WO1999022052A1 - Method for making carbon fibre preforms - Google Patents
Method for making carbon fibre preforms Download PDFInfo
- Publication number
- WO1999022052A1 WO1999022052A1 PCT/FR1998/002298 FR9802298W WO9922052A1 WO 1999022052 A1 WO1999022052 A1 WO 1999022052A1 FR 9802298 W FR9802298 W FR 9802298W WO 9922052 A1 WO9922052 A1 WO 9922052A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- wire
- fibers
- cable
- carbon
- preform
- Prior art date
Links
Classifications
-
- 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
-
- 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
- D01—NATURAL OR MAN-MADE THREADS OR FIBRES; SPINNING
- D01F—CHEMICAL FEATURES IN THE MANUFACTURE OF ARTIFICIAL FILAMENTS, THREADS, FIBRES, BRISTLES OR RIBBONS; APPARATUS SPECIALLY ADAPTED FOR THE MANUFACTURE OF CARBON FILAMENTS
- D01F11/00—Chemical after-treatment of artificial filaments or the like during manufacture
- D01F11/10—Chemical after-treatment of artificial filaments or the like during manufacture of carbon
-
- D—TEXTILES; PAPER
- D01—NATURAL OR MAN-MADE THREADS OR FIBRES; SPINNING
- D01F—CHEMICAL FEATURES IN THE MANUFACTURE OF ARTIFICIAL FILAMENTS, THREADS, FIBRES, BRISTLES OR RIBBONS; APPARATUS SPECIALLY ADAPTED FOR THE MANUFACTURE OF CARBON FILAMENTS
- D01F11/00—Chemical after-treatment of artificial filaments or the like during manufacture
- D01F11/10—Chemical after-treatment of artificial filaments or the like during manufacture of carbon
- D01F11/14—Chemical after-treatment of artificial filaments or the like during manufacture of carbon with organic compounds, e.g. macromolecular compounds
-
- D—TEXTILES; PAPER
- D01—NATURAL OR MAN-MADE THREADS OR FIBRES; SPINNING
- D01F—CHEMICAL FEATURES IN THE MANUFACTURE OF ARTIFICIAL FILAMENTS, THREADS, FIBRES, BRISTLES OR RIBBONS; APPARATUS SPECIALLY ADAPTED FOR THE MANUFACTURE OF CARBON FILAMENTS
- D01F9/00—Artificial filaments or the like of other substances; Manufacture thereof; Apparatus specially adapted for the manufacture of carbon filaments
- D01F9/08—Artificial filaments or the like of other substances; Manufacture thereof; Apparatus specially adapted for the manufacture of carbon filaments of inorganic material
- D01F9/12—Carbon filaments; Apparatus specially adapted for the manufacture thereof
- D01F9/14—Carbon filaments; Apparatus specially adapted for the manufacture thereof by decomposition of organic filaments
- D01F9/20—Carbon filaments; Apparatus specially adapted for the manufacture thereof by decomposition of organic filaments from polyaddition, polycondensation or polymerisation products
- D01F9/21—Carbon filaments; Apparatus specially adapted for the manufacture thereof by decomposition of organic filaments from polyaddition, polycondensation or polymerisation products from macromolecular compounds obtained by reactions only involving carbon-to-carbon unsaturated bonds
- D01F9/22—Carbon filaments; Apparatus specially adapted for the manufacture thereof by decomposition of organic filaments from polyaddition, polycondensation or polymerisation products from macromolecular compounds obtained by reactions only involving carbon-to-carbon unsaturated bonds from polyacrylonitriles
-
- D—TEXTILES; PAPER
- D02—YARNS; MECHANICAL FINISHING OF YARNS OR ROPES; WARPING OR BEAMING
- D02G—CRIMPING OR CURLING FIBRES, FILAMENTS, THREADS, OR YARNS; YARNS OR THREADS
- D02G1/00—Producing crimped or curled fibres, filaments, yarns, or threads, giving them latent characteristics
- D02G1/02—Producing crimped or curled fibres, filaments, yarns, or threads, giving them latent characteristics by twisting, fixing the twist and backtwisting, i.e. by imparting false twist
-
- D—TEXTILES; PAPER
- D02—YARNS; MECHANICAL FINISHING OF YARNS OR ROPES; WARPING OR BEAMING
- D02J—FINISHING OR DRESSING OF FILAMENTS, YARNS, THREADS, CORDS, ROPES OR THE LIKE
- D02J1/00—Modifying the structure or properties resulting from a particular structure; Modifying, retaining, or restoring the physical form or cross-sectional shape, e.g. by use of dies or squeeze rollers
- D02J1/22—Stretching or tensioning, shrinking or relaxing, e.g. by use of overfeed and underfeed apparatus, or preventing stretch
- D02J1/222—Stretching in a gaseous atmosphere or in a fluid bed
-
- D—TEXTILES; PAPER
- D02—YARNS; MECHANICAL FINISHING OF YARNS OR ROPES; WARPING OR BEAMING
- D02J—FINISHING OR DRESSING OF FILAMENTS, YARNS, THREADS, CORDS, ROPES OR THE LIKE
- D02J13/00—Heating or cooling the yarn, thread, cord, rope, or the like, not specific to any one of the processes provided for in this subclass
- D02J13/001—Heating or cooling the yarn, thread, cord, rope, or the like, not specific to any one of the processes provided for in this subclass in a tube or vessel
