite.
  • the weight fraction of said inclusions can reach 80 and even 95% relative to the total mass of the precursor mixture.
  • the products are intended for use as a lining for molten salt electrolysis cells (for example for the production of aluminum from a molten mixture of alumina and cryolite), it is preferred that at least 50 % by weight of the inclusions, and preferably at least 70%, consist of ⁇ -SiC. The same applies to products intended for the lining of incineration furnaces.
  • the solid constituting the inclusions is not limited to a precise macroscopic form but can be used in different forms such as powder, grains, fibers.
  • the fibers based on ⁇ -SiC are preferred as inclusions. These fibers can have a length that exceeds 100 ⁇ m.
  • inclusions are mixed with a carbonaceous resin, preferably thermosetting, containing a given amount of a ⁇ -SiC precursor, preferably in the form of a powder with a particle size ranging from 0.1 to several micrometers.
  • a composite material of the ⁇ -SiC / ⁇ -SiC type is thus obtained, comprising particles of ⁇ -SiC in a matrix of ⁇ -SiC, which does not need to contain other binders or additives.
  • the additional infiltration treatment can be carried out according to the same procedure described: soaking of said material in a mold containing the resin, polymerization then finally, carburetion treatment.
  • Said resin must contain a sufficient amount of the ⁇ -SiC precursor, for example in the form of silicon powder.
  • pure and porous ⁇ -SiC is obtained, which can be used as a catalyst support or as a catalyst.
  • the carbon and the silicon are intimately mixed in the following manner: the silicon powder (average grain size of approximately 10 ⁇ m), is mixed with a phenolic resin which, after polymerization, provides the carbon source necessary for the ⁇ -SiC formation reaction. The inclusions are then mixed with the resin and the whole is poured into a mold having the shape of the desired final composite. After polymerization, the solid formed is transferred to a receptacle placed in an oven allowing the final carburetion of the matrix to be carried out. If the receptacle is not full, you can add inert material, for example refractory bricks of the same type already cooked. The receptacle is closed by a closing means such as a cover or a plug made of ceramic material.
  • a closing means such as a cover or a plug made of ceramic material.
  • the method according to the present invention makes it possible to produce materials or composites with a matrix based on ⁇ -SiC which may contain inside inclusions based on silicon carbide or other materials resistant to use in aggressive, highly acidic or basic, and under strong temperature constraints.
  • the advantages which flow from the present invention are numerous compared to the methods of the prior art, and include in particular the following: (i) The material according to the invention can be manufactured with a significantly lower cost price compared to the methods known. This is due to three factors: First, the low cost and the limited number of raw materials (resin constituting the carbon source, silicon powder).
  • the process according to the invention can be carried out at relatively low temperatures, ie ⁇ 1400 ° C., compared to those used in the prior art.
  • the method according to the invention avoids the additional investment and operating costs associated with the management of the vacuum or inert gases, the consumption of inert gases and the maintenance of the vacuum pumps.
  • the shaping of the mixture can be carried out preferably before the polymerization by extrusion, by pressing or by molding. It is easy taking into account the nature of the starting material, namely a viscous matrix based on resin and silicon powder, which can contain dispersed ⁇ -SiC powder.
  • the part can be shaped by machining after polymerization of the resin, preferably before the heat treatment (step (d)).
  • step (d) the part can be shaped by machining after polymerization of the resin, preferably before the heat treatment.
  • the material or composite according to the invention has an extremely high resistance to corrosive media, in particular to fluorinated media, to concentrated acids or to alkaline media.
  • the parts made from this new material or composite according to the invention therefore allow better economy of use. More particularly, in a given aggressive medium, the lifetime of the parts according to the invention is greater than that of the known SiC-based parts. This also improves the safety of use of the SiC parts, in particular their sealing, and opens other applications impossible to envisage with SiC-based materials according to the state of the art whose binders are not chemically inert. (v) By varying the chemical and physical nature of the inclusions, the process according to the present invention also makes it possible to prepare other types of composite containing not only only silicon carbide but other materials such as alumina, silica or any other compound, provided that they can be dispersed in the resin and that they are not altered during synthesis.
