EP0251596A1 - Amélioration de la résistance à la traction de fibres de carbone - Google Patents
Amélioration de la résistance à la traction de fibres de carbone Download PDFInfo
- Publication number
- EP0251596A1 EP0251596A1 EP87305466A EP87305466A EP0251596A1 EP 0251596 A1 EP0251596 A1 EP 0251596A1 EP 87305466 A EP87305466 A EP 87305466A EP 87305466 A EP87305466 A EP 87305466A EP 0251596 A1 EP0251596 A1 EP 0251596A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- yarn
- fibers
- precursor
- fiber
- resin
- 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- Withdrawn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
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
- 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
Definitions
- This invention provides a method for increasing the tenacity of pitch-based carbon fiber yarn comprising impregnating a pitch-based carbonized or partially carbonized fiber yarn with a carbonizable resin precursor, polymerizing the precursor in situ to form the resin and subjecting the impregnated yarn to a temperature in excess of 1000°C in an inert atmosphere to carbonize the resin.
- the carbon fiber yarn to be strengthened in accordance with the present invention is a pitch-based yarn.
- This yarn may be prepared by the general procedures described in U.S. Patent No. 4,005,183. Either carbonized or partially carbonized yarn may be employed.
- a solution of a carbonizable resin precursor is applied to the yarn.
- the object is to impregnate the fibers of the yarn with a material which will polymerize or polymerize further to a resinous product which will remain in place and leave a carbon residue within the fiber upon carbonization.
- the term "resin precursor" is intended to include unpolymerized or partially polymerized materials. Polymerization or resinification is often facilitated by application of heat. The resin must be capable of being carbonized, the usual temperature of carbonization being above 1000°C.
- suitable carbonizable resin precursors are partially polymerized phenolic condensation products, epoxy resins, furfural, furfuryl alcohol, partially polymerized furfuryl alcohol resin, urea condensation products, acrylic resins, vinyl resins, propylene glycol, etc.
- a sufficient amount of carbonizable resin precursor must be absorbed by the yarn to provide strengthening. Amounts yielding between about 0.1 and 10% of resin based on the weight of the yarn prior to impregnation have been found satisfactory.
- the weight gain is kept below 5%, particularly with partially carbonized fiber because such fibers are less able to absorb the resin precursors.
- the resin precursor have a high coking factor, that is, a high percentage of carbon yield when subjected to carbonization. Volatile impregnants which are entirely driven off in the heating step are clearly unsuitable.
- the yarn is passed through a bath containing the carbonizable resin precursor.
- the resin precursor is furfuryl alcohol, a partially polymerized furfuryl alcohol or combination thereof, it is desirable to incorporate a latent catalyst along with the precursor.
- a latent catalyst are commercially available and recommended for the purpose of catalyzing the polymerization of the resin precursor at elevated temperatures.
- One such catalyst is a complex of boron trifluoride and monoethylamine.
- Another catalyst is maleic anhydride.
- Use of a latent catalyst permits application of a low viscosity solution to the fiber with subsequent polymerization at the elevated temperatures. If the precursor were to polymerize significantly prior to application, the treating bath would be so viscous as to allow only a coating to be formed.
- Suitable solvents are those which will readily evaporate without leaving any harmful residues. Acetone has been found useful for this purpose.
- the viscosity of the impregnation bath should be sufficiently low as to permit permeation of the resin precursor into the fibers of the yarn, i.e., to fill the voids, cracks and other defects of the fiber. If the bath is too viscous, the yarn itself, rather than the fibers thereof, will entrap such amounts of resin precursor as to cause the fibers to stick to each other. Such fibers often break when attempts are made to separate them from each other. It will be understood that the resin content of the impregnating solution increases with age because partial polymerization is taking place. As this occurs, the viscosity of the bath increases and will influence the degree of fiber permeation.
- T/E/M Tenacity, elongation and modulus
- the yarn contained 496 filaments each having a diameter of about 10 microns.
- the carbonized yarn (at 1600°C) had an initial modulus of about 900 to 1000 grams per denier (gpd).
- Carbon fiber yarn was impregnated with furfuryl alcohol containing 1% latent catalyst (commercially available complex of boron trifluoride and monoethylamine (BF3.MEA).
