EP0383614B1 - Process for producing carbon fiber fabrics - Google Patents
Process for producing carbon fiber fabrics Download PDFInfo
- Publication number
- EP0383614B1 EP0383614B1 EP19900301680 EP90301680A EP0383614B1 EP 0383614 B1 EP0383614 B1 EP 0383614B1 EP 19900301680 EP19900301680 EP 19900301680 EP 90301680 A EP90301680 A EP 90301680A EP 0383614 B1 EP0383614 B1 EP 0383614B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- heat treatment
- fibers
- primary heat
- fabric
- set forth
- 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 - Lifetime
Links
Classifications
-
- 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
- D01F9/145—Carbon filaments; Apparatus specially adapted for the manufacture thereof by decomposition of organic filaments from pitch or distillation residues
Definitions
- the present invention relates to a process for producing carbon fiber fabrics.
- the primary heat-treated fibers obtained by going through the above primary heat treatment, have a tensile strength exceeding 250 kgf/mm and a breaking elongation of 0.4% to 10%.
- the tensile strength of the primary heat-treated fibers should be in excess of 250 kgf/mm.
- the said tensile strength is not lower than 285 kgf/mm, more preferably not lower than 300 kgf/mm, and most preferably not lower than 330 kgf/mm.
- the tensile strength in question is usually not higher than 1000 kgf/mm. If the tensile strength is outside the range just specified, there will occur breakage of fibers and fuzz during weaving, with the result that a high fiber volume fabric cannot be obtained.
- the value of elastic modulus is determined optionally according to the combination of the above tensile strength and elongation to failure, but usually it is in the range of 5 to 100 x103 kgf/mm.
Landscapes
- Chemical & Material Sciences (AREA)
- Chemical Kinetics & Catalysis (AREA)
- General Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Textile Engineering (AREA)
- Inorganic Fibers (AREA)
- Woven Fabrics (AREA)
Description
- The present invention relates to a process for producing carbon fiber fabrics.
- As methods for producing carbon fiber fabrics there are known a method of weaving carbon fibers as a finished product and a method in which an intermediate product is subjected to weaving and the resulting fabric is carbonized or graphitized. As an example of the latter there is disclosed in Japanese Patent Laid-Open No.120136/1988 (corresponding to EP-A-0266788) a three-dimensional fabric containing a pitch based carbon fiber as one component thereof, the carbon fiber having, before heat treatment in a relaxed state, a strength of 15 to 250 kgf/mm, an elongation to failure of 0.5% to 8.0% and an elastic modulus of 400 to 40,000 kgf/mm, but, after the said heat treatment, capable of increasing in both strength and elastic modulus to 1.1 times as high as the strength and elastic modulus before the heat treatment and capable of a strength of 150 kgf/mm or higher and an elastic modulus 40,000 kgf/mm or higher.
- In Japanese Publication No.20281/1987 there is disclosed a process for producing a carbon fiber product in which as-spun pitch fibers are subjected to an initial carbonization treatment, then a bundle of the fibers is subjected to weaving and the resulting fabric is carbonized or graphitized.
- Further, in Carbon-Fiber-Reinforced Plastics, Bamberg, West Germany, May 11-12, 1977, there is a description to the effect that infusibilzed fibers can be woven if they have a strength of about 40 kgf/mm and elongation to failure of 5%, and can be carbonized into a carbon fiber fabric.
- As an additional example of the processes of the prior art JP-A-01 455,819 discloses a process for producing a carbon fiber which comprises making carbon fiber filaments having an elongation of 1.8 - 4.0% and a tensile strength of 20 - 40 kg/mm, said carbon fibers having been obtained by melt-spinning a 100% mesophase pitch, making the resulting fibers infusible, and then subjecting the infusibilized fibers to a heat treatment at 550-1000°C, collecting the fiber filaments into multifilament bundles composed of 100 to 1,000 filaments followed by twisting, knitting or weaving the multifilaments and then heat treating the fabric at a higher temperature.
- However,in producing fabrics according to the aforementioned conventional methods, breaking of fibers or fuzzing occurs because the strength of the fibers in the weaving stage is not sufficiently high, and therefore even if the resulting fabric is carbonized or graphitized, it is impossible to obtain a high fiber volume fabric. Also a permanent strain may remain after carbonization, so the inherent strength cannot be developed when used as a composite material.
- It is the object of the present invention to overcome the above mentioned problems, particularly to provide a process capable of efficiently producing carbon fiber fabrics with little fuzzing and free of permanent strain.
- The present invention is concerned with a process for oroducing a carbon fiber fabric, which process comprises making carbon fibers having a tensile strength exceeding 250 kgf/mm and an elongation to break of 0.4% to 10% into a two- or three-dimensional fabric, the said carbon fibers having been obtained by melt-spinning a carbonaceous pitch, making the resulting fibers infusible and then subjecting the thus-infusiblized fibers to a primary heat treatment at a temperature of at least 1500°C and not higher than 2,500°C, and subjecting the two- or three-dimensional fabric to a secondary heat treatment at a temperature which is higher than the temperature used in the primary heat treatment .