  • this ceramic material has many applications. It can be used, in particular in the form of refractory plates or bricks, as a coating material in various applications relating to thermal engineering, chemical engineering and / or electrometallurgical engineering which must respond to high mechanical and thermal stresses, and / or in the presence corrosive liquids or gases.
  • the material according to the invention can be used as an interior lining for ovens, such as aluminum smelting ovens, and as a lining for salt electrolysis cells. molten, for example for the production of aluminum by electrolysis from a mixture of alumina and cryolite.
  • the method according to the invention also allows the manufacture of parts of complex shape, in particular by molding, and of tubes, in particular by extrusion, as well as of granules.
  • a homogeneous paste is produced by mixing 49% of fine powder of metallic silicon, 18% of carbon black and 33% of phenolic resin. This paste is formed into granules of 3mm in diameter by extrusion, then heated in air for 3 hours at 200 ° C in order to harden the resin. Precursor granules are then obtained which can be transformed into SiC by heating under suitable conditions.
  • Example No. 2 15 cm 3 (16.3 g) of precursor extrudates prepared according to Example No. 1 are loaded into an alumina cartridge of 23 cm 3 . 16 g of ⁇ -SiC powder with a particle size of less than 200 ⁇ m are added thereto, then the assembly is subjected to vibrations so that the powder comes to fill the space left free between the extrudates. The cartridge is then closed with a ceramic felt packed to a thickness of 1 cm. The cartridge is then heated for 1 hour at 1400 ° C in a tabular oven through which a continuous stream of argon is passed. After treatment, the cartridge is emptied and the extrudates are separated from the ⁇ -SiC powder by sieving. Analysis by X-ray diffraction shows that the precursor granules have been transformed into ⁇ -SiC.
  • ⁇ -SiC granules are immersed in a 40% HF solution - vol. for 24 hours, then are rinsed with water and dried.
  • the treatment of the granules with HF leads to a loss of mass of approximately 6% without any incidence on the morphology of the grains.
  • Example 2 The test of Example 2 is repeated, except for the heating of the cartridge for 1 hour at 1400 ° C. which is carried out in an oven containing air in place of argon.
  • Comparative Example No. 1 15 cm 3 of precursor extracts prepared according to Example No. 1 are placed in an oven and then treated for 1 hour at 1400 ° C. in the open air. After treatment in the oven, the granules are immersed in the HF solution at 40% vol. for 24 hours. This HF treatment leads to a drastic transformation of the morphology of the granules which have dissolved almost entirely in the HF solution, a non-quantifiable solid residue being observed in the form of powder at the bottom of the HF tank.
  • Example No. 4 A binder is prepared by mixing 55% of phenolic resin and 45% of fine powder of metallic silicon. This binder is then used in admixture with ⁇ -SiC grains in respective proportions of 12% and 88%. The mixture thus formed is then pressed to form a brick which is hardened by heating for 3 hours at 150 ° C in air. At this stage, the brick consists of grains of ⁇ -SiC trapped in a precursor matrix which can be transformed into ⁇ -SiC by heating under suitable conditions.
  • Example 5 A binder is prepared by mixing 55% of phenolic resin and 45% of fine powder of metallic silicon. This binder is then used in admixture with ⁇ -SiC grains in respective proportions of 12% and 88%. The mixture thus formed is then pressed to form a brick which is hardened by heating for 3 hours at 150 ° C in air. At this stage, the brick consists of grains of ⁇ -SiC trapped in a precursor matrix which can be transformed into ⁇ -SiC by heating under suitable
  • a brick prepared according to Example 4 is treated for 1 hour at 1360 ° C in an inert oven by continuous scanning of argon. On leaving the oven, the brick exhibits good mechanical strength which is preserved after a stay of 24 hours in a hydrofluoric acid bath at 40% by volume. The mass loss during this HF treatment is less than 1%.
  • X-ray diffraction analysis also shows the presence of ⁇ -SiC which has formed from the binder and makes it possible to maintain the cohesion between the grains of ⁇ -SiC.
  • a brick prepared according to example n ° 4 is placed in a ceramic box covered with a cover and adjusted to the size of the room. The whole is then treated for 5 hours at 1380 ° C. in an oven swept by an oxidizing atmosphere. On leaving the oven, the brick exhibits good mechanical strength which is preserved after a stay of 24 hours in a hydrofluoric acid bath at 40% by volume. The loss of mass during this treatment with HF is of the order of 1.5%.
  • Comparative example n ° 2 A brick prepared according to example n ° 4 is treated directly for 5 hours at 1380 ° C in an oven swept by an oxidizing atmosphere, without confinement in a ceramic box. At the exit of the oven, the brick has good mechanical strength but it is completely reduced in grains after a stay of only 2 hours in a hydrofluoric acid bath at 40% by volume. Contrary to Examples 5 and 6, the cohesion between the grains of ⁇ -SiC is no longer ensured after treatment in HF medium because the precursor of ⁇ -SiC could not be correctly transformed by binding ⁇ -SiC during cooking at high temperature.

