WO2005037726A3 - Procede permettant de pratiquer des cavites dans des corps composites metal-ceramique - Google Patents

Procede permettant de pratiquer des cavites dans des corps composites metal-ceramique Download PDF

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Publication number
WO2005037726A3
WO2005037726A3 PCT/US2004/034112 US2004034112W WO2005037726A3 WO 2005037726 A3 WO2005037726 A3 WO 2005037726A3 US 2004034112 W US2004034112 W US 2004034112W WO 2005037726 A3 WO2005037726 A3 WO 2005037726A3
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cavity
infiltratable
metal
walls
ceramic
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Ceased
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PCT/US2004/034112
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WO2005037726A2 (fr
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Prashant G Karandikar
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M Cubed Technologies Inc
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M Cubed Technologies Inc
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Publication of WO2005037726A2 publication Critical patent/WO2005037726A2/fr
Publication of WO2005037726A3 publication Critical patent/WO2005037726A3/fr
Anticipated expiration legal-status Critical
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    • 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
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    • 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
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    • 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
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    • 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
    • C04B35/63Preparing or treating the powders individually or as batches ; preparing or treating macroscopic reinforcing agents for ceramic products, e.g. fibres; mechanical aspects section B using additives specially adapted for forming the products, e.g.. binder binders
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    • C04B37/00Joining burned ceramic articles with other burned ceramic articles or other articles by heating
    • C04B37/003Joining burned ceramic articles with other burned ceramic articles or other articles by heating by means of an interlayer consisting of a combination of materials selected from glass, or ceramic material with metals, metal oxides or metal salts
    • C04B37/006Joining burned ceramic articles with other burned ceramic articles or other articles by heating by means of an interlayer consisting of a combination of materials selected from glass, or ceramic material with metals, metal oxides or metal salts consisting of metals or metal salts
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    • C04B37/00Joining burned ceramic articles with other burned ceramic articles or other articles by heating
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    • 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
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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Ceramic Engineering (AREA)
  • Manufacturing & Machinery (AREA)
  • Materials Engineering (AREA)
  • Structural Engineering (AREA)
  • Organic Chemistry (AREA)
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  • Chemical Kinetics & Catalysis (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Ceramic Products (AREA)

Abstract

La présente invention concerne une structure composite métal-céramique présentant une cavité ou toute autre structure creuse à l'intérieur. La cavité n'est ni découpée, ni usinée dans la structure finale, mais elle est formée au cours du processus d'infiltration. Dans le système présentant des matériaux composites Si/SiC en particulier, une préforme est utilisée, laquelle présente ladite cavité souhaitée, ou encore, plusieurs préformes de sous-unités sont reliées ensemble de manière à former ou à définir ladite cavité. Un matériau essentiellement impénétrable par le matériau infiltrant fondu est mis en contact avec la quasi totalité des surfaces intérieures, par exemple, les parois, de la cavité. La mise en contact peut consister essentiellement en un enrobage des parois, ou elle peut consister en un remplissage substantiel de la cavité avec le matériau impénétrable, ou un matériau similaire. De préférence, le matériau impénétrable se présente sous une forme permettant un retrait rapide après le traitement, telle qu'une masse de matière particulaire collée de manière lâche. La préforme ou l'assemblage de sous-unités peuvent ensuite être imprégnés normalement par le matériau infiltrant fondu. Le matériau infiltrant ne s'infiltre pas dans la cavité, il est localement stoppé par le matériau impénétrable sur les parois de la cavité. Après solidification du matériau infiltrant pour former un corps RBSC, le matériau impénétrable est rapidement retiré, par exemple, par jets d'air ou d'eau, par agitation, application d'un vide d'air, etc. En outre, un ou plusieurs orifices d'accès provisoires à la cavité peuvent être usinés dans la structure composite, par exemple, pour permettre un accès supplémentaire à un moyen à jet de pression ou à un moyen de vide; ces orifices d'accès sont rebouchés après retrait du matériau impénétrable.
PCT/US2004/034112 2003-10-14 2004-10-14 Procede permettant de pratiquer des cavites dans des corps composites metal-ceramique Ceased WO2005037726A2 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US51157203P 2003-10-14 2003-10-14
US60/511,572 2003-10-14

Publications (2)

Publication Number Publication Date
WO2005037726A2 WO2005037726A2 (fr) 2005-04-28
WO2005037726A3 true WO2005037726A3 (fr) 2005-10-06

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PCT/US2004/034112 Ceased WO2005037726A2 (fr) 2003-10-14 2004-10-14 Procede permettant de pratiquer des cavites dans des corps composites metal-ceramique

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Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2021067459A1 (fr) 2019-09-30 2021-04-08 Corning Incorporated Fabrication de modules de réacteur à écoulement et modules produits
CN112340105A (zh) * 2020-12-07 2021-02-09 珠海晨新科技有限公司 一种盲孔自动贴膜装置
CN113909456B (zh) * 2021-09-14 2023-04-25 昆明理工大学 一种稀土掺杂颗粒增强钢铁基复合材料的制备方法
WO2023051905A1 (fr) 2021-09-29 2023-04-06 Schunk Ingenieurkeramik Gmbh Composant produit à l'aide d'un procédé d'infiltration, dispositif comprenant ledit composant et procédé d'infiltration pour la production d'un composant
FR3158963A1 (fr) * 2024-02-02 2025-08-08 Safran Ceramics Procédé de fabrication d'une pièce en CMC
EP4610240A1 (fr) 2024-02-28 2025-09-03 CeramTec GmbH Pâte broyable pour l'obtention de structures de cavité dans un composant céramique et procédé d'obtention desdites structures de cavité dans des composants céramiques

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3857744A (en) * 1970-01-19 1974-12-31 Coors Porcelain Co Method for manufacturing composite articles containing boron carbide
US5267601A (en) * 1988-11-10 1993-12-07 Lanxide Technology Company, Lp Method for forming a metal matrix composite body by an outside-in spontaneous infiltration process, and products produced thereby
US5666269A (en) * 1994-01-03 1997-09-09 Motorola, Inc. Metal matrix composite power dissipation apparatus
US5839329A (en) * 1994-03-16 1998-11-24 Baker Hughes Incorporated Method for infiltrating preformed components and component assemblies

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3857744A (en) * 1970-01-19 1974-12-31 Coors Porcelain Co Method for manufacturing composite articles containing boron carbide
US5267601A (en) * 1988-11-10 1993-12-07 Lanxide Technology Company, Lp Method for forming a metal matrix composite body by an outside-in spontaneous infiltration process, and products produced thereby
US5666269A (en) * 1994-01-03 1997-09-09 Motorola, Inc. Metal matrix composite power dissipation apparatus
US5839329A (en) * 1994-03-16 1998-11-24 Baker Hughes Incorporated Method for infiltrating preformed components and component assemblies

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