- the fibers were heated at 4°C/min. to 150°C and held at 150°C for 32 minutes to polymerize the furfuryl alcohol. After polymerization the fibers were found to have gained 1.45% of their original weight. The fibers were then carbonized at 1584°C.
- An 11% improvement in tensile strength over the control fiber resulted (T/E/M impregnated fiber: 14.6gpd/1.22%/1055gpd, T/E/M control fiber: 13.2gpd/1.17%/988 gpd).
- Carbon fiber yarn was impregnated with the solution used in Example 1. The solution had been aged for 22 days. The furfuryl alcohol was polymerized under the same conditions as in Example 1. After polymerization, the fibers were found to have gained 8.7% of their original weight. The fibers were then recarbonized at 1584°C. A 22% improvement in tensile strength over the control fiber resulted (T/E/M impregnated fiber: 16.1gpd/1.25%/997gpd, T/E/M control fiber: 13.2gpd/1.17%/988gpd).
- Carbon fiber yarn was impregnated using a 90/10% by wt. mixture of furfuryl alcohol and furfural modified furfuryl alcohol resin with 2% of the latent catalyst of Example 1.
- the fibers were heated at 4°C/min. to 120°C and held at 120°C for 32 minutes to polymerize the furfuryl alcohol/resin. After polymerization, the fibers were found to have gained 3.2% of their original weight.
- the fibers were then recarbonized at 1600°C. A 29% improvement in tensile strength over the control fiber resulted (T/E/M impregnated fiber: 14.2gpd/1.23%/1025gpd, T/E/M control fiber: 11.0gpd/.95%/1081gpd).
- Carbon fiber yarn was impregnated using a 90/10% by wt. mixture of furfuryl alcohol and furfural modified furfuryl alcohol resin with 2% of the latent catalyst of Example 1.
- the fibers were heated at 4°C/min to 120° and held at 120°C for 32 minutes to polymerize the furfural modified resin. After polymerization, the fibers were found to have gained 6.1% of their original weight.
- the fibers were then recarbonized at 1600°C. A 24% improvement in tensile strength over the control fiber resulted (T/E/M impregnated fiber: 15.1gpd/1.18%/1148gpd, T/E/M control fiber: 12.2gpd/1.023%/1095gpd).
- Carbon fiber yarn was impregnated using a 10% by wt. solution of furfural modified furfuryl alcohol resin dissolved in acetone. The fibers were then heated at 4°C/min to 120°C and held at 120°C for 32 minutes. The resulting weight gain was 7.7% of their original weight. The fibers were recarbonized at 1600°C. A 12% improvement in tensile strength over the control fiber resulted (T/E/M impregnated fiber: 15.0gpd/1.41%/945, T/E/M control fiber: 13.4gpd/1.34%/868gpd).
- Carbon fiber yarn was impregnated using acetone containing 5% of the latent catalyst of Example 1.
- the fibers were then heated to 4°C/min to 120°C. and held at 120°C for 32 minutes. The resulting weight gain was less than 1%.
- the fibers were then recarbonized at 1600°C. No increase in strength resulted (T/E/M impregnated fiber: 13.7gpd/1.13%/1131gpd, T/E/M control fiber: 14.2gpd/1.07%/1272gpd).
- This example shows treatment with a non-resin forming medium did not result in strength improvement.
- Carbon fiber yarn was impregnated using propylene glycol containing 5% of the latent catalyst of Example 1. The fibers were then heated at 4°C/min to 200°C and held at 200°C for 32 minutes. A resin was formed from propylene glycol under these conditions. The resulting weight gain was less than 1%. The fibers were then recarbonized at 1600°C. A 10% improvement in tensile strength over the control fiber resulted (T/E/M impregnated fiber: 13.2gpd/ 1.05%/1133gpd, T/E/M control fiber: 12.0gpd/.947%/1141gpd).
- Partially carbonized yarn (heated to 1000°C) was impregnated with furfuryl alcohol containing 2% of the latent catalyst of Example 1 which had been aged 72 hours.
- the fibers were heated at 4°C/min to 120°C and held at 120°C for 32 minutes to polymerize the furfuryl alcohol. The resulting weight gain was less than 1%.
- the fibers were then carbonized at 1599°C. A 24.5% improvement in tensile strength over the control fiber resulted.
