EP0276840A2 - Pechbasierte Kohlenstoffasern und Verfahren zu deren Herstellung - Google Patents
Pechbasierte Kohlenstoffasern und Verfahren zu deren Herstellung Download PDFInfo
- Publication number
- EP0276840A2 EP0276840A2 EP88101195A EP88101195A EP0276840A2 EP 0276840 A2 EP0276840 A2 EP 0276840A2 EP 88101195 A EP88101195 A EP 88101195A EP 88101195 A EP88101195 A EP 88101195A EP 0276840 A2 EP0276840 A2 EP 0276840A2
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- EP
- European Patent Office
- Prior art keywords
- fibers
- pitch
- carbonization
- oils
- carbon fibers
- 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.)
- Granted
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- 229920000049 Carbon (fiber) Polymers 0.000 title claims abstract description 36
- 239000004917 carbon fiber Substances 0.000 title claims abstract description 35
- 238000004519 manufacturing process Methods 0.000 title description 4
- 239000000835 fiber Substances 0.000 claims abstract description 100
- 238000000034 method Methods 0.000 claims abstract description 20
- 229920001296 polysiloxane Polymers 0.000 claims abstract description 17
- 239000011229 interlayer Substances 0.000 claims abstract description 7
- 238000003763 carbonization Methods 0.000 claims description 43
- 238000011282 treatment Methods 0.000 claims description 23
- 229920001187 thermosetting polymer Polymers 0.000 claims description 18
- 239000012298 atmosphere Substances 0.000 claims description 17
- 239000011261 inert gas Substances 0.000 claims description 10
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 8
- 239000008041 oiling agent Substances 0.000 claims description 7
- 230000001590 oxidative effect Effects 0.000 claims description 7
- 230000000694 effects Effects 0.000 claims description 5
- 238000005087 graphitization Methods 0.000 claims description 4
- 238000002074 melt spinning Methods 0.000 claims description 4
- 239000013078 crystal Substances 0.000 claims 2
- 229910002804 graphite Inorganic materials 0.000 claims 2
- 239000010439 graphite Substances 0.000 claims 2
- 239000003921 oil Substances 0.000 abstract description 48
- 239000010410 layer Substances 0.000 abstract description 12
- 230000006978 adaptation Effects 0.000 abstract description 2
- 239000011295 pitch Substances 0.000 description 49
- 238000010438 heat treatment Methods 0.000 description 24
- 238000009941 weaving Methods 0.000 description 15
- 235000019610 cohesiveness Nutrition 0.000 description 11
- 239000000654 additive Substances 0.000 description 10
- 230000000996 additive effect Effects 0.000 description 10
- 238000009987 spinning Methods 0.000 description 10
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 8
- 230000001965 increasing effect Effects 0.000 description 8
- 238000005299 abrasion Methods 0.000 description 7
- 239000011337 anisotropic pitch Substances 0.000 description 7
- 239000003795 chemical substances by application Substances 0.000 description 6
- 238000004513 sizing Methods 0.000 description 6
- 229910052799 carbon Inorganic materials 0.000 description 5
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 4
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 4
- 229910052786 argon Inorganic materials 0.000 description 4
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 4
- 239000011248 coating agent Substances 0.000 description 4
- 238000000576 coating method Methods 0.000 description 4
- 230000005484 gravity Effects 0.000 description 4
- 238000009940 knitting Methods 0.000 description 4
- 239000001301 oxygen Substances 0.000 description 4
- 229910052760 oxygen Inorganic materials 0.000 description 4
- 238000006748 scratching Methods 0.000 description 4
- 230000002393 scratching effect Effects 0.000 description 4
- 238000006467 substitution reaction Methods 0.000 description 4
- 239000002759 woven fabric Substances 0.000 description 4
- YXFVVABEGXRONW-UHFFFAOYSA-N Toluene Chemical compound CC1=CC=CC=C1 YXFVVABEGXRONW-UHFFFAOYSA-N 0.000 description 3
- 238000005452 bending Methods 0.000 description 3
- 230000000052 comparative effect Effects 0.000 description 3
- 238000000354 decomposition reaction Methods 0.000 description 3
- 230000033001 locomotion Effects 0.000 description 3
- 230000003647 oxidation Effects 0.000 description 3
- 238000007254 oxidation reaction Methods 0.000 description 3
- 230000001846 repelling effect Effects 0.000 description 3
- 229910052710 silicon Inorganic materials 0.000 description 3
- 239000010703 silicon Substances 0.000 description 3
- 238000004804 winding Methods 0.000 description 3
- -1 Polysiloxane Polymers 0.000 description 2
