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WO2015076534A1 - Isotropic pitch for manufacturing carbon fiber and method for preparing same - Google Patents

Isotropic pitch for manufacturing carbon fiber and method for preparing same Download PDF

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Publication number
WO2015076534A1
WO2015076534A1 PCT/KR2014/010968 KR2014010968W WO2015076534A1 WO 2015076534 A1 WO2015076534 A1 WO 2015076534A1 KR 2014010968 W KR2014010968 W KR 2014010968W WO 2015076534 A1 WO2015076534 A1 WO 2015076534A1
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WIPO (PCT)
Prior art keywords
pitch
isotropic pitch
carbon fiber
producing
isotropic
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Ceased
Application number
PCT/KR2014/010968
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French (fr)
Korean (ko)
Inventor
김진홍
박성범
유도애
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SK Innovation Co Ltd
SK Geo Centric Co Ltd
Original Assignee
SK Innovation Co Ltd
SK Global Chemical Co Ltd
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Publication of WO2015076534A1 publication Critical patent/WO2015076534A1/en
Anticipated expiration legal-status Critical
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Classifications

    • DTEXTILES; PAPER
    • D01NATURAL OR MAN-MADE THREADS OR FIBRES; SPINNING
    • D01FCHEMICAL FEATURES IN THE MANUFACTURE OF ARTIFICIAL FILAMENTS, THREADS, FIBRES, BRISTLES OR RIBBONS; APPARATUS SPECIALLY ADAPTED FOR THE MANUFACTURE OF CARBON FILAMENTS
    • D01F9/00Artificial filaments or the like of other substances; Manufacture thereof; Apparatus specially adapted for the manufacture of carbon filaments
    • D01F9/08Artificial filaments or the like of other substances; Manufacture thereof; Apparatus specially adapted for the manufacture of carbon filaments of inorganic material
    • D01F9/12Carbon filaments; Apparatus specially adapted for the manufacture thereof
    • D01F9/14Carbon filaments; Apparatus specially adapted for the manufacture thereof by decomposition of organic filaments
    • D01F9/145Carbon filaments; Apparatus specially adapted for the manufacture thereof by decomposition of organic filaments from pitch or distillation residues
    • D01F9/155Carbon filaments; Apparatus specially adapted for the manufacture thereof by decomposition of organic filaments from pitch or distillation residues from petroleum pitch
    • CCHEMISTRY; METALLURGY
    • C01INORGANIC CHEMISTRY
    • C01BNON-METALLIC ELEMENTS; COMPOUNDS THEREOF; METALLOIDS OR COMPOUNDS THEREOF NOT COVERED BY SUBCLASS C01C
    • C01B32/00Carbon; Compounds thereof
    • C01B32/05Preparation or purification of carbon not covered by groups C01B32/15, C01B32/20, C01B32/25, C01B32/30
    • CCHEMISTRY; METALLURGY
    • C10PETROLEUM, GAS OR COKE INDUSTRIES; TECHNICAL GASES CONTAINING CARBON MONOXIDE; FUELS; LUBRICANTS; PEAT
    • C10CWORKING-UP PITCH, ASPHALT, BITUMEN, TAR; PYROLIGNEOUS ACID
    • C10C1/00Working-up tar
    • C10C1/19Working-up tar by thermal treatment not involving distillation
    • CCHEMISTRY; METALLURGY
    • C10PETROLEUM, GAS OR COKE INDUSTRIES; TECHNICAL GASES CONTAINING CARBON MONOXIDE; FUELS; LUBRICANTS; PEAT
    • C10CWORKING-UP PITCH, ASPHALT, BITUMEN, TAR; PYROLIGNEOUS ACID
    • C10C3/00Working-up pitch, asphalt, bitumen
    • CCHEMISTRY; METALLURGY
    • C10PETROLEUM, GAS OR COKE INDUSTRIES; TECHNICAL GASES CONTAINING CARBON MONOXIDE; FUELS; LUBRICANTS; PEAT
    • C10CWORKING-UP PITCH, ASPHALT, BITUMEN, TAR; PYROLIGNEOUS ACID
    • C10C3/00Working-up pitch, asphalt, bitumen
    • C10C3/002Working-up pitch, asphalt, bitumen by thermal means
    • DTEXTILES; PAPER
    • D01NATURAL OR MAN-MADE THREADS OR FIBRES; SPINNING
    • D01FCHEMICAL FEATURES IN THE MANUFACTURE OF ARTIFICIAL FILAMENTS, THREADS, FIBRES, BRISTLES OR RIBBONS; APPARATUS SPECIALLY ADAPTED FOR THE MANUFACTURE OF CARBON FILAMENTS
    • D01F9/00Artificial filaments or the like of other substances; Manufacture thereof; Apparatus specially adapted for the manufacture of carbon filaments
    • D01F9/08Artificial filaments or the like of other substances; Manufacture thereof; Apparatus specially adapted for the manufacture of carbon filaments of inorganic material
    • D01F9/12Carbon filaments; Apparatus specially adapted for the manufacture thereof
    • D01F9/14Carbon filaments; Apparatus specially adapted for the manufacture thereof by decomposition of organic filaments
    • D01F9/145Carbon filaments; Apparatus specially adapted for the manufacture thereof by decomposition of organic filaments from pitch or distillation residues

