CN108004621A - A kind of polyamide resin resin-based composite carbon fiber and preparation method thereof - Google Patents

A kind of polyamide resin resin-based composite carbon fiber and preparation method thereof Download PDF

Info

Publication number
CN108004621A
CN108004621A CN201610968544.6A CN201610968544A CN108004621A CN 108004621 A CN108004621 A CN 108004621A CN 201610968544 A CN201610968544 A CN 201610968544A CN 108004621 A CN108004621 A CN 108004621A
Authority
CN
China
Prior art keywords
polyamide
preparation
starching
resin
carbon fiber
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
CN201610968544.6A
Other languages
Chinese (zh)
Other versions
CN108004621B (en
Inventor
季春晓
黄翔宇
曹阿民
刘瑞超
袁玉红
王平
张捷
吴嵩义
宋文迪
刘礼华
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
China Petroleum and Chemical Corp
Sinopec Shanghai Petrochemical Co Ltd
Original Assignee
China Petroleum and Chemical Corp
Sinopec Shanghai Petrochemical Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by China Petroleum and Chemical Corp, Sinopec Shanghai Petrochemical Co Ltd filed Critical China Petroleum and Chemical Corp
Priority to CN201610968544.6A priority Critical patent/CN108004621B/en
Publication of CN108004621A publication Critical patent/CN108004621A/en
Application granted granted Critical
Publication of CN108004621B publication Critical patent/CN108004621B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • DTEXTILES; PAPER
    • D01NATURAL OR MAN-MADE THREADS OR FIBRES; SPINNING
    • D01FCHEMICAL FEATURES IN THE MANUFACTURE OF ARTIFICIAL FILAMENTS, THREADS, FIBRES, BRISTLES OR RIBBONS; APPARATUS SPECIALLY ADAPTED FOR THE MANUFACTURE OF CARBON FILAMENTS
    • D01F9/00Artificial filaments or the like of other substances; Manufacture thereof; Apparatus specially adapted for the manufacture of carbon filaments
    • D01F9/08Artificial filaments or the like of other substances; Manufacture thereof; Apparatus specially adapted for the manufacture of carbon filaments of inorganic material
    • D01F9/12Carbon filaments; Apparatus specially adapted for the manufacture thereof
    • D01F9/14Carbon filaments; Apparatus specially adapted for the manufacture thereof by decomposition of organic filaments
    • D01F9/20Carbon filaments; Apparatus specially adapted for the manufacture thereof by decomposition of organic filaments from polyaddition, polycondensation or polymerisation products
    • D01F9/21Carbon filaments; Apparatus specially adapted for the manufacture thereof by decomposition of organic filaments from polyaddition, polycondensation or polymerisation products from macromolecular compounds obtained by reactions only involving carbon-to-carbon unsaturated bonds
    • D01F9/22Carbon filaments; Apparatus specially adapted for the manufacture thereof by decomposition of organic filaments from polyaddition, polycondensation or polymerisation products from macromolecular compounds obtained by reactions only involving carbon-to-carbon unsaturated bonds from polyacrylonitriles
    • CCHEMISTRY; METALLURGY
    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08KUse of inorganic or non-macromolecular organic substances as compounding ingredients
    • C08K7/00Use of ingredients characterised by shape
    • C08K7/02Fibres or whiskers
    • C08K7/04Fibres or whiskers inorganic
    • C08K7/06Elements
    • CCHEMISTRY; METALLURGY
    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08KUse of inorganic or non-macromolecular organic substances as compounding ingredients
    • C08K9/00Use of pretreated ingredients
    • C08K9/04Ingredients treated with organic substances
    • 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
    • D01F11/00Chemical after-treatment of artificial filaments or the like during manufacture
    • D01F11/10Chemical after-treatment of artificial filaments or the like during manufacture of carbon
    • D01F11/14Chemical after-treatment of artificial filaments or the like during manufacture of carbon with organic compounds, e.g. macromolecular compounds
    • DTEXTILES; PAPER
    • D06TREATMENT OF TEXTILES OR THE LIKE; LAUNDERING; FLEXIBLE MATERIALS NOT OTHERWISE PROVIDED FOR
    • D06MTREATMENT, NOT PROVIDED FOR ELSEWHERE IN CLASS D06, OF FIBRES, THREADS, YARNS, FABRICS, FEATHERS OR FIBROUS GOODS MADE FROM SUCH MATERIALS
    • D06M15/00Treating fibres, threads, yarns, fabrics, or fibrous goods made from such materials, with macromolecular compounds; Such treatment combined with mechanical treatment
