EP0154175A2 - Procédé de stabilisation rapide pour précurseurs de fibres de carbone - Google Patents

Procédé de stabilisation rapide pour précurseurs de fibres de carbone Download PDF

Info

Publication number
EP0154175A2
EP0154175A2 EP85101144A EP85101144A EP0154175A2 EP 0154175 A2 EP0154175 A2 EP 0154175A2 EP 85101144 A EP85101144 A EP 85101144A EP 85101144 A EP85101144 A EP 85101144A EP 0154175 A2 EP0154175 A2 EP 0154175A2
Authority
EP
European Patent Office
Prior art keywords
stage
fiber
temperature
polymer
oxidation
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.)
Ceased
Application number
EP85101144A
Other languages
German (de)
English (en)
Other versions
EP0154175A3 (fr
Inventor
Edward Mallary Mchenry
Francesco Demaria
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.)
Wyeth Holdings LLC
Original Assignee
American Cyanamid 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 American Cyanamid Co filed Critical American Cyanamid Co
Publication of EP0154175A2 publication Critical patent/EP0154175A2/fr
Publication of EP0154175A3 publication Critical patent/EP0154175A3/fr
Ceased legal-status Critical Current

Links

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
    • D01F9/00Artificial filaments or the like of other substances; Manufacture thereof; Apparatus specially adapted for the manufacture of carbon filaments
    • D01F9/08Artificial filaments or the like of other substances; Manufacture thereof; Apparatus specially adapted for the manufacture of carbon filaments of inorganic material
    • D01F9/12Carbon filaments; Apparatus specially adapted for the manufacture thereof
    • D01F9/14Carbon filaments; Apparatus specially adapted for the manufacture thereof by decomposition of organic filaments
    • D01F9/20Carbon filaments; Apparatus specially adapted for the manufacture thereof by decomposition of organic filaments from polyaddition, polycondensation or polymerisation products
    • D01F9/21Carbon 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
    • D01F9/22Carbon 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
    • D01F9/225Carbon 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 from stabilised polyacrylonitriles