Definitions

  • the present invention relates to an isotropic pitch for producing carbon fibers and a method for manufacturing the same. Specifically, the present invention relates to an isotropic pitch having a specific range of physical properties and structure, and is used to prepare carbon fibers having high strength and high elasticity compared to conventional isotropic carbon fibers. It relates to an isotropic pitch and a method for producing the same.
  • Body weight reduction can also be achieved by the use of high strength steels, aluminum alloys, etc., but carbon fiber reinforced plastics are highly effective, and engine hoods, propeller shafts and hydrogen tanks in automobiles. The trend is already in use.
  • CFRP CFRP is used as the main material of the body structure, weight reduction of about 50% is possible, and the impact energy absorption performance is also improved. Best of all, the lightest car bodies available today can be manufactured, and research is being conducted around the world.
  • CFRP also has a weak point. Tensile strength is weak compared to compression, and interlayer separation is likely to occur due to lamination. After impact, the compressive strength is drastically reduced. In addition, there is a disadvantage that the manufacturing cost is expensive, many applications are difficult. .
  • the carbon fibers included in CFRP may be classified into rayon, PAN, and pitch based on precursors.
  • liquid crystal pitch based carbon fibers and isotropic pitch based on pitch types of precursors It can be divided into carbon fiber.
  • isotropic pitch-based carbon fiber is called general-purpose carbon fiber because it has lower price than high performance grade, and it is produced in staple type carbon island channel by melt blown method, so it can be used as high temperature insulation material or filter. It is used as activated carbon fiber.
  • Japanese Patent Application Laid-Open No. 1996-144131 claims a round pitch for producing carbon fibers having a specific molecular weight, but has a low softening point of 180 to 200 ° C. and a tensile strength of the carbon fiber prepared from the pitch. Its strength is 89.3 kg / mitf (approximately 0.893 GPa) and shows low physical properties to be used for CFRP purposes for automotive steel plates.
  • Patent Document 1 Republic of Korea Patent Publication No. 2013-0059174 (June 05, 2013)"
  • Patent Document 2 Japanese Patent Laid-Open Publication 1996-144131 (June 04, 1996) ''
  • the present inventors conducted a study to solve the above problems, and as a result, invented a method for producing an isotropic pitch having a specific range of physical properties, molecular structure and laminated structure, the isotropic pitch prepared from the conventional isotropic carbon fiber It can be used to make carbon fibers with superior mechanical properties.
  • the present invention is the average diameter of the laminated structure formed by the condensed aromatic ring compound layer
  • An isotropic pitch includes a structure represented by an average number (M) of condensed aromatic ring compound layers included in the laminated structure, which can be represented by distance (d Y ) and (L c / d m ) + l.
  • the present invention is a pre-treatment of any one or a mixture of petroleum heavy oil, high-boiling residue, aromatic hydrocarbon mono- and naphtha cracking process residue to produce a raw material, in the raw material prepared It provides a filtration step of removing the solid material, polymerizing the filtered raw material to produce a basic pitch, and heating the basic pitch to produce the isotropic pitch.
  • the round pitch of the present invention has a softening point and a molecular weight in a specific range, and the generation of insoluble solids and mesophase is suppressed to the maximum in the pitch, so that the spinning property is excellent, the elongation is high, and the tensile strength is remarkably high. Increased to provide isotropic pitch-based carbon fibers that can be used for carbon composite applications.
  • FIG. 1 is a flowchart of a carbon fiber manufacturing process according to a preferred embodiment of the present invention.
  • FIG. 2 is an X-ray diffraction analysis of isotropic pitch in a manufacturing method including a halogenation step.
  • L 4 is an isotropic pitch structure analysis through X-ray diffraction analysis, where d 'is the average distance between condensed aromatic ring compounds in the laminated structure, and ⁇ is the average distance between aliphatic chains connected to the condensed aromatic ring compound.
  • L c is the average diameter of the laminated structure formed by the condensed aromatic ring compound layer
  • L a is the average diameter of the condensed aromatic ring compound layer
  • M is the average number of the condensed aromatic ring compound layers included in the laminated structure. to be.
  • the present invention relates to an isotropic pitch for producing carbon fibers, in which a layer of condensed aromatic cyclic compounds forms a laminated structure.
  • an isotropic pitch for producing carbon fibers and a method for producing the same, wherein the condensed aromatic ring compound is linked with an aliphatic chain.
  • the isotropic pitch of the present invention is excellent in spinning property, so that melt spinning is possible. No single yarn is generated or extremely rare during spinning, and the carbon fiber prepared therefrom has maximized physical properties of high strength and high elasticity.
  • the gamma band ( ⁇ -band) of the al iphat ic chain is found at 17 ⁇ 2 ⁇ ⁇ 18 in X-ray diffraction (XRD). It is an isotropic pitch that includes a structure in which a (002) plane band appears at 23 ⁇ 2 ⁇ ⁇ 25 and a (10) band appears at 43 ⁇ 2 ⁇ ⁇ 45, where the condensed aromatic ring compound is connected by an aliphatic chain.
  • the above structure has an average diameter of the laminated structure formed by the condensed aromatic ring compound layer.
  • the condensed aromatic ring compound may be different depending on the condensed structure but includes at least 2 to 7 aromatic rings, and the condensed aromatic ring compound layer is preferably aromatic.
  • It may be a layer consisting of a compound in which the rings are condensed or a compound layer containing a condensed aromatic ring compound, which may be connected by an aliphatic chain.
  • the laminated structure formed by the condensed aromatic Chora compound layer may be expressed as a nano cluster, and each measurement result of the crystal structure may be represented by XRD measurement results, Bragg equations, and scherrer equations. Can be represented by
  • (L c ) is 10 to 25, preferably 15 to 20, and the level of the condensed aromatic ring compound layer Average diameter (LJ is 5 to 15, preferably 8 to 12, and average distance between condensed aromatic ring compound layers in a laminated structure (dj is 3.50 to 4.50, preferably 3.55 to 4.00, and an aliphatic linked to the condensed aromatic ring compound
  • the average distance between chains ( ⁇ ) is from 4.50
  • the isotropic pitch prepared in the present invention has excellent radioactivity only when the structure satisfies the above range, and there is a very small amount such that non-fused solids and mesofaces are not produced or measured, and the mechanical properties of the carbon fiber produced therefrom This can be maximized.
  • the isotropic pitch of the present invention can be expressed as follows according to the analysis result.
  • the round pitch of the present invention has a (002) plane band at 23 ⁇ 2 ⁇ ⁇ 25, and the following formulas (1) to (4) in which the condensed aromatic ring compound is connected with an aliphatic chain It is an isotropic pitch for producing carbon fiber with a satisfactory structure.
  • the molecular weight of the isotropic pitch is too small, and thus the objective of the isotropic pitch of the present invention It does not satisfy the tensile strength of the carbon fiber, the elongation is too high, the elastic modulus falls.
  • the molecular weight of the isotropic pitch is not only low, but also Tensile strength is significantly reduced.
  • the isotropic pitch may be represented in more detail by further expressing an average distance dy between aliphatic chains connected to the condensed aromatic ring compound in the structure included in the isotropic pitch.
  • an isotropic pitch having better physical properties and radioactivity The mechanical properties of the high strength and high elasticity of the isotropic pitch-based carbon fiber can be produced and can be further maximized.
  • the isotropic pitch softening point of the present invention is 255 to 275 ° C., preferably 260 to
  • the isotropic pitch average molecular weight (Mw) of the present invention is 1500 to 3000, preferably
  • Isotropic pitches having an average molecular weight in the above preferred range can significantly increase the tensile strength in the production of carbon fibers and further increase the elongation rate.
  • the isotropic pitch viscosity is 200 to 500, but may be appropriately adjusted according to the method of producing carbon fibers.
  • the filtration step of b) in the above manufacturing method may be performed even after preparing the basic pitch of C), and the basic pitch of C) is an intermediate material for producing an isotropic pitch. Physical properties may vary.
  • the raw material may include pyrolysis fuel oil (PF0), which is a kind of naphtha decomposition residue oil.
  • PF0 is produced at the bottom (bottom) of the naphtha cracking center (NCC) and has a high degree of aromaticity and abundant resin, which can be used as a raw material of the present invention.
  • Aromatic hydrocarbons are ethyl benzene (ethylbenzene), 1-butenyl eu eu 3-methylbenzene (l- e thenyl-3- methyl benzene ), indene (Indene), 1-ethyl-3-methylbenzene (l -ethyl-3-methyl benzene), 1-methylethyl benzene, 2-ethyl-1,3-dimethylbenzene, 2-dime (hyl benzene), propylenebenzene ( propyl benzene), 1-methyl-4- (2-propenyl) -benzene (l-methyl-4- (2-propenyl) benzene), 1,1a, 6, 6a-tetrahydro-cyclopropanedene (1 , La , 6 , 6a-tetrahydro-
  • Raw material according to an embodiment of the present invention may further include a high boiling point oil.
  • the high boiling fraction according to an embodiment of the present invention refers to a component having a high boiling point and a high carbon number among components that can be obtained by fractional distillation of crude oil, and mainly a hard or heavy aromatic naphtha having 5 or more carbon atoms, preferably 7 or more carbon atoms. May include
  • the high boiling point oil may include an oil having 9 carbon atoms.
  • it may be made of styrene, vinyltoluene, indene, alphamethylstyrene and benzene / luluene / xylene (BTX).
  • the oil having 9 carbon atoms may preferably include indene.
  • Indene is combined with the side chain of the aromatic component in the raw material to prevent the tendency to dehydrate and etherify as the side chain of the aromatic component is oxidized in the stabilization step after melt spinning, resulting in lowering carbonization temperature and time. Can contribute.
  • the high boiling fraction is preferably contained in an amount of 5 to 15% by weight based on 100% by weight of the total raw material. If the content is less than 5% by weight, the effect may be insignificant. The effect may not be obvious
  • the degree of aroma (fa) of the raw material may be 0.7 to 0.9. If the degree of aroma is less than 0.7, the carbonization yield may be lowered. There is no particular limitation on the case where the aromaticity is higher than 0.9, but when the aromaticity is 0.9 or more, the effect by the series of pitch synthesis methods disclosed in the present invention may not be significant.
  • the molecular weight of the raw material may have a distribution of 75 to 350, and preferably may have a distribution of 100 to 250.
  • step a removes low molecular weight substances that are less likely to form oligomers by a polymerization reaction among the compounds included in the raw material, and simultaneously reacts reactions between the compounds contained in the raw material. This is a step of converting a highly reactive and unstable compound contained in the raw material into a more stable and effective compound for producing isotropic pitch.
  • the pretreatment may be carried out by atmospheric distillation at a temperature of 130 to 240 ° C., preferably 150 to 230 ° C., more preferably 190 to 220 ° C. until no volatiles are generated. have.
  • the heating temperature can affect the physical properties of the basic pitch and isotropic pitch, such as the composition ratio of the raw materials and the degree of aroma, and also the mechanical properties of the carbon fibers.
  • the pretreatment step may proceed at atmospheric pressure, but may proceed under reduced pressure. At this time, the pretreatment process may be performed at a lower temperature through decompression, and the pressure and temperature may be freely adjusted within a range capable of obtaining the same effect as the normal pressure.
  • step b) is a filtration step of the pretreated fuel to remove the solid material, and the solid material is a residue of a solid phase containing impurities such as metal, sulfur, and nitrogen from the isotropic pitch. It can act as a cracker in the structure of the carbon fiber to be produced may cause a decrease in strength.
  • Filtration may be carried out in a manner conventionally performed in the art, for example, by filtration, centrifugation, sedimentation, adsorption, extraction, etc.
  • ⁇ 62> filtration step may also be performed after the polymerization of the basic pitch diameter: Yiwu thus is the pre-treatment step may be carried out all of the following basic pitch and polymerization steps. That is, the manufacturing method may be performed after step (c), and in some cases, may be performed after steps (a) and (c), respectively.
  • step C) is a basic pitch manufacturing step, in which a raw pitch having a high softening point is produced without generating mesophases by heating the raw material that has undergone the filtration step at the same time. It can proceed by law or thermal polymerization.
  • the halogenation method may proceed by heating after further adding a halogen compound and a radical initiator, and preferably by adding and mixing a halogen compound after the addition of the radical initiator.
  • Halogenated compounds are chlorine (Cl 2 ), thionyl chloride (S0C 1 2 ), sulfuryl chloride
  • radical initiator is benzoyl peroxide (B enZ0 yi peroxide), di-butyl hydroperoxide oxazol id (di-t-butyl hydroperoxide) , acetyl peroxide (Acetyl peroxide) such yugigwa oxide (Organi c Peroxide) and, Azo Azo compounds such as bisisobutyronitrile (AIBN; ⁇ , ⁇ '-Azobisisobutyroni tr ile), azobismethylisobutylate ( ⁇ , a' -Azobi smethyl i sobutyrate), or a group consisting of a combination of two or more of these The one selected from can be used.
  • the radical initiator may be included in an amount of 1 to 30 parts by weight, more preferably 5 to 20 parts by weight, based on 100 parts by weight of the halogen compound.
  • Halogenation is carried out by halogenation reaction at 100 to 12 (0.5 to 2 hours at C to replace hydrogen in the aromatic alkyl group with halogen, followed by polymerization by dehalogenation reaction at 300 to 330 ° C. for 2 to 4 hours.
  • the dehalogenation reaction can further enhance the purity of the basic pitch produced by decomposing halogen compounds and radical initiators that may remain in the basic pitch after the reaction, particularly in the dehalogenation reaction.
  • banung temperature is good is not more than 330 ° C, 330 ° C in excess of, the process advances upset anisotropic screen or coking of the basic pitch of the excess polymerization only occurs actively decomposition of the halogenated compound and a radical initiator as a result of the carbon fiber machine Physical properties are greatly reduced.
  • the basic pitch prepared by the halogenation method may have a softening point of 70 to 130 C, preferably 115 to 125 ° C.
  • Thermal polymerization can be carried out at 350 to 380 ° C. for 0.1 to 2 hours.
  • the thermal polymerization method may proceed in an inert gas atmosphere, and may proceed by fractionating gaseous by-products generated during the process of nitrogen and polycondensat ion.
  • the reaction temperature should not exceed 380 ° C. However, when the reaction temperature exceeds 380 ° C, the reaction temperature exceeds the range of uniform anisotropy pitch for the present invention, as in the halogenation method. Excess mesophase may be produced or coking may result in uneven carbon fibers.
  • the basic pitch prepared by the thermal polymerization method may have a softening point of 85 to 140 ° C., preferably 115 to 125 ° C.
  • the physical properties of the basic pitch can be adjusted according to the configuration convenience.
  • the condensation aromatics of the basic pitch manufactured from the step (c) To the absolute amount of the ligomer linked to the ring compound It may further include a compound having a low boiling point in a range that does not significantly affect.
  • step (c) is carried out under pressurization, where the ' softening point of the basic pitch is applied to the physical properties, molecular structure and laminated structure of the isotropic pitch that is finally manufactured according to the convenience of the process configuration. You can freely adjust the range without affecting it.
  • step d) may be a process of manufacturing isotropic pitch capable of suppressing mesophase generation by promoting evaporation by heating the basic pitch as an isotropic manufacturing step.
  • the isotropic pitch manufacturing step may proceed with a conventional thin film distillation method, and thus, there is an advantage that an additional process of suppressing the formation of mesophase and removing insoluble solids is not necessary.
  • the isotropic pitch manufacturing step according to an embodiment of the present invention may correspond to the composition and state change of the isotropic pitch manufactured with a multi-stage thin film distillation apparatus.
  • the isotropic pitch manufacturing step may be performed by heating in a vacuum atmosphere for 0.1 to 1 hour at 300 to 350 ° C.
  • the heating temperature exceeds 350 ° C.
  • meso phases are partially formed, and insoluble carbon solids may be generated by the continuous heating, and it is preferable to observe the heating temperature and the heating time.
  • Isotropic pitch may have a softening point of 255 to 275 ° C, preferably 260 to 270 ° C.
  • the isotropic pitch average molecular weight (Mw) of the present invention may be 1500 to 3000, preferably 1700 to 2850. Since the average molecular weight and softening point of the isotropic pitch can greatly affect the physical properties of the carbon fibers to be produced, it is preferable to comply with the manufacturing process conditions.
  • the isotropic pitch produced in the present invention is capable of melt spinning, and does not have single yarn or extremely rare spinning when spinning.
  • Melt spinning is a method of melting polymer materials or pitches into continuous fibers, eliminating the need for expensive solvents for spinning, and simplifying the construction of spinning processes and significantly reducing costs. Way.
  • pitch spinning should be excellent, but the isotropic pitch prepared according to the present invention has very good spinning property, and melt spinning for carbon fiber manufacturing is possible, but the single yarn is extremely rare. Does not happen.
  • the isotropic pitch capable of melt-spinning of the present invention has a very high radioactivity compared to the isotropic pitch which was used to produce short fibers through melt-blowing, and thus it has high strength and high elastic carbon long fibers. It can also be manufactured. According to one embodiment of the present invention, as a result of measuring the isotropic pitch for 20 minutes in a row with the frequency of melt spinning off as a single shot frequency, it can be seen that the single yarn frequency corresponds to 0, which is very excellent in radioactivity.
  • the isotropic pitch of the present invention can be carbonized at a low temperature of 700 to 1200 ° C or less to minimize the energy consumption during the carbonization process.
  • the isotropic pitch prepared according to the present invention may produce carbon fibers through a stabilization step and a carbonization step after melt spinning.
  • the carbon fiber is manufactured from the isotropic pitch prepared according to the embodiment of the present invention, it is possible to produce an isotropic pitch-based carbon fiber having a high tensile strength of at least 1.5 GPa or more and an elongation rate of at least 1.5 GPa.
  • the isotropic pitch-based carbon fiber as described above is maximized in physical properties, unlike conventional isotropic pitch-based carbon fiber is used as a general-purpose carbon material can be used in various ways to the carbon composite material required high strength, high elastic carbon fiber.
  • the isotropic pitch of the present invention is preferably used for producing carbon fibers, but is not limited thereto, and may be used for manufacturing various carbon materials.
  • Yield Yield was calculated by the weight of the final pitch obtained relative to the weight of the naphtha cracking residue oil charged.
  • the stress-strain curve was measured with a UTM Jniversal Test Machine equipped with a 2N load cell on a sample of carbon fiber. Calculated from the diameter of the fiber analyzed by and electron microscopy.
  • the molecular composition of the pitch was analyzed by GOAED and the distribution of molecular weight was measured by GPC and the average molecular weight was obtained from the results.
  • X-ray diffractometer for molecular structure analysis of isotropic pitch uses Cu cathode.
  • the K-c wavelength was 1.540598, the voltage of the X-ray generator was 40KV, and the tube current was 3 (1 ⁇ 2A).
  • JE0L's T0F-MS was used to analyze the molecular structure.
  • the laser source was analyzed using Nd: YAG, laser intensity 5OT, mass range 10-3,000 and spiral measurement mode.
  • Oi KNCBO Oi KNCBO
  • Examples 1 to 4 prepared NCB0 at 190, 200, 210 and 220 ° C., respectively.
  • Comparative Example 3 was each subjected to a pretreatment step at 250 ° C. atmospheric distillation, after which the solid material was removed by filtration. In Comparative Example 1, the solid material was removed by filtration without performing the pretreatment step.
  • the structure of the prepared isotropic pitch was analyzed by X-ray diffractometer, and the gamma band ( ⁇ -band) of aliphatic chain was found in XRD of 17 ⁇ 2 ⁇ ⁇ 18, In the laminate structure of the condensed aromatic ring compound at 23 ⁇ 2 ⁇ ⁇ 25, the (10) plane band was shown at 43 ⁇ 2 ⁇ ⁇ 45 (FIG. 2). Table 6 below shows the results of the structural analysis.
  • Examples 5 to 8 performed the pre-treatment steps of the prepared NCB0 at 190, 200, 210, and 220 ° C, respectively, in Comparative Example 4 at 120 ° C, and Comparative Example 5 by atmospheric distillation at 250 ° C. The solids were removed by filtration. Comparative Example 3 removed the solid material through filtration without performing the pretreatment step.
  • an isotropic pitch was prepared by heating the basic pitches in a vacuum atmosphere at 340 ° C. for 30 minutes. After the process was completed, the softening point, viscosity and average molecular weight of the isotropic pitch were measured and described in Table 8 below.
  • the isotropic pitch produced by the halogenation method and the thermal polymerization method in the manufacturing step of the basic pitch was 17 ⁇ 2 ⁇ ⁇ 18 and the gamma band ( ⁇ ) of aliphatic chain ( ⁇ ) — Band), the (002) plane and the (10) plane band appeared at 43 ⁇ 2 ⁇ ⁇ 45 in the laminate structure of the condensed aromatic ring compound at 23 ⁇ 2 ⁇ ⁇ 25.
  • Table 10 shows the measurement results of the physical properties and structures of the isotropic pitch prepared according to all the above Examples and Comparative Examples.
  • the condensed aromatic ring compound in the structure of the isotropic pitch contained at least 2 to 7 aromatic rings, and in Table 10, the average interplanar distance (d m ) of the condensed aromatic ring compound layer was 3.594-3.965 A. Average diameter ( ⁇ ) of aliphatic chains connected to the condensed aromatic ring compound was 4.829--5.172A, and the average diameter of the isotropic pitch cluster ( L c ) belongs to 16-20 A.
  • the average number of condensed aromatic ring compound layers stacked in an isotropic pitch cluster (M) can be expressed as (L c / d + l and in 5.3 to 6.5 genus did.
  • the average number (M) of condensed aromatic ring compound layers stacked in an isotropic pitch cluster can be expressed as (L c / d + l and belongs to 5.3 to 6.5.
  • Carbon fibers were prepared using an isotropic pitch.
  • an isotropic pitch was injected into a cylindrical container, and then melt spun by applying a pressure of 0.8 kgf / cm 2 in a nitrogen atmosphere. At this time, the diameter of the winding machine was 150 ⁇ , the winding speed was 700rpm.
  • the spun fibers were each charged in a tubular electric furnace and then fed with air at a flow rate of 150 i / min.
  • the temperature was raised at a rate of 1 ° C / min, stabilized by maintaining for 1 hour after reaching 290 ° C.
  • nitrogen was injected at a rate of 150ml / min and at the same time heated up at a rate of 5 ° C / niin to reach 800 ° C and maintained for 0.5 hours to prepare a carbon fiber.
  • the radioactivity of the isotropic pitch and the physical properties of the prepared carbon fiber are shown in Table 1 below.
  • Comparative Examples and Examples were melt-spun, and in Table 11, high-strength carbon fibers having a tensile strength of at least 1.5 GPa and at most 2.0 GPa without single yarns were produced in each Example. 2. It belongs to 1 ⁇ 2.7%, and the diameter of carbon fiber belongs to 4.30-11.40 ⁇ . On the other hand, Comparative Example 1 has a low elastic modulus due to excessively high elongation ratio of 3.2 GPa to 3.2%, and Comparative Example 2 l.
  • the elastic modulus was low because the elongation ratio was too high compared to the tensile strength of lGPa, and Comparative Examples 3 and 4 had a high single yarn frequency, and Comparative Examples 4, 5, and 6 each carried out a tensile strength of 0.7, 0.9, and 0.9, respectively. Compared to yes Significantly lowered tensile strength.

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Abstract

The present invention relates to an isotropic pitch for manufacturing a carbon fiber and a method for preparing the same, wherein an isotropic pitch having particular ranges of a softening point, viscosity, a molecular weight, and a crystal structure can be prepared, and such a feature can maximize mechanical properties of the carbon fiber by maximally suppressing the generation of insoluble solids and mesophase of the pitch, and can also reduce energy consumption since a carbonization process is performed at a low temperature.

Description

【망세서】  [Hostess]

【발명의 명칭】  [Name of invention]

탄소섬유 제조용 등방성 피치 및 이의 제조방법  Isotropic pitch for producing carbon fiber and its manufacturing method

【기술분야】  Technical Field

<ι> 본 발명은 탄소섬유 제조용 등방성 피치 및 이의 제조방법에 관한 것으로, 구체적으로 특정범위의 물성 및 구조를 가지는 등방성 피치로서 기존의 등방성 탄 소섬유에 비하여 고강도, 고탄성인 탄소섬유의 제조에 사용될 수 있는 등방성 피치 및 이의 제조방법에 관한 것이다.  The present invention relates to an isotropic pitch for producing carbon fibers and a method for manufacturing the same. Specifically, the present invention relates to an isotropic pitch having a specific range of physical properties and structure, and is used to prepare carbon fibers having high strength and high elasticity compared to conventional isotropic carbon fibers. It relates to an isotropic pitch and a method for producing the same.