    • D06M15/19Treating fibres, threads, yarns, fabrics, or fibrous goods made from such materials, with macromolecular compounds; Such treatment combined with mechanical treatment with synthetic macromolecular compounds
    • D06M15/21Macromolecular compounds obtained by reactions only involving carbon-to-carbon unsaturated bonds
    • D06M15/285Macromolecular compounds obtained by reactions only involving carbon-to-carbon unsaturated bonds of unsaturated carboxylic acid amides or imides
    • DTEXTILES; PAPER
    • D06TREATMENT OF TEXTILES OR THE LIKE; LAUNDERING; FLEXIBLE MATERIALS NOT OTHERWISE PROVIDED FOR
    • D06MTREATMENT, NOT PROVIDED FOR ELSEWHERE IN CLASS D06, OF FIBRES, THREADS, YARNS, FABRICS, FEATHERS OR FIBROUS GOODS MADE FROM SUCH MATERIALS
    • D06M15/00Treating fibres, threads, yarns, fabrics, or fibrous goods made from such materials, with macromolecular compounds; Such treatment combined with mechanical treatment
    • D06M15/19Treating fibres, threads, yarns, fabrics, or fibrous goods made from such materials, with macromolecular compounds; Such treatment combined with mechanical treatment with synthetic macromolecular compounds
    • D06M15/37Macromolecular compounds obtained otherwise than by reactions only involving carbon-to-carbon unsaturated bonds
    • D06M15/53Polyethers
    • DTEXTILES; PAPER
    • D06TREATMENT OF TEXTILES OR THE LIKE; LAUNDERING; FLEXIBLE MATERIALS NOT OTHERWISE PROVIDED FOR
    • D06MTREATMENT, NOT PROVIDED FOR ELSEWHERE IN CLASS D06, OF FIBRES, THREADS, YARNS, FABRICS, FEATHERS OR FIBROUS GOODS MADE FROM SUCH MATERIALS
    • D06M15/00Treating fibres, threads, yarns, fabrics, or fibrous goods made from such materials, with macromolecular compounds; Such treatment combined with mechanical treatment
    • D06M15/19Treating fibres, threads, yarns, fabrics, or fibrous goods made from such materials, with macromolecular compounds; Such treatment combined with mechanical treatment with synthetic macromolecular compounds
    • D06M15/37Macromolecular compounds obtained otherwise than by reactions only involving carbon-to-carbon unsaturated bonds
    • D06M15/59Polyamides; Polyimides
    • DTEXTILES; PAPER
    • D06TREATMENT OF TEXTILES OR THE LIKE; LAUNDERING; FLEXIBLE MATERIALS NOT OTHERWISE PROVIDED FOR
    • D06MTREATMENT, NOT PROVIDED FOR ELSEWHERE IN CLASS D06, OF FIBRES, THREADS, YARNS, FABRICS, FEATHERS OR FIBROUS GOODS MADE FROM SUCH MATERIALS
    • D06M2101/00Chemical constitution of the fibres, threads, yarns, fabrics or fibrous goods made from such materials, to be treated
    • D06M2101/40Fibres of carbon
    • DTEXTILES; PAPER
    • D06TREATMENT OF TEXTILES OR THE LIKE; LAUNDERING; FLEXIBLE MATERIALS NOT OTHERWISE PROVIDED FOR
    • D06MTREATMENT, NOT PROVIDED FOR ELSEWHERE IN CLASS D06, OF FIBRES, THREADS, YARNS, FABRICS, FEATHERS OR FIBROUS GOODS MADE FROM SUCH MATERIALS
    • D06M2200/00Functionality of the treatment composition and/or properties imparted to the textile material
    • D06M2200/40Reduced friction resistance, lubricant properties; Sizing compositions

Landscapes

  • Chemical & Material Sciences (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Engineering & Computer Science (AREA)
  • Textile Engineering (AREA)
  • General Chemical & Material Sciences (AREA)
  • Health & Medical Sciences (AREA)
  • Medicinal Chemistry (AREA)
  • Polymers & Plastics (AREA)
  • Organic Chemistry (AREA)
  • Treatments For Attaching Organic Compounds To Fibrous Goods (AREA)
  • Inorganic Fibers (AREA)

Abstract

The invention discloses a kind of polyamide resin resin-based composite carbon fiber and preparation method thereof, preparation method of the present invention includes the step of polymerization, spinning, pre-oxidation, low-temperature carbonization, high temperature cabonization, surface treatment, starching, drying and winding receive silk.The present invention selects polyamide resin aliphatic radical suspension sizing agent, and starching is realized by infusion process.Heated during carbon fiber starching at the same time using steam hot-rolling;Dry after starching and be dried by the way of the drying of vertical hot air drier.The beneficial effects of the present invention are:Preparation method of the present invention is simple, and prepared carbon fiber is suitable for preparing polyamide resin resin-based composite, and prepared composite technology excellent performance, interface mechanical characteristic is high, and wear resistance is good.