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Ceramic Engineering (AREA)
  • Materials Engineering (AREA)
  • Organic Chemistry (AREA)
  • Manufacturing & Machinery (AREA)
  • Structural Engineering (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Electrochemistry (AREA)
  • Metallurgy (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Ceramic Products (AREA)
  • Carbon And Carbon Compounds (AREA)
  • Compositions Of Oxide Ceramics (AREA)
EP05770958A 2004-05-14 2005-05-10 Verfahren zur herstellung von rohteilen auf beta-sic-basis zur verwendung für aggressive medien Withdrawn EP1751077A2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0405284A FR2870233B1 (fr) 2004-05-14 2004-05-14 PROCEDE DE FABRICATION DE PIECES DE FORME A BASE DE BETA-SiC POUR UTILISATION DANS DES MILIEUX AGRESSIFS
PCT/FR2005/001163 WO2005121044A2 (fr) 2004-05-14 2005-05-10 PROCEDE DE FABRICATION DE PIECES DE FORME A BASE DE β-SIC POUR UTILISATION DANS DES MILIEUX AGRESSIFS

Publications (1)

Publication Number Publication Date
EP1751077A2 true EP1751077A2 (de) 2007-02-14

Family

ID=34945902

Family Applications (1)

Application Number Title Priority Date Filing Date
EP05770958A Withdrawn EP1751077A2 (de) 2004-05-14 2005-05-10 Verfahren zur herstellung von rohteilen auf beta-sic-basis zur verwendung für aggressive medien

Country Status (8)

Country Link
US (1) US20080095692A1 (de)
EP (1) EP1751077A2 (de)
CN (1) CN100579934C (de)
AU (1) AU2005251983B2 (de)
CA (1) CA2566869A1 (de)
FR (1) FR2870233B1 (de)
RU (1) RU2375331C2 (de)
WO (1) WO2005121044A2 (de)

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BR0109283A (pt) 2000-03-14 2002-12-17 James Hardie Res Pty Ltd Materiais para construção de cimento com fibra contendo aditivos de baixa densidade
JP4490816B2 (ja) * 2002-08-23 2010-06-30 ジェームズ ハーディー インターナショナル ファイナンス ベスローテン フェンノートシャップ 合成中空小球体
MXPA05003691A (es) 2002-10-07 2005-11-17 James Hardie Int Finance Bv Material mixto de fibrocemento de densidad media durable.
US20090146108A1 (en) * 2003-08-25 2009-06-11 Amlan Datta Methods and Formulations for Producing Low Density Products
US20090156385A1 (en) * 2003-10-29 2009-06-18 Giang Biscan Manufacture and use of engineered carbide and nitride composites
TW200538610A (en) 2004-01-12 2005-12-01 James Hardie Int Finance Bv Composite fiber cement article with radiation curable component
US7998571B2 (en) * 2004-07-09 2011-08-16 James Hardie Technology Limited Composite cement article incorporating a powder coating and methods of making same
EP1856003A2 (de) 2005-02-24 2007-11-21 James Hardie International Finance B.V. Alkaliresistente glaszusammensetzungen
US8609244B2 (en) * 2005-12-08 2013-12-17 James Hardie Technology Limited Engineered low-density heterogeneous microparticles and methods and formulations for producing the microparticles
US8993462B2 (en) 2006-04-12 2015-03-31 James Hardie Technology Limited Surface sealed reinforced building element
CN101580390B (zh) * 2008-05-15 2012-10-03 中国科学院金属研究所 一种碳化硅陶瓷管状制品的制备方法
WO2010101572A1 (en) * 2009-03-05 2010-09-10 James Hardie Technology Limited Manufacture and use of engineered carbide and nitride composites
CN102368397B (zh) * 2011-06-16 2013-01-16 哈尔滨工业大学 一种耐冰晶石腐蚀的绝缘材料及其制备方法和应用
RU2559965C1 (ru) * 2014-05-07 2015-08-20 Акционерное общество "Научно-исследовательский институт конструкционных материалов на основе графита "НИИграфит" Композиция тонкостенных трубчатых элементов и способ получения тонкостенных трубчатых элементов
CN111285385A (zh) * 2020-02-18 2020-06-16 大同碳谷科技孵化器有限公司 一种从煤矸石灰渣中提取三氧化二铝和二氧化硅的方法

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4744922A (en) * 1986-07-10 1988-05-17 Advanced Refractory Technologies, Inc. Neutron-absorbing material and method of making same
DE68901429D1 (de) * 1988-08-15 1992-06-11 Shinetsu Chemical Co Verbindungsmittelzusammensetzungen fuer siliciumcarbidkeramiken.
FR2675713B1 (fr) * 1991-04-29 1993-07-02 Pechiney Electrometallurgie Systeme catalytique, notamment pour la postcombustion de gaz d'echappement et procede pour le fabriquer.
DE4413127C1 (de) * 1994-04-19 1995-10-05 Forschungszentrum Juelich Gmbh Verfahren zur Herstellung poröser, durchströmbarer Formkörper aus Siliciumcarbid und Formkörper
DE4420294C2 (de) * 1994-06-10 1998-04-09 Didier Werke Ag Abfallverbrennungsofen
US5560809A (en) * 1995-05-26 1996-10-01 Saint-Gobain/Norton Industrial Ceramics Corporation Improved lining for aluminum production furnace
US6555031B2 (en) * 2000-06-19 2003-04-29 Corning Incorporated Process for producing silicon carbide bodies
FR2857009A1 (fr) * 2003-04-16 2005-01-07 Sicat Materiau ceramique a base de carbure de silicium pour utilisation dans des milieux agressifs
FR2857008B1 (fr) * 2003-04-16 2006-05-19 Sicat Materiau ceramique a base de carbure de silicium pour utilisation dans des milieux agressifs