Definitions

  • acrylonitrile polymer carbon precursor fibers are subjected to low temperatures i.e. 220-250 o c for relatively long periods of time in order to avoid too rapid an exotherm which leads to breakage of the tows.
  • U.S. Patent 3,412,062 is representative of the prior art which teaches the stabilization of such fibers for 24-50 hours at 220°C while preventing the fibers from shrinking more than 12% by applying tension thereto. In some instances, the fiber is allowed to stretch up to 36%.
  • the process of the present invention involves the stabilization of carbon fiber precursors in at least two stages.
  • the first stage is conducted at a temperature at which the maximum plasticity of the polymer is attained while stretching the fiber from about 10-50%.
  • the second stage is conducted, while the fiber is under tension, at a temperature ranging from about 200-300 o C, but higher than that of the first stage. Total residence time in both stages is 10-60 minutes.
  • the process of the present invention is directed to the production of a carbon fiber precursor wherein an acrylonitrile polymer fiber is subjected to oxidation by heating said fiber in an oxidizing atmosphere for a time sufficient to permit substantially complete permeation of oxygen throughout the fiber structure.
  • the processes encompasses the improvement which comprises conducting the stabilization (oxidation) in at least two stages, the first stage at a temperature substantially at which the maximum plasticity of the polymer is attained and while stretching the fiber from about 10-50%.
  • the second stage is conducted while the fiber is maintained under a tension of from about 0.01-0.2 g/d and at a temperature ranging from about 200-300 o C but in any event, higher than the temperature employed in the first stage.
  • the total residence time of the fiber in the oxidation procedure ranges from about 15-60 minutes.
  • the tension of the fiber is maintained as in the second stage and at a temperature ranging from about 200-300°C, but at least equal to that of the second stage.
  • the acrylonitrile fibers used herein are produced from polymers well known to those skilled in the art. Although polyacrylonitrile per se can be employed, the polymer is usually a copolymer or terpolymer of at least about 85 weight percent of acrylonitrile and the remainder a comonomer or comonomers copolymerizable with the acrylonitrile.
  • Useful comonomers include methyl methacrylate, acrylic acid, methacrylic acid, methylacrylate, acrylamide, .6-hydroxypropyl acrylate and the like.
  • the polymer fiber is heated substantially to its maximum plasticity.
  • the temperature at which the polymer exhibits its maximum plasticity is, of course, different for each polymeric system undergoing stabilization. Such temperature can be ascertained by testing of the polymer beforehand to determine at what temperature maximum plasticity is achieved.
  • said temperature usually ranges from about 200-275°C, generally from about 240-260°C, and it is to this temperature most polymers must be heated in the first stage of the novel process set forth herein.
  • the polymer is stretched from about 10-50%, preferably from about 20-30% during the first stage heat treatment.
  • the oxidation may be conducted in any oxygen containing media with air being preferred. Extraneous oxygen may be added, if desired.
  • the fiber from the first oxidation stage is heated in the second stage to a temperature ranging from about 200-300°C, preferably from about 220-270°C, but higher than that temperature employed in the first stage.
  • the total residence time of the polymer fiber in the stages of the oxidation treatment ranges from about 15-60 minutes, preferably 20-45 minutes.
  • the residence time of the fiber in the second stage should be at least about twice that of the fiber in the first stage.
  • the residence time of the third stage should be about equal to that of the second stage, the second stage again being at least about twice that of the first stage.
  • the stabilized polymer fiber is recovered from the stabilization treatment, it can then be carbonized in the usual manner i.e. by heating to about 700-1200°C in an inert atmosphere.
  • the carbonized fiber can then be further treated i.e. graphitized, by heating to a temperature of about 1200-3000°C, again under inert conditions, such as taught in U.S. Patent 4,411,110, incorporated herein by reference.
  • Run B utilizing temperatures below those of Run A, i.e. those normally employed in carbon fiber precursor stabilization, requires 2 hours of total residence time to achieve a stabilized fiber having properties substantially equivalent to those of the fiber resulting from Run A.
  • Run C shows, that when utilizing temperatures similar to those of Run B while stretching in accordance with Run A, the tow breaks and no useful fiber results.
  • a precursor fiber tow containing 3,000, 1.3 denier filaments of the polymer of Example 1 is subjected to stabilization according to the conditions set forth in Table II, below (Runs E, F, H and I). Comparative runs utilizing conditions outside the scope of the process of the present invention, (Runs D and G) and other, commercially available, carbon fiber precursors (Runs H and I) are also shown.
  • the stabilized fibers are subsequently carbonized by passing the fibers through a detarring furnace at a temperature of 600°C while the fiber is stretched 4%.
  • the tow is then exposed to a graphtizing temperature of 1250°C for 30 seconds while relaxing 5%. Carbon fiber properties are also shown in Table II.
  • Runs E and F of Table II A comparison of Runs E and F of Table II with Run D clearly shows that the process of the present invention (Runs E and F) produce carbon fibers having properties at least equivalent to, if not superior to, those using the lower stabilization temperatures of the prior art procedures (Run D).
  • Run H l results in a carbon fiber at least as good as the prior art process, Run G l .
  • Run 1 2 using the present process, provided a very poor carbon fiber, probably because the fiber was damaged during stabilization by the temperatures employed. Since the exact structural and chemical nature of the precursor fibers of Run 1 2 is not known, further discussion of why the polymer failed is pure -speculation.
  • Example 1 Following the procedure of Example 1 (Run A) except that the polymer comprises 91.2% acrylonitrile, 4.8% meth- ylmethylacrylate, 2.0% methacrylic acid and 2.0% -hydroxypropylacrylate, similar results are achieved.
  • the polymer is subjected to stabilization in accordance with the conditions set forth in Table III, below.
  • the stabilized fiber is subsequently carbonized by passing the fiber through a detarring furnace at a temperature of 600°C for 30 seconds while the fiber is stretched 4%, and then graphitized by passing the carbonized fiber at 1350°C for 30 seconds while relaxing 5%.
  • the resultant carbon fiber properties are also shown in Table III.