-
- 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
- D04H13/00—Other non-woven fabrics
-
- 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
- D04H3/00—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length
- D04H3/002—Inorganic yarns or filaments
-
- 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
- D04H3/00—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length
- D04H3/08—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length characterised by the method of strengthening or consolidating
- D04H3/10—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length characterised by the method of strengthening or consolidating with bonds between yarns or filaments made mechanically
- D04H3/105—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length characterised by the method of strengthening or consolidating with bonds between yarns or filaments made mechanically by needling
Definitions
- the present invention relates to the manufacture of carbon fiber preforms for the production of parts made of composite material comprising a fibrous preform densified by a matrix.
- a particular field of application of the invention is the production of preforms for parts made of carbon / carbon composite material (C / C), that is to say having a preform or reinforcement of carbon fibers densified by a matrix carbon.
- Parts made of C / C composite material are used in various fields, in particular that of friction, in the form of brake discs or clutches.
- a technique commonly used to obtain a carbon fiber preform consists in preparing a fiber preform of carbon precursor, and then performing at least one carbonization step to transform the precursor into carbon.
- Various precursors can be used, such as pitch-based, or phenolic, or cellulosic, or even pre-oxidized polyacrylonitrile (PAN) precursors.
- a desired advantage of using precursor fibers is that it is possible to carry out textile operations, in particular needling, to develop preforms having the desired characteristics, while needling could have a destructive effect if it were made directly on commercially available carbon threads.
- the object of the invention is to provide a process for producing carbon fiber preforms which makes it possible to combine the advantages of the prior techniques, while eliminating the main drawbacks. This object is achieved thanks to a process according to which:
- At least one wire or cable formed from continuous fibers from carbon precursor fibers having undergone intermediate carbonization is used such that the fibers have a carbon content of between 70% and 90% and will have a tensile breaking strength at less equal to 3000 MPa after their carbonization has been completed without necessarily being tensioned, - the wire or cable is used to manufacture the preform, and
- the preform is subjected to a heat treatment at least in order to complete the transformation of the staple fibers into carbon fibers.
- a characteristic of the process resides in the use of wires or cables formed of continuous fibers resulting from a carbonization of a carbon precursor which is not complete but sufficient to ultimately give the fibers mechanical properties similar to those of carbon fibers obtained from same precursor but fully charred under tension.
- the intermediate carbonization being carried out before preparation of the preform, it can advantageously be carried out under tension in order to obtain optimal mechanical properties in the end, carbonization then being completed statically, after preparation of the preform.
- wires or cables at an intermediate stage of carbonization by using wires or cables at an intermediate stage of carbonization, certain disadvantages already mentioned linked to the use of carbon wires are avoided.
- wires or cables of at least 50 K are used, that is to say formed from at least 50,000 filaments.
- the heat treatment carried out on the preform may aim not only to complete the transformation of the precursor, by bringing the temperature to at least about 1200 ° C., but also to remove impurities, by prolonging it at a higher temperature at least equal to 1 600 ° C.
- the method therefore does not introduce any additional step.
- the method makes it possible not only to achieve a preform in which the fibers have far superior mechanical properties, but also to avoid taking into account a subsequent withdrawal of the preform. This can therefore be produced as close as possible to its final dimensions, therefore by optimizing the duration of the textile operations necessary for this purpose.