- SMWDFEZZVXVKRB-UHFFFAOYSA-N Quinoline Chemical compound N1=CC=CC2=CC=CC=C21 SMWDFEZZVXVKRB-UHFFFAOYSA-N 0.000 description 2
- 238000002441 X-ray diffraction Methods 0.000 description 2
- 238000001816 cooling Methods 0.000 description 2
- 238000012937 correction Methods 0.000 description 2
- 230000003028 elevating effect Effects 0.000 description 2
- 239000004744 fabric Substances 0.000 description 2
- 239000007789 gas Substances 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 2
- 229910052757 nitrogen Inorganic materials 0.000 description 2
- 238000012545 processing Methods 0.000 description 2
- 239000002994 raw material Substances 0.000 description 2
- 239000011347 resin Substances 0.000 description 2
- 229920005989 resin Polymers 0.000 description 2
- 230000035945 sensitivity Effects 0.000 description 2
- NINIDFKCEFEMDL-UHFFFAOYSA-N Sulfur Chemical compound [S] NINIDFKCEFEMDL-UHFFFAOYSA-N 0.000 description 1
- 238000010521 absorption reaction Methods 0.000 description 1
- 239000000853 adhesive Substances 0.000 description 1
- 230000001070 adhesive effect Effects 0.000 description 1
- 239000000956 alloy Substances 0.000 description 1
- 229910045601 alloy Inorganic materials 0.000 description 1
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 1
- 238000004458 analytical method Methods 0.000 description 1
- 239000003963 antioxidant agent Substances 0.000 description 1
- 230000003078 antioxidant effect Effects 0.000 description 1
- 239000003575 carbonaceous material Substances 0.000 description 1
- 239000011336 carbonized pitch Substances 0.000 description 1
- 238000010000 carbonizing Methods 0.000 description 1
- 238000004523 catalytic cracking Methods 0.000 description 1
- 239000013043 chemical agent Substances 0.000 description 1
- 239000000571 coke Substances 0.000 description 1
- 239000000470 constituent Substances 0.000 description 1
- 238000002425 crystallisation Methods 0.000 description 1
- 230000008025 crystallization Effects 0.000 description 1
- 238000009792 diffusion process Methods 0.000 description 1
- 239000003085 diluting agent Substances 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 238000000921 elemental analysis Methods 0.000 description 1
- 239000003733 fiber-reinforced composite Substances 0.000 description 1
- 238000007429 general method Methods 0.000 description 1
- 239000003365 glass fiber Substances 0.000 description 1
- 230000009931 harmful effect Effects 0.000 description 1
- 238000011835 investigation Methods 0.000 description 1
- 239000000314 lubricant Substances 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 239000011302 mesophase pitch Substances 0.000 description 1
- 230000000116 mitigating effect Effects 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 238000006864 oxidative decomposition reaction Methods 0.000 description 1
- 230000010287 polarization Effects 0.000 description 1
- 229910052573 porcelain Inorganic materials 0.000 description 1
- 239000000843 powder Substances 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 230000002265 prevention Effects 0.000 description 1
- 238000000197 pyrolysis Methods 0.000 description 1
- 229910052705 radium Inorganic materials 0.000 description 1
- HCWPIIXVSYCSAN-UHFFFAOYSA-N radium atom Chemical compound [Ra] HCWPIIXVSYCSAN-UHFFFAOYSA-N 0.000 description 1
- 230000002787 reinforcement Effects 0.000 description 1
- 238000004062 sedimentation Methods 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
- 239000011863 silicon-based powder Substances 0.000 description 1
- 239000010802 sludge Substances 0.000 description 1
- 239000002904 solvent Substances 0.000 description 1
- 239000007921 spray Substances 0.000 description 1
- 230000003068 static effect Effects 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 229910052717 sulfur Inorganic materials 0.000 description 1
- 239000011593 sulfur Substances 0.000 description 1
- 239000004094 surface-active agent Substances 0.000 description 1
- 230000003245 working effect Effects 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
- D01F9/145—Carbon filaments; Apparatus specially adapted for the manufacture thereof by decomposition of organic filaments from pitch or distillation residues
Definitions
- This invention relates to pitch-based high performance carbon fibers having superior workability and their production method. More particularly, it relates to pitch-based carbon fibers obtained by mitigating carbonization treatment to such an extent that silicone types spin finish oils coated at the time of spinning of pitch are remained, having a high cohesiveness of bundles and lubricity by the remaining silicone type spin finish oils and having a superior workability and to their producing method.
