GB1549687A - Production of carbon fibre reinforced carbon composite materials - Google Patents

Production of carbon fibre reinforced carbon composite materials

Info

Publication number
GB1549687A
GB1549687A GB29855/76A GB2985576A GB1549687A GB 1549687 A GB1549687 A GB 1549687A GB 29855/76 A GB29855/76 A GB 29855/76A GB 2985576 A GB2985576 A GB 2985576A GB 1549687 A GB1549687 A GB 1549687A
Authority
GB
United Kingdom
Prior art keywords
production
composite materials
fibre reinforced
carbon
carbon composite
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.)
Expired
Application number
GB29855/76A
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.)
Dunlop Ltd
Original Assignee
Dunlop 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
Application filed by Dunlop Ltd filed Critical Dunlop Ltd
Priority to GB29855/76A priority Critical patent/GB1549687A/en
Publication of GB1549687A publication Critical patent/GB1549687A/en
Expired legal-status Critical Current

Links

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
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/06—Fibrous reinforcements only
    • B29C70/10—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres
    • B29C70/16—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length
    • B29C70/24—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in at least three directions forming a three dimensional structure
    • 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
    • B32B3/00—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar form; Layered products having particular features of form
    • B32B3/26—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar form; Layered products having particular features of form characterised by a particular shape of the outline of the cross-section of a continuous layer; characterised by a layer with cavities or internal voids ; characterised by an apertured layer
    • B32B3/266—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar form; Layered products having particular features of form characterised by a particular shape of the outline of the cross-section of a continuous layer; characterised by a layer with cavities or internal voids ; characterised by an apertured layer characterised by an apertured layer, the apertures going through the whole thickness of the layer, e.g. expanded metal, perforated layer, slit layer regular cells B32B3/12
    • 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
    • B32B5/024—Woven fabric
    • 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
    • B32B5/026—Knitted fabric
    • 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
    • B32B9/005—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00 comprising one layer of ceramic material, e.g. porcelain, ceramic tile
    • B32B9/007—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00 comprising one layer of ceramic material, e.g. porcelain, ceramic tile comprising carbon, e.g. graphite, composite carbon
    • 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
    • D—TEXTILES; PAPER
    • D04—BRAIDING; LACE-MAKING; KNITTING; TRIMMINGS; NON-WOVEN FABRICS
    • D04H—MAKING TEXTILE FABRICS, e.g. FROM FIBRES OR FILAMENTARY MATERIAL; FABRICS MADE BY SUCH PROCESSES OR APPARATUS, e.g. FELTS, NON-WOVEN FABRICS; COTTON-WOOL; WADDING ; NON-WOVEN FABRICS FROM STAPLE FIBRES, FILAMENTS OR YARNS, BONDED WITH AT LEAST ONE WEB-LIKE MATERIAL DURING THEIR CONSOLIDATION
    • D04H18/00—Needling machines
    • D04H18/02—Needling machines with needles
    • 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—Compositions 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
    • B32B38/00—Ancillary operations in connection with laminating processes
    • B32B38/04—Punching, slitting or perforating
    • B32B2038/042—Punching
    • 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
    • B32B2250/00—Layers arrangement
    • B32B2250/20—All layers 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
    • 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
    • B32B2305/00—Condition, form or state of the layers or laminate
    • B32B2305/10—Fibres of continuous length
    • B32B2305/18—Fabrics, textiles
    • B32B2305/186—Knitted fabrics
    • 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
    • B32B2305/00—Condition, form or state of the layers or laminate
    • B32B2305/10—Fibres of continuous length
    • B32B2305/18—Fabrics, textiles
    • B32B2305/188—Woven fabrics
GB29855/76A 1977-07-06 1977-07-06 Production of carbon fibre reinforced carbon composite materials Expired GB1549687A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB29855/76A GB1549687A (en) 1977-07-06 1977-07-06 Production of carbon fibre reinforced carbon composite materials

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB29855/76A GB1549687A (en) 1977-07-06 1977-07-06 Production of carbon fibre reinforced carbon composite materials

Publications (1)

Publication Number Publication Date
GB1549687A true GB1549687A (en) 1979-08-08

Family

ID=10298310

Family Applications (1)

Application Number Title Priority Date Filing Date
GB29855/76A Expired GB1549687A (en) 1977-07-06 1977-07-06 Production of carbon fibre reinforced carbon composite materials

Country Status (1)

Country Link
GB (1) GB1549687A (en)