- the wire or cable formed from continuous fibers is subjected to a drawing-cracking operation so as to obtain a wire or cable formed from staple fibers, and the wire is imparted or cable formed of staple fibers sufficient cohesion for use in manufacturing the preform.
- Cohesion can be brought about by imposing on the wire or cable formed of staple fibers a slight twist.
- twisting imposed on the thread or cable formed of staple fibers is meant here a sufficient twisting to give the thread or cable the necessary resistance to be able to undergo textile operations, in particular weaving, in particular weaving at high speed, while leaving the possibility of at least one subsequent needling during which staple fibers can be removed by needles without significantly damaging the wires or cables.
- the twist may vary depending on the title of the wire or cable. Preferably, it is between 20 rpm and about 120 rpm.
- the cohesion of the wire or cable formed of staple fibers can be provided by covering, for example by means of synthetic or natural filaments.
- the wire or cable formed from continuous fibers is used directly as is to manufacture the preform.
- the manufacture of the preform advantageously comprises at least one needling step.
- FIG. 1 shows successive steps of an embodiment of a method according to the invention
- a first step (10) of the method consists in providing wires or cables made of fibers originating from a carbon precursor having undergone intermediate carbonization.
- intermediate carbonization is meant here an intermediate carbonization between the precursor state and the carbon state.
- This intermediate carbonization is carried out under tension so as to obtain fibers having optimal mechanical characteristics.
- the degree of carbonization is preferably chosen so as to reach a level of mechanical characteristics close to or substantially equal to that of the characteristics obtained after complete transformation of the precursor under tension. Such a level of carbonization is reached when the carbon content is between 70 and 90%, this can vary depending on the carbon precursor used.
- Intermediate carbonization is obtained by heat treatment at a temperature and / or for a period lower than those necessary to achieve complete carbonization.
- wires or cables of relatively high titer are used, preferably wires or cables of 50 K or more, that is to say formed of 50,000 filaments or more.
- the wires or cables are commercially available at a cost related to the unit mass which decreases when the titer increases.
- wires or cables offered under the name "Pyon" by the British company SGL Technics Ltd., cables from 320 K to 480 K being commercially available. These wires or cables are formed of continuous filaments originating from PAN precursor from the British company Courtaulds after intermediate carbonization carried out under tension until a carbon content of between 70 and 80% is obtained.
- the wire or cable 11 is subjected to a stretching-cracking operation, in order to transform it into wire or cable 12 formed of discontinuous filaments substantially parallel to the longitudinal direction of the wire or cable.
- the stretch-cracking operation is well known and is generally carried out by stretching the wire or cable 11 and causing it to break between two pairs of rollers 22, 23 of a stretch train 21 (FIG.
- FIG. 3 shows a stretch-cracking installation in which several roller stretching trains 21a to 21JD are provided for drawing-cracking a corresponding number of wires or cables 11a to 11 ⁇ .
- the wires or cables 12a to 12 ⁇ formed from staple fibers can then be mixed by passing through a drawing device with bars 25.
- the latter comprising combs mounted on an endless chain, makes it possible to mix the staple fibers of the different wires or cables, while carrying out a drawing, so that the wire or cable obtained 13 has the same title as each of the wires or cables received by the device 25.
- the device 25 is adjusted to carry out a stretching with multiplication by 16 of the length.
- the wires 11a to 11JD may include: - one or more wires or cables formed from continuous fibers originating from carbon precursor fibers having undergone intermediate carbonization such that the fibers have a rate of carbon between
- one or more wires or cables formed from continuous fibers originating from carbon precursor giving fibers having a lower breaking strength for example continuous fibers originating from phenolic, cellulosic or isotropic precursor, - one or more wires or cables formed continuous fibers from ceramic precursor, for example from silicon carbide, alumina, silica precursor, etc., and
- wires or cables formed of continuous carbon or almost carbon fibers such as wires or cables of continuous fibers originating from anisotropic pitch intrinsically having a high resistance to breakage.
- the strip drawing device 25 allows intimate mixing of the staple fibers coming from the different yarns after drawing-cracking.
- the wires or cables obtained after stretching-cracking undergo a slight twisting (step 30) in order to give them sufficient strength or cohesion allowing them to undergo subsequent textile operations.
