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 PDF

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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Withdrawn
Application number
EP87305466A
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German (de)
English (en)
Inventor
Manfred Katz
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.)
EIDP Inc
Original Assignee
EI Du Pont de Nemours and Co
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 EI Du Pont de Nemours and Co filed Critical EI Du Pont de Nemours and Co
Publication of EP0251596A1 publication Critical patent/EP0251596A1/fr
Withdrawn legal-status Critical Current

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Classifications

    • DTEXTILES; PAPER
    • D01NATURAL OR MAN-MADE THREADS OR FIBRES; SPINNING
    • D01FCHEMICAL FEATURES IN THE MANUFACTURE OF ARTIFICIAL FILAMENTS, THREADS, FIBRES, BRISTLES OR RIBBONS; APPARATUS SPECIALLY ADAPTED FOR THE MANUFACTURE OF CARBON FILAMENTS
    • D01F11/00Chemical after-treatment of artificial filaments or the like during manufacture
    • D01F11/10Chemical after-treatment of artificial filaments or the like during manufacture of carbon
    • D01F11/14Chemical 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)
EP87305466A 1986-06-25 1987-06-19 Amélioration de la résistance à la traction de fibres de carbone Withdrawn EP0251596A1 (fr)

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)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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

Patent Citations (2)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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

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