- The process for producing carbon fiber fabrics according to the present invention will be described in detail hereinunder.
- As the carbonaceous pitch there is used a coal or petroleum pitch having a softening point of 100°C to 400°C, preferably 150° to 350°C. Both optically isotropic and anisotropic pitches are employable examples of the carbonaceous pitch, but particularly preferred is an optically anisotropic pitch having an optically anisotropic phase content of 60% to 100%.
- The melt spinning may be carried out by any suitable known method. The resulting pitch fibers are then rendered infusible.
- The infusiblization treatment may be perforred at a temperature of 50°C to 400°C, preferably 100° to 350°C, in an oxidizing gas atmosphere. As the oxidizing gas there may be used air, oxygen, nitrogen oxide, sulfur oxide, halogen, and mixtures thereof.
- The primary heat treatment is conducted in an inert gas at a temperature of at least 1500°C and not higher than 2,500°C, preferably in the range of 1500° to 2000°C. The treatment time is selected suitably so as to obtain primary heat-treated fibers having later-described tensile strength and elongation to failure, but usually it is in the range of 1 second to 10 hours. According to a method wherein fibers which have been treated at a temperature Icer than the above range are subjected to weaving, followed by heat treatment at a high temperature, there remain so-called permanent strain or permanent deformation of the fibers because of a low carbonized state, and thus since the fibers are woven in a bent state, breakage will result at inflection points if pulled.
- The primary heat-treated fibers, obtained by going through the above primary heat treatment, have a tensile strength exceeding 250 kgf/mm and a breaking elongation of 0.4% to 10%.
- It is an essential condition that the tensile strength of the primary heat-treated fibers should be in excess of 250 kgf/mm. Preferably, the said tensile strength is not lower than 285 kgf/mm, more preferably not lower than 300 kgf/mm, and most preferably not lower than 330 kgf/mm. Although there is no upper limit, the tensile strength in question is usually not higher than 1000 kgf/mm. If the tensile strength is outside the range just specified, there will occur breakage of fibers and fuzz during weaving, with the result that a high fiber volume fabric cannot be obtained.
- The elongation to break is in the range of 0.4% to 10% preferably 0.4% to 1.3%, more preferably 0.6% to 10%, still more preferably 0.6% to 5% preferably, 0.4% to 1.3%. In the case of a three-dimensional fabric it is preferable that the elongation to failure be not lower than 0.6% because of small radius of curvature of bundle in a fabric.
- The value of elastic modulus is determined optionally according to the combination of the above tensile strength and elongation to failure, but usually it is in the range of 5 to 100 x10³ kgf/mm.
- The fiber diameter is in the range of 3 to 100 µm, preferably 5 to 30 µm.
- In the present invention, the foregoing primary heat-treated fibers are made into a two- or three-dimensional fabric. Examples of the "fabric" as referred to herein are fabrics obtained using 100 to 25,000 continuous filaments. More concrete examples include two-dimensional fabrics such as plain weave, satin weave, twill weave, bias weave fabrics braid, and stitch knit, three-dimensional fabrics such as three-dinensional orthogonal fabric, leno, interlock and braid, as well as fabrics reinforced in three or more directions such as special shape fabrics, mat-like fabric and felt-like fabric.
- The fabric of the primary heat-treated fibers is subjected to a secondary heat treatment. The secondary heat treatment is performed at a temperature which is higher than the temperature in the primary heat treatment. Usually, the secondary heat treatment temperature is higher by 50°C or more preferably by 100-2,000°C, more preferably by 200-1,000°C, than the primary heat treatment temperature. The treatment time in the secondary heat treatment is selected optionally for obtaining the secondary heat-treated fabric falling under the scope. of the present invention, but usually it is in the range of 1 second to 10 hours.
- According to the process of the present invention there can be obtained a carbon fiber fabric with little fuzzing and free of permanent strain.
- The following examples are given to illustrate the present invention more concretely.
- A carbonaceous pitch was melt-spun and the resultant fibers were rendered infusible. The fibers thus infusiblized were subjected to a primary heat treatment at temperatures ranging from 1,700°C to 2,450°C. Using the fibers thus heat treated, three-dimensional orthogonal fabrics were produced. Then, the fabrics were each subjected to a secondary heat treatment at 2,500°C. The three-dimensional fabrics thus heat treated were evaluated, the results of which are as shown in Table 1.
- Three-dimensional orthogonal fabrics were produced using the primary heat-treated fibers shown in Table 1, and then subjected to a secondary heat treatment at 2,500°C. The three-dimensional fabrics thus heat treated were evaluated, the results of which are as set forth in Table 1.