Description

A kind of polyamide resin resin-based composite carbon fiber and preparation method thereof
Technical field
The invention belongs to carbon fiber preparation field, more particularly to a kind of polyamide resin resin-based composite carbon fiber and its Preparation method.
Background technology
Become increasingly conspicuous recently as the problems such as energy shortage, environmental pollution, carbon fibre composite Lightweight Technology, follow Ring is accelerated using technology, rapid shaping technique development, is especially increasingly closed in industrial circles such as automotive field, pressurized tanks Note.As breach, fibre reinforced thermoplasticity composite material is able to fast development.Carbon fiber reinforced polyamide resin with Its excellent wear-resistant and mechanical property etc. receives significant attention, but there are resin dipping is tired using multiple material prepared by current technology Difficult, many technological difficulties such as serious, the multiple material performance of hole defect is unstable, to find out its cause, being due on the one hand to be processed at present Type technology still has some deficits, and in addition answers material system primarily directed to thermosetting epoxy resin mainly due to current carbon fiber and grinds System, the coating of its surface is mostly epoxy resin or modified epoxy class sizing agent.Such sizing agent standing time it is long or Part or all of curing can be produced under higher drying, processing temperature, causes fibre bundle to be hardened, ossify, reunite, further Cause matrix resin impregnation difficulties, easily produce fault gap, multiple material is produced local mechanical defect.Particular for polyamide resin Carbon fiber prepared by resin-based composite is more rare.Chinese patent (Application No. 201310052755.1) provide it is a kind of by The modified polyamide class sizing agent and its carbon fiber of preparation that polyamide, organic solvent, surface modifier, water etc. are prepared, But due to containing solvent, its security stability is poor, has been eliminated substantially in sizing agent industrial application.
The content of the invention
In order to overcome the prior art, it is an object of the invention to provide a kind of polyamide resin resin-based composite carbon fiber And preparation method thereof.It is controllable using carbon fiber starching amount height made of the method for the present invention, it can sprawl to form wide ribbon-like fibre, Increase tow width, reduce the difficulty of product processing among follow-up, the product among follow-up that reduce process required resin demand, improve Prepreg processing uniformity and stability.Prepared carbon fiber surface coats one layer of starching prepared completely by polyamide Agent, without epoxy resin group, suitable for preparing polyamide resin resin-based composite, prepared composite technology performance is excellent Different, interface mechanical characteristic is high, and wear resistance is good.
The present invention is using polymerization, spinning, pre-oxidation, low-temperature carbonization, high temperature cabonization, surface treatment, starching, drying and winding Receive silk production process.The problems such as to solve bad polyamide substrate resin dipping and fiber ageing hardening, the present invention is used with poly- Amide resin powder is main body, introduces polyacrylamide amine dispersant, while introduce the fatty alcohol polyoxy with long chain oleophillic group Vinethene stabilizer, can produce with polyacrylamide with polyamide and effectively combine, have well amphipathic, can prepare Obtain suspension sizing agent stable and reliable for performance;To solve the problems, such as that fiber is dried under the conditions of high starching amount, improves polyamide resin The uniformity that cosmetics end is sprawled in carbon fiber surface, present invention back tender after sizing process introduces the heating of steam hot-rolling, starching Sequence introduces the drying process of vertical hot air drier drying.
