US3656882A - ACRYLIC FIBER STABILIZATION CATALYZED BY Co(II) AND Ce(III) CATIONS - Google Patents
ACRYLIC FIBER STABILIZATION CATALYZED BY Co(II) AND Ce(III) CATIONS Download PDFInfo
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- US3656882A US3656882A US17965A US3656882DA US3656882A US 3656882 A US3656882 A US 3656882A US 17965 A US17965 A US 17965A US 3656882D A US3656882D A US 3656882DA US 3656882 A US3656882 A US 3656882A
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- fibrous material
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- per cent
- metallic cations
- acrylic fibrous
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Links
- 230000006641 stabilisation Effects 0.000 title claims abstract description 30
- 238000011105 stabilization Methods 0.000 title claims abstract description 30
- XLJKHNWPARRRJB-UHFFFAOYSA-N cobalt(2+) Chemical compound [Co+2] XLJKHNWPARRRJB-UHFFFAOYSA-N 0.000 title claims abstract description 5
- 150000001768 cations Chemical class 0.000 title description 10
- 229920002972 Acrylic fiber Polymers 0.000 title description 5
- 239000002657 fibrous material Substances 0.000 claims abstract description 116
- NIXOWILDQLNWCW-UHFFFAOYSA-N acrylic acid group Chemical group C(C=C)(=O)O NIXOWILDQLNWCW-UHFFFAOYSA-N 0.000 claims abstract description 82
- 150000001457 metallic cations Chemical class 0.000 claims abstract description 59
- 238000000034 method Methods 0.000 claims abstract description 50
- 238000010438 heat treatment Methods 0.000 claims abstract description 11
- 230000001590 oxidative effect Effects 0.000 claims abstract description 10
- 230000003197 catalytic effect Effects 0.000 claims abstract description 9
- 239000000243 solution Substances 0.000 claims description 34
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 claims description 27
- 239000001301 oxygen Substances 0.000 claims description 27
- 229910052760 oxygen Inorganic materials 0.000 claims description 27
- 238000006243 chemical reaction Methods 0.000 claims description 23
- 229920002239 polyacrylonitrile Polymers 0.000 claims description 14
- NLHHRLWOUZZQLW-UHFFFAOYSA-N Acrylonitrile Chemical group C=CC#N NLHHRLWOUZZQLW-UHFFFAOYSA-N 0.000 claims description 12
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 12
- 239000007864 aqueous solution Substances 0.000 claims description 12
- 229910052799 carbon Inorganic materials 0.000 claims description 11
- 229920001577 copolymer Polymers 0.000 claims description 11
- 239000002904 solvent Substances 0.000 claims description 11
- 238000001035 drying Methods 0.000 claims description 9
- GVPFVAHMJGGAJG-UHFFFAOYSA-L cobalt dichloride Chemical compound [Cl-].[Cl-].[Co+2] GVPFVAHMJGGAJG-UHFFFAOYSA-L 0.000 claims description 7
- 229940097267 cobaltous chloride Drugs 0.000 claims description 7
- 229910004664 Cerium(III) chloride Inorganic materials 0.000 claims description 6
- VYLVYHXQOHJDJL-UHFFFAOYSA-K cerium trichloride Chemical compound Cl[Ce](Cl)Cl VYLVYHXQOHJDJL-UHFFFAOYSA-K 0.000 claims description 6
- 230000002708 enhancing effect Effects 0.000 claims description 3
- 239000000835 fiber Substances 0.000 abstract description 11
- 238000004132 cross linking Methods 0.000 abstract description 8
- 229920000642 polymer Polymers 0.000 abstract description 4
- 230000009970 fire resistant effect Effects 0.000 abstract description 2
- 230000001737 promoting effect Effects 0.000 abstract description 2
- 239000004753 textile Substances 0.000 abstract description 2
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 10
- ZMXDDKWLCZADIW-UHFFFAOYSA-N N,N-Dimethylformamide Chemical compound CN(C)C=O ZMXDDKWLCZADIW-UHFFFAOYSA-N 0.000 description 9
- 239000007858 starting material Substances 0.000 description 8
- 150000001875 compounds Chemical class 0.000 description 7
- 238000004458 analytical method Methods 0.000 description 5
- 229910052757 nitrogen Inorganic materials 0.000 description 5
- 238000011282 treatment Methods 0.000 description 5
- MYMOFIZGZYHOMD-UHFFFAOYSA-N Dioxygen Chemical compound O=O MYMOFIZGZYHOMD-UHFFFAOYSA-N 0.000 description 3