- the carbon fibers obtained from a pitch according to a method of the present invention is incomplete in crystallization and orientation structure of carbon hexagonal network and yet have capability of increasing their tensile strength and modulus of elasticity greatly by an additive heat treatment carried out under a relaxed state whereby the growth of graphitic crystalline and orientation structure proceed.
- the carbon fibers of the present invention are superior in adaptation to various kinds of processes such as taking up on bobbins, transportation to a higher grade of carbonization or graphitization step, weaving,knitting and working for the reinforcement of resin.
- the pitch-based carbon fibers of the present invention are easy in working because of their lower carbonization grade, and their cost is lower than those of a higher carbonization grade. Thus even when working loss is produced, they have an advantage because the influence upon the cost of product is small.
- the carbon fibers derived from a pitch according to the present invention are patient against bending of small radius of curvature compared with carbon fibers subjected to higher grade of carbonization and have superior characteristic properties because their bent portions receive stress relaxation by the carbonization treatment applied thereafter and show superior resistance to abrasion, flexion and scratching.
- a method for obtaining carbon fibers by subjecting a pitch having a high softening point to melt-spinning, oxidizing the resulting fibers to make them infusible, followed by carbonization carried out in an inert gas atmosphere is disclosed in Japanese official gazette of examined application (Tokuko) 15728 of 1966.
- This is certainly a superior production method of pitch-based carbon fibers but according to the disclosed method, it is necessary to keep fibers in a stretched state during the carbonization to obtain fibers having high modulus of elasticity. Since thermoset pitch fibers are extremely brittle, it is difficult to hold them in a stretched state. It is considered actually to be impossible to obtain high modulus carbon fibers by this method.
- optically anisotropic pitch is easily graphitizable material and has superior properties as raw material for high strength, high modulus carbon fibers. Particularly, there is no need of being kept in a stretched state during the carbonization; it is considered to be an advantageous method in view of cost and quality.
- Carbon fibers from an optically anisotropic pitch can be easily made into a high strength and high modulus fibers but on the other hand, they have such weak points, that they are liable to be flawed, e.g. liable to be broken at the time of working. Such weak points exist more or less in case of brittle fibers.
- Glass fibers, PAN-based carbon fibers, etc. are coated by sizing agents to give lubricity and cohesiveness of bundles.
- repelling a sizing agent due to harmful effect of easily graphitizable property. Since uniform coating is difficult, shortages of lubricity and cohesiveness of bundles are also weak points.
- Japanese unexamined patent application (Tokukai) 21911 of 1985 discloses a method in which light grade of carbonization is carried out at a temperature of 400 - 650°C after thermosetting. This method is effective to some-extent for keeping the modulus of elasticity of carbon fibers small and for preventing them from being flawed but since bundles of the fibers have no cohesiveness and no lubricity, there are problems in insufficiency of workability.
- thermosetting which is a heat treatment carried out in the oxidative atmosphere.
- second oils after thermosetting process The problem of this method is the liability of being flawed at the time of imparting the second oils because the pitch fibers after thermosetting are equally or more brittle than the pitch fibers after spinning.
- the carbonization of pitch-based fibers is carried out generally by the heat treatment in the atmosphere of an inert gas and its effect is considered, in general, to be depend on temperature and time.
- spin finish oils there is the effect of spin finish oils remained.