- T/E/M impregnated fiber 14.5gpd/1.18%/1083gpd
- T/E/M control fiber 11.6gpd/97%/1080gpd).
- Carbon fiber was impregnated with furfural containing 2% of the catalyst of Example 1.
- the fibers were heated at 4°C/min to 120°C and held at 120°C for 32 minutes to polymerize the furfural. After polymerization, the fibers were found to have gained 0.1% of their orginal weight (weight gain from dipping was 3%).
- the fibers were then recarbonized at 1600°C. A 14% improvement in tensile strength over the control fiber resulted (T/E/M impregnated fiber: 13.8gpd/1.06%/1194gpd, T/E/M control fiber: 12.2gpd/1.023%/1095gpd).
- Carbon fiber was impregnated using a 95/5% by wt. mixture of furfuryl alcohol and furfural modified furfuryl alcohol resin with 5% maleic anhydride added as a latent catalyst.
- the fibers were heated at 4°C/min to 120°C and held at 120°C for 32 minutes to polymerize the furfuryl alcohol/resin. After polymerization, the fibers were found to have gained 6.1% of their original weight (weight gain after dipping was 160%). The fibers were then recarbonized at 1594°C.
- T/E/M impregnated fiber 14.6gpd/1.17%/1155gpd
- T/E/M control fiber 12.2gpd/1.02%/1087gpd
Landscapes
- Chemical & Material Sciences (AREA)
- Chemical Kinetics & Catalysis (AREA)
- General Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Textile Engineering (AREA)
- Ceramic Products (AREA)
- Reinforced Plastic Materials (AREA)
- Inorganic Fibers (AREA)
- Chemical Treatment Of Fibers During Manufacturing Processes (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US87821786A | 1986-06-25 | 1986-06-25 | |
US878217 | 1986-06-25 |
Publications (1)
Publication Number | Publication Date |
---|---|
EP0251596A1 true EP0251596A1 (fr) | 1988-01-07 |
Family
ID=25371603
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP87305466A Withdrawn EP0251596A1 (fr) | 1986-06-25 | 1987-06-19 | Amélioration de la résistance à la traction de fibres de carbone |
Country Status (4)
Country | Link |
---|---|
EP (1) | EP0251596A1 (fr) |
JP (1) | JPS636115A (fr) |
AU (1) | AU7458587A (fr) |
CA (1) | CA1255544A (fr) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0457510A2 (fr) * | 1990-05-11 | 1991-11-21 | Nippon Oil Company, Limited | ProcÀ©dé de production de matériau composite de carbone/carbone |
EP0457509A2 (fr) * | 1990-05-11 | 1991-11-21 | Nippon Oil Company, Limited | Procédé de production de matériau composite de carbone/carbone |
US5096519A (en) * | 1989-02-23 | 1992-03-17 | Mitsubishi Pencil Co., Ltd. | Process for preparation of carbon fiber composite reinforced carbonaceous material |
WO1993016013A1 (fr) * | 1992-02-06 | 1993-08-19 | Dunlop Limited | Materiau composite au carbone-carbone |
US9550701B2 (en) | 2013-07-25 | 2017-01-24 | Honeywell International Inc. | Carbon-carbon composites including isotropic carbon encapsulating layer and methods of forming the same |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP5483701B2 (ja) | 2010-02-08 | 2014-05-07 | 日曹金属化学株式会社 | 亜鉛基合金 |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3908061A (en) * | 1972-03-10 | 1975-09-23 | Dow Chemical Co | Composite materials comprising resin matrix and carbon fibers |
US4115528A (en) * | 1977-08-15 | 1978-09-19 | United Technologies Corporation | Method for fabricating a carbon electrode substrate |
-
1987
- 1987-06-19 EP EP87305466A patent/EP0251596A1/fr not_active Withdrawn
- 1987-06-22 AU AU74585/87A patent/AU7458587A/en not_active Abandoned
- 1987-06-23 CA CA000540393A patent/CA1255544A/fr not_active Expired
- 1987-06-23 JP JP15458387A patent/JPS636115A/ja active Pending
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3908061A (en) * | 1972-03-10 | 1975-09-23 | Dow Chemical Co | Composite materials comprising resin matrix and carbon fibers |