- 229910001882 dioxygen Inorganic materials 0.000 description 3
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 3
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 2
- BAPJBEWLBFYGME-UHFFFAOYSA-N Methyl acrylate Chemical compound COC(=O)C=C BAPJBEWLBFYGME-UHFFFAOYSA-N 0.000 description 2
- PPBRXRYQALVLMV-UHFFFAOYSA-N Styrene Chemical compound C=CC1=CC=CC=C1 PPBRXRYQALVLMV-UHFFFAOYSA-N 0.000 description 2
- 230000002411 adverse Effects 0.000 description 2
- 229910003481 amorphous carbon Inorganic materials 0.000 description 2
- 238000003763 carbonization Methods 0.000 description 2
- UFMZWBIQTDUYBN-UHFFFAOYSA-N cobalt dinitrate Chemical compound [Co+2].[O-][N+]([O-])=O.[O-][N+]([O-])=O UFMZWBIQTDUYBN-UHFFFAOYSA-N 0.000 description 2
- 238000009792 diffusion process Methods 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 229920000058 polyacrylate Polymers 0.000 description 2
- 238000007363 ring formation reaction Methods 0.000 description 2
- OEPOKWHJYJXUGD-UHFFFAOYSA-N 2-(3-phenylmethoxyphenyl)-1,3-thiazole-4-carbaldehyde Chemical compound O=CC1=CSC(C=2C=C(OCC=3C=CC=CC=3)C=CC=2)=N1 OEPOKWHJYJXUGD-UHFFFAOYSA-N 0.000 description 1
- KGIGUEBEKRSTEW-UHFFFAOYSA-N 2-vinylpyridine Chemical compound C=CC1=CC=CC=N1 KGIGUEBEKRSTEW-UHFFFAOYSA-N 0.000 description 1
- 101100264195 Caenorhabditis elegans app-1 gene Proteins 0.000 description 1
- 229920000049 Carbon (fiber) Polymers 0.000 description 1
- 229920013683 Celanese Polymers 0.000 description 1
- -1 Co(II) metallic cations Chemical class 0.000 description 1
- 241001522296 Erithacus rubecula Species 0.000 description 1
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 1
- VVQNEPGJFQJSBK-UHFFFAOYSA-N Methyl methacrylate Chemical compound COC(=O)C(C)=C VVQNEPGJFQJSBK-UHFFFAOYSA-N 0.000 description 1
- FXHOOIRPVKKKFG-UHFFFAOYSA-N N,N-Dimethylacetamide Chemical compound CN(C)C(C)=O FXHOOIRPVKKKFG-UHFFFAOYSA-N 0.000 description 1
- XTXRWKRVRITETP-UHFFFAOYSA-N Vinyl acetate Chemical compound CC(=O)OC=C XTXRWKRVRITETP-UHFFFAOYSA-N 0.000 description 1
- BZHJMEDXRYGGRV-UHFFFAOYSA-N Vinyl chloride Chemical compound ClC=C BZHJMEDXRYGGRV-UHFFFAOYSA-N 0.000 description 1
- 238000002441 X-ray diffraction Methods 0.000 description 1
- 230000001133 acceleration Effects 0.000 description 1
- 229910052786 argon Inorganic materials 0.000 description 1
- 230000004888 barrier function Effects 0.000 description 1
- 239000011230 binding agent Substances 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 239000004917 carbon fiber Substances 0.000 description 1
- 230000015556 catabolic process Effects 0.000 description 1
- HSJPMRKMPBAUAU-UHFFFAOYSA-N cerium(3+);trinitrate Chemical compound [Ce+3].[O-][N+]([O-])=O.[O-][N+]([O-])=O.[O-][N+]([O-])=O HSJPMRKMPBAUAU-UHFFFAOYSA-N 0.000 description 1
- OZECDDHOAMNMQI-UHFFFAOYSA-H cerium(3+);trisulfate Chemical compound [Ce+3].[Ce+3].[O-]S([O-])(=O)=O.[O-]S([O-])(=O)=O.[O-]S([O-])(=O)=O OZECDDHOAMNMQI-UHFFFAOYSA-H 0.000 description 1
- 229910000333 cerium(III) sulfate Inorganic materials 0.000 description 1
- 230000015271 coagulation Effects 0.000 description 1
- 238000005345 coagulation Methods 0.000 description 1
- 239000011248 coating agent Substances 0.000 description 1
- 238000000576 coating method Methods 0.000 description 1
- KTVIXTQDYHMGHF-UHFFFAOYSA-L cobalt(2+) sulfate Chemical compound [Co+2].[O-]S([O-])(=O)=O KTVIXTQDYHMGHF-UHFFFAOYSA-L 0.000 description 1
- ZOTKGJBKKKVBJZ-UHFFFAOYSA-L cobalt(2+);carbonate Chemical compound [Co+2].[O-]C([O-])=O ZOTKGJBKKKVBJZ-UHFFFAOYSA-L 0.000 description 1
- QAHREYKOYSIQPH-UHFFFAOYSA-L cobalt(II) acetate Chemical compound [Co+2].CC([O-])=O.CC([O-])=O QAHREYKOYSIQPH-UHFFFAOYSA-L 0.000 description 1
- 229910000001 cobalt(II) carbonate Inorganic materials 0.000 description 1
- BZRRQSJJPUGBAA-UHFFFAOYSA-L cobalt(ii) bromide Chemical compound Br[Co]Br BZRRQSJJPUGBAA-UHFFFAOYSA-L 0.000 description 1
- 229940045032 cobaltous nitrate Drugs 0.000 description 1
- 238000005056 compaction Methods 0.000 description 1
- 239000002131 composite material Substances 0.000 description 1
- 238000007796 conventional method Methods 0.000 description 1