- the effect for lubricity and cohesiveness of bundles are notable. Further there seems to be a difference of effectiveness between apparatus for carbonization.
- the present invention comprises coating spun pitch fibers with silicone type spin finish oils, introducing said pitch fibers in the oxidative atmosphere at a maximum temperature of 200 - 400°C to effect the thermosetting and subsequently subjecting said pitch fibers to the carbonization treatment in the atmosphere of an inert gas at a temperature of 400 - 1000°C under the condition that the silicone type finish oils remained on said pitch fibers are in the range of 0.1% - 2.0% by weight of said fibers and transferring them to a next working step.
- a high softening point pitch referred to in the present invention is an easily graphitizing pitch such as an optically anisotropic pitch.
- the easily graphitizing pitch forms needle cokes by dry distillation. Further, at the time of carbonization of pitch fibers, it produces high modulus carbon fibers even under a tensionless condition.
- the easily graphitizing pitches include, besides optically anisotropic pitches, dormant mesophase pitches, and premesophase carbonaceous materials which show similar graphitizing property.
- the silicone type oil used in the present invention is preferably a matter having a heat resistance of 500°C or more.
- the heat resistance of oils is defined as a temperature at which a reduction of the weight of oils measured by using a thermobalance (TG high temperature type CN 8068 AZ manufactured by Rigaku Denki was used; Sample size 10 mg, flow amount of nitrogen; 40 ml/min. cell diameter; 5mm, cell depth 2.5 mm) at a heating rate of 10°C/min. in the stream of nitrogen becomes practically zero. (It means that the change of the weight in a temperature range of 100°C becomes less than the sensitivity. The sensitivity is adjusted as 0.1% of the initial weight.)
- silicone type spin finish oils those which show smaller amount of decomposition sludge by heating is preferable.
- Polysiloxane type and polyaminosiloxane type are preferable.
- a solvent as a diluent those such as a surfactant which is not a silicone type, a lubricant or an antioxidant.
- carbon fibers of the present invention were determined to contain 2.0 - 15.0% by weight of oxygen, 0.07 - 0.7% by weight of sulfur. If these contents are too little, those inferior in workability are resulted. On the contrary, if they are too much, there is a tendency that the properties of ultimate products which are carbonized at a temperature of 2000°C or more, are lowered.
- the remaining amount of the oils is preferably in the range of 0.2 - 1.0% by weight of fibers.
- the remaining amount of the oils being too small, the cohesiveness and lubricity of bundle of filament yarns become poor and are liable to produce trouble by static electricity.
- the remaining amount of the oils being too much, it is not preferable not only because of the increase of the amount of oils imparted at the time of spinning which is disadvantageous in view of the cost but also because of reduction of thermosetting velocity.
- the reason for reduction of thermosetting velocity is not clear completely but it seems to be caused by the prevention of diffusion of oxygen by the film of the oils and reduction of the effective oxygen concentration caused by the large amount of vapour due to the oils generated in the inside of a furnace which drives oxygen out of the furnace.
- Carbon fibers produced by the present invention have a tensile strength of 5 - 50 Kgf/mm2, an elongation of 0.3 - 8.0% and a capability of increasing its tensile strength to 150 Kgf/mm2 or more and its modulus of elasticity to 30,000 Kgf/mm2 or more by the additive heat treatment carried out in the relaxed state. If the tensile strength becomes smaller than this range, it is not preferable because fibers become liable to be flawed at the step of next working. If the tensile strength becomes greater than this range, it is not preferable because fibers become liable to be broken at the time of working and abrasion resistance is reduced.
- the tensile strength is preferably in the range of 10 - 45 Kgf/mm2.
- the elongation is preferably in the range of 0.6 - 5.0%.
- Increase of tensile strength and increase of modulus of elasticity by the additive heat treatment carried out in the relaxed state are phenomena usually observable in case of easily graphitizing pitch but those having a tensile strength smaller than above-mentioned range after an additive heat treatment is not preferable because resistance to fatique and resistance to oxidation are inferior.
- the tensile strength after the additive heat treatment is preferably in the range of 200 - 450 Kgf/mm2.