The present invention provides a kind of preparation method of polyamide resin resin-based composite carbon fiber, which includes poly- The step of conjunction, spinning, pre-oxidation, low-temperature carbonization, high temperature cabonization, surface treatment, starching, drying and winding receive silk;Wherein:Starching When by infusion process using polyamide resin aliphatic radical suspension sizing agent carry out;The polyamide resin aliphatic radical suspension sizing agent is by gathering Amide resin, dispersant, stabilizer and deionized water composition;Counted according to the gross mass of solid constituent for 100%, polyamide 60~80% are accounted for, dispersant accounts for 5~15%, and stabilizer accounts for 15~25%.
In the present invention, low-temperature carbonization carries out in low temperature carbonization furnace, and low temperature carbonization furnace has 6 warm areas, temperature control difference For 0~650 DEG C, 0~650 DEG C, 0~750 DEG C, 0~900 DEG C, 0~900 DEG C, 0~900 DEG C.
In the present invention, high temperature cabonization carries out in high temperature carbonization furnace, and high temperature carbonization furnace has 6 warm areas, temperature control difference For 0~1250 DEG C, 0~1350 DEG C, 0~1600 DEG C, 0~1800 DEG C, 0~2000 DEG C and 0~2000 DEG C.
In the present invention, the preparation method of the polyamide resin aliphatic radical suspension sizing agent is as follows:First by polyamide, point Powder is uniformly mixed in deionized water, adds stabilizer, is emulsified in high-speed emulsifying machine with 2000~10000rpm rotating speeds Suspension sizing agent is obtained after 10~25min.
In the present invention, the polyamide has the general structure such as following formula I:
Wherein p is the degree of polymerization of polyamide, m and n numerical value can be identical or different.The equal molecule of polyamide number Amount is 1.0 ten thousand~3.0 ten thousand, preferably 1.5 ten thousand~2.5 ten thousand.The polyamide powder average diameter is excellent between 20~50 microns Select 30~40 microns.
In the present invention, the polyamide is selected from polyamide 6, polyamide 11, polyamide 12, polyamide 66, polyamide 610th, any one or a few in polyamide 612, polyamide 1010 or polyamide 1012.
In the present invention, the dispersant is polyacrylamide, and number-average molecular weight is between 1.0 ten thousand~3.0 ten thousand, preferably 1.5 ten thousand~2.0 ten thousand.The stabilizer is fatty alcohol polyoxyethylene ether, it has such as the general structure of formula II:
Wherein, R is selected from the saturated aliphatic groups for including 15~20 carbon atoms;Polyoxyethylene polymerization degree n scope is 20 ~40.
In the present invention, in polyamide resin aliphatic radical suspension sizing agent, the content of solid constituent is 5%~30%;During starching Starching amount control 1%~20%.
In the present invention, during starching, the carbon fiber after starching passes through steam hot-rolling again.Temperature control model on steam hot-rolling roll surface Enclose 0~360 DEG C.When fiber after starching is by steam hot-rolling, partial moisture is on the one hand removed, prevents fiber from entering rear road high temperature Violent vaporization causes dangerous during drying box;On the other hand, the polyamide powder that surface is stained with melts at high temperature to be sprawled, just Step forms more homogeneous continuous one layer of polyamide resin.
It is dry to be carried out using vertical hot air drier in the present invention;The warm area of the vertical drying case is 4, each area's temperature Degree control is respectively 0~350 DEG C, 0~300 DEG C, 0~200 DEG C and 0~150 DEG C.The method that vertical drying is used in the present invention, Make the further melt-flow of carbon fiber surface polyamide, the slow levelling under Gravitative Loads, makes carbon fiber surface polyamide Resin film is more uniformly distributed completely;It can ensure all to remove fiber surface moisture under the conditions of high starching amount at the same time.
The present invention also provides the polyamide resin resin-based composite carbon fiber that a kind of above-mentioned preparation method obtains.