- 238000006731 degradation reaction Methods 0.000 description 1
- 238000004090 dissolution Methods 0.000 description 1
- 238000000578 dry spinning Methods 0.000 description 1
- 239000004744 fabric Substances 0.000 description 1
- 229910002804 graphite Inorganic materials 0.000 description 1
- 239000010439 graphite Substances 0.000 description 1
- 238000005087 graphitization Methods 0.000 description 1
- 230000017525 heat dissipation Effects 0.000 description 1
- 239000001257 hydrogen Substances 0.000 description 1
- 229910052739 hydrogen Inorganic materials 0.000 description 1
- 230000001771 impaired effect Effects 0.000 description 1
- 239000000543 intermediate Substances 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 239000011159 matrix material Substances 0.000 description 1
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 239000000178 monomer Substances 0.000 description 1
- 125000002560 nitrile group Chemical group 0.000 description 1
- 239000002243 precursor Substances 0.000 description 1
- 230000003014 reinforcing effect Effects 0.000 description 1
- 238000009987 spinning Methods 0.000 description 1
- 238000005507 spraying Methods 0.000 description 1
- 238000002166 wet spinning Methods 0.000 description 1
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
- D01F9/20—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
- D01F9/225—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 from stabilised polyacrylonitriles
-
- D—TEXTILES; PAPER
- D06—TREATMENT OF TEXTILES OR THE LIKE; LAUNDERING; FLEXIBLE MATERIALS NOT OTHERWISE PROVIDED FOR
- D06M—TREATMENT, NOT PROVIDED FOR ELSEWHERE IN CLASS D06, OF FIBRES, THREADS, YARNS, FABRICS, FEATHERS OR FIBROUS GOODS MADE FROM SUCH MATERIALS
- D06M11/00—Treating fibres, threads, yarns, fabrics or fibrous goods made from such materials, with inorganic substances or complexes thereof; Such treatment combined with mechanical treatment, e.g. mercerising
- D06M11/32—Treating fibres, threads, yarns, fabrics or fibrous goods made from such materials, with inorganic substances or complexes thereof; Such treatment combined with mechanical treatment, e.g. mercerising with oxygen, ozone, ozonides, oxides, hydroxides or percompounds; Salts derived from anions with an amphoteric element-oxygen bond
- D06M11/34—Treating fibres, threads, yarns, fabrics or fibrous goods made from such materials, with inorganic substances or complexes thereof; Such treatment combined with mechanical treatment, e.g. mercerising with oxygen, ozone, ozonides, oxides, hydroxides or percompounds; Salts derived from anions with an amphoteric element-oxygen bond with oxygen, ozone or ozonides
Definitions
- a process is provided wherein the thermal stabilization of an acrylic fibrous material is accelerated by heating in an oxygencontaining atmosphere in the presence of a catalytic quantity of Co(ll) and Ce(lll) metallic cations which have been found capable of promoting the oxidative cross-linking of adjoining polymer molecules.
- the resulting stabilized fibrous materials are non-buming when subjected to an ordinary match flame, and may be utilized as fire resistant textile fibers, or optionally converted to a carbonized fibrous material by heating in an inert atmosphere at a more highly elevated temperature.
- the stabilization reaction must by necessity be conducted at relatively low temperatures i.e. below about 300 C.), since the cyclization reaction is exothermic in nature and must be controlled if the original fibrous configuration of the material undergoing stabilization is'to'be preserved. Accordingly the stabilization reaction tends to be time consuming, and economically demanding because of low productivity necessitated by the excessive time requirements.
- Prior processes proposed to shorten the period required by the stabilization reaction include that disclosed in U.S. Pat. No. 3,4l6,874.
- While stabilized acrylic fibrous materials may be used directly in applications where a non-burning fiber is required, demands for the same have been increasingly presented by manufacturers of carbonized fibrous materials.