- Those having a modulus of elasticity smaller than above-mentioned range are not preferable because resistance to fatique and resistance to oxidation is inferior and change of dimension at the time of working is greater.
- the modulus of elasticity after the additive heat treatment is preferably in the range of 40,000 - 100,000 Kgf/mm2.
- the carbon fibers produced according to the present invention have, preferably a specific gravity of 1.30 - 1.70, a specific electric resistance of 5 ⁇ 108 - 5 ⁇ cm, a stack height of graphitic layers L c (002) of 8 - 32 ⁇ , a graphitic interlayer spacing distance d 002 of 3.46 - 3.49 ⁇ and after strength and modulus have been increased by the additive heat treatment, a stack height of graphitic layers L c (002) of 36 ⁇ or more, increase of a stack height L c (002) of 5 ⁇ or more, a graphitic interlayer spacing distance d 002 is 3.46 ⁇ or less and decrease of interlayer spacing distance d 002 is 0.03 ⁇ or more.
- a specific gravity is 1.35 - 1.60
- a specific electric resistance is 1 ⁇ 108 ⁇ 1 ⁇ 102 ⁇ cm and after strength and modulus have been increased by the additive heat treatment
- a stack height of graphitic layers Lc (002) of 70 -240 ⁇ and a graphitic interlayer spacing distance d 002 is 3.36 - 3.44 ⁇ .
- resulting pitch fibers are wound up on bobbins or without being wound up on bobbins and introduced continuously into an oxidative atmosphere at a maximum temperature of 200 - 400°C while being placed on a transportation belt for thermosetting, subsequently the fibers are subjected to carbonizing treatment in the atmosphere of an inert gas at a temperature of 400 - 1000°C while being placed on a transportation belt, under the condition to make the silicone type oils remaining on the pitch fibers in the adhered state in the amount of 0.1% - 2.0% by weight of said fibers and said fibers are transferred to a next step.
- the spin finish oils and a sizing agent are imparted during the spinning step before the pitch fibers are placed on a transportation belt. The remaining of these chemical agents is effective in improving handling property at the time of winding up of fibers after carbonization or various kind of working.
- any way is allowable so long as reversal of order of fiber-bundles does not occur e.g. such a way where it does not occur that fibers placed afterwards get into the previously formed fiber layers and order of fibers is disturbed.
- a transportation belt is a net conveyer When the fiber-bundles are delivered from a direction close to the vertical to the transportation belt surface, it often happens that they get into the holes of belt or previously formed fiber layers.
- the fibers are subjected to thermosetting in the oxidative atmosphere at a maximum temperature of 200° - 400°C preferably while being placed on a transportation belt after spinning.
- heating temperature it is preferable to select a temperature lower than 200°C at the inlet and to elevate the temperature slowly to give the highest temperature at the outlet, rather than to keep a fixed temperature throughout the whole process.
- Most preferably the maximum temperature is 250 - 350°C.
- the pitch fibers after thermosetting are extremely weak, they cannot be subjected to a treatment in which a force is applied to the fibers. It is preferable to send them into a carbonization apparatus as they are in the state placed on the transportation belt. During the treatment carried out in the state placed on the transportation belt, there is no need of imparting oils or sizing agents.
- the carbonization treatment is carried out at a temperature of 400 - 1000°C in an inert gas atmosphere under the condition in which silicone type oils are remaining in the state adhered on the pitch-based fibers in an amount of 0.1% - 2.0% by weight based upon said fibers.
- an inert gas it is preferable to start from the substitution of the oxidative atmosphere by an inert gas at a temperature close to about 400°C. If the substitution by the inert gas is insufficient, a problem such as a decrease of fiber diameter, insufficiency of an increase of strength or the like may occur.
- Treatment time varies according to the diameter of fibers but it is preferable to elevate the temperature slowly at a rate of 10 - 100°C/min at the beginning and carry out the substitution of the atmosphere sufficiently by an inert gas and to maintain at a constant temperature for several seconds or several hundred seconds in the final stage.
