FR2378888A1 - Composite carbone-carbone - Google Patents
Composite carbone-carboneInfo
- Publication number
- FR2378888A1 FR2378888A1 FR7715379A FR7715379A FR2378888A1 FR 2378888 A1 FR2378888 A1 FR 2378888A1 FR 7715379 A FR7715379 A FR 7715379A FR 7715379 A FR7715379 A FR 7715379A FR 2378888 A1 FR2378888 A1 FR 2378888A1
- Authority
- FR
- France
- Prior art keywords
- carbon
- fibres
- cable
- brake discs
- esp
- 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- Withdrawn
Links
- 239000002131 composite material Substances 0.000 title abstract 3
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 title abstract 2
- 229910052799 carbon Inorganic materials 0.000 title abstract 2
- CREMABGTGYGIQB-UHFFFAOYSA-N carbon carbon Chemical compound C.C CREMABGTGYGIQB-UHFFFAOYSA-N 0.000 title abstract 2
- 239000011203 carbon fibre reinforced carbon Substances 0.000 title abstract 2
- 229920002239 polyacrylonitrile Polymers 0.000 title abstract 2
- 239000002243 precursor Substances 0.000 abstract 2
- 230000015572 biosynthetic process Effects 0.000 abstract 1
- 230000001427 coherent effect Effects 0.000 abstract 1
- 239000000835 fiber Substances 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
- B32B5/22—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed
- B32B5/24—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer
- B32B5/26—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer another layer next to it also being fibrous or filamentary
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B9/00—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B18/00—Layered products essentially comprising ceramics, e.g. refractory products
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
- B32B5/02—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer
- B32B5/06—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer characterised by a fibrous or filamentary layer mechanically connected, e.g. by needling to another layer, e.g. of fibres, of paper
-
- 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
- C04B35/83—Carbon fibres in a carbon matrix
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16D—COUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
- F16D69/00—Friction linings; Attachment thereof; Selection of coacting friction substances or surfaces
- F16D69/02—Composition of linings ; Methods of manufacturing
- F16D69/023—Composite materials containing carbon and carbon fibres or fibres made of carbonizable material
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
- B32B2262/10—Inorganic fibres
- B32B2262/106—Carbon fibres, e.g. graphite fibres
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2307/00—Properties of the layers or laminate
- B32B2307/30—Properties of the layers or laminate having particular thermal properties
- B32B2307/302—Conductive
-
- 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
- C04B2237/00—Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
- C04B2237/30—Composition of layers of ceramic laminates or of ceramic or metallic articles to be joined by heating, e.g. Si substrates
- C04B2237/32—Ceramic
- C04B2237/36—Non-oxidic
- C04B2237/363—Carbon
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Ceramic Engineering (AREA)
- Composite Materials (AREA)
- Materials Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Manufacturing & Machinery (AREA)
- Structural Engineering (AREA)
- Organic Chemistry (AREA)
- Ceramic Products (AREA)
- Braking Arrangements (AREA)
- Inorganic Fibers (AREA)
- Nonwoven Fabrics (AREA)
Abstract
Composite carbone-carbone. Il est obtenu par infiltration de carbone dans un corps de fibres constitué en empilant successivement des longueurs d'un arrangement d'une multiplicité de fibres alignées pratiquement parallèlement les unes aux autres, ces fibres étant des fibres de carbone ou d'un précurseur de fibres de carbone.