In the prior art, when carrying out carbon fiber starching using emulsion-type epoxy resin-matrix sizing agent, due to epoxy resin Softening temperature is relatively low, therefore cannot use excessive drying temperature.Under the conditions of drying temperature and drying time are restricted, adopt The starching amount that carbon fiber is prepared with emulsion-type epoxy resin-matrix sizing agent cannot be too high, no to be difficult to dry it will cause sized fiber Dry, large quantity of moisture is contained on surface, influences rear road processed and applied, while also limit carbon fiber and must be prepared into collection bundle fiber.
Compared with using emulsion-type epoxy resin-matrix sizing agent starching production Carbon Fiber Technology, polyamides of the present invention Polyimide resin base suspension starching carbon fiber can use the starching agent concentration of higher, have the starching amount of higher, prepared carbon It can sprawl to form broadband after the drying process that fiber is dried using the heating of steam hot-rolling, vertical hot air drier described in this patent Shape fiber, increases tow width, and breadth improves 50%~130%, effectively reduces fiber thickness.Carbon fiber can be sprawled preferably Difficulty even, that polyamide is infiltrated to fibrous inside infiltration when advantageously reducing product processing among follow-up composite material, at the same time The dosage of resin film, improves prepreg processing uniformity and stability when can reduce prepreg processing, reduces production cost.
Compared to the prior art, the beneficial effects of the present invention are:
(1) a kind of polyamide resin resin-based composite carbon fiber surface of the present invention, polyamide coating resin base Carbon fiber sizing agent, without epoxy resin group, long-time storage will not produce ageing hardening phenomenon, can and polyamide substrate Resin has good infiltration and binding ability, and processing performance and abrasion resistance properties are excellent.
(2) suspension carbon fiber sizing agent of the present invention introduces polyacrylamide amine dispersant, while introduces to have and grow The fatty alcohol polyoxyethylene ether stabilizer of chain lipophilic group, can produce with polyamide and polyacrylamide and effectively combine, With good amphipathic, prepared sizing agent is of low cost, simple process, safety and stability meet engineering process need Will.
(3) drying process of the heating of steam hot-rolling and the drying of starching rear vertical type hot air drier when the present invention uses starching, Both the polyamide powder that can be stained with carbon fiber surface melts at high temperature to be sprawled, and forms homogeneous continuous polyamide Film, while the slow levelling under Gravitative Loads, polyamide resin powders can quickly and evenly sprawl infiltration carbon fiber, carbon fiber Starching is more uniform.
(4) polyamide resin resin-based composite of the present invention controllable, the Ke Yipu of carbon fiber surface starching amount height Spread increases tow width, improves tow breadth, reduce fiber thickness, reduce among follow-up composite material into wide ribbon-like fibre The difficulty of product processing, reduces the resin demand of the follow-up centre of material again product processing, improves processing uniformity and stability.
Embodiment
With reference to specific embodiment, the present invention is further explained.It is to be understood that these embodiments are merely to illustrate the present invention Rather than limit the scope of the invention.In addition, it should also be understood that, after reading the content taught by the present invention, people in the art Member can make various changes or modifications the present invention, and such equivalent forms equally fall within the application the appended claims and limited Scope.
Comparative example 1
Comparative example 1 is a kind of manufacture method of 3K carbon fibers, and detailed process includes polymerization, spinning, pre-oxidation, cryogenic carbon Change, high temperature cabonization, surface treatment, starching, drying, winding receive silk production process.The detailed process of comparative example 1 and embodiment 1~4 Detailed process it is identical, wherein polymerization, pre-oxidation, low-temperature carbonization, high temperature cabonization, the parameter of starching are different.
Step 1, it polymerize.The polymerization process is identical with the described method of 1~4 step 1 of embodiment, wherein polymerizeing The parameter that production process changes is that the comonomer type of ternary aqueous polymerization reaction is different with proportioning, acrylonitrile, metering system Sour methyl esters, the weight ratio of itaconic acid are 95.2:3.0:1.8, the input concentration of total polymerization monomer is 22wt%, and initiator uses chlorine Sour sodium and sodium pyrosulfite, sodium chlorate dosage are calculated as 0.05wt%, sodium pyrosulfite and sodium chlorate with all polymerized monomer total amounts The ratio between molal quantity is 1.4:1.60 DEG C of polymeric reaction temperature, reaction time are 102 minutes.