- Resulting fibers are subsequently taken up on bobbin or the like and subjected to a next processing. If necessary after subjecting to a further processing, such as weaving, knitting or the like, an additional carbonization can be applied to produce high strength, high modulus carbon fibers. Further it is possible to treat the fibers at higher temperature to graphitize the fibers. At the time of the additional carbonization, it is possible to stretch the fibers to increase a tensile strength and a modulus of elasticity.
- the carbon fibers obtained according to the present invention differently from the fibers highly carbonized, have a smaller modulus of elasticity, a superiority in cohesiveness of bundles and a superiority in workability to such works as those containing a step of bending at a small radius of curvature e.g. weaving and knitting. Further since the fibers of the present invention are of lower cost than fibers of advanced carbonization state, they are extremely advantageous in case of products which cause a large amount of working loss. Since relaxation of strain occurs at the time of carbonization, they are superior in abrasion resistance and fatique resistance of bent parts of small radium of curvature. Further they show a resistance against a fluff forming by abrasion and against a flexion and a scratching.
- the carbon fibers obtained according to the present invention are liable to be wetted by a resin prepolymer, an adhesive, an oiling agent and a sizing agent and have superior workability.
- the graphitic interlayer spacing distance of the pitch-based carbon fibers of the present invention was measured by using a X-ray diffraction apparatus. Fibers were ground to powder. About 10% by weight of high purity silicon powder for X-ray standard was admixed as a internal standard substance, and mixture was filled in a sample cell. By a X-ray diffractometer method, in which Cu K ⁇ ray was used as a source of ray, carbon 002 diffraction line and the standard. silicon 111 diffraction line were measured,then the diffraction angle of( ⁇ )of carbon 002 plane was calculated from 002 diffraction peak position to which correction relating to Lorentz polarization factor, atomic scattering factor and absorption factor have been made.
- a distillate fraction of a residual oil of a thermal catalytic cracking (FCC) having an initial fraction of 450°C and a final fraction of 560°C (converted to an atmospheric pressure) was subjected to heat treatment at a temperature of 400°C for 6 hours while sending methane gas therein and further heated at a temperature of 330°C for 8 hours to grow mesophase and the mesophase pitch was separated by sedimentation taking advantage of difference of specific gravities.
- This pitch had an optically anisotropic portion of 100%, a quinoline insoluble portion of 43% and a toluene insoluble portion of 82%.
- This pitch was spun through a spinning hole having an enlarged part at an outlet.
- spin finish oils were coated upon the spun fibers according to a common procedure, the pitch fibers were taken up at a rate of 270 m/min. and piled up on a transportation belt while giving waving motion so as to form spiral shape locus.
- the spin finish oils silicone type oils having a heat resistance of 630°C and a viscosity of 230 centi-Stokes was used.
- the amount of adhered spin finish oils was 3.0% based upon the weight of the pitch fibers.
- resulting fibers were subjected to thermosetting by an oxidation treatment with air while elevating a temperature at a rate of 3°C/min. in a furnace having a temperature of 160°C at an inlet and 320°C at an outlet.
- the fibers which came out of a furnace were sent into a carbonization furnace while being kept on the transportation belt.
- the temperature at the inlet was 420°C.
- elevating temperature at a rate of 5°C/min. till 500°C and at a rate of 20°C/min. till 580°C substitution of the atmosphere with an inert gas was carried out.
- the fibers were taken out of the furnace and after reversing the upper and lower layer while putting the fibers between the transportation belt and a second belt, the fibers were wound up on bobbins.
- the amount of the oils remaining on the resulting fibers was 0.25%.
- a tensile strength, a modulus of elasticity, an elongation, a specific gravity and a specific electric resistance were, 27 Kgf/mm2, 820 Kgf/mm2, 3.3%, 1.52 and 2 ⁇ 107 ⁇ cm, respectively.
- the properties of plain woven fabrics before and after the heat treatment in the atmosphere of argon were investigated.
- the woven fabrics of the fibers before the heat treatment were compared after an additive heat treatment carried out in the atmosphere of argon. Both did not show big difference in a tensile strength, an elongation and a modulus of elasticity but the woven fabrics made from the fibers after the heat treatment were slightly bulky, had a tendency of being fluffy by abrasion, and were slightly inferior in resistance to flexion and scratching and the resistance to abrasion of their selvage parts was inferior greatly.