Applications Claiming Priority (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2053576 | 1976-05-18 | ||
GB2053476 | 1976-05-18 | ||
GB2640676 | 1976-06-24 | ||
GB2640576 | 1976-06-24 |
Publications (1)
Publication Number | Publication Date |
---|---|
FR2378888A1 true FR2378888A1 (fr) | 1978-08-25 |
Family
ID=27448498
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR7715379A Withdrawn FR2378888A1 (fr) | 1976-05-18 | 1977-05-18 | Composite carbone-carbone |
Country Status (3)
Country | Link |
---|---|
JP (1) | JPS534011A (fr) |
DE (1) | DE2722575A1 (fr) |
FR (1) | FR2378888A1 (fr) |
Cited By (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2434964A1 (fr) * | 1978-08-29 | 1980-03-28 | Kulakov Valery | Procede d'obtention d'une piece de friction |
EP0029851A1 (fr) * | 1979-06-11 | 1981-06-10 | Goodrich Co B F | Methode de fabrication d'un article composite de carbone. |
FR2506672A1 (fr) * | 1981-06-02 | 1982-12-03 | Lorraine Carbone | Procede de fabrication de disques de frottement |
FR2584107A1 (fr) * | 1985-06-27 | 1987-01-02 | Europ Propulsion | Procede de fabrication de structures de revolution tridimensionnelles par aiguilletage de couches de materiau fibreux et materiau utilise pour la mise en oeuvre du procede |
US4790052A (en) * | 1983-12-28 | 1988-12-13 | Societe Europeenne De Propulsion | Process for manufacturing homogeneously needled three-dimensional structures of fibrous material |
US5323523A (en) * | 1986-01-28 | 1994-06-28 | Aerospace Preforms Limited | Production of shaped filamentary structures |
US5388320A (en) * | 1987-01-27 | 1995-02-14 | Aerospace Preforms Limited | Production of shaped filamentary structures |
US5705264A (en) * | 1987-01-27 | 1998-01-06 | Aerpspace Preforms Limited | Production of shaped filamentary structures |
FR2759387A1 (fr) * | 1997-02-12 | 1998-08-14 | Carbone Ind | Realisation de preforme fibreuse annulaire par enroulement de ruban |
US5882781A (en) * | 1986-01-28 | 1999-03-16 | Aerospace Preforms Limited | Shaped fibrous fabric structure comprising multiple layers of fibrous material |
CN106365666A (zh) * | 2015-07-20 | 2017-02-01 | 上海航天设备制造总厂 | 导弹固体火箭发动机碳/碳复合材料隐身二元喷管制造方法 |
Families Citing this family (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS59174510A (ja) * | 1983-03-25 | 1984-10-03 | Mitsubishi Pencil Co Ltd | 炭素成形品の製造方法 |
JPS6042213A (ja) * | 1983-08-19 | 1985-03-06 | Showa Denko Kk | 炭素薄板の製造法 |
JPS60155516A (ja) * | 1983-12-27 | 1985-08-15 | Showa Denko Kk | 炭素薄板の製造法 |
US4776995A (en) * | 1985-03-22 | 1988-10-11 | Fiber Materials, Inc. | Method of making a structure |
US4776994A (en) * | 1985-03-22 | 1988-10-11 | Fiber Materials, Inc. | Method of making a structure from carbonaceous fibers |
FR2659949B1 (fr) * | 1990-03-26 | 1992-12-04 | Europ Propulsion | Procede de conformation d'une texture fibreuse de renfort pour la fabrication d'une piece en materiau composite. |
US5205888A (en) * | 1990-07-03 | 1993-04-27 | Mitsubishi Gas Chemical Company, Inc. | Process for producing carbon fiber reinforced carbon materials |
FR2664889B1 (fr) * | 1990-07-17 | 1992-09-25 | Lorraine Carbone | Support poreux de membrane filtrante en composite carbone-carbone a substrat en mat de fibres de carbone et son procede de fabrication. |
FR2671735B1 (fr) * | 1991-01-18 | 1994-04-08 | Pechiney Recherche | Procede de fabrication de tubes poreux, de permeabilite elevee, en materiau composite carbone-carbone et leurs applications. |
EP0554024B1 (fr) * | 1992-01-24 | 1997-07-02 | NIPPON OIL Co. Ltd. | Procédé de fabrication de préforme de composite carbone-carbone et composite carbone-carbone |