Cited By (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5727746A (en) * 1980-07-25 1982-02-15 Toho Beslon Co Three dimensional fiber reinforcing composite material and its manufacture
FR2533499A1 (en) * 1982-09-29 1984-03-30 Avco Corp FIBER-BASED COMPOSITE AND PROCESS FOR PREPARING SAME
FR2584107A1 (en) * 1985-06-27 1987-01-02 Europ Propulsion METHOD FOR MANUFACTURING THREE-DIMENSIONAL REVOLUTION STRUCTURES BY NEEDLEING LAYERS OF FIBROUS MATERIAL AND MATERIAL USED FOR THE IMPLEMENTATION OF THE PROCESS
FR2584106A1 (en) * 1985-06-27 1987-01-02 Europ Propulsion METHOD FOR MANUFACTURING THREE-DIMENSIONAL STRUCTURES BY NEEDLEING PLANE LAYERS OF SUPERIMPOSED FIBROUS MATERIAL AND FIBROUS MATERIAL USED FOR THE IMPLEMENTATION OF THE PROCESS
FR2607069A1 (en) * 1986-11-20 1988-05-27 Dunlop Ltd LIGHTWEIGHT PANEL, ESPECIALLY FOR AIRCRAFT, AND METHOD OF MANUFACTURING THE SAME
US4790052A (en) * 1983-12-28 1988-12-13 Societe Europeenne De Propulsion Process for manufacturing homogeneously needled three-dimensional structures of fibrous material
FR2616779A1 (en) * 1987-06-18 1988-12-23 Aerospatiale METHOD FOR MANUFACTURING A PIECE, IN PARTICULAR A CARBON-CARBON BRAKE DISC AND PART OBTAINED
FR2660591A1 (en) * 1990-04-09 1991-10-11 Europ Propulsion PROCESS FOR CONFORMING PREFORMS FOR THE MANUFACTURE OF PARTS OF THERMOSTRUCTURAL COMPOSITE MATERIAL, PARTICULARLY OF PARTS IN THE FORM OF SAILS OR PANELS.
US5360500A (en) * 1986-11-20 1994-11-01 Dunlop Limited Method of producing light-weight high-strength stiff panels
US5405560A (en) * 1987-06-18 1995-04-11 Societe Nationale Industrielle Et Aerospatiale Process for the production of a part, particularly a carbon-carbon brake disk and to the part obtained
EP0695823A2 (en) 1994-07-25 1996-02-07 The B.F. Goodrich Company An improved process for forming fibrous preform structures
US5546880A (en) * 1994-12-29 1996-08-20 The Bf Goodrich Company Annular filamentary structures and methods of making
US5597611A (en) * 1990-10-01 1997-01-28 Fiber Materials, Inc. Reinforced carbon composites
EP0767264A1 (en) 1995-10-04 1997-04-09 The B.F. Goodrich Company Brake disk having a functional gradient Z-fiber distribution
US5705264A (en) * 1987-01-27 1998-01-06 Aerpspace Preforms Limited Production of shaped filamentary structures
US5858890A (en) * 1994-07-25 1999-01-12 The B. F. Goodrich Company Laminar fibrous structure having Z-fibers that penetrate a constant number of layers
US5882781A (en) * 1986-01-28 1999-03-16 Aerospace Preforms Limited Shaped fibrous fabric structure comprising multiple layers of fibrous material
US6029327A (en) * 1994-07-25 2000-02-29 The B.F. Goodrich Company Process for forming fibrous structures with predetermined Z-fiber distributions
US6105223A (en) * 1997-04-30 2000-08-22 The B. F. Goodrich Company Simplified process for making thick fibrous structures
US6405417B1 (en) 1994-07-25 2002-06-18 Goodrich Corporation Process for forming fibrous structures with predetermined Z-fiber distributions
GB2462534A (en) * 2008-08-13 2010-02-17 Goodrich Corp A method for preparing a needled preform