【배경기술】 ' [Background Art] "

<2> 자동차의 저연비화는 석유자원의 고갈과 가격 인상 및 환경문제 등으로 더욱 요구되고 있다. 워킹그룹 보고서에 의하면 2020년에는 지금보다 에너지효율이 600% 이상 증대될 것으로 예견하고 있는데, 엔진의 하이브리드화를 통해 가장 큰 효과가 있으며, 엔진효율 개선, 차체의 경량화, 에너지의 전달효율 개선 순으로 효과가 있 음을 언급하고 있다. ᅳ특히 미국에너지국 (DOE)에 따르면. 차체 무게를 10% 감소시키 면 대략 7%의 연료 절감이 가능하다고 밝히고 있어, 차체의 경량화에 대한 기술개 발이 더욱 요구되는 실정이다. <2> Low fuel consumption of automobiles is increasingly required due to exhaustion of petroleum resources, price hikes and environmental issues. According to the Working Group's report, energy efficiency is expected to increase by more than 600% by 2020. The most effective is the hybridization of the engine, followed by the improvement of the engine efficiency, the weight of the car body, and the efficiency of energy transfer. It is said to work. In particular, according to the US Department of Energy. Reducing the body weight by 10% reduces fuel consumption by approximately 7%, which requires more technical development to reduce the weight of the body.

<3> 차체 경량화는 고장력강, 알루미늄 합금 등의 사용으로도 달성할 수 있으나, 탄소섬유강화플라스틱 (carbon f iber reinforced pl ast i c)적용이 효과가 크며, 자동 차에서 엔진후드, 프로펠러샤프트 및 수소탱크 등에 이미 사용하고 있는 추세이다. CFRP를 차체구조의 주요재료로 사용하는 경우, 50% 가량의 중량경감이 가능하며, 여기에 충돌에너지 흡수성능도 향상된다. 무엇보다도, 현재 이용 가능한 재료 중에 제일 가벼운 차체를 제조할 수 있어 세계 각국에서 연구가 활발하다.  <3> Body weight reduction can also be achieved by the use of high strength steels, aluminum alloys, etc., but carbon fiber reinforced plastics are highly effective, and engine hoods, propeller shafts and hydrogen tanks in automobiles. The trend is already in use. When CFRP is used as the main material of the body structure, weight reduction of about 50% is possible, and the impact energy absorption performance is also improved. Best of all, the lightest car bodies available today can be manufactured, and research is being conducted around the world.

<4> 그러나 CFRP에도 약점이 있는데, 인장강도가 압축에 비해 약하며, 층격에 의 해 층간박리가 발생하기 쉬어. 충격 후 압축강도가 급격히 감소하게 된다. 또한 제 조비용이 비싸 많은 적용이 어렵다는 단점이 있다. .  <4> However, CFRP also has a weak point. Tensile strength is weak compared to compression, and interlayer separation is likely to occur due to lamination. After impact, the compressive strength is drastically reduced. In addition, there is a disadvantage that the manufacturing cost is expensive, many applications are difficult. .

<5> 일반적으호 CFRP에 포함되는 탄소섬유는 전구체에 따라 레이온계, PAN계, 피 치계 등으로 나눌 수 있으며, 이 중 피치계는 전구체인 피치의 종류에 따라 액정 피치계 탄소섬유와 등방성 피치계 탄소섬유로 나눌 수 있다. 그 증에서도 등방성 피치계 탄소섬유는 고성능 그레이드에 비해 저렴한 가격을 가져 범용 탄소섬유라고 도 불리고 있으며, 멜트 블로운 (mel t bl own) 방식에 의해 스테이폴 형태의 탄소섬 유로 생산되어 고온 단열재나 필터용 활성탄소섬유로 사용되고 있다.  <5> In general, the carbon fibers included in CFRP may be classified into rayon, PAN, and pitch based on precursors. Among them, liquid crystal pitch based carbon fibers and isotropic pitch based on pitch types of precursors It can be divided into carbon fiber. In addition, isotropic pitch-based carbon fiber is called general-purpose carbon fiber because it has lower price than high performance grade, and it is produced in staple type carbon island channel by melt blown method, so it can be used as high temperature insulation material or filter. It is used as activated carbon fiber.

<6> 석유, 콜 타르, 또는 화학 피치를 원료로 하여 탄소섬유를 제조하는 것은 많 은 이점이 있는데, 그 이유 중 하나는 이들 원료의 탄소 대 수소 비가 높다는 것이 다. 예를 들어, PAN 수지로부터 제조되는 탄소섬유의 이론 수득률은 50%정도에 그 치지만, 잘 정제된 피치로부터 제조되는 탄소섬유의 이론 수득률은 90%에 달한다. 그러나, 우주, 항공 분야 등에 복합재로 사용 가능한 층분한 인장강도와 모들러스 를 갖춘 피치계 탄소섬유는 액정 피치로부터 제조되며, 석유, 콜 타르, 또는 화학 피치로부터 액정 피치를 제조하기 위해서는 전처리, 수소화, 퀴놀린 불용분의 분리 등의 복잡한 공정이 필요하며, 이에 따라 생산 비용이 증가하여 가격이 비싸다는 단점이 있다. [6] There are many advantages to producing carbon fibers from petroleum, coal tar, or chemical pitches. One of the reasons is the high carbon-to-hydrogen ratio of these raw materials. All. For example, the theoretical yield of carbon fiber produced from PAN resin is about 50%, while the theoretical yield of carbon fiber produced from well-purified pitch reaches 90%. However, pitch-based carbon fibers with striking tensile strength and modulus that can be used as composites in aerospace, aerospace, etc. are manufactured from liquid crystal pitches. To prepare liquid crystal pitches from petroleum, coal tar, or chemical pitches, pretreatment, hydrogenation, Complex processes such as the separation of quinoline insolubles are required, and thus, there is a disadvantage that the production cost increases and the price is high.

<7> 등방성 피치계 탄소섬유 또는 탄소섬유 제조를 위한 등방성 피치에 관한 종 래기술로는 대한민국 공개특허 10-2013-0059174, 일본 공개특허 1996-144131 등이 있다. 이중 10-2013— 0059174에서는 고연화점을 갖는 탄소섬유용 전구체 제조법을 기재하고 있으나, 피치의 가열온도가 360 °C 이상으로 부분적으로 불융 고형분이 생 성되거나 메조페이즈가 생성되어, 그 결과 제조된 탄소섬유의 물성이 떨어지는 단 점이 있다. Conventional techniques related to isotropic pitch-based carbon fibers or isotropic pitches for producing carbon fibers include Korean Patent Laid-Open Publication No. 10-2013-0059174, Japanese Patent Laid-Open Publication No. 1996-144131, and the like. 10-2013—0059174 describes a method for preparing a precursor for carbon fibers having a high softening point, but partially melted solids or mesophases are formed at a pitch heating temperature of 360 ° C. or higher, resulting in carbon produced. There is a disadvantage of poor physical properties of the fiber.

<8> 또한 일본 공개특허 1996-144131에서는 특정범위의 분자량을 가지는 탄소섬 유 제조용 둥방성 피치를 청구하고 있으나, 피치의 연화점이 180 내지 200°C로 낮 으며, 피치로부터 제조된 탄소섬유의 인장강도가 89.3 kg/mitf (약 0.893 GPa)로 차량 용 강판 등을 목적으로 한 CFRP용도로사용되기에는 낮은 물성을 보이고 있다.In addition, Japanese Patent Application Laid-Open No. 1996-144131 claims a round pitch for producing carbon fibers having a specific molecular weight, but has a low softening point of 180 to 200 ° C. and a tensile strength of the carbon fiber prepared from the pitch. Its strength is 89.3 kg / mitf (approximately 0.893 GPa) and shows low physical properties to be used for CFRP purposes for automotive steel plates.

<9> 이처럼 CFRP에 사용될 수 있는 필요 물성올 모두 만족하면서 낮은 생산비용 으로 대량 생산이 가능한 등방성 피치를 이용한 탄소섬유 제조기술의 개발이 강력 히 요구되고 있다. As such, there is a strong demand for the development of carbon fiber manufacturing technology using isotropic pitches that satisfy all the necessary properties that can be used for CFRP and can be mass-produced at low production costs.

<ιο> 「(특허문헌 1)대한민국 공개특허 1으 2013-0059174(2013년 06월 05일)」 <ιο> "(Patent Document 1) Republic of Korea Patent Publication No. 2013-0059174 (June 05, 2013)"

<ι ι> 「(특허문헌 2)일본 특허공개공보 1996-144131( 1996년 06월 04일)」 <ι ι> `` (Patent Document 2) Japanese Patent Laid-Open Publication 1996-144131 (June 04, 1996) ''

【발명의 상세한 설명】  [Detailed Description of the Invention]

【기술적 과제】  [Technical problem]

본 발명자들은 상기 문제점을 해소하기 위해 연구를 거듭한 결과, 특정 범위 의 물성, 분자구조와 적층구조를 가지는 등방성 피치의 제조방법을 발명하였고, 이 로부터 제조된 등방성 피치는 종래의 등방성 탄소섬유에 비해 월등한 기계적 물성 을 가지는 탄소섬유를 제조하는데 사용될 수 있다.  The present inventors conducted a study to solve the above problems, and as a result, invented a method for producing an isotropic pitch having a specific range of physical properties, molecular structure and laminated structure, the isotropic pitch prepared from the conventional isotropic carbon fiber It can be used to make carbon fibers with superior mechanical properties.

【기술적 해결방법】  Technical Solution

<13> 본 발명은 축합방향족 고리 화합물 층이 형성하는 적층 구조의 평균 직경 <13> The present invention is the average diameter of the laminated structure formed by the condensed aromatic ring compound layer

(Lc) , 적층 구조에서 축합방향족 고리 화합물 층간 평균 거리 (dj , 축합방향족 고리 화합물 층의 평균 직경 (La) , 축합방향족 고리 화합물에 연결된 지방족 사슬간 평균 거리 (dY ) 및 (Lc/dm)+l로 나타낼 수 있는 상기 적층 구조에 포함된 축합방향족 고리 화합물 층의 평균 개수 (M)로 표현되는 구조를 포함하는 등방성 피치를 제공한다. <14> 본 발명은 석유계 중질유, 고비점 잔사유, 방향족 탄화수소 단물질 및 나프 타 분해공정 잔사유에서 선택되는 어느 하나 또는 이들의 혼합물인 전처리하여 원 료를 생성하는 단계, 상기 제조된 원료에서 고상 물질을 제거하는 여과단계, 여과 된 원료를 중합하여 베이직 피치를 제조하는 단계 및 베이직 피치를 가열하여 상기 등방성 피치를 제조하는 제조방법을 제공한다. (L c ), the average distance between condensed aromatic ring compound layers in the laminated structure (dj, the average diameter of the condensed aromatic ring compound layer (L a ), the average of aliphatic chains connected to the condensed aromatic ring compound An isotropic pitch is provided that includes a structure represented by an average number (M) of condensed aromatic ring compound layers included in the laminated structure, which can be represented by distance (d Y ) and (L c / d m ) + l. <14> The present invention is a pre-treatment of any one or a mixture of petroleum heavy oil, high-boiling residue, aromatic hydrocarbon mono- and naphtha cracking process residue to produce a raw material, in the raw material prepared It provides a filtration step of removing the solid material, polymerizing the filtered raw material to produce a basic pitch, and heating the basic pitch to produce the isotropic pitch.

【유리한 효과】  Advantageous Effects

<15> 본 발명의 둥방성 피치는 특정범위의 연화점 및 분자량을 가지고, 상기 피치 내에서 불용고형분과 메조페이스 (tnesophase ) 생성이 최대한 억제되어 방사성이 매 우 우수하며, 신장률이 높고 인장강도가 현저히 증가되어 탄소복합재 용도로 사용 가능한 등방성 피치계 탄소섬유를 제공한다.  The round pitch of the present invention has a softening point and a molecular weight in a specific range, and the generation of insoluble solids and mesophase is suppressed to the maximum in the pitch, so that the spinning property is excellent, the elongation is high, and the tensile strength is remarkably high. Increased to provide isotropic pitch-based carbon fibers that can be used for carbon composite applications.

【도면의 간단한 설명】  [Brief Description of Drawings]

<16> 도 1은 본 발명의 바람직한실시예에 따른 탄소섬유 제조공정의 흐름도이다. <17> 도 2는 할로겐화 단계를 포함하는 제조방법에서의 등방성 피치의 X-선 회절 분석 결과이다.  1 is a flowchart of a carbon fiber manufacturing process according to a preferred embodiment of the present invention. FIG. 2 is an X-ray diffraction analysis of isotropic pitch in a manufacturing method including a halogenation step.

<! 8> 도 3은 열중합 단계를 포함하는 제조방법에서의 등방성 피치의 X-선 회절분 석 결과이다.  <! 8> X-ray diffraction analysis of the isotropic pitch in the manufacturing method including the thermal polymerization step.

<19> 도 4은 X—선 회절분석을 통한 등방성피치 구조 해석 그림으로, d„,는 적층 구 조에서 축합방향족 고리 화합물 층간 평균 거리이고, ^는 축합방향족 고리 화합물 에 연결된 지방족 사슬간 평균 거리이고, Lc는 축합방향족 고리 화합물 층이 형성하 는 적층 구조의 평균 직경이고, La는 축합방향족 고리 화합물 층의 평균 직경이며, M은 상기 적층 구조에 포함된 축합방향족 고리 화합물 층의 평균 개수이다. 4 is an isotropic pitch structure analysis through X-ray diffraction analysis, where d 'is the average distance between condensed aromatic ring compounds in the laminated structure, and ^ is the average distance between aliphatic chains connected to the condensed aromatic ring compound. L c is the average diameter of the laminated structure formed by the condensed aromatic ring compound layer, L a is the average diameter of the condensed aromatic ring compound layer, and M is the average number of the condensed aromatic ring compound layers included in the laminated structure. to be.