- Carbonized fibrous materials are commonly formed by heating a stabilized acrylic fibrous material in an inert atmosphere, such as nitrogen or argon, at a more highly elevated temperature. During the carbonization reaction elements present in the fiber such as nitrogen, oxygen, and hydrogen are substantially expelled. Accordingly, the term carbonized" fibrous material as used in the art commonly designates a fibrous material consisting of at least about 90 per cent carbon by weight, and generally at least about 95 per cent carbon by weight.
- the carbonized fibrous material may or may not contain graphitic carbon as determined by the characteristic x-ray diffraction pattern of graphite. See, for instance, commonly assigned U.S. Ser. No. 777,275, filed Nov. 20, 1968, of Charles M. Clarke for a preferred procedure for forming carbonized and graphitized fibrous materials from a stabilized acrylic fibrous material.
- An alternate approach for forming carbonized fibers directly from acrylic fibers while coated with a refractory barrier coating is proposed in U.S. Pat. Nos. 3,242,000 and 3,281,261 to Lynch.
- an improved process for the stabilization of an acrylic fibrous material selected from the group consisting of an acrylonitrile homopolymer and acrylonitrile copolymers containing at least about 85 mol per cent of acrylonitrile units and up to about mol per cent of one or more monovinyl units copolymerized-therewith comprises:
- the stabilized products formed in accordance with the present process commonly exhibit a bound oxygen content of at least about 7 per cent by weight, and a carbon content of about to 'per cent by weight.
- the acrylic fibrous materials undergoing stabilization in the present process may be formed by conventional solution spinning techniques (i.e. may be dry spun or wet spun), and are commonly drawn to increase their orientation.
- dry spinning is commonly conducted by dissolving the polymer in an appropriate solvent, such as N,N- dimethyl formamide or N,N-dimethyl acetamide, and passing the solution through an opening of predetermined shape into an evaporative atmosphere (e.g. nitrogen) in which much of the solvent is evaporated.
- evaporative atmosphere e.g. nitrogen
- Wet spinning is commonly conducted by passing a solution of the polymer through an opening of predetermined shape into an aqueous coagulation bath.
- the acrylic polymer utilized as the starting material is formed primarily of recurring acrylonitrile units.
- the acrylic polymer should generally contain not less than about mol per cent of acrylonitrile units and not more than about 15 mol per cent of units derived from a monovinyl compound which is copolymerizable with acrylonitrile such as styrene, methyl acrylate, methyl methacrylate, vinyl acetate, vinyl chloride, vinylidene chloride, vinyl pyridine, and the like, or a plurality of such monomers.
- the preferred acrylic fibrous material is an acrylonitrile homopolymer.
- Preferred acrylonitrile copolymers contain at least about mol per cent of acrylonitrile units and up to about 5 mol per cent of one or more monovinyl units copolymerized therewith.
- the acrylic fibrous materials are provided as continuous lengths and may be in a variety of physical configurations.
- the acrylic fibrous materials may be present in the form of continuous lengths of multifilament yarns, tows, tapes,
- a twist may be imparted to the same to improve the handling characteristics. For instance, a twist of about 0.l to 5 tpi,
- false twist may be used instead of or in addition to a real twist.
- the starting material may be drawn in accordance with conventional techniques in order to improve its orientation.
- the starting material may be drawn by stretching while in contact with a hot shoe at a temperature of about to C. Additional representative drawing techniques are disclosed in U.S. Pat. Nos. 2,455,173; 2,948,581; and 3,122,412. It is recommended that the acrylic fibrous materials selected for use in the process be drawn to a single filament tenacity of at least about 3 grams per denier. If desired, however, the starting material may be more highly oriented, e.g. drawn up to a single filament tenacity of about 7.5 to 8 grams per denier, or more.
- the fibrous material Prior to heating the acrylic fibrous material in an oxygencontaining atmosphere to accomplish the desired stabilization (as described hereafter), the fibrous material is provided in intimate association with a catalytic quantity up to about 0.5 per cent by weight based upon the weight of the fibrous material of Co(ll) or Ce(lll) metallic cations, or mixtures of the same.
- the source of the metallic cations may be varied.
- Illustrative examples of compounds capable of yielding the desired Co(II) metallic cations are as follows: cobaltous chloride [CoCl '6 H O], cobaltous nitrate [Co(NO "l-I O], cobaltous carbonate [2CoCO '3 Co(OH) cobaltous sulfate [CoSO 'H O], cobaltous bromide [CoBr '6 H and cobaltous acetate [Co(C H O 4H Oa)
- the preferred source of Co (II) metallic cations is cobaltous chloride [CoCl '6 H O].
- Illustrative examples of compounds capable of yielding the desired Ce(lll) metallic cations are as follows: cerous chloride [CeClJ H O], cerous nitrate [Ce(NO -6H O], and cerous sulfate [Ce(SO '8I-I O].