- the production of fibrous preforms from son or cables can involve different operations such as weaving, unidirectional tablecloths, winding, needling. Some operations, in particular weaving, require minimum cohesion of the son or cables formed of discontinuous filaments, in particular when they are produced at high speed, that is to say, for weaving, a speed which can reach 400 strokes / min or more .
- the twisting in order to be able to be carried out without appreciable damage to the wires or cables, requires that discontinuous filaments can be easily removed.
- the twisting must be sufficient to give minimum cohesion to the wires or cables, but limited to allow subsequent needling.
- the degree of twist is preferably between 20 rpm and 120 rpm. It can be chosen at a higher value for a relatively weak title thread (expressed in tex) than for a relatively strong title thread.
- the coefficient ⁇ giving the ratio between the twist in rpm and the square root of the title in metric number (Nm) is preferably between 30 and 60.
- the twisting can be carried out, in a well known manner, by means for example a bench with spindles, or a continuous spinning machine, or else a sleeve wiper, the latter carrying out rather a "scrambling" of the fibers than a real twist.
- the slightly twisted wires or cables can then be used for the production of the desired preforms (step 40). To this end, operations such as weaving, tableclothing, winding and needling can be carried out, as indicated above.
- a preform can be produced by stacking two-dimensional, flat or draped layers on a shape, and bonding the layers together by needling.
- the two-dimensional layers can be layers of fabric or unidirectional layers formed of wires or cables parallel to one another and superimposed in different directions.
- very fine needles are preferably used, due to the slight twisting of the wires or cables.
- very fine needles is meant here, for example, needles whose active part has, in section, a triangle shape whose height is relatively small, that is to say less than 0.5 mm.
- step 50 After preparation of the preform, it is subjected to a heat treatment (step 50) in order to complete the transformation of the fiber precursor.
- This treatment is carried out at a temperature preferably at least equal to 1200 ° C., for example around 1400 ° C. After a plateau at this temperature, the heat treatment can be continued by raising the temperature to a plateau, for example at least about 1600 ° C., in order to remove undesirable impurities present in the carbon fibers, for example sodium.
- the preform is finally obtained in the desired carbon fibers, with fibers having high mechanical properties, and without significant shrinkage during the heat treatment.
- FIG. 4 shows another embodiment of a method according to the invention, which differs from that of FIG.
- the covering can be carried out using natural or synthetic filaments.
- the filaments can be made of a removable material, for example by dissolution before the complete transformation of the staple fibers into carbon fibers, or by heat treatment or before or during this transformation. It is also possible to choose filaments made of a material leaving a carbon residue after complete transformation of the staple fibers into carbon fibers. Examples of materials which can be used for covering filaments are cotton, viscose, polyethylene, polyester, polyvinyl alcohol.
- the wrapped wires or cables are used for the preparation of the preform (step 40), before heat treatment (step 50).
- the preparation of the preform includes a needling phase, the possible elimination of the covering filaments can be carried out before or after the needling.
- FIG. 5 shows yet another embodiment of a method according to the invention, which differs from that of FIG. 1 in that the steps 40, 50 of preparation of the preform and of heat treatment are carried out directly on the son or cables of precursor fibers supplied after intermediate carbonization (step 10), the steps of stretch-cracking and of cohesion by slight twisting being omitted.
- Example 1 An exemplary embodiment of preforms of discs and brake pads in composite C / C according to a method of the type of that of FIG. 1, and tests carried out with discs and brake pads incorporating such preforms will now be described.
- Cables of linear mass of 30 g / m that is to say a title of 30 ktex sold by the British company SGL Technics Ltd under the name "Pyon 15" are used. These are fiber cables from pre-oxidized PAN having undergone intermediate carbonization under tension such that the fibers have a carbon content of 76%, the rest being essentially constituted by nitrogen.
- the thread obtained is used to make a fabric (twill weaving of 2) having a surface mass of 840 g / m 2 and a thickness under load (50 g / m 2 ) of 1.8 mm.
- Layers of fabric are stacked and needled layer by layer, as described in document FR-A-2 726 013, to bring the volume content of fibers to a value of approximately 20%.