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See references of WO2005121044A2 *

Also Published As

Publication number Publication date
CA2566869A1 (fr) 2005-12-22
WO2005121044A3 (fr) 2006-06-08
WO2005121044A2 (fr) 2005-12-22
CN100579934C (zh) 2010-01-13
RU2006144450A (ru) 2008-06-20
RU2375331C2 (ru) 2009-12-10
AU2005251983B2 (en) 2010-04-08
WO2005121044A8 (fr) 2006-12-28
AU2005251983A1 (en) 2005-12-22
FR2870233B1 (fr) 2006-12-01
FR2870233A1 (fr) 2005-11-18
US20080095692A1 (en) 2008-04-24
CN1980871A (zh) 2007-06-13

Similar Documents

Publication Publication Date Title
EP1751077A2 (de) Verfahren zur herstellung von rohteilen auf beta-sic-basis zur verwendung für aggressive medien
EP0023869B1 (de) Verfahren zur Herstellung von Sialons
LU87550A1 (fr) Procede de formation d'une masse refractaire sur une surface et melange de particules destine a ce procede
FR2657603A1 (fr) Procede d'obtention de corps solides poreux a base de carbure refractaire a l'aide de composes organiques et de metal ou metallouide.
FR2528823A1 (fr) Procede de fabrication d'articles en carbone ou en graphite contenant du carbure de silicium lie par reaction
CH625195A5 (de)
EP1828077A2 (de) Gesinterter feuerfester block auf basis von siliciumcarbid mit einer siliciumnitridbindung
JPH0774108B2 (ja) 炭素存在下での反応によって結合したケイ素粉末を主成分とするセラミック材料およびその製造方法
FR3074171A1 (fr) Materiau ceramique composite particulaire, piece le comprenant, et procede de preparation de cette piece.
FR2669920A1 (fr) Procede de fabrication de materiaux refractaires et leurs applications en fonderie d'alliages corrosifs.
EP1888813B1 (de) Verfahren zur schnellen verdichtung eines porösen fasersubstrats mit bildung einer festen ablage innerhalb der substratporosität
EP0807093B1 (de) Zusammensetzung für eine beschichtung von kohlenstoffenthaltenden produkten und solche beschichtung
WO1984002335A1 (fr) Produits refractaires constitues de grains lies par des residus carbones et du silicium metal en poudre, et procede de fabrication
EP1618079B1 (de) Verwendung eines auf siliciumcarbid basierenden keramikwerkstoffs in aggressiven umgebungen
EP0577735B1 (de) Mischung von chemischen substanzen zur herstellung einer feuerfesten zusammensetzung, verfahren zur herstellung dieser zusammensetzung und verfahren zur ihrer anwendung
BE1006501A4 (fr) Procede pour la fabrication de briques siliceuses de masse volumique apparente elevee.
BE1017675A3 (fr) Melange sec pour le traitement de substrats refractaires et procede le mettant en oeuvre.
FR2857008A1 (fr) Materiau ceramique a base de carbure de silicium pour utilisation dans des milieux agressifs
EP2340408A1 (de) Ofen zur verbrennung von kohlenstoffblöcken
EP1756019B1 (de) Basiszusammensetzung zur herstellung refraktärer formprodukte auf sic-basis und herstellungsverfahren dafür
BE516951A (de)
BE664911A (de)
BE400083A (de)
FR2569577A1 (fr) Bloc de catalyseur en grains, aux oxydes de fer, a activite renforcee, pour la synthese de l'ammoniac, et procede de preparation dudit bloc de catalyseur

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

17P Request for examination filed

Effective date: 20061214

AK Designated contracting states

Kind code of ref document: A2

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IS IT LI LT LU MC NL PL PT RO SE SI SK TR

AX Request for extension of the european patent

Extension state: AL BA HR LV MK YU

DAX Request for extension of the european patent (deleted)
17Q First examination report despatched

Effective date: 20071123

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE APPLICATION IS DEEMED TO BE WITHDRAWN

18D Application deemed to be withdrawn

Effective date: 20101201