- the preferred source of Ce(lll) metallic cations is cerous chloride [CeCl '7I-I O].
- the intimate association of the acrylic fibrous material and the metallic cations is preferably accomplished by contacting the fibrous material with a solution containing the Co(II) or Ce(III) cations dissolved therein, and subsequently drying the fibrous material whereby the solvent of the solution in contact with the acrylic fibrous material is substantially expelled.
- the solution from which the metallic cations are applied is preferably aqueous in nature.
- Solvents other than water, which are capable of dissolving the source compounds for the Co(ll) and Ce(lll) cations, may likewise be selected provided the solvents do not adversely influence the properties of the acrylic fibrous material.
- compounds capable ofyielding the Co(ll) and Ce(lll) metallic cations upon dissolution are provided as aqueous solutions ofabout 0.0001 to 10 molarity.
- the temperature of the solution containing the metallic cations while contacted with the acrylic fibrous material may be from below ambient up to below that temperature at which the properties of the acrylic fibrous material are adversely influenced.
- the acrylic fibrous material is contacted with an aqueous solution containing the Co(ll) or Ce(lll) metallic cations which is at a temperature of about 10 to 95 C.
- the solution is conveniently providcd at ambient temperature (i.e. at about C.).
- contact is made by immersing the acrylic fibrous material in a vessel containing a solution of the metallic cations.
- contact may be made by spraying the acrylic fibrous material with a solution of the metallic cations.
- the duration of the period of contact between the acrylic fibrous material and the solution is not critical provided the requisite catalytic quantity ofthe metallic cations up to about 0.5 per cent by weight based upon the weight of the acrylic fibrous material is ultimately provided in intimate association with the fibrous material upon drying.
- the quantity of the metallic cations, provided in intimate association with the acrylic fibrous material may be from about 0.000l to 0.5 per cent by weight based upon the weight of the dried acrylic fibrous material.
- the duration of the period of contact will be influenced to some degree by the metallic cations concentration of the solution, the temperature of the solution, the degree of compaction of the acrylic fibrous material undergoing treatment, and the denier of the acrylic fibrous material. Contact times of about 5 seconds to 48 hours, or more, may be selected. A greater diffusion ofthe metallic cations into the acrylic fibrous material occurs with longer residence times.
- a continuous length of the acrylic fibrous material may be wound upon a support and statically contacted with the solution containing the metallic cations. Alternatively, a continuous length of the acrylic fibrous material may be continuously passed in the direction of its length through a vessel or zone in which the solution is provided.
- the drying of the fibrous material following contact with the solution containing the metallic cations may be conducted in any convenient manner.
- the fibrous material may be simply exposed to ambient conditions until the solvent adhering thereto is substantially evaporated.
- the drying step can, of course, be expedited by exposure to a circulating gaseous atmosphere provided at an elevated-temperature, as will be apparent to those skilled in the art. If desired, the drying may be conveniently conducted in the same zone in which the stabilization reaction is carried out, as described hereafter.
- Upon removal of the solvent a thin catalytic residue of Co(ll) and Ce(lll) metallic cations is deposited upon the fiber surface. Also, internal diffusion of the metallic cations into the fibrous material is achieved.
- the acrylic fibrous material while in intimate association with the metallic cations is next exposed to an oxygen-containing atmosphere at a temperature of about 200 to 290 C. until a stabilized fibrous product is formed.
- the oxygen-containing atmosphere is air.
- Preferred temperatures for the oxygen-containing atmosphere are about 220 to 260 C., and most preferably about 240 to 250 C.
- the acrylic fibrous material may be placed in the oxygen-containing atmosphere while wound upon a support to a limited thickness.
- the acrylic fibrous material while in intimate association with the metallic cations is continuously passed in the direction of its length through the heated oxygen-containing atmosphere.
- a continuous length of the acrylic fibrous material may be passed through a circulating oven or the tube of a muffiefurnace. The speed of passage through the heated oxygen-containing atmosphere will be determined by the size of the heating zone and the desired residence time.
- the period of time required to complete the stabilization reaction within the oxygen-containing atmosphere is generally inversely related to the temperature of the atmosphere, and is also influenced by the denier of the acrylic fibrous material undergoing treatment. Treatment times in the oxygen-containing atmosphere accordingly commonly range from about 30 minutes to hours. Regardless of the stabilization temperature selected within the range of about 200 to 290 C. the intimate presence of the Co(ll) or Ce(IIl) metallic cations as described results in an accelerated oxidative cross-linking reaction for a given temperature.
- the stabilized acrylic fibrous materials formed in accordance with the present process are black in appearance, retain essentially the same fibrous configuration as the starting material, are non-burning when subjected to an ordinary match flame, commonly have a bound oxygen content of at least 7 per cent by weight as determined by the Unterzaucher analysis, and commonly contain from about 50 to 65 per cent carbon by weight.
- the stabilization reaction Since the oxidative-cross linking reaction is accelerated in the present process, one optionally may elect to carry out the stabilization reaction at a less severe temperature than heretofore commonly utilized. Under milder temperature conditions a more uniform stabilized fiber may be achieved in the absence of undue chain degradation.
- the stabilized fibrous material resulting from the stabilization treatment of the present invention is suitable for use in applications where a fire resistance fibrous material is required. For instance, non-burning fabrics may be formed from the same.
- the stabilized acrylic fibrous materials are particularly suited for use as intermediates in the production of carbonized fibrous materials.
- Such amorphous carbon or graphitic carbon fibrous products may be incorporated in a binder or matrix and serve as a reinforcing medium.
- the carbon fiber component may accordingly serve as a light weight load bearing component in high performance composite structures which find particular utility in the aerospace industry.
- a continuous length of a 800 fil dry spun acrylonitrile homopolymer continuous filament yarn having a total denier of 1200 was selected as the starting material.
- the yarn was dry spun from a solution of the same in N,N-dimethyl formamide solvent into an evaporative atmosphere of nitrogen.
- the fibrous material was dry spun as a 40 fil bundle, and plied to form the 800 fil yarn which ex hibited a twist of about 0.5 tpi.
- the yarn was next drawn at a draw ratio of about 5:1 to a single filament tenacity of about 4 grams per denier by stretching while passing over a hot shoe at a temperature of about 160 C. for a residence time of about 0.5 second.
- Four segments of the yarn were wound on four different porous bobbins and were given the following treatments:
- Sample A was designated the control, and was placed in a circulating air oven maintained at 220 C. for 90 minutes. At the end of this period of time a bound oxygen content within the fibrous material of 0.78 per cent by weight as determined by the Unterzaucher analysis was observed.
- Sample B was immersed in a vessel containing a 0.042 Molar aqueous solution of cobaltous chloride [CoCl 6H O] provided at 25 C. for 16 hours, was removed from the vessel, was allowed to dry at ambient conditions, and was placed in a circulating air oven at 220 C. for 90 minutes. At the end of this period of time a bound x e .sqnt t t Z-iLPstEsn by e tta determined by the Unterzaucher analysis was observed.
- Sample C was immersed in a vessel containing a 0.17 Molar aqueous solution of cobaltous chloride [CoCl 6H O] provided at 25 C. for 16 hours, was removed from the vessel, was allowed to dry at ambient condi-. tions, and was placed in a circulating air oven at 220 C. for 90 minutes. At the end of this period of time a bound oxygen content of 3.52 percent by weight as e m ned by theiln ziqsb QBFllL lLWQQWEEl EQ- Sample D was immersed in a vessel containing a 0.07 Molar aqueous solution of cerous chloride [CeCl -7l-l O] provided at 25 C.
- EXAMPLE I This example illustrates the stabilization of an acrylic fibrous material in the presence of Co(ll) metallic cations in accordance with the present invention.
- a continuous length of a 1600 fil dry spun acrylonitrile homopolymer continuous filament yam having a total denier of 1920 is selected as the starting material.
- the yarn is initially dry spun from a solution of the same in N,N-dimethyl formamide solvent into an evaporative atmosphere of nitrogen.
- the yarn is spun as a 40 fil bundle, and plied to form the 1600 fil yarn which exhibits a twist of about 0.5 tpi.
- the yarn is next drawn at a draw ratio of about 5:1 to a single filament tenacity of about 4 grams per denier by stretching while passing over a hot shoe at a temperature of about 160 C. for a resistance time of about 0.5 second.
- a solution containing Co(ll) metallic cations is formed by dissolving cobaltous chloride [CoCl 2'6H O] in water to form a 0.2 Molar solution of the compound.
- the acrylonitrile homopolymer yarn while wound upon a perforated bobbin is immersed for 10 hours in a vessel containing the aqueous solution provided at 25 C., is removed from the vessel, is allowed to dry at ambient conditions (i.e. 25 C.) for l hour, and is placed in a circulating air oven at 245 C. for 3 hours.
- the resulting stabilized yarn retains its original fibrous configuration essentially intact, and is non-burning when subjected to an ordinary match flame.
- the bound oxygen content of the yarn as determined by the Unterzaucher analysis is in excess of 7 per cent by weight, and the carbon content is less than 65 per cent by weight.
- the product is capable of undergoing carbonization and graphitization in accordance with the teachings of commonly assigned U.S. Ser. No. 777,275, filed Nov. 20,1968, of Charles M. Clarke which is herein incorporated by reference.
- Example I is repeated with the exception that the stabilization reaction is catalyzed by Ce(lll) metallic cations rather than Co(ll) metallic cations. More specifically, a solution containing Ce(llI) metallic cations is formed by dissolving cerous chloride [CeCl '7H O] in water to form a 0.2 Molar solution of the compound. The yarn is immersed in this solution as described in Example I. Substantially similar results are achieved.
- An improved process for the stabilization of an acrylic fibrous material selected from the group consisting of an acrylonitrile homopolymer and acrylonitrile copolymers containing at least about mol per cent of acrylonitrile units and up to about 15 mol per cent of one or more monovinyl units copolymerized therewith comprising:
- said acrylic fibrous material is an acrylonitrile copolymer containing at least about 95 mol per cent of acrylonitrile units and up to about mol per cent of one or more monovinyl units copolymerized therewith.
- a process according to claim 1 wherein said metallic cations in intimate association with said acrylic fibrous material are provided in a quantity of about 0.0001 to 0.5 per cent by weight based upon the weight of said acrylic fibrous material.
- An improved process for enhancing the thermal stability of an acrylic fibrous material selected from the group consisting of an acrylonitrile homopolymer and acrylonitrile copolymers containing at least about 85 mol per cent of acrylonitrile units and up to about mol per cent of one or more monovinyl units copolymerized therewith comprising:
- said acrylic fibrous material is an acrylonitrile copolymer containing at least about mol per cent of acrylonitrile units and up to about 5 mol per cent of one or more monovinyl units copolymerized therewith.
- a process according to claim 8 wherein said solution containing said metallic cations contacted with said acrylic fibrous material is an aqueous solution which is at a temperature of about 10 to 95 C.
- a process according to claim 8 wherein said solution containing said metallic cations is an aqueous solution of cobaltous chloride.
- a process according to claim 8 wherein said solution containing said metallic cations is an aqueous solution of cerous chloride.
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- Engineering & Computer Science (AREA)
- Textile Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Chemical Kinetics & Catalysis (AREA)
- General Chemical & Material Sciences (AREA)
- Inorganic Fibers (AREA)
- Artificial Filaments (AREA)
Abstract
Description
Claims (15)
- 2. A process according to claim 1 wherein said acrylic fibrous material is an acrylonitrile homopolymer.
- 3. A process according to claim 1 wherein said acrylic fibrous material is an acrylonitrile copolymer containing at least about 95 mol per cent of acrylonitrile units and up to about 5 mol per cent of one or more monovinyl units copolymerized therewith.
- 4. A process according to claim 1 wherein said acrylic fibrous material has been drawn to a single filament tenacity of at least abOut 3 grams per denier.
- 5. A process according to claim 1 wherein said metallic cations in intimate association with said acrylic fibrous material are provided in a quantity of about 0.0001 to 0.5 per cent by weight based upon the weight of said acrylic fibrous material.
- 6. A process according to claim 1 wherein said metallic cations are Co(II).
- 7. A process according to claim 1 wherein said metallic cations are Ce(III).
- 8. An improved process for enhancing the thermal stability of an acrylic fibrous material selected from the group consisting of an acrylonitrile homopolymer and acrylonitrile copolymers containing at least about 85 mol per cent of acrylonitrile units and up to about 15 mol per cent of one or more monovinyl units copolymerized therewith comprising: a. contacting said acrylic fibrous material with a solution containing metallic cations selected from the group consisting of Co(II) and Ce(III), b. drying said fibrous material whereby the solvent of said solution in contact with said acrylic fibrous material is substantially expelled and said fibrous material is provided in intimate association with a catalytic quantity up to about 0.5 per cent by weight based upon the weight of the acrylic fibrous material of said metallic cations, and c. heating the resulting acrylic fibrous material in an oxygen-containing atmosphere at a temperature of about 200* to 290* C. while in intimate association with said metallic cations until a stabilized product is formed which retains its original fibrous configuration essentially intact, is non-burning when subjected to an ordinary match flame, contains a bound oxygen content of at least about 7 per cent by weight, and a carbon content of about 50 to 65 per cent by weight, with said metallic cations serving to accelerate the oxidative portion of said stabilization reaction.
- 9. A process according to claim 8 wherein said acrylic fibrous material is an acrylonitrile homopolymer.
- 10. A process according to claim 8 wherein said acrylic fibrous material is an acrylonitrile copolymer containing at least about 95 mol per cent of acrylonitrile units and up to about 5 mol per cent of one or more monovinyl units copolymerized therewith.
- 11. A process according to claim 8 wherein said acrylic fibrous material has been drawn to a single filament tenacity of at least about 3 grams per denier.