- Example 1 The pitch fibers spun as in Example 1 were wound up on bobbins made of alumina porcelain and subjected to a thermosetting and a carbonization treatment under a condition for heating similar to Example 1. The amount of the oils remaining was 0.09%. It seems that a cooling rate after the carbonization treatment was slow and on this account decomposition loss was large.
- the tensile strength, the elongation, the modulus of elasticity and the crystalline state did not show much difference from Example 1 but the weaving property was greatly inferior, and weaving of the multiple axial fabrics and the three-dimensional fabrics were difficult.
- Example 1 Further when the amount of the spin finish oils after spinning was increased than in Example 1 and the remaining amount was 0.25%, the weaving property became close to Example 1, but the wound-up shape of filaments was worse, breakage of filaments occurred frequently and it was difficult to pass through the preparation step for weaving.
- Pitch fibers spun as Example 1 were taken in a cans made of a heat-proof alloy and subjected to a thermosetting and a carbonization treatment under a temperature-elevating condition similar to Example 1. The remaining amount of the oils was 0.08%. Since a cooling rate after the carbonization treatment was slow as in Comparative example 1, it seems that decomposition loss increased. The tensile strength, the elongation, the modulus of elasticity and the crystalline state of the fibers were not different greatly from these values of Example 1. But because taking out of the cans was difficult, the estimation of the weaving property was difficult.
- Example 1 By using the pitch same with Example 1, spinning was carried out under the same spinning condition with Example 1.
- the fibers after a thermosetting in the state piled up on a transportation belt were subjected to a carbonization treatment by changing the maximum temperature of a carbonization furnace. Then the fibers were wound up on bobbins and the remaining amount of the oils was measured and the working property was evaluated by weaving. The result thereof is shown in Table 1.
- the pitch-based carbon fibers produced according to the present invention are superior in cohesiveness and lubricity of bundles and in processability or workability even when second oils or the like are not imparted after the thermosetting or the carbonization.
- the pitch-based carbon fibers produced according to the present invention can be easily processed than conventional products with no remaining spin finish oils and having higher carbonization grade and are inexpensive in cost because there is no need of an additional imparting of second oils or the like.
- the carbon fibers produced according to the present invention are patient against a bending of small radius of curvature and are superior in resistance to abrasion, to flexion and to scratching of bent parts because the bent parts receive a stress relaxation by the carbonization treatment carried out in the later stage.
- the carbon fibers produced according to the present invention can be used in various kind of fiber reinforced composite materials as they are or after the carbonization treatment or the graphitization treatment. Further they can be used as raw materials for activated carbon fibers.
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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)
- Chemical Treatment Of Fibers During Manufacturing Processes (AREA)
- Treatments For Attaching Organic Compounds To Fibrous Goods (AREA)
Applications Claiming Priority (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP17509/87 | 1987-01-28 | ||