<20>  <20>

【발명의 실시를 위한 형태】  [Form for implementation of invention]

<21> 이하 첨부된 도면들을 참조하여 본 발명에 따른 탄소섬유 제조용 등방성 피 치 및 이의 제조방법에 대하여 상세히 설명한다. 다음에 소개되는 도면들은 당업자 에게 본 발명의 사상이 층분히 전달될 수 있도록 하기 위해 예로서 제공되는 것이 다. 따라서, 본 발명은 이하 제시되는 도면들에 한정되지 않고 다른 형태로 구체화 될 수도 있으며, 이하 제시되는 도면들은 본 발명의 사상을 명확히 하기 위해 과장 되어 도시될 수 있다. 또한 명세서 전체에 걸쳐서 동일한 참조번호들은 동일한 구 성요소들을 나타낸다. Hereinafter, an isotropic pitch for producing carbon fibers and a method for manufacturing the same according to the present invention will be described in detail with reference to the accompanying drawings. The drawings introduced below are provided as examples in order to enable those skilled in the art to fully convey the spirit of the present invention. Therefore, the present invention is not limited to the drawings presented below and may be embodied in other forms, and the drawings presented below may be exaggerated to clarify the spirit of the present invention. Also, like reference numerals designate like elements throughout the specification. Represents the elements.

<22> 이때, 사용되는 기술 용어 및 과학 용어에 있어서 다른 정의가 없다면, 이 발명이 속하는 기술 분야에서 통상의 지식을 가진 자가 통상적으로 이해하고 있는 의미를 가지며, 하기의 설명 및 첨부 도면에서 본 발명의 요지를 불필요하게 흐릴 수 있는 공지 기능 및 구성에 대한 설명은 생략할 수 있다.  In this case, unless there is another definition in the technical terms and scientific terms used, it has the meaning commonly understood by those of ordinary skill in the art to which the present invention belongs, the present invention in the following description and the accompanying drawings Descriptions of well-known functions and configurations that may unnecessarily obscure the subject matter may be omitted.

<23> 본 발명은 탄소섬유 제조용 등방성 피치에 관한 것으로 축합방향족 고리 화 합물 층이 적층구조를 형성하고 . 축합방향족 고리 화합물이 지방족사슬로 연결된 구조를 포함하는 탄소섬유 제조용 등방성 피치 및 이의 제조방법을 제공한다.  The present invention relates to an isotropic pitch for producing carbon fibers, in which a layer of condensed aromatic cyclic compounds forms a laminated structure. Provided is an isotropic pitch for producing carbon fibers and a method for producing the same, wherein the condensed aromatic ring compound is linked with an aliphatic chain.

<24> 본 발명의 등방성 피치는 방사성이 매우 우수하여 용융방사가 가능하며, 방 사시 단사가 발생하지 않거나 극히 드물고 , 이로부터 제조된 탄소섬유는 고강도 및 고탄성의 극대화된 물성을 가진다.  The isotropic pitch of the present invention is excellent in spinning property, so that melt spinning is possible. No single yarn is generated or extremely rare during spinning, and the carbon fiber prepared therefrom has maximized physical properties of high strength and high elasticity.

<25> 먼저, 본 발명의 등방성 피치에 대하여 자세히 설명한다.  First, the isotropic pitch of the present invention will be described in detail.

<26> 본 발명의 등방성 피치는 X-선 회절분석 (X-ray di f fract ion , XRD)에서 17<2 θ<18에서 지방족사슬 (al iphat i c chain)의 감마 밴드 ( γ -band)가 나타나고, 23<2 θ<25에서 (002)면 밴드가 나타나며, 43<2 Θ<45에서 ( 10) 밴드가 나타나는 축합방 향족 고리 화합물이 지방족 사슬로 연결된 구조를 포함하는 등방성 피치이다.  In the isotropic pitch of the present invention, the gamma band (γ-band) of the al iphat ic chain is found at 17 <2 θ <18 in X-ray diffraction (XRD). It is an isotropic pitch that includes a structure in which a (002) plane band appears at 23 <2θ <25 and a (10) band appears at 43 <2θ <45, where the condensed aromatic ring compound is connected by an aliphatic chain.

<27> 상기 구조는 축합방향족 고리 화합물 층이 형성하는 적층 구조의 평균 직경 The above structure has an average diameter of the laminated structure formed by the condensed aromatic ring compound layer.

(Lc) , 축합방향족 고리 화합물 층의 평균 직경 (L , 적층 구조에서 축합방향족 고리 화합물 층간 평균 거리 (d,,,) 및 (Lc/d,,,)+l로 나타낼 수 있는 상기 적층 구조에 포함 된 축합방향족 고리 화합물 층의 평균 개수 (M)로 설명될 수 있다. 그리고.. 축합방 향족 고리 화합물들은 지방족 사슬로 연결되어 있고 축합방향족 고리 화합물에 연 결된 지방족 사슬간의 평균 거리 ( )도 상기 구조를 설명하는데 더해질 수 있다. 상기 축합방향족 고리 화합물은 축합된 구조에 따라 상이할 수 있으나 최소 2 내지 최대 7개의 방향족 고리를 포함한 화합물이고, 상기 축합방향족 고리 화합물 층이 란 바람직하게는 방향족고리들이 축합된 화합물로 이루어진 층이나 축합방향족 고 리 화합물이 포함된 화합물 층일 수 있고 이들이 지방족 사슬에 의하여 연결되어 있을 수 있다. 또한, 상기 축합방향족 고라 화합물 층이 형성하는 적층 구조는 나 노 클러스터 (nano cluster)라고 표현될 수도 있다. 상기 결정구조의 각 측정결과 는 XRD측정결과, 브래그식 (Bragg) 및 scherrer식에 의해 나타낼 수 있다. (L c ), the average diameter of the condensed aromatic ring compound layer (L, the lamination structure represented by the average distance (d ,,,) and (L c / d ,,,) + l between the condensed aromatic ring compound layers in the laminated structure. It can be described as the average number of condensed aromatic ring compound layers (M) in the structure, and the average distance between aliphatic chains connected by condensed aromatic ring compounds and connected to the condensed aromatic ring compound (M). The condensed aromatic ring compound may be different depending on the condensed structure but includes at least 2 to 7 aromatic rings, and the condensed aromatic ring compound layer is preferably aromatic. It may be a layer consisting of a compound in which the rings are condensed or a compound layer containing a condensed aromatic ring compound, which may be connected by an aliphatic chain. In addition, the laminated structure formed by the condensed aromatic Chora compound layer may be expressed as a nano cluster, and each measurement result of the crystal structure may be represented by XRD measurement results, Bragg equations, and scherrer equations. Can be represented by

<28> 구체적으로 , 축합방향족 고리 화합물 층이 형성하는 적층 구조의 평균 직경 Specifically, the average diameter of the laminated structure formed by the condensed aromatic ring compound layer

(Lc)은 10 내지 25 , 바람직하게는 15 내지 20이고, 축합방향족 고리 화합물 층의 평 균 직경 (LJ은 5 내지 15, 바람직하게는 8 내지 12이고, 적층 구조에서 축합방향족 고리 화합물 층간 평균 거리 (dj는 3.50 내지 4.50, 바람직하게는 3.55 내지 4.00이 고, 축합방향족 고리 화합물에 연결된 지방족 사슬간의 평균 거리 (^ )는 4.50 내지(L c ) is 10 to 25, preferably 15 to 20, and the level of the condensed aromatic ring compound layer Average diameter (LJ is 5 to 15, preferably 8 to 12, and average distance between condensed aromatic ring compound layers in a laminated structure (dj is 3.50 to 4.50, preferably 3.55 to 4.00, and an aliphatic linked to the condensed aromatic ring compound The average distance between chains (^) is from 4.50

5.50 , 바람직하게는 4.80 내지 5.20이며, 적층 구조에 포함된 축합방향족 고리 화 합물 층의 평균 개수 (M)은 4.00 내지 8.00 , 바람직하게는 5.00 내지 7.00이다. <29> 본 발명에서 제조된 등방성 피치는 구조가 상기 범위를 만족해야 방사성이 우수하고 불융고형분 및 메조페이스가 생성되지 않거나 측정되지 않을 정도의 극미 량이 존해하고, 이로부터 제조된 탄소섬유의 기계적 물성이 극대화 될 수 있다. 상 기 범위를 벗어나는 경우 불융고형분 및 메조페이스가 생성될 수 있고 방사시 잦은 단사가 발생하며 , 이로부터 제조된 탄소섬유의 인장강도가 현저히 감소하거나 신장 f ΰΙ낮거나 지나치게 높아져 탄성률이 좋지 못하다. 5.50, preferably 4.80 to 5.20, and the average number (M) of condensed aromatic ring compound layers included in the laminated structure is 4.00 to 8.00, preferably 5.00 to 7.00. <29> The isotropic pitch prepared in the present invention has excellent radioactivity only when the structure satisfies the above range, and there is a very small amount such that non-fused solids and mesofaces are not produced or measured, and the mechanical properties of the carbon fiber produced therefrom This can be maximized. If it is out of the above range, an unfused solid and mesophase may be formed and frequent single yarns may occur during spinning, and the tensile strength of the carbon fiber produced therefrom may be significantly reduced or the elongation f ΰΙ may be too low or too high, resulting in poor elastic modulus.

<30> 본 발명의 등방성 피치는 분석 결과에 따라 아래와 같이 나타낼 수 있다. The isotropic pitch of the present invention can be expressed as follows according to the analysis result.

<31> 본 발명의 둥방성 피치는 X-선 회절분석에서 23<2 Θ<25에서 (002)면 밴드를 가지고, 축합방향족 고리 화합물이 지방족 사슬로 연결된 하기 식 ( 1)~(4)를 만족 하는 구조를 포함하는 탄소섬유 제조용 등방성 피치이다. In the X-ray diffraction analysis, the round pitch of the present invention has a (002) plane band at 23 <2 Θ <25, and the following formulas (1) to (4) in which the condensed aromatic ring compound is connected with an aliphatic chain It is an isotropic pitch for producing carbon fiber with a satisfactory structure.

<32> 5 < La < 15 A ― ( 1) <32> 5 <L a <15 A-(1)

<33> 10 < Lc < 25 A ― (2) <33> 10 <L c <25 A-(2)

<34> 3.50 < dm < 4.50A —― (3) ' <34> 3.50 <d m < 4.50A - (3) '

<35> 4.00 < M < 8.00A ― (4)  <35> 4.00 <M <8.00 A-(4)

<36> 본 발명의 일 실시예에 따르면, 상기 식 ( 1), (2) 및 (3)을 만족하여도 (4) 를 만족하지 않으면 등방성 피치의 분자량이 지나치게 적어 본 발명의 등방성 피치 로부터 목적하는 탄소섬유의 인장강도를 만족하지 못하고 신장률이 지나치게 높아 져 탄성률이 떨어진다. 본 발명의 다른 일 실시예에 따르면, 상기 식 (2) 및 (3)을 만족하여도 (1) 및 (4)를 만족하지 않으면 등방성 피치의 방사시 잦은 단사가 발생 하고 이로부터 제조되는 탄소섬유의 인장강도가 현저히 감소하고 신장률 역시 낮아 진다. 본 발명의 또 다른 일 실시예에 따르면, 상기 식 ( 1) 및 (3)을 만족하여도 (2) 및 (4)를 만족하지 않으면 등방성 피치의 분자량이 적을뿐만 아니라 이로부터 제조되는 탄소섬유의 인장강도가 현저히 감소하게 된다.  According to one embodiment of the present invention, even if the above formulas (1), (2) and (3) are satisfied, if the content of (4) is not satisfied, the molecular weight of the isotropic pitch is too small, and thus the objective of the isotropic pitch of the present invention It does not satisfy the tensile strength of the carbon fiber, the elongation is too high, the elastic modulus falls. According to another embodiment of the present invention, even if the above formulas (2) and (3) are satisfied, if (1) and (4) are not satisfied, frequent single yarns occur during spinning of the isotropic pitch, and the carbon fiber manufactured therefrom The tensile strength of is significantly reduced and the elongation is also lowered. According to another embodiment of the present invention, if the formulas (1) and (3) are satisfied, but not satisfying (2) and (4), the molecular weight of the isotropic pitch is not only low, but also Tensile strength is significantly reduced.

<37> 상기 등방성 피치에 포함되는 구조에 축합방향족 고리 화합물에 연결된 지방 족 사슬간의 평균 거리 (dy )를 추가로 표현하여 보다 상세히 등방성 피치를 나타낼 수 있다. <38> 본 발명의 상기 식 ( 1) 내지 (4) 및 축합방향족 고리 화합물에 연결된 지방 족 사슬간의 평균 거리 ( dY )가 각각 바람직한 범위로 더 구체화된 보다 우수한 물성 및 방사성을 가지는 등방성 피치가 제조될 수 있고, 이로부터 제조되는 등방성 피 치계 탄소섬유의 고강도, 고탄성의 기계적 물성은 더욱 극대화 될 수 있다. The isotropic pitch may be represented in more detail by further expressing an average distance dy between aliphatic chains connected to the condensed aromatic ring compound in the structure included in the isotropic pitch. In the formulas (1) to (4) and the average distance (d Y ) between the aliphatic chains linked to the condensed aromatic ring compound of the present invention, an isotropic pitch having better physical properties and radioactivity The mechanical properties of the high strength and high elasticity of the isotropic pitch-based carbon fiber can be produced and can be further maximized.

<39> 본 발명의 등방성 피치 연화점은 255 내지 275 °C , 바람직하게는 260 내지The isotropic pitch softening point of the present invention is 255 to 275 ° C., preferably 260 to

270°C이고, 연화점이 지나치게 낮거나 높으면 일정 길이 이상의 장섬유의 방사가 어렵거나 일정 길이 이상으로 방사가 되더라도 균일도가 떨어지며 형상, 직경 등이 균일하지 못하고 인장강도등의 물성 측면에서도 취약한 섬유가 제조될 수 있다.270 ° C and, even if the softening point is too low or too high field above a certain length of the radiation is difficult or radiation over a certain length of the fibers falls the uniformity of the shape, diameter, etc. are not uniform the vulnerable fibers made in physical properties terms of tensile strength Can be.

<40> 본 발명의 등방성 피치 평균분자량 (Mw)은 1500 내지 3000, 바람직하게는The isotropic pitch average molecular weight (Mw) of the present invention is 1500 to 3000, preferably

1650 내지 2850이다. 상기 바람직한 범위의 평균분자량을 가지는 등방성 피치는 탄 소섬유 제조시 인장 강도를 현저히 상승시키고, 나아가 신장률 또한 높이는데 영향 -을 미—칠―수 있다. 1650 and 2850. Isotropic pitches having an average molecular weight in the above preferred range can significantly increase the tensile strength in the production of carbon fibers and further increase the elongation rate.

<41 > 본 발명의 일 실시예에 따르면 등방성 피치 점도는 200 내지 500이나, 탄소 섬유의 제조방법에 따라 적합하게 조절될 수 있다.  According to one embodiment of the present invention, the isotropic pitch viscosity is 200 to 500, but may be appropriately adjusted according to the method of producing carbon fibers.

<42> 다음으로, 본 발명의 탄소섬유 제조용 등방성 피치의 제조방법에 대하여 자 세히 설명한다.  Next, the manufacturing method of the isotropic pitch for carbon fiber manufacture of this invention is demonstrated in detail.