Cited By (37)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6225094B2 (en) * 1980-07-25 1987-06-01 Toho Rayon Kk
JPS5727746A (en) * 1980-07-25 1982-02-15 Toho Beslon Co Three dimensional fiber reinforcing composite material and its manufacture
FR2533499A1 (en) * 1982-09-29 1984-03-30 Avco Corp FIBER-BASED COMPOSITE AND PROCESS FOR PREPARING SAME
US4790052A (en) * 1983-12-28 1988-12-13 Societe Europeenne De Propulsion Process for manufacturing homogeneously needled three-dimensional structures of fibrous material
FR2584107A1 (en) * 1985-06-27 1987-01-02 Europ Propulsion METHOD FOR MANUFACTURING THREE-DIMENSIONAL REVOLUTION STRUCTURES BY NEEDLEING LAYERS OF FIBROUS MATERIAL AND MATERIAL USED FOR THE IMPLEMENTATION OF THE PROCESS
FR2584106A1 (en) * 1985-06-27 1987-01-02 Europ Propulsion METHOD FOR MANUFACTURING THREE-DIMENSIONAL STRUCTURES BY NEEDLEING PLANE LAYERS OF SUPERIMPOSED FIBROUS MATERIAL AND FIBROUS MATERIAL USED FOR THE IMPLEMENTATION OF THE PROCESS
US5882781A (en) * 1986-01-28 1999-03-16 Aerospace Preforms Limited Shaped fibrous fabric structure comprising multiple layers of fibrous material
FR2607069A1 (en) * 1986-11-20 1988-05-27 Dunlop Ltd LIGHTWEIGHT PANEL, ESPECIALLY FOR AIRCRAFT, AND METHOD OF MANUFACTURING THE SAME
US5360500A (en) * 1986-11-20 1994-11-01 Dunlop Limited Method of producing light-weight high-strength stiff panels
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
WO1988010245A1 (en) * 1987-06-18 1988-12-29 Aerospatiale Societe Nationale Industrielle Process for manufacturing a carbon-carbon component, in particular a brake disk, and part thus obtained
US5405560A (en) * 1987-06-18 1995-04-11 Societe Nationale Industrielle Et Aerospatiale Process for the production of a part, particularly a carbon-carbon brake disk and to the part obtained
US5454990A (en) * 1987-06-18 1995-10-03 Aerospatiale Societe Nationale Industrielle Process for the production of a part, particularly a carbon-carbon brake disk and to the part obtained
FR2616779A1 (en) * 1987-06-18 1988-12-23 Aerospatiale METHOD FOR MANUFACTURING A PIECE, IN PARTICULAR A CARBON-CARBON BRAKE DISC AND PART OBTAINED
FR2660591A1 (en) * 1990-04-09 1991-10-11 Europ Propulsion PROCESS FOR CONFORMING PREFORMS FOR THE MANUFACTURE OF PARTS OF THERMOSTRUCTURAL COMPOSITE MATERIAL, PARTICULARLY OF PARTS IN THE FORM OF SAILS OR PANELS.
EP0452199A1 (en) * 1990-04-09 1991-10-16 Societe Europeenne De Propulsion Method of strengthening preforms for the fabrication of heat resistant composite material parts, in particular parts in the shape of sails or panels
US5160471A (en) * 1990-04-09 1992-11-03 Societe Europeenne De Propulsion Process for manufacturing a thermostructural composite by chemical vapor deposition using linking threads
US5597611A (en) * 1990-10-01 1997-01-28 Fiber Materials, Inc. Reinforced carbon composites
US5773122A (en) * 1990-10-01 1998-06-30 Fiber Materials, Inc. Reinforced carbon composites
US5858890A (en) * 1994-07-25 1999-01-12 The B. F. Goodrich Company Laminar fibrous structure having Z-fibers that penetrate a constant number of layers
US6405417B1 (en) 1994-07-25 2002-06-18 Goodrich Corporation Process for forming fibrous structures with predetermined Z-fiber distributions
US5581857A (en) * 1994-07-25 1996-12-10 The B. F. Goodrich Co. Process for forming fibrous preform structures
US6029327A (en) * 1994-07-25 2000-02-29 The B.F. Goodrich Company Process for forming fibrous structures with predetermined Z-fiber distributions
US5740593A (en) * 1994-07-25 1998-04-21 The B. F. Goodrich Company Process for forming fibrous preform structures
US5515585A (en) * 1994-07-25 1996-05-14 The Bf Goodrich Company Process for forming needled fibrous structures using determined transport depth
EP0695823A3 (en) * 1994-07-25 1998-12-16 The B.F. Goodrich Company An improved process for forming fibrous preform structures
US5504979A (en) * 1994-07-25 1996-04-09 The Bfgoodrich Company Process for forming fibrous preform structures
EP0695823A2 (en) 1994-07-25 1996-02-07 The B.F. Goodrich Company An improved process for forming fibrous preform structures
US5546880A (en) * 1994-12-29 1996-08-20 The Bf Goodrich Company Annular filamentary structures and methods of making
US5908792A (en) * 1995-10-04 1999-06-01 The B. F. Goodrich Company Brake disk having a functional gradient Z-fiber distribution
US6237203B1 (en) 1995-10-04 2001-05-29 The B. F. Goodrich Company Process for forming fibrous structures with predetermined Z-fiber distributions
EP0767264A1 (en) 1995-10-04 1997-04-09 The B.F. Goodrich Company Brake disk having a functional gradient Z-fiber distribution
US6105223A (en) * 1997-04-30 2000-08-22 The B. F. Goodrich Company Simplified process for making thick fibrous structures
EP0910690B2 (en) † 1997-04-30 2009-07-29 Goodrich Corporation Simplified process for making thick fibrous structures
GB2462534A (en) * 2008-08-13 2010-02-17 Goodrich Corp A method for preparing a needled preform
GB2462534B (en) * 2008-08-13 2012-05-16 Goodrich Corp Method and system for enabling Z fiber transfer in needled preform

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Legal Events

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PS Patent sealed
PCNP Patent ceased through non-payment of renewal fee