- 12. A process according to claim 8 wherein said solution containing said metallic cations contacted with said acrylic fibrous material is an aqueous solution which is at a temperature of about 10* to 95* C.
- 13. A process according to claim 8 wherein said solution containing said metallic cations is an aqueous solution of cobaltous chloride.
- 14. A process according to claim 8 wherein said solution containing said metallic cations is an aqueous solution of cerous chloride.
- 15. A process according to claim 8 wherein said drying yields said fibrous material in intimate association with about 0.0001 to 0.5 per cent by weight of said metallic cations based upon the weight of said acrylic fibrous material.
- 16. A process according to claim 8 wherein said resulting acrylic fibrous material is heated in an oxygen-containing atmosphere at a temperature of about 240* to 250* C.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US1796570A | 1970-03-09 | 1970-03-09 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US3656882A true US3656882A (en) | 1972-04-18 |
Family
ID=21785524
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US17965A Expired - Lifetime US3656882A (en) | 1970-03-09 | 1970-03-09 | ACRYLIC FIBER STABILIZATION CATALYZED BY Co(II) AND Ce(III) CATIONS |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US3656882A (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3917776A (en) * | 1970-12-12 | 1975-11-04 | Mitsubishi Rayon Co | Process for producing carbon fiber |
| US3923950A (en) * | 1971-11-18 | 1975-12-02 | Celanese Corp | Production of stabilized acrylic fibers and films |
| US6156287A (en) * | 1995-05-22 | 2000-12-05 | National Science Council | Method for preparing pan-based activated carbon fabrics |
| US20180001244A1 (en) * | 2016-07-01 | 2018-01-04 | Hollingsworth & Vose Company | Multi-layered electret-containing filtration media |
| US12420221B2 (en) | 2016-07-01 | 2025-09-23 | Hollingsworth & Vose Company | Multi-layered electret-containing filtration media |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2799915A (en) * | 1953-03-30 | 1957-07-23 | Johns Manville | Thermal modification of acrylonitrile polymers |
| US3242000A (en) * | 1963-08-30 | 1966-03-22 | Deering Milliken Res Corp | Impregnated carbonized acrylic textile product and method for producing same |
| US3412062A (en) * | 1964-04-24 | 1968-11-19 | Nat Res Dev | Production of carbon fibres and compositions containing said fibres |
| US3416874A (en) * | 1964-02-21 | 1968-12-17 | Crylor | Production of polyacrylonitrile-based articles |
| US3497318A (en) * | 1967-09-01 | 1970-02-24 | Union Carbide Corp | Preparation of carbon textiles from polyacrylonitrile base textiles |
| US3529934A (en) * | 1967-01-06 | 1970-09-22 | Nippon Carbon Co Ltd | Process for the preparation of carbon fibers |
-
1970
- 1970-03-09 US US17965A patent/US3656882A/en not_active Expired - Lifetime
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2799915A (en) * | 1953-03-30 | 1957-07-23 | Johns Manville | Thermal modification of acrylonitrile polymers |
| US3242000A (en) * | 1963-08-30 | 1966-03-22 | Deering Milliken Res Corp | Impregnated carbonized acrylic textile product and method for producing same |
| US3416874A (en) * | 1964-02-21 | 1968-12-17 | Crylor | Production of polyacrylonitrile-based articles |
| US3412062A (en) * | 1964-04-24 | 1968-11-19 | Nat Res Dev | Production of carbon fibres and compositions containing said fibres |
| US3529934A (en) * | 1967-01-06 | 1970-09-22 | Nippon Carbon Co Ltd | Process for the preparation of carbon fibers |
| US3497318A (en) * | 1967-09-01 | 1970-02-24 | Union Carbide Corp | Preparation of carbon textiles from polyacrylonitrile base textiles |
Non-Patent Citations (1)
| Title |
|---|
| Vosburgh, Textile Research Journal, Vol. 30, 1960, pages 882 896 * |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3917776A (en) * | 1970-12-12 | 1975-11-04 | Mitsubishi Rayon Co | Process for producing carbon fiber |
| US3923950A (en) * | 1971-11-18 | 1975-12-02 | Celanese Corp | Production of stabilized acrylic fibers and films |
| US6156287A (en) * | 1995-05-22 | 2000-12-05 | National Science Council | Method for preparing pan-based activated carbon fabrics |
| US20180001244A1 (en) * | 2016-07-01 | 2018-01-04 | Hollingsworth & Vose Company | Multi-layered electret-containing filtration media |
| CN109562313A (en) * | 2016-07-01 | 2019-04-02 | 霍林斯沃思和沃斯有限公司 | The filter medium containing electret of multilayer |
| US12420221B2 (en) | 2016-07-01 | 2025-09-23 | Hollingsworth & Vose Company | Multi-layered electret-containing filtration media |
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