FR2729726B1 (fr) * | 1995-01-23 | 1997-04-18 | Antonov Automotive Europ | Embrayage multi-disques, transmission automatique ainsi equipee et procede de realisation |
FR2767365A1 (fr) * | 1997-08-18 | 1999-02-19 | Antonov Automotive Europ | Procede pour fabriquer un disque de friction en carbone, disque et dispositif de friction s'y rapportant |
IT1276483B1 (it) * | 1995-07-07 | 1997-10-31 | Fiat Auto Spa | Procedimento di fabbricazione di un prodotto composito sinterizzato e di un prodotto internedio composito sinterizzabile |
CN1119522C (zh) * | 1998-08-19 | 2003-08-27 | 阿利安特技术系统公司 | 由作为母体的短纤维素纤维制成的火箭组件的烧蚀材料及采用这种材料绝热和热保护火箭组件的方法 |
US6479148B1 (en) | 1998-08-19 | 2002-11-12 | Cordant Technologies Inc. | Rocket assembly ablative materials formed from solvent-spun cellulosic precursors, and method of insulating or thermally protecting a rocket assembly with the same |
-
1977
- 1977-05-18 FR FR7715379A patent/FR2378888A1/fr not_active Withdrawn
- 1977-05-18 JP JP5654277A patent/JPS534011A/ja active Pending
- 1977-05-18 DE DE19772722575 patent/DE2722575A1/de active Pending
Cited By (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2434964A1 (fr) * | 1978-08-29 | 1980-03-28 | Kulakov Valery | Procede d'obtention d'une piece de friction |
EP0029851A1 (fr) * | 1979-06-11 | 1981-06-10 | Goodrich Co B F | Methode de fabrication d'un article composite de carbone. |
EP0029851A4 (fr) * | 1979-06-11 | 1981-10-27 | Goodrich Co B F | Methode de fabrication d'un article composite de carbone. |
FR2506672A1 (fr) * | 1981-06-02 | 1982-12-03 | Lorraine Carbone | Procede de fabrication de disques de frottement |
US4790052A (en) * | 1983-12-28 | 1988-12-13 | Societe Europeenne De Propulsion | Process for manufacturing homogeneously needled three-dimensional structures of fibrous material |
FR2584107A1 (fr) * | 1985-06-27 | 1987-01-02 | Europ Propulsion | Procede de fabrication de structures de revolution tridimensionnelles par aiguilletage de couches de materiau fibreux et materiau utilise pour la mise en oeuvre du procede |
DE3620833A1 (de) * | 1985-06-27 | 1987-01-08 | Europ Propulsion | Verfahren zum herstellen dreidimensionaler rotationsstrukturen durch vernadelung von lagen aus fasermaterial und material zur durchfuehrung des verfahrens |
US5882781A (en) * | 1986-01-28 | 1999-03-16 | Aerospace Preforms Limited | Shaped fibrous fabric structure comprising multiple layers of fibrous material |
US5323523A (en) * | 1986-01-28 | 1994-06-28 | Aerospace Preforms Limited | Production of shaped filamentary structures |
US6174594B1 (en) | 1986-01-28 | 2001-01-16 | Aerospace Preforms Limited | Shaped filamentary structures |
US5388320A (en) * | 1987-01-27 | 1995-02-14 | Aerospace Preforms Limited | Production of shaped filamentary structures |
US5737821A (en) * | 1987-01-27 | 1998-04-14 | Aerospace Preforms Limited | Production of shaped filamentary structures |
US5705264A (en) * | 1987-01-27 | 1998-01-06 | Aerpspace Preforms Limited | Production of shaped filamentary structures |
FR2759387A1 (fr) * | 1997-02-12 | 1998-08-14 | Carbone Ind | Realisation de preforme fibreuse annulaire par enroulement de ruban |
WO1998036187A1 (fr) * | 1997-02-12 | 1998-08-20 | Messier-Bugatti | Realisation de preforme fibreuse annulaire par enroulement de ruban |
CN106365666A (zh) * | 2015-07-20 | 2017-02-01 | 上海航天设备制造总厂 | 导弹固体火箭发动机碳/碳复合材料隐身二元喷管制造方法 |
Also Published As
Publication number | Publication date |
---|---|
DE2722575A1 (de) | 1977-12-22 |
JPS534011A (en) | 1978-01-14 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |