US3677705A - Process for the carbonization of a stabilized acrylic fibrous material - Google Patents
Process for the carbonization of a stabilized acrylic fibrous material Download PDFInfo
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- US3677705A US3677705A US17780A US3677705DA US3677705A US 3677705 A US3677705 A US 3677705A US 17780 A US17780 A US 17780A US 3677705D A US3677705D A US 3677705DA US 3677705 A US3677705 A US 3677705A
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- carbonized
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- 239000002657 fibrous material Substances 0.000 title abstract description 115
- 238000000034 method Methods 0.000 title abstract description 49
- NIXOWILDQLNWCW-UHFFFAOYSA-N acrylic acid group Chemical group C(C=C)(=O)O NIXOWILDQLNWCW-UHFFFAOYSA-N 0.000 title description 73
- 238000003763 carbonization Methods 0.000 title description 37
- 238000010438 heat treatment Methods 0.000 abstract description 64
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 abstract description 25
- 229910052799 carbon Inorganic materials 0.000 abstract description 11
- 229920001577 copolymer Polymers 0.000 abstract description 11
- 239000007858 starting material Substances 0.000 abstract description 9
- 230000000704 physical effect Effects 0.000 abstract description 7
- 238000006243 chemical reaction Methods 0.000 abstract description 6
- 230000001747 exhibiting effect Effects 0.000 abstract description 4
- 229920001519 homopolymer Polymers 0.000 abstract 1
- 230000006698 induction Effects 0.000 description 27
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 22
- 238000001035 drying Methods 0.000 description 21
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 16
- 239000000463 material Substances 0.000 description 16
- 229910002804 graphite Inorganic materials 0.000 description 14
- 239000010439 graphite Substances 0.000 description 14
- 229920002239 polyacrylonitrile Polymers 0.000 description 14
- 238000005087 graphitization Methods 0.000 description 13
- 230000006641 stabilisation Effects 0.000 description 13
- 238000011105 stabilization Methods 0.000 description 13
- NLHHRLWOUZZQLW-UHFFFAOYSA-N Acrylonitrile Chemical group C=CC#N NLHHRLWOUZZQLW-UHFFFAOYSA-N 0.000 description 10
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 9
- 239000000835 fiber Substances 0.000 description 9
- 239000001301 oxygen Substances 0.000 description 9
- 229910052760 oxygen Inorganic materials 0.000 description 9
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 8
- 229910052757 nitrogen Inorganic materials 0.000 description 8
- 230000001965 increasing effect Effects 0.000 description 6
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 4
- 238000002441 X-ray diffraction Methods 0.000 description 4
- 229910052786 argon Inorganic materials 0.000 description 4
- 230000015572 biosynthetic process Effects 0.000 description 4
- 230000000052 comparative effect Effects 0.000 description 4
- 238000010924 continuous production Methods 0.000 description 4
- 229910052802 copper Inorganic materials 0.000 description 4
- 239000010949 copper Substances 0.000 description 4
- 239000002243 precursor Substances 0.000 description 4
- 229910001220 stainless steel Inorganic materials 0.000 description 4
- 239000010935 stainless steel Substances 0.000 description 4
- 238000004458 analytical method Methods 0.000 description 3
- 239000001257 hydrogen Substances 0.000 description 3
- 229910052739 hydrogen Inorganic materials 0.000 description 3
- 238000010926 purge Methods 0.000 description 3
- 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
- 239000001307 helium Substances 0.000 description 2
- 229910052734 helium Inorganic materials 0.000 description 2
- SWQJXJOGLNCZEY-UHFFFAOYSA-N helium atom Chemical compound [He] SWQJXJOGLNCZEY-UHFFFAOYSA-N 0.000 description 2
- 125000004435 hydrogen atom Chemical class [H]* 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 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
- 229920002972 Acrylic fiber Polymers 0.000 description 1
- 239000002841 Lewis acid Substances 0.000 description 1
- VVQNEPGJFQJSBK-UHFFFAOYSA-N Methyl methacrylate Chemical compound COC(=O)C(C)=C VVQNEPGJFQJSBK-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
- 238000010521 absorption reaction Methods 0.000 description 1
- 238000007605 air drying Methods 0.000 description 1
- 238000013459 approach Methods 0.000 description 1
- 235000015241 bacon Nutrition 0.000 description 1
- 239000011230 binding agent Substances 0.000 description 1
- 239000002131 composite material Substances 0.000 description 1
- 238000007796 conventional method Methods 0.000 description 1
- 230000001066 destructive effect Effects 0.000 description 1
- 238000000578 dry spinning Methods 0.000 description 1
- 238000010891 electric arc Methods 0.000 description 1
- 230000003028 elevating effect Effects 0.000 description 1
- 238000011031 large-scale manufacturing process Methods 0.000 description 1
- 150000007517 lewis acids Chemical class 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000011159 matrix material Substances 0.000 description 1
- QSHDDOUJBYECFT-UHFFFAOYSA-N mercury Chemical compound [Hg] QSHDDOUJBYECFT-UHFFFAOYSA-N 0.000 description 1
- 229910052753 mercury Inorganic materials 0.000 description 1
- 230000001590 oxidative effect Effects 0.000 description 1
- 230000003014 reinforcing effect Effects 0.000 description 1
- 238000012360 testing method Methods 0.000 description 1
- 238000012546 transfer Methods 0.000 description 1
- 239000011800 void material Substances 0.000 description 1
- 238000002166 wet spinning Methods 0.000 description 1
- 238000004804 winding Methods 0.000 description 1
Images
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
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S264/00—Plastic and nonmetallic article shaping or treating: processes
- Y10S264/19—Inorganic fiber
Definitions
- a process is provided for the rapid conversion of a continuous length of an inherently hygroscopic stabilized acrylonitrile homopolymer or copolymer to a carbonized form exhibiting improved physical properties.
- the stabilized starting material is supplied in an essentially anhydrous form immediately prior to its passage through a heating zone containing an inert atmosphere in which its temperature is relatively rapidly elevated to produce a carbonized fibrous material.
- the resulting continuous length of carbonized fibrous material may be subsequently converted to a continuous length of fibrous graphitic carbon possessing superior properties.
- the present invention represents an improvement over the carbonization or carbonization and graphitization process disclosed in US. Ser. No. 777,275, filed Nov. 20, 1968, of Charles M. Clarke, entitled Process for the Continuous carbonization of a Stabilized Acrylic Fibrous Material, which is assigned to the same assignee as the present invention.
- carbonized fibrous material as used herein is defined to be a product consisting of at least about 90 percent carbon by Weight, and preferably at least about 95 percent carbon by weight.
- 1,093,084 discloses a heating schedule for graphitizing a polyacrylonitrile fibrous material comprising slowly heating from 100 C. to 300 C. at a rate of increase of to 55 C. per hour, and from 900 C. to around 3000 F. at a rate of up to 3000 C. per hour.
- British Pat. No. 1,110,791 discloses a batch carbonization procedure in which a bundle of preoxidized polyacrylonitrile fibers is heated from 200 C. to 1000 C. in 24 hours.
- Belgian Pat. No. 690,072 discloses heating a preoxidized acrylic fibrous precursor from 400 C. to 720 C. or 1000" C. at a rate of 0.5 C. per minute to form a carbonized product.
- Belgian Pat. No. 700,655 discloses the continuous carbonization of an acrylonitrile copolymer in which the temperature is elevated from 300 C.
- SUMMARY OF INVENTION fibrous material selected from the group consisting of ,an acrylonitrile homopolymer and acrylonitrile copolymers which contain at least about mol percent of acrylonitrile units and up to about 15 mol percent of one or more monovinyl units copolymerized therewith comprising continuously passing a continuous length of the stabilized acrylic fibrous material having a temperature within the range of about 20 to about 500 C. through a heating zone provided with an inert atmosphere in which the fibrous material is raised within a period of about 3 seconds to about 10 minutes to a temperature within the range of about 900 to about 1600 C.
- a graphitized fibrous material may optionally be formed by subsequently passing the carbonized fibrous material through a heating zone provided with an inert atmosphere in which the carbonized fibrous material is heated at a temperature within the range of about 2400 to about 3100 C. until substantial graphitic carbon is formed.
- the stabilized acrylic fibrous material while in an essentially anhydrous form is continuously passed through a heating zone provided with a temperature gradient in which both carbonization and graphitization are relatively rapidly achieved.
- FIG. 1 is a photograph made with the aid of a scanning electron microscope of a graphite fiber produced in accordance with the present invention wherein the stabilized acrylic precursor was introduced into the carbonization zone in an essentially anhydrous form.
- FIG, 2 is a photograph made with the aid of a scanning electron microscope of a graphite fiber wherein the stabilized acrylic precursor was introduced into the carbonization zone while in intimate association with a substantial quantity of moisture adhering thereto.
- the continuous length of acrylic fibrous material which is carbonized or carbonized and graphitized in accordance with the present invention is preliminarily stabilized to a heat-resistant form, and supplied in an essentially anhydrous form to the heating zone in which a continuous length of carbonized product is produced.
- stabilized acrylic fibrous materia as used herein is defined as an acrylic fibrous material which is non-burning when subjected to an ordinary match flame and capable of undergoing carbonization while retaining its original fibrous configuration essentially intact.
- the stabilization reaction may be conducted by heating the acrylic fibrous material at relatively moderate temperatures. Such a stabilization procedure is commonly conducted in a presence of oxygen and results in the formation of a preoxidized product which exhibits thermal stability not exhibited by the unmodified acrylic material.
- the stabilized acrylic fibrous material is derived from a polymeric material formed primarily of recurring acrylonitrile units.
- the acrylic fibrous material should generally contain at least about 85 mol percent of acrylonitrile units and up to about 15 mol percent of one or more monovinyl units copolymerized therewith, such as styrene, methyl acrylate, methyl methacrylate, vinyl acetate, vinyl chloride, vinylidene chloride, vinyl pyridine, and the like.
- the stabilized acrylic fibrous material is derived from an acrylonitrile homopolymer.
- Preferred acrylonitrile copolymers contain at least about 95 mol percent of acrylonitrile units and up to about mol percent of one or more monovinyl units copolymerized therewith. Particularly preferred copolymers contain no more than about 1 mol percent of one or more monovinyl comonomers copolymerized with acrylonitrile.
- the continuous length of stabilized acrylic fibrous material which is carbonized or carbonized and graphitized in accordance with the present invention may be in any one of a variety of configurations.
- single continuous filaments, yarns, or tapes may be utilized.
- the stabilized acrylic fibrous material is in the form of a continuous filament yarn.
- Such a yarn may be formed prior to stabilization by conventional techniques which are well known to those skilled in the art. For instance, dry spinning or wet spinning techniques may be employed.
- the yarn may optionally be provided with a twist which improves its handling characteristics. For example, a twist of about 0.1 to 3 t.p.i., and preferably about 0.1 to 1.0 t.p.i., may be utilized.
- the acrylic fibrous material which serves as the starting material may be highly oriented prior to stabilization.
- the starting material may be highly oriented by hot drawing to a relatively high single filament tensile strength of at least about 4 grams per denier (e.g. 4 to 9 grams per denier) prior to stabilization.
- the stabilized acrylic fibrous materials commonly used as starting materials inthe production of carbonized products have been found to be hygroscopic in nature. When exposed to the atmospheric for even short periods of time (e.g. a few minutes), substantial quantities of water become absorbed by the same.
- the hygroscopic properties of the stabilized materials are generally not exhibited by the acrylic fibrous materials prior to their stabilization. For instance, when the unstabilized fibrous acrylic starting materials are placed in air having a temperature of 70 F., and a relative humidity of 65 percent, moisture gain of only about 0.5 percent by weight has been observed. However, following stabilization a moisture gain of about 11 to 15 percent by weight based upon the weight of the dry yarn has been observed under identical conditions.
- the continuous length of stabilized material may be stored exclusively under substantially anhydrous conditions or passed directly from the stabilization zone to the heating zone utilized to produce carbonization through a hermetically sealed tube from which water vapor is excluded.
- the stabilized acrylic fibrous material has commonly been stored under ambient conditions and/ or conveyed to the carbonization zone while in contact with moisture containing air.
- the absorbed water may be removed by the controlled drying of the material prior to supplying the same to the heating zone in which a carbonized product is formed. Suitable drying may be conducted by heating the material under relatively mild conditions until an essentially anhydrous form of the same is produced. The drying may be carried out by subjecting the stabilized fibrous material to a relatively constant drying temperature, or to a drying temperature profile (i.e. gradient) in which the temperature is gradually or incrementaliy raised.
- the drying conditions selected are such that the physical properties of the fibrous material are not adversely influenced; i.e. the volatilimtion of water is not so rapid as to harm the same.
- the drying of the hygroscopic stabilized acrylic fibrous material may be conveniently conducted on either a batch or a continuous basis. For instance, continuous lengths of the fibrous material may be placed in a circulating air oven for several hours (e.g. at least about two hours) while wound upon a bobbin or support.
- the temperature of the fibrous material under such circumstances is preferably below that at which additional preoxidation will occur to an appreciable degree.
- Preferred batch drying temperatures are about 80 to 150 C., and about 105 to 115 C. in a particularly preferred embodiment of the invention. If one chooses to conduct the drying under reduced pressure conditions, e.g. 25 inches of mercury, correspondingly lower temperatures may be conveniently selected as will be apparent to those skilled m the art.
- the hygroscopic stabilized acrylic fibrous material may be passed through a drying zone positioned immediately in front of the heating zone in which carbonization occurs.
- a drying zone positioned immediately in front of the heating zone in which carbonization occurs.
- the temperature profile i.e. gradient
- the hygroscopic stabilized fibrous materials may be passed through a drying oven positioned immediately in front of the heating zone (i.e. carbonization zone) which is provided at a relatively constant drying temperature, preferably below about 300 C., e.g. about 150 to 275 C.
- Continuous in line drying times are preferably about 2 to minutes depending upon the temperature, pressure, configuration of the continuous length of fibrous material, and the quantity of moisture adhering to the same.
- the drying zone is positioned at a location removed from the heating zone in which carbonization occurs, then the dried material is conveyed to carbonization zone under conditions whereby its essentially anhydrous form is preserved.
- a hermetically sealed tube from which water vapor is excluded may be selected for this purpose.
- the dried stabilized material may be stored under anhydrous conditions prior to transfer to the carbonization zone.
- the continuous length of hygroscopic fibrous material while in an essentially anhydrous form is rapidly carbonized by increasing its temperature from within the range of about to about 500 C. to a temperature within the range of about 900 to 1600 C. (preferably to a temperature within the range of about 1400 to about 1600 C.), within a period of about 3 seconds to about 10 minutes, and preferably within a period of about 3 seconds to about 5 minutes.
- the process is conducted by passing the continuous length of stabilized acrylic fibrous material through a heating zone capable of producing the requisite heating which is provided with an inert atmosphere. Suitable inert atmospheres in which the carbonization reaction may be conducted include nitrogen, argon, helium, etc.
- the carbonization reaction elements present in the continuous length of stabilized acrylic fibrous material other than carbon e.g. nitrogen, hydrogen, and oxygen, are expelled to a substantial degree.
- a carbonized fibrous product which retains essentially the same configuration as the starting material is produced. If the stabilized acrylic fibrous material is raised from a temperature within the range of about 20 to about 500 C. to a temperature within the range of about 900 to about 1600 C. in less than about 3 seconds, then the physical properties of the resulting product are adversely affected. If the period of temperature elevation is more than about 30 seconds, then any further improvement in physical properties resulting from the slower rate of temperature increase generally tends to be slight. Periods of temperature increase greater than about 10 minutes are generally to be avoided because of economic considerations.
- suitable mean heating rates for elevating the stabilized acrylic fibrous material to a temperature of about 1400 to about 1600 C. range from about 2 C. per second to about 300 C. per second.
- the continuous length of acrylic fibrous material is heated to a temperature of about 1400 to about 1600 C. in about 20 to about 60 seconds.
- Particularly preferred mean heating rates for heating to a temperature of about 1400 to about 1600 C. accordingly range from about 23 C. per second to about 45 C. per second.
- the heating rates employed need not be constant, but may be varied within the period of temperature elevation. Particularly satisfactory results have been achieved when the rate is progressively increased.
- the continuous length of stabilized acrylic fibrous material undergoing treatment may be maintained at a temperature within the range of about 900 to about 1600 C. for about 3 seconds to about 5 minutes to produce a carbonized fibrous product which is ready for use, or exposed to a more highly elevated temperature in the same or a different heating zone to form a carbonized and graphitized product as discussed in detail hereafter.
- the continuous length of stabilized fibrous material is heated to a temperature within the range of about 1400 to 1600 C. where it is maintained for about 3 seconds to about 60 seconds to produce a carbonized fibrous material.
- the carbonized fibrous material optionally may next be continuously passed through an inert atmosphere Where it is heated at a temperature of about 2400 to 3100 C. until substantial graphitic carbon is formed.
- a carbonized and graphitized product is formed by passing a continuous length of the fibrous material in an essentially anhydrous form through a heating zone provided with an inert at mosphere and a temperature gradient in which the fibrous material is initially raised within a period of about 3 seconds to about 10 minutes from a temperature in the range of about 20 to 500 C. to a temperature within the range of about 900 to 1600 C. to form a continuous length of carbonized fibrous material, and in which the carbonized fibrous material is subsequently raised to a temperature within the range of about 2400 to about 3100 C. where it is maintained until substantial graphitization occurs.
- the presence of graphitic carbon may be detected by the characteristic X-ray diffraction pattern of graphite.
- Suitable inert atmospheres include nitrogen, argon, helium, etc.
- a graphitized product of superior modulus may generally be formed in about 10 seconds to about 1 minute while heating at about 2400 to about 3100 C. Longer graphitization heating times may be used if desired.
- the modulus of the graphitized product tends to increase with the maximum temperature achieved during graphitization.
- the temperature of the continuous length of fibrous material is preferably progressively increased from a temperature within the range of about 900 to about 1600 C. (preferably about 1400 to about 1600 C.) to the graphitization temperature within a period of about 2 seconds to about 30 seconds.
- the equipment utilized to produce the requisite heating to carry out the process of the invention may be varied widely. It is essential that the apparatus selected be capable of producing the required temperatures while excluding the presence of an oxidizing atmosphere.
- suitable apparatus include induction furnaces, tube furnaces in which a hollow graphite susceptor is heated by direct resistance heating, direct resistance heating apparatus in which electric current is passed directly through the fibrous material, apparatus capable of producing reducing flames, electric arc furnaces, lasers, thermal image equipment such as solar furnaces, apparatus capable of producing low temperature plasma flames, and the like.
- the continuous length of fibrous material undergoing treatment is passed through one or more heating apparatus and subjected to the requisite temperatures.
- a temperature profile i.e. a gradient
- the mataerial may be successively passed through a series of apparatus maintained at progressively increasing temperatures.
- the stabilized acrylic fibrous material While in an essentially anhydrous form is heated by use of an induction furnace.
- the continuous length stabilized material is passed through a hollow graphite tube or susceptor which is situated Within the windings of an induction coil.
- a hollow graphite tube or susceptor which is situated Within the windings of an induction coil.
- EXAMPLE I A continuous length of 800 fil. water washed dry spun acrylonitrile homopolymer continuous filament yarn having a total denier of 1040 was selected as the starting material. The yarn was highly oriented and drawn to a single filament tenacity of about 8.2 grams per denier. The yarn was continuously stabilized in accordance with the teachings of US. Ser. Nos. 749,957 and 749,959, filed Aug. 5, 1968, of Dagobert E. Stuetz and Michael J. Ram, respectively, which are assigned to the same assignee as the present invention and are herein incorporated by reference. During the stabilization reaction (i.e. preoxidation) the yarn was continuously passed in the direction of its length through a mufile furnace provided with an air atmosphere at 285 C.
- a mufile furnace provided with an air atmosphere at 285 C.
- the yarn was allowed to shrink approximately 4 percent in length.
- the resulting stabilized yarn was black in appearance, contained a bound oxygen content of 9 percent by weight as determined by the Unterzaucher analysis, and was non-burning when subjected to an ordinary match ame.
- the stabilized yarn was exposed to ambient conditions (i.e. 25 C. and about 60 percent relative humidity) for 48 hours, and upon testing was found to be highly hygroscopic in nature and to have picked up approximately about 11.3 percent moisture by weight based upon the weight of the yarn when free of moisture.
- the hygroscopic stabilized yarn was dried on a batch basis to an essentially anhydrous form by heating at 110 C. while wound upon a support and present in a forced air drying oven for a residence time of 140 hours.
- the dried stabilized yarn immediately thereafter was passed in the direction of its length through a heating zone (i.e. carbonization zone) where it was converted to a carbonized form containing 93 percent carbon by weight and exhibiting an essentially amorphous X-ray diffraction pattern. Exposure of the dried yarn to a moisture containing atmosphere prior to its introduction into the carbonization zone was avoided by passage under an infra red lamp. The yarn was accordingly in an essentially anhydrous form and at a temperature of about C. when introduced into the heating zone.
- the apparatus utilized to produce carbonization comprised a stainless steel tube having a length of 48 inches, an inner diameter of 0.42 inch, and an outer diameter of 0.50 inch.
- a pair of electrodes were connected to the stainless steel tube at each end and were connected to an AC power source of 10 volts and 5 amps.
- a temperature gradient existed within the stainless steel tube having a maximum temperature of 1250 C. situated from about 12 to 36 inches from the entrance end.
- An inert atmosphere of argon was provided within the stainless steel tube. Air was substantially excluded from the tube by purging with argon.
- the dried yarn was continuously passed through the heating zone at a rate of 0.5 meter per minute (i.e. at about 20 inches per minute). A tension of grams was exerted upon the dried stabilized yarn as it passed through the heating zone. The yarn was raised from a temperature of 80 C. to a temperature of 1250 C. in approximately 36 seconds.
- the carbonized yarn was next passed through a Lepel 450 kc. induction furnace utilizing a 20 kw. power source.
- the induction furnace comprised a 10 turn water cooled copper coil having an inner diameter of inch and a length of 2 inches, and a hollow graphite tube suspended within the coil having a length of 8 /2 inches, an outer diameter of /2 inch and an inner diameter of inch through which the carbonized yarn was continuously passed.
- the copper coil which encompassed a portion of the hollow graphite tube was positioned at a location essentially equidistant from the respective ends of the graphite tube.
- An inert atmosphere of nitrogen was maintained within the induction furnace. Air was substantially excluded from the induction furnace by purging with nitrogen.
- the carbonized yarn was passed through the induction furnace at a rate of about 1.5 inches per minute.
- the carbonized yarn was raised to a maximum temperature of approximately 2900 C. while present within the induction furnace at which temperature it was maintained for approximately 40 seconds.
- a tension of 100 grams was exerted upon the carbonized yarn as it passed through the induction furnace.
- While present within the induction furnace the carbonized yarn was converted to a substantially graphitic form as evidenced by the characteristic X-ray diffraction pattern of graphite.
- the resulting graphitized yarn exhibited a single filament tenacity 11.3 grams per denier, and a single filament initial modulus of 2800 grams per denier.
- Example I In a comparative run Example I was repeated with the exception that the hygroscopic stabilized yarn was not dried prior to introduction into the carbonization zone. Following graphitization the yarn exhibited a single filament tenacity of 9.7 grams per denier and a single filament initial modulus of 3200 grams per denier. The comparison illustrates that a fiber of higher tenacity resulted when the process of the invention was practiced.
- Example II Example I is repeated with the exception that the dried stabilized yarn is passed through the heating zone at the increased rate of 2.0 meters per minute (i.e. at about 80 inches per minute). The yarn was raised from a temperature of 80 C. to a temperature of 1250" C. in approximately 9 seconds.
- a photograph of a representative fiber from the graphitized yarn made with the aid of a scanning electron microscope at a magnification of 4400 is provided as FIG. 1.
- the resulting graphitized yarn exhibited a single filament tenacity of 12.0 grams per denier and an initial modulus of 3100 grams per denier.
- Example II In a comparative run Example II was repeated with the exception that the hygroscopic stabilized yarn was not dried prior to introduction into the heating zone. Following graphitization the yarn exhibited a single filament tenacity of 6.8 grams per denier and an initial modulus of 2900. This comparison illustrates that a more accelerated heat-up rate during carbonization may be utilized when employing the process of the present invention while continuing to produce a more uniform fiber of improved tenacity.
- FIG. 2 A photograph of a representative fiber from the graphitized yarn made with the aid of a scanning electron microscope at a magnification of 4400 is provided as FIG. 2. Numerous voids and continuity breaches are visible in FIG. 2 which are absent in fibers formed in accordance with the present invention (e.g. FIG. 1).
- EXAMPLE III A continuous length of preoxidized acrylonitrile homopolymer yarn substantially similar to that utilized in Example I was selected as the starting material. The yarn following preoxidation was exposed to ambient conditions and picked up approximately 11 to 12 percent water by weight.
- the yarn was dried in an in line continuous manner immediately prior to its introduction into an induction furnace (i.e. heating zone) provided with an inert atmosphere and a temperature gradient wherein both carbonization and substantial graphitization occurred.
- an induction furnace i.e. heating zone
- the preoxidized yarn containing substantial moisture adhering thereto was continuously unwound from a bobbin and introduced into a 48 inch mufi'le furnace provided with a circulating air atmosphere at 200 C. through which it was continuously passed in the direction of its length.
- the yarn was passed through the muffle furnace at a rate about 1 meter per minute (i.e. about 40 inches per minute).
- the preoxidized yarn was in an essentially anhydrous form as it left the muffie furnace.
- the dried yarn was continuously introduced into the induction furnace.
- the dried yarn was continuously passed in the direction of its length through the induction furnace at a rate of about 1 meter per minute (i.e. about 40 inches per minute).
- a tension of about 0.41 gram per denier was exerted on the dried yarn as it passed through the induction furnace.
- the induction furnace comprised an Inductotherm model Integral 50 unit provided with a 50 kw. power source, a 12 turn water cooled copper coil having a length of 19 inches, a hollow graphite tube suspended within the coil having a length of 52 inches, an outer diameter of 3 inches, and an inner diameter of 0.75 inch.
- the copper coil which encompassed a portion of the hollow graphite tube was positioned at a location essentially equidistant from the respective ends of the graphite tube.
- An inert atmosphere of nitrogen was maintained within the induction furnace. Air was substantially excluded from the induction furnace by purging with nitrogen.
- the yarn was raised to a maximum temperature of 2850 C. while present within the induction furnace at which temperature it was maintained for approximately 12 seconds.
- the preoxidized yarn was initially carbonized and subsequently converted to a substantially graphitic form as evidenced by the characteristic X-ray diffraction pattern of graphite.
- the resulting graphitized yarn exhibited a single filament tenacity of 13.0 grams per denier, and a single filament initial modulus of 3015 grams per denier.
- Example III In a comparative run Example III was repeated with the exception that the preoxidized yarn was not passed through a muffle furnace prior to its introduction into the induction furnace, and was accordingly undried when introduced into the induction furnace.
- the resulting graphitized yarn exhibited a single filament tenacity of 9.62 grams per denier, and a single filament initial modulus of 2900 grams per denier.
- EXAMPLE IV A continuous length of 1600 fil. unwashed dry spun acrylonitrile homopolymer continuous filament yarn having a total denier of 2,880 was selected. The yarn was highly oriented and had been drawn at a draw ratio of 5:1. The yarn was subjected to a heating treatment by passage for 6.5 minutes through a muffie furnace provided with air at 200 C. during which time the yarn shrank 10.5 percent in length.
- the yarn was preoxidized on a continuous basis in the absence of shrinkage by passage for 160 minutes through a multi-wrap skewed roll oven provided with circulating air at 270 C.
- the stabilized yarn was black in appearance, non-burning when subjected to an ordinary match flame, and had a bound oxygen content of 9.7 percent by weight as determined by the Unterzaucher analysis.
- the preoxidized yarn was exposed to ambient conditions (i.e. 25 C. and about 60 percent relative humidity) during which time the yarn picked up approximately 11.5 percent moisture by weight.
- the preoxidized yarn was dried in an in line continuous manner immediately prior to its introduction into an induction furnace provided with an inert atmosphere and a temperature gradient wherein both carbonization and substantial graphitization occurred.
- the drying, carbonization, and graphitization were conducted as in Example III with the exception that the temperature in the drying zone was incrementally raised as the yarn approached the induction furnace and a yarn speed of 0.5 meter per minute (i.e. about 20 inches per minute) was utilized throughout.
- the drying zone consisted of four 12 inch muffle furnaces placed in an end to end relationship and provided with circulating air at 200 C., 250 C., 300 C., and 340 C., respectively. During passage through the induction furnace a tension of 200 grams was maintained upon the dried yarn.
- the resulting graphitized yarn exhibited a denier per filament of 0.56, a single filament tenacity of 15.5 grams per denier, and a single filament initial modulus of 3130 grams per denier.
- Example IV In a comparative run Example IV was repeated with the exception that the preoxidized yarn was not passed through the mufile furnaces prior to introduction into the induction furnace, and was accordingly undried.
- the resulting graphitized yarn exhibited a denier per filament of 0.89, a single filament tenacity of 14.2 grams per denier, and a single filament initial modulus of 2560 grams per denier.
- the fibrous products of the present invention may be incorporated in a binder or matrix and serve as a reinforcing medium. Such resulting composite materials may accordingly serve as light-weight load bearing structural elements in high performance structures which find particular utility in the aerospace industry.
- said hygroscopic stabilized acrylic fibrous material is derived from an acrylonitrile copolymer which contains at least about 95 mol percent of acrylonitrile units and up to about mol percent of one or more monovinyl units copolymerized therewith.
- said hygroscopic stabilized acrylic fibrous material is derived from an acrylonitrile copolymer which contains at least about 95 mol percent of acrylonitrile units and up to about 5 mol percent of one or more monovinyl units copolymerized therewith.
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- Chemical & Material Sciences (AREA)
- Chemical Kinetics & Catalysis (AREA)
- General Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Textile Engineering (AREA)
- Inorganic Fibers (AREA)
Abstract
Description
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US1778070A | 1970-03-09 | 1970-03-09 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US3677705A true US3677705A (en) | 1972-07-18 |
Family
ID=21784509
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US17780A Expired - Lifetime US3677705A (en) | 1970-03-09 | 1970-03-09 | Process for the carbonization of a stabilized acrylic fibrous material |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US3677705A (en) |
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3917776A (en) * | 1970-12-12 | 1975-11-04 | Mitsubishi Rayon Co | Process for producing carbon fiber |
| US3954950A (en) * | 1970-03-09 | 1976-05-04 | Celanese Corporation | Production of high tenacity graphitic fibrous materials |
| FR2554834A1 (en) * | 1983-11-10 | 1985-05-17 | Kashima Oil | Endless carbon fibre yarn prodn. |
| US4680093A (en) * | 1982-03-16 | 1987-07-14 | American Cyanamid Company | Metal bonded composites and process |
| EP0232051A3 (en) * | 1986-01-21 | 1988-08-24 | Clemson University | High strength, melt spun carbon fibers and method for producing same |
| US4915925A (en) * | 1985-02-11 | 1990-04-10 | Chung Deborah D L | Exfoliated graphite fibers and associated method |
| US5348397A (en) * | 1993-03-29 | 1994-09-20 | Ferrari R Keith | Medical temperature sensing probe |
| EP0778046A2 (en) | 1995-12-08 | 1997-06-11 | R. Keith Ferrari | X-ray transmissive transcutaneous stimulating electrode |
| US9683312B2 (en) | 2011-12-10 | 2017-06-20 | The Boeing Company | Fiber with gradient properties and method of making the same |
| US9683310B2 (en) | 2011-12-10 | 2017-06-20 | The Boeing Company | Hollow fiber with gradient properties and method of making the same |
-
1970
- 1970-03-09 US US17780A patent/US3677705A/en not_active Expired - Lifetime
Cited By (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3954950A (en) * | 1970-03-09 | 1976-05-04 | Celanese Corporation | Production of high tenacity graphitic fibrous materials |
| US3917776A (en) * | 1970-12-12 | 1975-11-04 | Mitsubishi Rayon Co | Process for producing carbon fiber |
| US4680093A (en) * | 1982-03-16 | 1987-07-14 | American Cyanamid Company | Metal bonded composites and process |
| FR2554834A1 (en) * | 1983-11-10 | 1985-05-17 | Kashima Oil | Endless carbon fibre yarn prodn. |
| US4915925A (en) * | 1985-02-11 | 1990-04-10 | Chung Deborah D L | Exfoliated graphite fibers and associated method |
| EP0232051A3 (en) * | 1986-01-21 | 1988-08-24 | Clemson University | High strength, melt spun carbon fibers and method for producing same |
| US5348397A (en) * | 1993-03-29 | 1994-09-20 | Ferrari R Keith | Medical temperature sensing probe |
| EP0778046A2 (en) | 1995-12-08 | 1997-06-11 | R. Keith Ferrari | X-ray transmissive transcutaneous stimulating electrode |
| US9683312B2 (en) | 2011-12-10 | 2017-06-20 | The Boeing Company | Fiber with gradient properties and method of making the same |
| US9683310B2 (en) | 2011-12-10 | 2017-06-20 | The Boeing Company | Hollow fiber with gradient properties and method of making the same |
| US10246798B2 (en) | 2011-12-10 | 2019-04-02 | The Boeing Company | Method of making fiber with gradient properties |
| US10253433B2 (en) | 2011-12-10 | 2019-04-09 | The Boeing Company | Method of making hollow fiber with gradient properties |
| US10774447B2 (en) | 2011-12-10 | 2020-09-15 | The Boeing Company | Method of making hollow fiber with gradient properties |
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