<43> 본 발명의 탄소섬유 제조용 등방성 피치의 제조방법은,  <43> The method for producing the isotropic pitch for producing carbon fibers of the present invention,

<44> a) 석유계 중질유, 고비점 잔사유, 방향족 탄화수소 단물질 및 나프타 분해 공정 잔사유에서 선택되는 어느 하나 또는 이들의 흔합물을 포함하는 원료를 열처 리 및 분획하는 전처리 단계;  A) a pretreatment step of thermally treating and fractionating a raw material including any one or a combination thereof selected from petroleum heavy oil, high boiling residue, aromatic hydrocarbon monomaterial and naphtha cracking process residue;

<45> b) 전처리된 원료에서 고상물질을 제거하는 여과단계;  B) a filtration step of removing solid matter from the pretreated raw material;

<46> C ) 여과된 원료로 베이직 피치를 제조하는 단계; 및  C) preparing a basic pitch from the filtered raw material; And

<47> d) 상기 베이직 피치를 가열하여 등방성 피치를 제조하는.단계; D) heating the basic pitch to produce an isotropic pitch . step;

<48> 를 포함하는 탄소섬유 제조용 등방성 피치의 제조방법이다.  It is a method for producing an isotropic pitch for producing carbon fibers including <48>.

<49> 상기의 제조 방법 중 b)의 여과 단계는 C )의 베이직 피치를 제조한 후에도 수행할 수 있으며, C )의 베이직 피치는 등방성 피치 제조의 중간 물질로 공정 구성 의 편이에 따라 그 조성과 물성이 달라질 수 있다.  The filtration step of b) in the above manufacturing method may be performed even after preparing the basic pitch of C), and the basic pitch of C) is an intermediate material for producing an isotropic pitch. Physical properties may vary.

<50> 원료로 더욱 상세하게는 나프타 분해 잔사유의 일종인 열분해 연료유 (PF0)를 포함할 수 있다. PF0는 나프타 크래킹 공정 (naphtha cracking center ; NCC)의 탑저 부위 ( bot t om)에서 생성되는 것으로 방향화도가 높고 수지의 함량이 풍부하여 본 발 명의 원료로사용될 수 있다ᅳ  More specifically, the raw material may include pyrolysis fuel oil (PF0), which is a kind of naphtha decomposition residue oil. PF0 is produced at the bottom (bottom) of the naphtha cracking center (NCC) and has a high degree of aromaticity and abundant resin, which can be used as a raw material of the present invention.

<5 i> 열분해 연료유는 납사크래킹 공정의 탑저부위에서 생성되는 것으로, 다양한 방향족 탄화수소류를 포함할 수 있다. 방향족 탄화수소류의 구체예로는 에틸벤젠 (ethylbenzene), 1-에테닐ᅳ3ᅳ메틸벤젠 (l-ethenyl-3— methyl benzene) , 인덴 (Indene), 1-에틸 -3-메틸벤젠 (l-ethyl-3-methyl benzene), 1-메틸에틸벤젠 (1_ methyl ethyl benzene), 2-에틸 -1,3-디메틸벤젠 (2-ethy卜 l,3-dime[hyl benzene), 프 로필벤젠 (propyl benzene), 1-메틸 -4-(2-프로페닐) -벤젠 (l-methyl-4-(2-propenyl) benzene), 1,1a, 6, 6a-테트라히드로—시클로프로파인덴 ( 1, la, 6, 6a-tetrahydro- cycloprop[a]i ndene ), 2-에틸— 1H-인덴 ( 2-e t hy 1 - 1H- i ndene ), 1-메틸 - 1H-인덴 ( 1- methyl-lH-indene) , 4 , 7-디메틸 -1H-인덴 (4, 7-dimethyl-lH-indene), 1-메틸 -9H-플루 오렌 (1-tnethyl— 9HFluorene), 1,7-디메틸 나프탈렌 (1,7-dimethyl naphthalene), 2- 메틸인덴 (2-methyl indene), 4,4'-디메틸비페닐 (4,4' -dimethyl bi henyl), 나프탈렌 (naphthalene), 4-메틸 -1, 1'ᅳ비페닐 (4-methyl_l, Γ -biphenyl ), 안트라센<5 i> Pyrolysis fuel oil is produced at the bottom of the naphtha cracking process. Aromatic hydrocarbons. Specific examples of the aromatic hydrocarbon is ethyl benzene (ethylbenzene), 1-butenyl eu eu 3-methylbenzene (l- e thenyl-3- methyl benzene ), indene (Indene), 1-ethyl-3-methylbenzene (l -ethyl-3-methyl benzene), 1-methylethyl benzene, 2-ethyl-1,3-dimethylbenzene, 2-dime (hyl benzene), propylenebenzene ( propyl benzene), 1-methyl-4- (2-propenyl) -benzene (l-methyl-4- (2-propenyl) benzene), 1,1a, 6, 6a-tetrahydro-cyclopropanedene (1 , La , 6 , 6a-tetrahydro-cycloprop [a] i ndene), 2-ethyl— 1H-indene (2-et hy 1-1H- i ndene), 1-methyl-1H-indene (1-methyl-lH -indene), 4, 7-dimethyl-lH-indene (4, 7-dimethyl-lH-indene), 1-methyl-9H-fluorene, 1,7-dimethyl naphthalene (1, 7-dimethyl naphthalene, 2-methyl indene, 4,4'-dimethyl bihenyl, naphthalene, 4-methyl-1, 1 ' ᅳ biphenyl (4-methyl_l, Γ -biphenyl) , anthracene

(Anthracene) , 2—메틸나프탈렌 (2-methylnaphthalene) 및 1-메틸나프탈렌 (1- methylnaphthalene) 등이 있을 수 있다. (Anthracene), 2-methylnaphthalene, 1-methylnaphthalene, and the like.

<52> 본 발명의 일 실시예에 따른 원료는 고비점 유분이 더 포함될 수 있다. 본 발명의 일 실시예에 따른 고비점 유분은 원유를 분별 증류하여 얻을 수 있는 성분 중 비점이 높고 탄소수가 많은 성분을 뜻하는 것으로, 주로 탄소수 5이상, 바람직 하게는 7 이상의 경질 또는 중질 방향족 나프타를 포함할수 있다.  Raw material according to an embodiment of the present invention may further include a high boiling point oil. The high boiling fraction according to an embodiment of the present invention refers to a component having a high boiling point and a high carbon number among components that can be obtained by fractional distillation of crude oil, and mainly a hard or heavy aromatic naphtha having 5 or more carbon atoms, preferably 7 or more carbon atoms. May include

<53> 고비점 유분으로 더욱 상세하게는 탄소수 9의 유분이 포함될 수 있다. 구체 적으로 예를 들면 스티렌, 비닐틀루엔, 인덴, 알파메틸스티렌 및 벤젠 /를루엔 /크실 렌 (BTX) 등으로 이루어질 수 있다.  More specifically, the high boiling point oil may include an oil having 9 carbon atoms. Specifically, for example, it may be made of styrene, vinyltoluene, indene, alphamethylstyrene and benzene / luluene / xylene (BTX).

<54> 탄소수 9의 유분으로 바람직하게는 인덴이 포함될 수 있다. 인덴은 원료 중 아로마틱 성분의 측쇄와 결합하여 용융방사 후 안정화 단계에서 아로마틱 성분의 측쇄가 산화함에 따라 탈수결합하여 에테르 (ether)화 되려는 경향올 방지할 수 있 어, 결과적으로 탄화온도 및 시간을 낮추는데 기여할수 있다.  The oil having 9 carbon atoms may preferably include indene. Indene is combined with the side chain of the aromatic component in the raw material to prevent the tendency to dehydrate and etherify as the side chain of the aromatic component is oxidized in the stabilization step after melt spinning, resulting in lowering carbonization temperature and time. Can contribute.

<55> . 고비점 유분은 전체 원료 100 중량%에 대하여 5 내지 15 중량 %포함되는 것 이 바람직하며, 5 중량 % 미만의 경우에는 그 효과가 미미할 수 있으며, 15 중량 %를 초과하는 경우에는 증가된 양에 대해 효과가뚜렷하지 않을 수 있다 <55> . The high boiling fraction is preferably contained in an amount of 5 to 15% by weight based on 100% by weight of the total raw material. If the content is less than 5% by weight, the effect may be insignificant. The effect may not be obvious

<56> 원료의 방향족화도 (fa)는 0.7 내지 0.9 일 수 있다. 방향족화도가 0.7 미만 인 경우 탄화 수율이 저하될 수 있다. 방향족도가 0.9보다 높은 경우에 대해서는 특별한 제한은 없으나, 방향족도가 0.9이상인 경우 본 발명에서 개시한 일련의 피 치 합성 방법에 의한 효과가크지 않을 수 있다.  The degree of aroma (fa) of the raw material may be 0.7 to 0.9. If the degree of aroma is less than 0.7, the carbonization yield may be lowered. There is no particular limitation on the case where the aromaticity is higher than 0.9, but when the aromaticity is 0.9 or more, the effect by the series of pitch synthesis methods disclosed in the present invention may not be significant.

<57> 원료의 분자량은 75 내지 350의 분포를 가질 수 있으며 , 바람직하게는 100 내지 250의 분포를 가질 수 있다. <58> 상기 등방성 피치의 제조방법에서 a)단계는 원료에 포함된 화합물들 중 증합 반응에 의해 올리고머를 생성할 가능성이 낮은 저분자 물질을 제거하는 단계이며, 동시에 원료에 포함된 화합물들 간 반웅을 수반하여 원료에 포함된 반응성이 강하 며 불안정한 화합물을 보다 안정적이며 등방성 피치의 제조에 유효한 화합물로 전 환하는 단계이다. The molecular weight of the raw material may have a distribution of 75 to 350, and preferably may have a distribution of 100 to 250. In the method for producing the isotropic pitch, step a ) removes low molecular weight substances that are less likely to form oligomers by a polymerization reaction among the compounds included in the raw material, and simultaneously reacts reactions between the compounds contained in the raw material. This is a step of converting a highly reactive and unstable compound contained in the raw material into a more stable and effective compound for producing isotropic pitch.

<59> a)단계에서 상기 전처리는 130 내지 240 °C , 바람직하게는 150 내지 230 °C , 보다 바람직하게는 190 내지 220°C의 온도에서 휘발분이 발생하지 않을 때까지 상 압 증류하여 진행할 수 있다. 전처리에서 가열온도는 원료의 조성비, 방향족화도 등 베이직피치 및 등방성 피치의 물성, 나아가서는 탄소섬유의 기계적인 물성에 영 향을 줄 수 있다. 또한 전처리 단계는 상압에서도 진행할 수 있으나, 감압 하에서 진행할 수 있다. 이때 감압을 통해 보다 낮은 온도에서 전처리 공정을 진행할 수 있으며, 상압과 동일한 효과를 얻을 수 있는 범위 내에서 압력 및 온도를 자유롭게 조절할 수 있다. In step a), the pretreatment may be carried out by atmospheric distillation at a temperature of 130 to 240 ° C., preferably 150 to 230 ° C., more preferably 190 to 220 ° C. until no volatiles are generated. have. In the pretreatment, the heating temperature can affect the physical properties of the basic pitch and isotropic pitch, such as the composition ratio of the raw materials and the degree of aroma, and also the mechanical properties of the carbon fibers. In addition, the pretreatment step may proceed at atmospheric pressure, but may proceed under reduced pressure. At this time, the pretreatment process may be performed at a lower temperature through decompression, and the pressure and temperature may be freely adjusted within a range capable of obtaining the same effect as the normal pressure.

<60> 상기 등방성 피치의 제조방법에서 b)단계는 전처리된 연료의 여과단계로 고 상 물질올 제거하며 상기 고상 물질은 금속, 황, 질소 등의 불순물이 포함된 고체 상의 잔류물로서 등방성 피치로부터 제조되는 탄소섬유의 구조에서 크래커 (cracker )로 작용하여 강도저하를 유발할수 있다.  In the manufacturing method of the isotropic pitch, step b) is a filtration step of the pretreated fuel to remove the solid material, and the solid material is a residue of a solid phase containing impurities such as metal, sulfur, and nitrogen from the isotropic pitch. It can act as a cracker in the structure of the carbon fiber to be produced may cause a decrease in strength.

<61 > 여과단계는 당업계에서 통상적으로 수행하는 방식, 예를 들어 여과, 원심분 리, 침강, 흡착, 추출 등으로 수행할수 있다ᅳ  Filtration may be carried out in a manner conventionally performed in the art, for example, by filtration, centrifugation, sedimentation, adsorption, extraction, etc.

<62> 여과단계는 베이직피치의 중합 이 후 수행할 수도 있으며, 경 :우에 따라서는 전처리 단계 다음 및 베이직피치 중합 단계 다음에 모두 수행할 수 있다. 즉, 상기 제조방법에서 (c) 단계 이 후에 수행할 수 있으며, 경우에 따라서는 ( a) 및 ( c) 단 계 이 후에 각각수행할수도 있다. <62> filtration step may also be performed after the polymerization of the basic pitch diameter: Yiwu thus is the pre-treatment step may be carried out all of the following basic pitch and polymerization steps. That is, the manufacturing method may be performed after step (c), and in some cases, may be performed after steps (a) and (c), respectively.

<63> 상기 등방성 피치의 제조방법에서 C )단계는 베이직 피치 제조단계로 여과단 계를 거친 원료를 가열과 동시에 반웅시켜 메조페이즈의 생성 없이 고연화점을 가 지는 베이직 피치를 제조하는 단계로서, 할로겐화법 또는 열중합법으로 진행할 수 있다.  In the method for producing the isotropic pitch, step C) is a basic pitch manufacturing step, in which a raw pitch having a high softening point is produced without generating mesophases by heating the raw material that has undergone the filtration step at the same time. It can proceed by law or thermal polymerization.

<64> 할로겐화법은 할로겐화합물 및 라디칼개시제를 더 첨가한 후 가열하여 진행 할 수 있으며, 바람직하게는 라디칼개시제를 첨가한 후 할로겐화합물을 첨가하고 혼합하여 진행할수 있다.  The halogenation method may proceed by heating after further adding a halogen compound and a radical initiator, and preferably by adding and mixing a halogen compound after the addition of the radical initiator.

<65> 할로겐화합물은 염소 (Cl2) , 티오닐클로라이드 (S0C 12) , 설푸릴클로라이드Halogenated compounds are chlorine (Cl 2 ), thionyl chloride (S0C 1 2 ), sulfuryl chloride

(S02C12) , 브름 (Br2) , 요오드 ( 12) 또는 이들 중 둘 이상의 흔합물로 이루어진 그룹 중에서 선택된 것이 사용될 수 있다. Group consisting of (S0 2 C1 2 ), brm (Br 2 ), iodine (1 2 ) or a combination of two or more thereof Selected from among them may be used.