- a heat treatment is carried out first at around 1400 ° C. to complete the carbonization of the precursor, then the temperature is raised to
- Annular preforms of brake discs are cut, as well as preforms of brake pads, then are densified by a pyrolytic carbon matrix by chemical vapor infiltration, in a manner well known per se, in order to obtain discs and pads C / C composite brake shoe.
- reference brake discs and pads in C / C composite are produced in a similar manner, but starting from cables made of preoxidized PAN fibers, which have not undergone intermediate carbonization, the carbonization being carried out after needling , therefore not energized.
- the reference brake discs and pads and according to the invention are subjected to the same high energy braking tests and the resulting wear is evaluated by measuring the loss of thickness expressed in mm. The results are given in the table below.
- the reduction in wear, with the C / C material according to the invention, is 38% for the discs and 27% for the pads.
- cables marketed by the British company SGL Technics Ltd. under the name "Pyon 18" are cables formed from 320,000 filaments (320 K) made of fibers from pre-oxidized PAN having undergone intermediate carbonization under tension such that the fibers have a carbon content of 73%.
- the title of the starting cables is 34 g / m, or 34 ktex.
- the cable is subjected to a stretch-cracking operation in order to obtain an 833 tex thread, the cohesion of which is ensured by covering with a cotton filament of 14.7 tex title.
- the wrapped yarn is used to make a fabric (satin weaving of 8) with a surface mass equal to 780 g / m 2 and a thickness under load equal to 1.7 mm.
- the fabric is steamed at 250 ° C in air so as to thermally degrade the cotton covering thread.
- Example 1 Several layers of fabric are superimposed and needled without difficulty and the preform obtained is subjected to a heat treatment as in Example 1.
- Example 2 The procedure is as in Example 2, but without degrading the cotton covering before needling. This is done successfully on the wrapped threads. The cotton covering is degraded during the rise in temperature for the final heat treatment of transformation of the precursor.
- the threads are woven directly, without any special technical preparation.
- the fabric obtained has a surface mass of 1.2 kg / m 2 .
- Several strata of fabric obtained are superimposed and needled without difficulty, despite the fact that these are yarns formed from continuous filaments.
- the preform obtained is then subjected to a heat treatment for transformation of the precursor.
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Textile Engineering (AREA)
- Chemical Kinetics & Catalysis (AREA)
- General Chemical & Material Sciences (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Composite Materials (AREA)
- Ceramic Engineering (AREA)
- Inorganic Chemistry (AREA)
- Manufacturing & Machinery (AREA)
- Structural Engineering (AREA)
- Organic Chemistry (AREA)
- Inorganic Fibers (AREA)
- Yarns And Mechanical Finishing Of Yarns Or Ropes (AREA)
- Woven Fabrics (AREA)
Abstract
Description
Claims
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2000518137A JP2001521073A (en) | 1997-10-27 | 1998-10-27 | Manufacturing method of carbon fiber preform |
EP98952798A EP1025295A1 (en) | 1997-10-27 | 1998-10-27 | Method for making carbon fibre preforms |
CA002307137A CA2307137A1 (en) | 1997-10-27 | 1998-10-27 | Method for making carbon fibre preforms |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR97/13424 | 1997-10-27 | ||
FR9713424A FR2770233B1 (en) | 1997-10-27 | 1997-10-27 | PROCESS FOR MANUFACTURING CARBON FIBER PREFORMS |
Publications (1)
Publication Number | Publication Date |
---|---|
WO1999022052A1 true WO1999022052A1 (en) | 1999-05-06 |
Family
ID=9512669
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/FR1998/002298 WO1999022052A1 (en) | 1997-10-27 | 1998-10-27 | Method for making carbon fibre preforms |