JP1750987 | 1987-01-28 | ||
JP219224/87 | 1987-09-03 | ||
JP62219224A JPH0651928B2 (ja) | 1987-01-28 | 1987-09-03 | ピッチ系炭素繊維と製造方法 |
Publications (3)
Publication Number | Publication Date |
---|---|
EP0276840A2 true EP0276840A2 (de) | 1988-08-03 |
EP0276840A3 EP0276840A3 (de) | 1991-08-07 |
EP0276840B1 EP0276840B1 (de) | 1994-06-29 |
Family
ID=26354041
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP88101195A Expired - Lifetime EP0276840B1 (de) | 1987-01-28 | 1988-01-27 | Pechbasierte Kohlenstoffasern und Verfahren zu deren Herstellung |
Country Status (4)
Country | Link |
---|---|
EP (1) | EP0276840B1 (de) |
JP (1) | JPH0651928B2 (de) |
CA (1) | CA1311883C (de) |
DE (1) | DE3850419T2 (de) |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2767908B2 (ja) * | 1989-07-14 | 1998-06-25 | 三菱化学株式会社 | ピッチ系炭素繊維用処理剤 |
KR102113534B1 (ko) * | 2014-07-24 | 2020-06-02 | 코오롱인더스트리 주식회사 | 원단화가 가능한 전기전도성 탄소섬유 및 그의 제조방법 |
KR102113535B1 (ko) * | 2014-07-24 | 2020-05-21 | 코오롱인더스트리 주식회사 | 탄소섬유 스테이플을 포함하는 방적사 및 그의 제조방법 |
KR20210141499A (ko) * | 2019-03-28 | 2021-11-23 | 도레이 카부시키가이샤 | 탄소 섬유 다발 및 그 제조 방법 |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS6021911A (ja) * | 1983-07-12 | 1985-02-04 | Agency Of Ind Science & Technol | 炭素繊維製品の製造法 |
EP0133457A1 (de) * | 1983-05-27 | 1985-02-27 | Mitsubishi Kasei Corporation | Verfahren zur Herstellung von Kohlenstoffasern aus Pechmaterial |
GB2169920A (en) * | 1985-01-18 | 1986-07-23 | Nippon Oil Co Ltd | Pitch carbon fibres |
JPS62177220A (ja) * | 1986-01-27 | 1987-08-04 | Mitsubishi Chem Ind Ltd | ピツチ系炭素繊維の製造方法 |
EP0297702A2 (de) * | 1987-04-23 | 1989-01-04 | Toa Nenryo Kogyo Kabushiki Kaisha | Kohlenstoff- oder Graphitfasern aus Pech |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS60126324A (ja) * | 1983-12-07 | 1985-07-05 | Nippon Steel Corp | フィラメントの揃いの良い炭素繊維束を製造する方法 |
JPS60173121A (ja) * | 1984-02-16 | 1985-09-06 | Toa Nenryo Kogyo Kk | 炭素繊維及び黒鉛繊維の製造方法 |
JPS6257392A (ja) * | 1985-09-05 | 1987-03-13 | Clarion Co Ltd | 立体バツクアイカメラ |
JPS62133123A (ja) * | 1985-12-05 | 1987-06-16 | Toa Nenryo Kogyo Kk | 炭素繊維及び黒鉛繊維の製造方法 |
-
1987
- 1987-09-03 JP JP62219224A patent/JPH0651928B2/ja not_active Expired - Lifetime
-
1988
- 1988-01-26 CA CA000557363A patent/CA1311883C/en not_active Expired - Fee Related
- 1988-01-27 EP EP88101195A patent/EP0276840B1/de not_active Expired - Lifetime
- 1988-01-27 DE DE19883850419 patent/DE3850419T2/de not_active Expired - Fee Related
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0133457A1 (de) * | 1983-05-27 | 1985-02-27 | Mitsubishi Kasei Corporation | Verfahren zur Herstellung von Kohlenstoffasern aus Pechmaterial |
JPS6021911A (ja) * | 1983-07-12 | 1985-02-04 | Agency Of Ind Science & Technol | 炭素繊維製品の製造法 |
GB2169920A (en) * | 1985-01-18 | 1986-07-23 | Nippon Oil Co Ltd | Pitch carbon fibres |
JPS62177220A (ja) * | 1986-01-27 | 1987-08-04 | Mitsubishi Chem Ind Ltd | ピツチ系炭素繊維の製造方法 |
EP0297702A2 (de) * | 1987-04-23 | 1989-01-04 | Toa Nenryo Kogyo Kabushiki Kaisha | Kohlenstoff- oder Graphitfasern aus Pech |
Non-Patent Citations (1)
Title |
---|
CHEMICAL ABSTRACTS, vol. 107, no. 18, November 1987, page 105, abstract no. 156254z, Columbus, Ohio, US; & JP-A-62 177 220 (MITSUBISHI CHEMICAL INDUSTRIES CO., LTD) 04-08-1987 * |
Also Published As
Publication number | Publication date |
---|---|
DE3850419T2 (de) | 1994-12-01 |
EP0276840A3 (de) | 1991-08-07 |
CA1311883C (en) | 1992-12-29 |
DE3850419D1 (de) | 1994-08-04 |
EP0276840B1 (de) | 1994-06-29 |
JPH0651928B2 (ja) | 1994-07-06 |
JPS63303123A (ja) | 1988-12-09 |
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