Landscapes

  • Chemical & Material Sciences (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • General Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Textile Engineering (AREA)
  • Inorganic Fibers (AREA)
EP85101144A 1984-03-07 1985-02-04 Procédé de stabilisation rapide pour précurseurs de fibres de carbone Ceased EP0154175A3 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US58710084A 1984-03-07 1984-03-07
US587100 1984-03-07

Publications (2)

Publication Number Publication Date
EP0154175A2 true EP0154175A2 (fr) 1985-09-11
EP0154175A3 EP0154175A3 (fr) 1989-05-03

Family

ID=24348348

Family Applications (1)

Application Number Title Priority Date Filing Date
EP85101144A Ceased EP0154175A3 (fr) 1984-03-07 1985-02-04 Procédé de stabilisation rapide pour précurseurs de fibres de carbone

Country Status (2)

Country Link
EP (1) EP0154175A3 (fr)
JP (1) JPS60209019A (fr)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP6998923B2 (ja) * 2019-09-19 2022-01-18 株式会社豊田中央研究所 耐炎化繊維、その製造方法、及び炭素繊維の製造方法
JP7166233B2 (ja) * 2019-09-19 2022-11-07 株式会社豊田中央研究所 耐炎化繊維、その製造方法、及び炭素繊維の製造方法

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4100004A (en) * 1976-05-11 1978-07-11 Securicum S.A. Method of making carbon fibers and resin-impregnated carbon fibers
GB2014971A (en) * 1977-12-14 1979-09-05 Securicum Sa Carbon Fibre
GB2084975A (en) * 1980-10-02 1982-04-21 Fiber Materials Carbon fibres
EP0066389A2 (fr) * 1981-05-15 1982-12-08 Monsanto Company Stabilisation thermique de fibres de copolymères d'acrylonitrile

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4100004A (en) * 1976-05-11 1978-07-11 Securicum S.A. Method of making carbon fibers and resin-impregnated carbon fibers
GB2014971A (en) * 1977-12-14 1979-09-05 Securicum Sa Carbon Fibre
GB2084975A (en) * 1980-10-02 1982-04-21 Fiber Materials Carbon fibres
EP0066389A2 (fr) * 1981-05-15 1982-12-08 Monsanto Company Stabilisation thermique de fibres de copolymères d'acrylonitrile

Also Published As

Publication number Publication date
EP0154175A3 (fr) 1989-05-03
JPS60209019A (ja) 1985-10-21

Similar Documents

Publication Publication Date Title
US4069297A (en) Process for producing carbon fibers
Frank et al. Carbon fibers: precursors, manufacturing, and properties
US3539295A (en) Thermal stabilization and carbonization of acrylic fibrous materials
US4080417A (en) Process for producing carbon fibers having excellent properties
US4113847A (en) Process for producing carbon fibers
US5051216A (en) Process for producing carbon fibers of high tenacity and modulus of elasticity
US5078926A (en) Rapid stabilization process for carbon fiber precursors
JPS6328132B2 (fr)
US3556729A (en) Process for oxidizing and carbonizing acrylic fibers
WO2000000683A1 (fr) Procede de preparation de fibres de carbone
EP0255109A2 (fr) Procédé de fabrication de fibres acryliques à hautes caractéristiques
US4397831A (en) Production of carbon fibers from acrylonitrile based fibers
EP0154175A2 (fr) Procédé de stabilisation rapide pour précurseurs de fibres de carbone
US4452601A (en) Process for the thermal stabilization of acrylic fibers and films
EP0169023A2 (fr) Méthode de production de fibres de carbone à base de brai
US4295844A (en) Process for the thermal stabilization of acrylic fibers
US3988426A (en) Method for producing carbon fibers
JPS58144128A (ja) 高性能炭素繊維の製法
US4154807A (en) Process for the production of carbon fibers
EP0242401B1 (fr) Procede de production de fibres de carbone
US5292408A (en) Pitch-based high-modulus carbon fibers and method of producing same
US4079122A (en) Preparation of carbon fibres
JPS6127487B2 (fr)
US3399260A (en) Production of acrylonitrile polymer fibers
JPS6250574B2 (fr)

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

Designated state(s): BE DE FR GB SE

PUAL Search report despatched

Free format text: ORIGINAL CODE: 0009013

AK Designated contracting states

Kind code of ref document: A3

Designated state(s): BE DE FR GB SE

17P Request for examination filed

Effective date: 19890721

17Q First examination report despatched

Effective date: 19900213

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE APPLICATION HAS BEEN REFUSED

18R Application refused

Effective date: 19911024

RIN1 Information on inventor provided before grant (corrected)

Inventor name: DEMARIA, FRANCESCO

Inventor name: MCHENRY, EDWARD MALLARY