Table 1 Primary Heat-Treated Fibers Evaluation of three-dimensional fabrics after sencondary heat treatment at 2,500°C Tensile Strength kgf/mm Elongation to break % Elastic Modulus 10³kgf/mm Treating Temp °C Ex. 1 280 0.7 40 2100 Good 2 300 0.75 40 2100 Good 3 330 0.83 40 2100 Good 4 370 1.2 30 2000 Good 5 430 1.3 33 2000 Good 6 350 0.7 50 2450 Good Comp.Ex.1 205 0.7 29.3 1700 Fuzz 2 245 0.5 48.8 2450 fuzz 3 10 3.0 0.3 600 Permanent strain
Claims (7)
- A process for producing a carbon fiber fabric, which process comprises making carbon fibers having a tensile strength exceeding 2.45 GPa (250 kgf/mm) and an elongation to break of 0.4% to 10% into a two- or three-dimensional fabric, said carbon fibers having been obtained by melt-spinning a carbonaceous pitch, making the resulting fibers infusible and then subjecting the thus-infusibilized fibers to a primary heat treatment at a temperature of at least 1500°C and not higher than 2,500°C, and subjecting said two- or three-dimensional fabric to a secondary heat treatment at a temperature which is higher than the temperature used in said primary heat treatment.
- A process as set forth in Claim 1, wherein said carbonaceous pitch is an optically anisotropic pitch having an optically anisotropic phase content of 60% to 100%.
- A process as set forth in Claim 1 or Claim 2 wherein the fibers after said primary heat treatment have a tensile strength of not lower than 2.94 GPa (300 kgf/mm).
- A process as set forth in any one of the preceding claims wherein the fibers after said primary heat treatment have an elongation to break in the range of 0.6% to 10%.
- A process as set forth in any one of the preceding claims wherein the temperature used in said secondary heat treatment is higher by at least 50°C than the temperature used in said primary heat treatment.
- A process as set forth in any one of the preceding claims wherein the temperature used in said secondary heat treatment is higher by 100° to 2,000°C than the temperature used in said primary heat treatment.
- A process as set forth in any one of claims 1 to 10 wherein the carbon fibres have an elongation to break of 0.4% to 1.3%.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP35008/89 | 1989-02-16 | ||
JP1035008A JP2981667B2 (en) | 1989-02-16 | 1989-02-16 | Manufacturing method of carbon fiber fabric |
Publications (3)
Publication Number | Publication Date |
---|---|
EP0383614A2 EP0383614A2 (en) | 1990-08-22 |
EP0383614A3 EP0383614A3 (en) | 1991-06-12 |
EP0383614B1 true EP0383614B1 (en) | 1996-05-01 |
Family
ID=12430060
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP19900301680 Expired - Lifetime EP0383614B1 (en) | 1989-02-16 | 1990-02-16 | Process for producing carbon fiber fabrics |
Country Status (3)
Country | Link |
---|---|
EP (1) | EP0383614B1 (en) |
JP (1) | JP2981667B2 (en) |
DE (1) | DE69026736T2 (en) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP3401716B2 (en) * | 1995-12-18 | 2003-04-28 | 新日本製鐵株式会社 | Triaxial fabric and method for producing the same |
EP0892099A1 (en) * | 1997-07-15 | 1999-01-20 | Mitsubishi Chemical Corporation | Carbon fiber woven fabric |
JP4353672B2 (en) * | 2002-02-15 | 2009-10-28 | 東邦テナックス株式会社 | Polyacrylonitrile-based carbon fiber spun yarn fabric, carbon fiber spun yarn fabric roll, and method for producing carbon fiber spun yarn fabric |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4138525A (en) * | 1976-02-11 | 1979-02-06 | Union Carbide Corporation | Highly-handleable pitch-based fibers |
JP2648711B2 (en) * | 1986-11-07 | 1997-09-03 | 株式会社 ペトカ | Manufacturing method of pitch-based carbon fiber three-dimensional fabric |
JP2593654B2 (en) * | 1987-03-27 | 1997-03-26 | 正三 渡部 | Industrial production of high-strength and high-elastic carbon fiber knitted and woven fabrics |
JPS6445819A (en) * | 1987-08-14 | 1989-02-20 | Toa Nenryo Kogyo Kk | Production of woven fabric of graphite fiber |
-
1989
- 1989-02-16 JP JP1035008A patent/JP2981667B2/en not_active Expired - Fee Related
-
1990
- 1990-02-16 EP EP19900301680 patent/EP0383614B1/en not_active Expired - Lifetime
- 1990-02-16 DE DE1990626736 patent/DE69026736T2/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
EP0383614A2 (en) | 1990-08-22 |
DE69026736T2 (en) | 1996-09-12 |
DE69026736D1 (en) | 1996-06-05 |
JPH02216219A (en) | 1990-08-29 |
EP0383614A3 (en) | 1991-06-12 |
JP2981667B2 (en) | 1999-11-22 |
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