<66> 라디칼개시제는 벤조일퍼옥사이드 (BenZ0yi peroxide) , 디부틸히드로퍼 옥사 이드 (di-t-butyl hydroperoxide) , 아세틸퍼옥사이드 (Acetyl peroxide) 등의 유기과 산화물 (Organi c Peroxide)과, 아조비스이소부티로니트릴 (AIBN ; α , α ' - Azobisisobutyroni tr i le), 아조비스메틸이소부틸레이트( α, a ' -Azobi smethyl i sobutyrate) 등의 아조화합물 또는 이들 증 둘 이상의 흔합물로 이루어진 그룹 중 에서 선택된 것이 사용될 수 있다. <66> radical initiator is benzoyl peroxide (B enZ0 yi peroxide), di-butyl hydroperoxide oxazol id (di-t-butyl hydroperoxide) , acetyl peroxide (Acetyl peroxide) such yugigwa oxide (Organi c Peroxide) and, Azo Azo compounds such as bisisobutyronitrile (AIBN; α, α '-Azobisisobutyroni tr ile), azobismethylisobutylate (α, a' -Azobi smethyl i sobutyrate), or a group consisting of a combination of two or more of these The one selected from can be used.

<67> 라디칼개시제는 할로겐화합물 100 중량부에 대하여 1 내지 30중량부 포함될 수 있으나 보다 바람직하게는 5 내지 20 중량부 포함될 수 있다.  The radical initiator may be included in an amount of 1 to 30 parts by weight, more preferably 5 to 20 parts by weight, based on 100 parts by weight of the halogen compound.

<68> 할로겐화법은 100 내지 12( C에서 0.5 내지 2시간 할로겐화반웅을 진행하여 방향족 알킬그룹 내 수소를 할로겐으로 치환한 후, 300 내지 330°C에서 2 내지 4시 간 탈할로겐화반웅에 의한 중합을 진행할 수 있다. 또한 탈할로겐화반웅은 후속공 정으로서, 반웅 후에 베이직피치 중에 잔존할 수 있는 할로겐화합물과 라디칼개시 제를 분해시켜 제조되는 베이직피치의 순도를 더욱 높일 수 있다. 특히 탈할로겐화 반응에서 반웅온도가 330°C를 넘지 않는 것이 좋은데, 330°C 초과 시에는 할로겐화 합물 및 라디칼개시제의 분해가 활발히 일어나지만 과다한 중합에 따른 베이직피치 의 이방성화 또는 코크스화가 진행하여 결과적으로 탄소섬유의 기계적인 물성이 크 게 떨어지게 된다. Halogenation is carried out by halogenation reaction at 100 to 12 (0.5 to 2 hours at C to replace hydrogen in the aromatic alkyl group with halogen, followed by polymerization by dehalogenation reaction at 300 to 330 ° C. for 2 to 4 hours. In addition, the dehalogenation reaction can further enhance the purity of the basic pitch produced by decomposing halogen compounds and radical initiators that may remain in the basic pitch after the reaction, particularly in the dehalogenation reaction. banung temperature is good is not more than 330 ° C, 330 ° C in excess of, the process advances upset anisotropic screen or coking of the basic pitch of the excess polymerization only occurs actively decomposition of the halogenated compound and a radical initiator as a result of the carbon fiber machine Physical properties are greatly reduced.

<69> 본 발명의 일 실시예에 따르면, 할로겐화법에 의해 제조된 베이직피치는 연 화점이 70 내지 130 C , 바람직하게는 115 내지 125°C일 수 있다. According to one embodiment of the present invention, the basic pitch prepared by the halogenation method may have a softening point of 70 to 130 C, preferably 115 to 125 ° C.

<70> 열중합법은 350 내지 380°C에서 0. 1 .내지 2시간 진행할 수 있다. 열중합법은 진행 시 불활성기체 분위기에서 진행할 수 있으며, 질소와 폴리콘덴세이션 (poly- condensat ion) 진행 중에 발생하는 기체 부산물올 분취하여 진행할 수 있다. 또한 열중합법에서도 할로겐화법과 마찬가지로 반웅온도가 380 °C를 넘지 않는 것이 좋은 데, 반웅온도가 380°C를 초과하는 경우, 할로겐화법과 마찬가지로 본 발명에서 목 적으로 하는 균일한 이방성 피치의 범위를 초과하는 과량의 메조페이즈가 생성되거 나또는 코크스화가 진행되어 불균일한 탄소섬유가 생성될 수 있다. Thermal polymerization can be carried out at 350 to 380 ° C. for 0.1 to 2 hours. The thermal polymerization method may proceed in an inert gas atmosphere, and may proceed by fractionating gaseous by-products generated during the process of nitrogen and polycondensat ion. In the thermal polymerization method, as in the halogenation method, the reaction temperature should not exceed 380 ° C. However, when the reaction temperature exceeds 380 ° C, the reaction temperature exceeds the range of uniform anisotropy pitch for the present invention, as in the halogenation method. Excess mesophase may be produced or coking may result in uneven carbon fibers.

<71> 열중합법에 의해 제조된 베이직피치는 연화점이 85 내지 140°C , 바람직하게 는 115 내지 125ᅳ C일 수 있다. The basic pitch prepared by the thermal polymerization method may have a softening point of 85 to 140 ° C., preferably 115 to 125 ° C.

<72> 등방성 피치의 제조 공정에서 구성상의 편의에 따라 베이직 피치의 물성을 조절할 수 있다. 예를 들어, 상기 제조방법의 ( C )단계에서 ( d)단계를 연속적으로 흐르는 유체의 흐름을 원할히 할 목적으로 공정을 구성할 경우, 상기 (c)단계로부 터 제조된 베이직 피치 중 축합방향족 고리 화합물이 연결된 을리고머의 절대양에 큰 영향을 주자 않는 범위에서 비점이 낮은 화합물을 추가로 포함할 수도 있다. 이 러한 효과는 (c)단계를 가압 상태에서 수행하는 경우에 얻어질 수 있으며, 이 때 베이직 피치의' 연화점은 공정 구성의 편의에 따라 최종 제조되는 등방성 피치의 물 성, 분자구조 및 적층구조에 영향을 주지 않은 범위에 내에서 자유롭게 조절할 수 있다. In the manufacturing process of the isotropic pitch, the physical properties of the basic pitch can be adjusted according to the configuration convenience. For example, when the process is configured for the purpose of smoothly flowing the fluid flowing in the step (c) to the step (d) of the manufacturing method, the condensation aromatics of the basic pitch manufactured from the step (c) To the absolute amount of the ligomer linked to the ring compound It may further include a compound having a low boiling point in a range that does not significantly affect. This effect can be obtained when step (c) is carried out under pressurization, where the ' softening point of the basic pitch is applied to the physical properties, molecular structure and laminated structure of the isotropic pitch that is finally manufactured according to the convenience of the process configuration. You can freely adjust the range without affecting it.

<73> 상기 등방성 피치의 제조방법에서 d )단계는 등방성 제조단계로 베이직 피치 를 가열하여 증발을 촉진함으로써 메조페이즈 생성을 억제하고, 용융방사가 가능한 등방성 피치를 제조하는 공정일 수 있다.  In the manufacturing method of the isotropic pitch, step d) may be a process of manufacturing isotropic pitch capable of suppressing mesophase generation by promoting evaporation by heating the basic pitch as an isotropic manufacturing step.

<74> 등방성 피치 제조단계는 통상적인 박막증류법으로 진행할 수 있으며, 이를 통해 메조페이스의 생성을 억제하고 불용고형분을 제거하는 추가적인 공정이 필요 하지 않다는 장점이 있다. 또한 본 발명의 일 실시예에 따른 등방성 피치 제조단계 는 다단계의 박막증류장치를 구비하여 제조되는 등방성 피치의 조성 및 상태변화에 대응할수 있다.  The isotropic pitch manufacturing step may proceed with a conventional thin film distillation method, and thus, there is an advantage that an additional process of suppressing the formation of mesophase and removing insoluble solids is not necessary. In addition, the isotropic pitch manufacturing step according to an embodiment of the present invention may correspond to the composition and state change of the isotropic pitch manufactured with a multi-stage thin film distillation apparatus.

<75> 등방성 피치 제조단계는 진공분위기, 300 내지 350°C에서 0. 1 내지 1시간 동 안 가열하여 진행할 수 있다. 특히 가열온도가 350 °C를 초과하면, 부분적으로 메조 페이즈가 생성되며, 계속된 가열에 의해 불용성 탄소 고형분이 생성될 수 있으므 로, 가열온도 및 가열시간을 준수하는 것이 바람직하다. The isotropic pitch manufacturing step may be performed by heating in a vacuum atmosphere for 0.1 to 1 hour at 300 to 350 ° C. In particular, when the heating temperature exceeds 350 ° C., meso phases are partially formed, and insoluble carbon solids may be generated by the continuous heating, and it is preferable to observe the heating temperature and the heating time.

<76> 본 발명의 일 실시예에 따른 등방성 피치는 연화점이 255 내지 275°C , 바람 직하게는 260 내지 270 °C일 수 있다. 또한 본 발명의 등방성 피치 평균분자량 (Mw) 은 1500 내지 3000 , 바람직하게는 1700 내지 2850일 수 있다. 등방성 피치의 평균 분자량 및 연화점은 제조되는 탄소섬유의 물성에 큰 영향을 줄 수 있으므로 제조공 정의 조건을 준수하는 것이 바람직하다. Isotropic pitch according to an embodiment of the present invention may have a softening point of 255 to 275 ° C, preferably 260 to 270 ° C. In addition, the isotropic pitch average molecular weight (Mw) of the present invention may be 1500 to 3000, preferably 1700 to 2850. Since the average molecular weight and softening point of the isotropic pitch can greatly affect the physical properties of the carbon fibers to be produced, it is preferable to comply with the manufacturing process conditions.

<77> 본 발명에서 제조되는 등방성 피치는 용융방사 (me l t spinning)가 가능하고, 섬유 방사시 단사가 일어나지 않거나 극히 드문 우수한 방사성을 가진다. 용융방사 는 고분자 물질이나 피치를 용융하여 연속 섬유로 제조하는 방법으로 섬유 방사시 필요한 고가의 용매를 사용할 필요가 없어, 방사 공정의 구성을 단순화시킬 수 있 고 비용을 현저히 감소시킬 수 있는 매우 경제적인 방법이다. 탄소섬유 제조를 위 한 상기 용융방사가 가능하기 위해서는 피치의 방사성이 우수해야 하는데 본 발명 에 따라 제조되는 등방성 피치는 방사성이 매우 우수하여 탄소섬유 제조를 위한 용 융방사가 가능하면서 단사가 극히 드물거나 일어나지 않는다. 또한, 본 발명의 용 융방사가 가능한 등방성 피치는 기존의 멜트-블로잉 (mel t-b l owing)올 통해 단섬유 를 제조하는데 그치던 등방성 피치에 비해 방사성이 매우 뛰어나 이로부터 고강도, 고탄성의 탄소장섬유를 제조할수도 있다. <78> 본 발명의 일 실시예에 따르면, 등방성 피치를 20분 연속으로 용융방사 증 끊김의 빈도를 단사빈도로 하여 측정한 결과 단사빈도가 0에 해당하여 방사성이 매 우 우수한 것을 알 수 있다. The isotropic pitch produced in the present invention is capable of melt spinning, and does not have single yarn or extremely rare spinning when spinning. Melt spinning is a method of melting polymer materials or pitches into continuous fibers, eliminating the need for expensive solvents for spinning, and simplifying the construction of spinning processes and significantly reducing costs. Way. In order to enable the melt spinning for the production of carbon fibers, pitch spinning should be excellent, but the isotropic pitch prepared according to the present invention has very good spinning property, and melt spinning for carbon fiber manufacturing is possible, but the single yarn is extremely rare. Does not happen. In addition, the isotropic pitch capable of melt-spinning of the present invention has a very high radioactivity compared to the isotropic pitch which was used to produce short fibers through melt-blowing, and thus it has high strength and high elastic carbon long fibers. It can also be manufactured. According to one embodiment of the present invention, as a result of measuring the isotropic pitch for 20 minutes in a row with the frequency of melt spinning off as a single shot frequency, it can be seen that the single yarn frequency corresponds to 0, which is very excellent in radioactivity.

<79> 또한, 본 발명의 등방성 피치는 700 내지 1200 °C이하의 낮은 온도에서도 탄 화가 가능하여 탄화과정에서 에너지 소비를 최소화할 수 있다. In addition, the isotropic pitch of the present invention can be carbonized at a low temperature of 700 to 1200 ° C or less to minimize the energy consumption during the carbonization process.

<80> 본 발명에 따라 제조된 등방성 피치는 용융방사후 안정화 단계 및 탄화단계 를 거쳐 탄소섬유를 제조할 수 있다. 본 발명의 일 실시예에 따라 제조된 등방성 피치로부터 탄소섬유 제조시, 인장강도가 최소 1.5GPa 이상의 고강도이고 신장률이 이상인 등방성 피치계 탄소장섬유를 제조할 수 있다. 상기와 같은 등방성 피치계 탄소섬유는 물성이 극대화 된 것으로 기존의 등방성 피치계 탄소섬유가 범용 탄소 재료로 사용되는 것과 달리 고강도, 고탄성 탄소섬유가 요구되던 탄소복합재에 다 양하게 웅용되어 사용될 수 있다.  The isotropic pitch prepared according to the present invention may produce carbon fibers through a stabilization step and a carbonization step after melt spinning. When the carbon fiber is manufactured from the isotropic pitch prepared according to the embodiment of the present invention, it is possible to produce an isotropic pitch-based carbon fiber having a high tensile strength of at least 1.5 GPa or more and an elongation rate of at least 1.5 GPa. The isotropic pitch-based carbon fiber as described above is maximized in physical properties, unlike conventional isotropic pitch-based carbon fiber is used as a general-purpose carbon material can be used in various ways to the carbon composite material required high strength, high elastic carbon fiber.

<81> 본 발명의 등방성 피치는 탄소섬유 제조용이 바람직하나, 이에 제한되는 것 은 아니며 다양한 탄소재료 제조에도 이용될 수 있다. The isotropic pitch of the present invention is preferably used for producing carbon fibers, but is not limited thereto, and may be used for manufacturing various carbon materials.

<82> 이하 실시예 및 비교예를 통해 본 발명에 따른 등방성 피치의 제조방법 및 이로부터 제조된 등방성 피치에 대하여 더욱 상세히 설명한다. 다만 다음에 서술하 는 실시예 및 비교예는 본 발명의 이해 또는 실시를 돕기 위한 하나의 예시일 뿐, 본 발명이 실시예 및 비교예에 제한되는 것은 아니다.  Hereinafter, a method for producing an isotropic pitch and an isotropic pitch prepared therefrom according to the present invention will be described in more detail with reference to Examples and Comparative Examples. However, the examples and comparative examples described below are only examples to assist in understanding or implementing the present invention, and the present invention is not limited to the examples and comparative examples.