US4115528A (en) * | 1977-08-15 | 1978-09-19 | United Technologies Corporation | Method for fabricating a carbon electrode substrate |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5096519A (en) * | 1989-02-23 | 1992-03-17 | Mitsubishi Pencil Co., Ltd. | Process for preparation of carbon fiber composite reinforced carbonaceous material |
EP0457510A2 (fr) * | 1990-05-11 | 1991-11-21 | Nippon Oil Company, Limited | ProcÀ©dé de production de matériau composite de carbone/carbone |
EP0457509A2 (fr) * | 1990-05-11 | 1991-11-21 | Nippon Oil Company, Limited | Procédé de production de matériau composite de carbone/carbone |
EP0457510A3 (en) * | 1990-05-11 | 1993-01-20 | Nippon Oil Co., Ltd. | Process for preparing carbon/carbon composite |
EP0457509A3 (en) * | 1990-05-11 | 1993-01-20 | Nippon Oil Co., Ltd. | Process for preparing carbon/carbon composite |
WO1993016013A1 (fr) * | 1992-02-06 | 1993-08-19 | Dunlop Limited | Materiau composite au carbone-carbone |
US9550701B2 (en) | 2013-07-25 | 2017-01-24 | Honeywell International Inc. | Carbon-carbon composites including isotropic carbon encapsulating layer and methods of forming the same |
Also Published As
Publication number | Publication date |
---|---|
CA1255544A (fr) | 1989-06-13 |
JPS636115A (ja) | 1988-01-12 |
AU7458587A (en) | 1988-01-07 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US3837904A (en) | A method of sizing carbon fibers | |
US4321298A (en) | Carbon fabrics sequentially resin coated with (1) a metal-containing composition and (2) a boron-containing composition are laminated and carbonized | |
CA1157603A (fr) | Materiau de friction, sa production et son emploi dans des elements de friction | |
US5382392A (en) | Process for fabrication of carbon fiber-reinforced carbon composite material | |
US4080417A (en) | Process for producing carbon fibers having excellent properties | |
US4101354A (en) | Coating for fibrous carbon material in boron containing composites | |
CA1255544A (fr) | Tenacite des fibres de carbone | |
US4100314A (en) | Method for increasing the strength and density of carbonaceous products | |
US4024227A (en) | Process for producing carbon fibers having excellent properties | |
US3607672A (en) | Method for producing febrous carbon structures | |
US4581437A (en) | Method of treating filaments of poly(p-phenylene-trans-benzobisthiazole) or poly(p-phenylene-cis-benzobisoxazole) | |
JP2664047B2 (ja) | 炭素繊維強化炭素複合材料の製造方法 | |
DE69222817T2 (de) | Verfahren zur Herstellung von Kohlenstofffasern auf Pechbasis | |
JP3520530B2 (ja) | 炭素繊維強化炭素複合材および摺動材 | |
GB2151221A (en) | High strength oxidation resistant carbon/carbon composites | |
US4039341A (en) | Production of carbon articles | |
GB2112827A (en) | Carbon fiber materials | |
US4164601A (en) | Coating for fibrous carbon material in boron containing composites | |
US4776995A (en) | Method of making a structure | |
EP0213711A2 (fr) | Traitement de surface de fibres de carbone à base de brai | |
JP3031626B2 (ja) | 粘結剤,含浸剤及びこれらの製造方法 | |
US6291537B1 (en) | Encapsulation of oxidants for pitch stabilization | |
US4503215A (en) | Furfural or furfural alchol impregnants for carbonacious bodies | |
US4425316A (en) | Densified carbonaceous bodies with improved surface finishes | |
JP2864304B2 (ja) | ブレーキ摺動部 |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
|
AK | Designated contracting states |
Kind code of ref document: A1 Designated state(s): BE DE FR GB IT NL |
|
17P | Request for examination filed |
Effective date: 19880525 |
|
17Q | First examination report despatched |
Effective date: 19890526 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: THE APPLICATION IS DEEMED TO BE WITHDRAWN |
|
18D | Application deemed to be withdrawn |
Effective date: 19891206 |
|
RIN1 | Information on inventor provided before grant (corrected) |
Inventor name: KATZ, MANFRED |