Country Status (6)
Country | Link |
---|---|
EP (1) | EP1025295A1 (en) |
JP (1) | JP2001521073A (en) |
CN (1) | CN1092723C (en) |
CA (1) | CA2307137A1 (en) |
FR (1) | FR2770233B1 (en) |
WO (1) | WO1999022052A1 (en) |
Families Citing this family (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2842192B1 (en) * | 2002-07-12 | 2004-10-01 | Snecma Propulsion Solide | PROCESS AND PLANT FOR OBTAINING CARBON PRODUCTS FROM CARBON PRECURSOR PRODUCTS |
US6783851B2 (en) * | 2002-08-07 | 2004-08-31 | Albany International Techniweave, Inc. | Pitch based graphite fabrics and needled punched felts for fuel cell gas diffusion layer substrates and high thermal conductivity reinforced composites |
EP2155476B1 (en) * | 2007-06-12 | 2011-09-14 | Hexcel Reinforcements | Method for making a composite material having at least one twisted thread deposited therein |
CN101245503B (en) * | 2008-03-01 | 2011-07-27 | 威海拓展纤维有限公司 | Method for producing carbon fiber |
FR2953826B1 (en) * | 2009-12-16 | 2019-10-11 | Safran Landing Systems | PROCESS FOR MANUFACTURING A FRICTION PIECE BASED ON COMPOSITE C / C MATERIAL |
CN102041597B (en) * | 2010-11-16 | 2012-08-08 | 江苏澳盛复合材料科技有限公司 | Carbon fiber cloth and application thereof to antifriction parts of automobile |
CN103274714B (en) * | 2013-06-05 | 2014-09-17 | 东南大学 | Improved Z-pin method for two-dimensional ceramic matrix composite |
FR3025810B1 (en) * | 2014-09-12 | 2016-12-09 | Herakles | PROCESS FOR PRODUCING A FIBROUS STRUCTURE |
JP6607026B2 (en) * | 2015-12-22 | 2019-11-20 | 株式会社豊田自動織機 | Fiber reinforced composite |
KR102208680B1 (en) * | 2016-06-03 | 2021-01-28 | 슝크 코렌슈토프테크닉 게엠베하 | Carrier plate manufacturing method and carrier plate |
CN110616493B (en) * | 2019-09-23 | 2021-09-10 | 潘魏豪 | Manufacturing method of flexible conductive carbon cloth |
CN111455522A (en) * | 2020-04-02 | 2020-07-28 | 广州蓝墨科技有限公司 | Preparation method of antistatic fabric |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0278139A1 (en) * | 1984-10-12 | 1988-08-17 | Zoltek Corporation | Manufacture of controlled surface resistance carbon fibre sheet products |
EP0329128A2 (en) * | 1988-02-16 | 1989-08-23 | Hercules Incorporated | Novel method of manufacturing carbon fiber using preliminary stretch |
WO1993009278A1 (en) * | 1991-10-30 | 1993-05-13 | Dennis John Gerard Curran | Ceramic fibres |
Family Cites Families (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN2057177U (en) * | 1989-05-04 | 1990-05-16 | 中国科学院山西煤炭化学研究所 | Device for producing pre-oxidation fibre |
FR2669940B1 (en) * | 1990-12-03 | 1994-10-21 | Europ Propulsion | WIRE FORMED FROM REFRACTORY FIBERS OR PRECURSORS THEREOF AND ITS APPLICATION TO THE MANUFACTURE OF PARTS OF COMPOSITE MATERIAL. |
-
1997
- 1997-10-27 FR FR9713424A patent/FR2770233B1/en not_active Expired - Fee Related
-
1998
- 1998-10-27 CN CN98810543A patent/CN1092723C/en not_active Expired - Fee Related
- 1998-10-27 CA CA002307137A patent/CA2307137A1/en not_active Abandoned
- 1998-10-27 WO PCT/FR1998/002298 patent/WO1999022052A1/en not_active Application Discontinuation
- 1998-10-27 EP EP98952798A patent/EP1025295A1/en not_active Withdrawn
- 1998-10-27 JP JP2000518137A patent/JP2001521073A/en active Pending
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0278139A1 (en) * | 1984-10-12 | 1988-08-17 | Zoltek Corporation | Manufacture of controlled surface resistance carbon fibre sheet products |
EP0329128A2 (en) * | 1988-02-16 | 1989-08-23 | Hercules Incorporated | Novel method of manufacturing carbon fiber using preliminary stretch |
WO1993009278A1 (en) * | 1991-10-30 | 1993-05-13 | Dennis John Gerard Curran | Ceramic fibres |
Also Published As
Publication number | Publication date |
---|---|
FR2770233A1 (en) | 1999-04-30 |
CN1092723C (en) | 2002-10-16 |
JP2001521073A (en) | 2001-11-06 |
CA2307137A1 (en) | 1999-05-06 |
CN1277642A (en) | 2000-12-20 |
FR2770233B1 (en) | 2000-01-14 |
EP1025295A1 (en) | 2000-08-09 |
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