<83> 실시예 및 비교예를 통해 측정한 물성의 측정방법 및 원료의 조성비는 다음 과 같다,  The measurement method of the physical properties and the composition ratio of the raw materials measured through Examples and Comparative Examples are as follows.

<84> 물성 측정 방법  <84> Property Measurement Method

<85> 1.탄소와수소 원자비 (H/C)  <85> 1. Atomic Carbon / Hydrogen Ratio (H / C)

<86> CHNS 원소분석기로.분석  <86> CHNS elemental analyzer.

<87> 2 .방향족화도 ( f a) <87> 2. Aromatization Degree (f a)

<88> C NMR로 분석 (ASTM D5292) Analysis by C NMR (ASTM D5292)

<8 > 3.원료의 조성  <8> 3.The composition of raw materials

<90> 2D-GC로 분석  <90> Analysis with 2D-GC

<9i > 4.점도 (Pa - s) <9i> 4.Viscosity (Pa-s)

<92> 점도는 TMA (Thermo Mechan i cal Analyzer )로 측정  <92> Viscosity measured by TMA (Thermo Mechan i cal Analyzer)

<93> 5. 연화점 ( °C ) 5. Softening point ( ° C)

<94> 연화점은 TMA (Thermo Mechani cal Analyzer )로 측정  Softening point is measured by TMA (Thermo Mechani cal Analyzer)

<95> 6. 수율 <96> 수율은 투입된 나프타 분해 잔사유 중량 대비 최종 수득된 피치의 중량에 의해 계 산되었다. 6. Yield Yield was calculated by the weight of the final pitch obtained relative to the weight of the naphtha cracking residue oil charged.

< 7> 7. 기계적 물성  <7> 7. Mechanical Properties

<98> 인장강도 (GPa)와 신장율 (%)을 산출하기 위해 탄소섬유의 샘플에 대해 2N의 로드셀 을 장착한 UTM Jniversal Test Machine)으로 Stress-Strain 커브를 측정하였고, 인 장강도는 상기 측정 결과와 전자현미경에 의해 분석된 섬유의 직경으로부터 계산되 었다.  In order to calculate the tensile strength (GPa) and elongation (%), the stress-strain curve was measured with a UTM Jniversal Test Machine equipped with a 2N load cell on a sample of carbon fiber. Calculated from the diameter of the fiber analyzed by and electron microscopy.

<99> 8. 피치의 분자 조성  8. Molecular Composition of the Pitch

<ιοο> 피치의 분자 조성은 GOAED로 분석하였고 분자량의 분포는 GPC로 측정하였고 그 결 과로부터 평균분자량을 구했다.  The molecular composition of the pitch was analyzed by GOAED and the distribution of molecular weight was measured by GPC and the average molecular weight was obtained from the results.

<ιοι> 9. X선 회절 분석 <ιοι> 9. X-ray diffraction analysis

<102> 등방성 피치의 분자 구조 분석을 위한 X선 회절분석기는 Cu음극을 사용하고. K- c 파장은 1.540598, X선 발생장치의 전압은 40KV , 튜브 전류는 3(½A이었다.  X-ray diffractometer for molecular structure analysis of isotropic pitch uses Cu cathode. The K-c wavelength was 1.540598, the voltage of the X-ray generator was 40KV, and the tube current was 3 (½A).

<1.03> 10. T0F-MS 분석 <1.03> 10. T0F-MS Analysis

<104> 분자구조를 해석하기 위해 JE0L사의 T0F-MS를 사용하였다. 레이저 소스는 Nd :YAG , 레이저 강도는 5OT , 질량범위는 10~3,000 , 스파이럴 측정 모드를 사용하여 분석하 였다.  JE0L's T0F-MS was used to analyze the molecular structure. The laser source was analyzed using Nd: YAG, laser intensity 5OT, mass range 10-3,000 and spiral measurement mode.

<105> <실시예 1~4> 및 <비교예 1~3> 베이직피치 제조단계에서 할로겐화법을 이용 한 등방성 피치의 제조  <Examples 1 to 4> and <Comparative Examples 1 to 3> Preparation of an isotropic pitch using a halogenation method in the basic pitch manufacturing step

<106> 조성 및 방향족화도는 표 1 내지 3과 같은 Naphtha Cracker Bot tom <106> Composition and aromatization degree of Naphtha Cracker Bot tom shown in Table 1 to 3

Oi KNCBO)를 원료로 준비하였다. Oi KNCBO) was prepared as a raw material.

<107> 【표 1】

Figure imgf000014_0001
<107> [Table 1]
Figure imgf000014_0001

< 108> 【표 2]  <108> [Table 2]

Figure imgf000014_0002
Figure imgf000014_0002

<10 > 【표 3】 . NCBO화합물 조성 함량 (%) <10> [Table 3] . NCBO Compound Composition Content (%)

포화타소화합물 1.8  Saturated Tasso Compound 1.8

방향족 고리를 한 개 포함하는 화합물 51.8  Compounds containing one aromatic ring 51.8

방향족 고리를 두 개 포함하는 화합물 43.1  Compounds Containing Two Aromatic Rings 43.1

방향족 고리를 세 개 포함하는 화합물 3.3  Compound containing three aromatic rings 3.3

방함족 고리를 네 개 이상포함하는 화합물 0  Compounds Containing Four or More Anti-Half Rings 0

총합 100  Total 100

실시예 1~4는 준비된 NCB0를 각각 190, 200, 210, 220°C에서 비교예 2는 120Examples 1 to 4 prepared NCB0 at 190, 200, 210 and 220 ° C., respectively.

V, 비교예 3은 250°C에세 상압 증류로 각각 전처리 단계를 수행하였고 이 후 여 과를 통해 고상 물질을 제거하였다. 비교예 1은 전처리 단계를 수행하지 않고 여과 를 통해 고상물질을 제거하였다. V, Comparative Example 3 was each subjected to a pretreatment step at 250 ° C. atmospheric distillation, after which the solid material was removed by filtration. In Comparative Example 1, the solid material was removed by filtration without performing the pretreatment step.

<ιιι> 여과 단계 이 후 증간단계에서 생성된 원료 100 중량부에 대하여 브롬 20 중 량부 첨가하였다. 그리고 11CTC에서 1시간 동안 브롬화반응을 진행한 후, 다시 320 °C에서 3시간 동안 탈브롬화반응을 진행하여 베이직 피치를 제조하였다. 베이직 피 치 제조 공정이 종료된 후 연화점 및 수율을 측정하였고 표 4는 측정결과를 나타낸 다. After the filtration step, 20 parts by weight of bromine was added to 100 parts by weight of the raw material produced in the thickening step. The bromination reaction was carried out at 11 CTC for 1 hour, and then debrominated at 320 ° C for 3 hours to prepare a basic pitch. Softening point and yield were measured after the completion of the basic pitch manufacturing process. Table 4 shows the measurement results.

<)12> 【표 4】  <) 12> [Table 4]

Figure imgf000015_0001
Figure imgf000015_0001

제조된 베이직 피치를 박막 증발장치에 각각 투입한 후, 진공분위기, 340°C 에서 30분간 베이직 피치를 가열하여 등방성 피치를 제조하였다. 공정이 종료된 후 , 둥방성 피치의 연화점, 점도 및 평균분자량올 측정하여 하기 표 5에 기재하였다. 【표 5】 After putting the prepared basic pitch into the thin film evaporator, the basic pitch was heated for 30 minutes in a vacuum atmosphere, 340 ° C. to produce an isotropic pitch. After the process was completed, the softening point, viscosity, and average molecular weight of the round pitch were measured and shown in Table 5 below. Table 5

Figure imgf000015_0002
Figure imgf000015_0002

제조된 등방성 피치의 구조를 X-선 회절분석기를 이용하여 분석하였고 XRD 결과 17<2Θ<18에서 지방족사슬 (aliphatic chain)의 감마 밴드 ( κ -band), 23<2Θ<25에서 축합방향족 고리 화합물의 적층구조에서 (002)면, 43<2Θ<45에서 (10)면 밴드가 나타났다 (도 2). 하기 표 6은 구조 분석 결과를 나타낸다ᅳ The structure of the prepared isotropic pitch was analyzed by X-ray diffractometer, and the gamma band (κ -band) of aliphatic chain was found in XRD of 17 <2Θ <18, In the laminate structure of the condensed aromatic ring compound at 23 <2Θ <25, the (10) plane band was shown at 43 <2Θ <45 (FIG. 2). Table 6 below shows the results of the structural analysis.

<Π6> 【표 6】  <Π6> [Table 6]

Figure imgf000016_0001
Figure imgf000016_0001

<1 Ι7> - La(A) : 축합방향족 고리 화합물 층의 평균 직경 ' <1 Ι7> -L a (A): Average diameter of the condensed aromatic ring compound layer '

<118> - Lc(A) : 축합방향족 고리 화합물 층이 형성하는 적층 구조의 평균 직경 <118>-Lc (A): Average diameter of the laminated structure formed by the condensed aromatic ring compound layer.

119> - dm(A) : 적층 구조에서 축합방향족 고리 화합물 층간 평균 거리 119>-d m (A): Average distance between condensed aromatic ring compounds in laminated structure

<120> - dY(A) : 축합방향족 고리 화합물에 연결된 지방족 사슬간의 평균 거리 D Y (A): average distance between aliphatic chains linked to a condensed aromatic ring compound

<121> - M : 적층 구조에 포함된 축합방향족 고리 화합물 층의 평균 개수 (=(Lc/dm) + 1)<121>-M: average number of condensed aromatic ring compound layers included in the laminated structure (= (L c / d m ) + 1)

<Ι22> <Ι22>

<123> <실시예 5~8> 및 <비교예 4~6> 베이직피치 제조단계에서 열증합법을 이용한 등방성 피치의 제조 <Examples 5 to 8> and <Comparative Examples 4 to 6> Preparation of an isotropic pitch using the thermal polymerization method in the basic pitch manufacturing step

<Ι24> 상기 실시예 1~4 및 비교예 1~3과 동일한 NCB0를 준비하였다.  <Ι24> The same NCB0 as said Examples 1-4 and Comparative Examples 1-3 was prepared.

<125> 실시예 5~8은 준비된 NCB0를 각각 190, 200, 210, 220°C에서 비교예 4는 120 °C, 비교예 5는 250 °C에서 상압 증류로 각각 전처리 단계를 수행하였고 이 후 여 과를 통해 고상 물질올 제거하였다. 비교예 3은 전처리 단계를 수행하지 않고 여과 를 통해 고상 물질을 제거하였다. Examples 5 to 8 performed the pre-treatment steps of the prepared NCB0 at 190, 200, 210, and 220 ° C, respectively, in Comparative Example 4 at 120 ° C, and Comparative Example 5 by atmospheric distillation at 250 ° C. The solids were removed by filtration. Comparative Example 3 removed the solid material through filtration without performing the pretreatment step.

<Ι26> 여과 단계 이 후 증간단계에서 생성된 원료 100 중량부를 금속 재질의 용기 에 투입하고 370°C에서 0.5시간 동안 가열하여 베이직 피치를 제조하였다. 베이직 피치 제조 공정이 종료된 후 연화점 및 수율을 측정하였고 표 7는 측정결과를 나타 낸다. After the filtration step, 100 parts by weight of the raw material produced in the thickening step was added to a metal container, and heated at 370 ° C. for 0.5 hour to prepare a basic pitch. Softening point and yield were measured after the completion of the basic pitch manufacturing process. Table 7 shows the measurement results. Serve

<127> 【표 7】 <127> [Table 7]

Figure imgf000017_0001
Figure imgf000017_0001

<128> 제조된 베이직 피치를 박막 증발장치에 각각 투입한 후, 진공분위기, 340 °C 에서 30분간 베이직 피치를 가열하여 등방성 피치를 제조하였다. 공정이 종료된 후 , 등방성 피치의 연화점, 점도 및 평균분자량을 측정하여 하기 표 8에 기재하였다.After the prepared basic pitches were respectively introduced into the thin film evaporator, an isotropic pitch was prepared by heating the basic pitches in a vacuum atmosphere at 340 ° C. for 30 minutes. After the process was completed, the softening point, viscosity and average molecular weight of the isotropic pitch were measured and described in Table 8 below.

<129> 【표 8】 <129> [Table 8]

Figure imgf000017_0002
Figure imgf000017_0002

<i3o> 제조된 등방성 피치의 구조를 X-선 회절분석기를 이용하여 분석하였고 XRD 분석 결과 17<2Θ<18에서 지방족사슬 (aliphatic chain)의 감마 밴드 (γ-band), 23<2Θ<25에서 축합방향족 고리 화합물의 적층 구조에서 (002)면, 43<2Θ<45에서 (10)면 밴드가 나타났다 (도 3). 하기 표 9는 구조 분석결과를 나타낸다.  <i3o> The structure of the prepared isotropic pitch was analyzed by X-ray diffractometer, and XRD analysis showed that the gamma band (γ-band) of aliphatic chain (γ-band) at 23 <2Θ <25 at 17 <2Θ <18. In the laminated structure of the condensed aromatic ring compound, the (10) plane band appeared at (002) plane and 43 <2Θ <45 (FIG. 3). Table 9 shows the results of the structural analysis.

<131> [표 9】 Table 9

Figure imgf000018_0001
Figure imgf000018_0001

<132> - La(A) : 축합방향족 고리 화합물 층의 평균 직경 -L a (A): average diameter of the condensed aromatic ring compound layer

<133> — LC(A): 축합방향족 고리 화합물 층이 형성하는 적층 구조의 평균 직경 <133> — L C (A): Average diameter of the laminated structure formed by the condensed aromatic ring compound layer

<134> - dm(A): 적층 구조에서 축합방향족 고리 화합물 층간 평균 거리 ' D m (A): average distance between condensed aromatic ring compounds in a laminated structure ''

<135> ― dY(A): 축합방향족 고리 화합물에 연결된 지방족사슬간의 평균 거리 D Y (A): average distance between aliphatic chains linked to condensed aromatic ring compounds

<136> - M : 적층 구조에 포함된 축합방향족 고리 화합물 층의 평균 개수 (=(Lc/d,„) + 1)-M: Average number of condensed aromatic ring compound layers included in the laminated structure (= (L c / d, „) + 1)

<137> <137>

<138> 제조된 듀방성 피치 물성 및 구조의 해석  <138> Analysis of the manufactured duotropic pitch properties and structure

<139> 등방성 피치의 XRD 분석 결과 베이직 피치의 제조단계에서 할로겐화법 및 열 중합법을 이용한 제조방법으로 제조된 등방성 피치는 모두 17<2Θ<18에서 지방족사 슬 (aliphatic chain)의 감마 밴드 (γ— band), 23<2Θ<25에서 축합방향족 고리 화 합물의 적층구조에서 (002)면, 43<2Θ<45에서 (10)면 밴드가 나타났다.  As a result of XRD analysis of isotropic pitch, the isotropic pitch produced by the halogenation method and the thermal polymerization method in the manufacturing step of the basic pitch was 17 <2Θ <18 and the gamma band (γ) of aliphatic chain (γ) — Band), the (002) plane and the (10) plane band appeared at 43 <2Θ <45 in the laminate structure of the condensed aromatic ring compound at 23 <2Θ <25.

<140> 하기 표 10은 상기 모든 실시예 및 비교예에 따라 제조된 등방성 피치의 물 성 및 구조의 측정결과를 나타낸 것이다.  Table 10 shows the measurement results of the physical properties and structures of the isotropic pitch prepared according to all the above Examples and Comparative Examples.

【표 10】 Table 10

Figure imgf000019_0001
Figure imgf000019_0001

각 실시예에서 등방성 피치의 구조에서 축합방향촉 고리 화합물은 최소 2 내 지 최대 7개의 방향족 고리를 포함하였고, 표 10을 보면 축합방향족 고리 화합물 층의 평균 면간 거리 (dm)가 3.594-3.965 A속했고, 축합방향족 고리 화합물 층의 평 균 직경 (LJ은 9-12A속했고, 축합방향족 고리 화합물에 연결된 지방족사슬 간 평균 거리 (^)는 4.829—5.172A속했고, 등방성 피치 클러스터 (cluster)의 평균 직경 (Lc) 은 16~20A에 속했다. £한, 각 실시예에서 등방성 피치 클러스터에서 적층된 축합 방향족 고리 화합물 층의 평균 개수 (M)는 (Lc/d +l로 나타낼 수 있고 5.3~6.5에 속 했다. 또한, 각 실시예에서 등방성 피치 클러스터에서 적층된 축합방향족 고리 화 합물 층의 평균 개수 (M)는 (Lc/d +l로 나타낼 수 있고 5.3~6.5에 속했다. In each example, the condensed aromatic ring compound in the structure of the isotropic pitch contained at least 2 to 7 aromatic rings, and in Table 10, the average interplanar distance (d m ) of the condensed aromatic ring compound layer was 3.594-3.965 A. Average diameter (^) of aliphatic chains connected to the condensed aromatic ring compound was 4.829--5.172A, and the average diameter of the isotropic pitch cluster ( L c ) belongs to 16-20 A. In each example, the average number of condensed aromatic ring compound layers stacked in an isotropic pitch cluster (M) can be expressed as (L c / d + l and in 5.3 to 6.5 genus did. In addition, in each example, the average number (M) of condensed aromatic ring compound layers stacked in an isotropic pitch cluster can be expressed as (L c / d + l and belongs to 5.3 to 6.5.

<143> 등방성 피치를사용한 탄소섞유의 제조  Preparation of Carbon Mixed Oil Using Isotropic Pitch

<144> 등방성 피치를 사용하여 탄소섬유를 제조하였다. 먼저, 등방성 피치를 원통 형의 용기에 각각 주입한 후, 질소분위기에서 0.8kgf/cm2의 압력을 가하여 용융방사 하였다. 이때 권취기의 직경은 150 醒였으며, 권취속도는 700rpm이었다. Carbon fibers were prepared using an isotropic pitch. First, an isotropic pitch was injected into a cylindrical container, and then melt spun by applying a pressure of 0.8 kgf / cm 2 in a nitrogen atmosphere. At this time, the diameter of the winding machine was 150 醒, the winding speed was 700rpm.

<145> 방사된 섬유는 관형 전기로에 각각 장입한 후 공기를 150 i /mi n의 유량으로 공급하였다. 또한 1 °C /min의 속도로 승온하여, 290°C에 도달한 후 1시간 동안 유 지하여 안정화 시켰다. 안정화단계 후, 질소 150ml /min의 속도로 주입함과 동시에 5°C/niin의 속도로 승온하여 800°C에 도달한 후 0.5시간 동안 유지하여 탄소섬유를 제조하였다. The spun fibers were each charged in a tubular electric furnace and then fed with air at a flow rate of 150 i / min. In addition, the temperature was raised at a rate of 1 ° C / min, stabilized by maintaining for 1 hour after reaching 290 ° C. After the stabilization step, nitrogen was injected at a rate of 150ml / min and at the same time heated up at a rate of 5 ° C / niin to reach 800 ° C and maintained for 0.5 hours to prepare a carbon fiber.

<146> 등방성 피치의 방사성 및 제조된 탄소섬유의 물성은 하기 표 1]에 나타내었 다.  The radioactivity of the isotropic pitch and the physical properties of the prepared carbon fiber are shown in Table 1 below.

< 147> [표 11】 ' <Table 11>'

Figure imgf000020_0001
Figure imgf000020_0001

<148> 비교예 및 실시예 모두 용융방사 가능하였고, 표 11을 보면 각 실시예에서 단사가 일어나지 않으면서 인장강도가 최소 1.5GPa 이상, 최대 2.0GPa에 달하는 고 강도 탄소섬유가 제조되었고, 신장률도 2. 1~2.7%에 속하고, 탄소섬유의 직경은 4.30-11.40圆에 속했다. 반면, 비교예 1은 1.3GPa의 인장강도 대비 신장률이 3.2% 로 지나치게 높아 탄성율이 낮았고, 비교예 2도 l . lGPa의 인장강도 대비 신장률이 지나치게 높아 탄성율이 낮았고, 비교예 3 및 4는 단사빈도가 높았으며, 비교예 4 , 5 및 6는 제조된 탄소섬유의 인장강도가 각각 0.7 , 0.9, 0.9로 각 실시예에 비해 현저히 인장강도가 떨어졌다. Both Comparative Examples and Examples were melt-spun, and in Table 11, high-strength carbon fibers having a tensile strength of at least 1.5 GPa and at most 2.0 GPa without single yarns were produced in each Example. 2. It belongs to 1 ~ 2.7%, and the diameter of carbon fiber belongs to 4.30-11.40 圆. On the other hand, Comparative Example 1 has a low elastic modulus due to excessively high elongation ratio of 3.2 GPa to 3.2%, and Comparative Example 2 l. The elastic modulus was low because the elongation ratio was too high compared to the tensile strength of lGPa, and Comparative Examples 3 and 4 had a high single yarn frequency, and Comparative Examples 4, 5, and 6 each carried out a tensile strength of 0.7, 0.9, and 0.9, respectively. Compared to yes Significantly lowered tensile strength.

이는 각 실시예에서 제조된 등방성 피치의 물성 및 구조가 고강도의 등방성 피치계 탄소섬유를 제조하는데 적합한 것을 보여준다.  This shows that the physical properties and structure of the isotropic pitch produced in each example are suitable for producing high strength isotropic pitch-based carbon fibers.

Claims

【청구의 범위】 [Range of request] 【청구항 1】  [Claim 1] X-선 회절분석 (XRD)에서 23<2 Θ<25에서 (002)면 밴드가 나타나고 축합방향족 고리 화합물이 지방족 사슬로 연결된 하기 식 ( 1)~(4)를 만족하는 구조를 포함하는 탄소 섬유 제조용 등방성 피치.  X-ray diffraction analysis (XRD) shows a (002) plane band at 23 <2 Θ <25 and a carbon fiber comprising a structure satisfying the following formulas (1) to (4) in which the condensed aromatic ring compound is connected by an aliphatic chain Isotropic pitch for manufacturing. 5 < La < 15 A一— ( 1) 5 <L a <15 A 一 — (1) 10 < Lc < 25A ― (2) 10 <L c <25 A-(2) 3.50 < dm < 4.50A ― (3) 3.50 <d m <4.50 A-(3) 4.00 < M < 8.00A ― (4)  4.00 <M <8.00 A-(4) (상기 식에서 La는 축합방향족 고리 화합물 층의 평균 직경을 의미하고, Lc 는 축합방향족 고리 화합물 층이 형성하는 적층 구조의 평균 직경을 의미하고, (^은 적층 구조에서 .축합방향족 고리 화합물 층간 평균 거리를 의미하고, M은 적층 구조 에 포함된 축합방향족 고리 화합물 층의 평균 개수 (Lc/d,,,)+l을 의미한다)(Wherein L a means the average diameter of the condensed aromatic ring compound layer, L c means the average diameter of the laminated structure formed by the condensed aromatic ring compound layer, (^ in the laminated structure. Mean distance, M means the average number of condensed aromatic ring compound layers (L c / d ,,,) + l included in the laminated structure) 【청구항 2】 [Claim 2] 제 1항에 있어서' The method of claim 1 연화점이 260 내지 270°C 인 탄소섬유 제조용 등방성 피치. Isotropic pitch for the production of carbon fibers with a softening point of 260 to 270 ° C. 【청구항 3】  [Claim 3] 제 1 항에 있어서, The method of claim 1, 상기 평균분자량이 1650 내지 2850인 탄소섬유 제조용 등방성 피치. ' Isotropic pitch for producing carbon fibers having an average molecular weight of 1650 to 2850. ' 【청구항 4】  [Claim 4] 제 1항에 있어서, The method of claim 1, 4.80 < dv ' < 5.20 A인 탄소섬유 제조용 등방성 피치. Isotropic pitch for making carbon fibers with 4.80 <d v ' <5.20 A. (상기 식에서 (1、.는 축합방향족 고리에 연결된 지방족사슬간 평균 거리를 '의미한다) [청구항 5】 (Wherein R (1 ,. means the average distance between the aliphatic chain attached to the fused aromatic ring ") [Claim 5] a) 석유계 중질유, 고비점 잔사유, 방향족 탄화수소 단물질 및 나프타 분해 공정 잔사유에서 선택되는 어느 하나 또는 이들의 혼합물을 포함하는 원료를 열처 리 및 분획하는 전처리 단계;  a) a pretreatment step of thermally treating and fractionating a raw material comprising any one or a mixture thereof selected from petroleum heavy oil, high boiling residues, aromatic hydrocarbon shorts and naphtha cracking process residues; b) 전처리된 원료에서 고상물질을 제거하는 여과단계;  b) a filtration step of removing solid matter from the pretreated raw material; c) 여과된 원료로 베이직 피치를 제조하는 단계; 및  c) preparing a basic pitch from the filtered raw material; And d) 베이직 피치를 가열하여 등방성 피치를 제조하는 단계;  d) heating the basic pitch to produce an isotropic pitch; 를 포함하는 탄소섬유 제조용 등방성 피치의 제조방법ᅳ [청구항 6】 Method for producing an isotropic pitch for producing carbon fiber comprising a ᅳ [Claim 6] 제 5항에 있어서, The method of claim 5, 상기 전처리 단계는 원료를 130 내지 240°C로 열처리 및 분획하여 진행하는 것인 탄소섬유 제조용 등방성 피치의 제조방법. The pretreatment step is to proceed by heat treatment and fractionation of the raw material to 130 to 240 ° C. Method for producing isotropic pitch for carbon fiber production. [청구항 7】  [Claim 7] 제 5항에 있어서,상기 c) 단계는 원료에 할로겐화합물 및 라디칼개시제를 더 첨가한 후 가열하여 제조하는 할로겐화법 또는 불활성기체 분위기에서 교반 및 가 열하여 질소 및 기체부산물을 분취하는 열중합법으로 베이직 피치를 제조하는 것인 탄소섬유 제조용 등방성 피치의 제조방법.  The method according to claim 5, wherein the step c) is basic by a halogenation method prepared by further adding a halogen compound and a radical initiator to the raw material or by heating and stirring and heating in an inert gas atmosphere to fractionate nitrogen and gaseous by-products. The manufacturing method of the isotropic pitch for carbon fiber manufacture which manufactures a pitch. 【청구항 8】  [Claim 8] 제 7항에 있어서,  The method of claim 7, 상기 할로겐화법은 100 내지 120 °C에서 0. 1 내지 2시간 할로겐화반웅을 진행 시킨 후, 300 내지 330 °C에서 2 내지 4시간 탈할로겐화반응을 진행하는 것인 탄소 섬유 제조용 등방성 피치의 제조방법. The halogenation method is a method of producing an isotropic pitch for carbon fiber manufacturing is to proceed a halogenated reaction at 0.1 to 2 hours at 100 to 120 ° C, 2 to 4 hours at 300 to 330 ° C. 【청구항 9】  [Claim 9] 제 7항에 있어서,  The method of claim 7, wherein 상기 할로겐화합물은 염소, 티오닐클로라이드, 설푸릴클로라이드, 브름 및 요오드에서 선택되는 어느 하나 또는 이들의 흔합물인 탄소섬유 제조용 등방성 피 치의 제조방법.  The halogen compound is any one or a combination thereof selected from chlorine, thionyl chloride, sulfyl chloride, bromide and iodine or a method for producing an isotropic pitch for producing carbon fibers. 【청구항 10】  [Claim 10] 제 7항에 있어서,  The method of claim 7, wherein 상기 라디칼개시제는 벤조일퍼옥사이드, 디부틸히드로퍼옥사이드, 아세틸퍼 옥사이드, 아조비스이소부티로니트릴 및 아조비스메틸이소부틸레이트 에서 선택되 는 어느 하나 또는 이들의 흔합물인 탄소섬유 제조용 등방성 피치의 제조방법. 【청구항 111  The radical initiator is a benzoyl peroxide, dibutyl hydroperoxide, acetyl peroxide, azobisisobutyronitrile and azobismethyl isobutylate any one or a combination thereof is a method for producing isotropic pitch for producing carbon fiber . [Claim 111] 제 7항에 있어서, The method of claim 7, wherein 상기 열중합법은 350 내지 38CTC에서 0 . 1 내지 2시간 진행하는 것인 탄소섬 유 제조용 둥방성 피치의 제조방법.  The thermal polymerization method is 0 to 350 to 38CTC. The manufacturing method of the round pitch for carbon fiber manufacturing which is advanced for 1 to 2 hours. 【청구항 12】  [Claim 12] 제 7항에 있어서, The method of claim 7, 상기 할로겐화법으로 제조된 베이직 피치의 연화점은 70 내지 130°C이고, 상 기 열중합법으로 제조된 베이직 피치의 연화점은 85 내지 140°C인 탄소섬유 제조용 등방성 피치의 제조방법. 【청구항 13】 The softening point of the basic pitch prepared by the halogenation method is 70 to 130 ° C, the softening point of the basic pitch prepared by the thermal polymerization method is 85 to 140 ° C. [Claim 13] 제 5항에 있어서, The method of claim 5, 상기 d) 단계는 진공분위기, 300 내지 350°C에서 0. 1 내지 1시간 동안 가열 하여 진행하는 것인 탄소섬유 제조용 등방성 피치의 제조방법. The d) step is a vacuum atmosphere, the method of producing an isotropic pitch for producing carbon fiber is to proceed by heating for 0.1 to 1 hour at 300 to 350 ° C.
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