Step 2, spinning.The spinning production process and the described method of 1~4 step 2 of embodiment.
Step 3, pre-oxidize.The pre-oxidation production process is identical with the described method of 1~4 step 3 of embodiment.Wherein It is No. 1 oxidation furnace, No. 2 oxidation furnaces, No. 3 oxidation furnaces, No. 4 oxidation furnaces, No. 5 oxidation furnaces, 6 to pre-oxidize the parameter that production process changes Number oxidation furnace stove area temperature is respectively 223 DEG C, 232 DEG C, 245 DEG C, 250 DEG C, 256 DEG C, 264 DEG C.Between each warm area of oxidation furnace Drafting multiple is respectively -0.2%, -1.3%, -4.2%, -4.2%, -0.5%, -0.5%.
Step 4, low-temperature carbonization.The low-temperature carbonization production process is identical with the described method of 1~4 step 4 of embodiment. The parameter that wherein low-temperature carbonization production process changes is the 1st area of low temperature carbonization furnace, the 2nd area, the 3rd area, the 4th area, the 5th area, the 6th area Temperature control is respectively 450 DEG C, 520 DEG C, 580 DEG C, 650 DEG C, 720 DEG C, 760 DEG C.It is 3.0% to control drafting multiple.
Step 5, high temperature cabonization.The high temperature cabonization production process is identical with the described method of 1~4 step 5 of embodiment. The parameter that wherein high temperature cabonization production process changes is the 1st area of high temperature carbonization furnace, the 2nd area, the 3rd area, the 4th area, the 5th area, the 6th area Temperature control is respectively 820 DEG C, 920 DEG C, 1200 DEG C, 1250 DEG C, 1300 DEG C, 1350 DEG C.It is -4.0% to control drafting multiple.
Step 6, it is surface-treated.The surface treatment production process is identical with the described method of 1~4 step 6 of embodiment.
Step 7, starching and drying, winding receive silk.Sizing agent uses bisphenol A epoxide resin base emulsion type carbon fiber sizing agent (Chinese Academy of Sciences's Shanghai Institute of Organic Chemistry production, KTM-1 types), starching agent concentration 3.0%, directly uses horizontal circulation heated-air drying after starching, 120 DEG C of drying temperature, winding receives silk and 3K starching carbon fibers is prepared under 1000~1350cN tension force.
Comparative example 2
Comparative example 2 is a kind of manufacture method of 6K carbon fibers, and detailed process includes polymerization, spinning, pre-oxidation, cryogenic carbon Change, high temperature cabonization, surface treatment, starching, drying, winding receive silk production process.The polymerization of comparative example 2, Pre oxidation and each Area's drafting multiple, low-temperature carbonization temperature and drafting multiple, high temperature cabonization temperature and drafting multiple, surface treatment detailed process and Parameter is identical with comparative example 1.Pre-oxidize total residence time, low-temperature carbonization total residence time, high temperature cabonization total residence time and reality It is identical to apply 5~8 step 3~5 of example.The spinning parameter of comparative example 2 is identical with 5~8 step 2 of embodiment.The sizing process of comparative example 2 Identical with comparative example 1, the parameter of wherein starching is different.Sizing agent uses bisphenol F epoxy resin base emulsion type carbon fiber sizing agent (Chinese Academy of Sciences's Shanghai Institute of Organic Chemistry production, KTM-2 types), starching agent concentration 2.5%, directly uses horizontal circulation heated-air drying after starching, 130 DEG C of drying temperature, winding receives silk and 6K starching carbon fibers is prepared under 1400~1650cN tension force.
Embodiment 1~4
The present embodiment is a kind of manufacture method of the 3K carbon fibers suitable for polyamide resin resin-based composite, including poly- Conjunction, spinning, pre-oxidation, low-temperature carbonization, high temperature cabonization, surface treatment, starching, drying, winding receive silk production process.Detailed process It is as follows:
Step 1:Polymerization.
Polymerisation is carried out using acrylonitrile aqueous suspension polymerization technique, with acrylonitrile, methyl methacrylate, itaconic acid Ammonium is polymerized monomer, and acrylonitrile, methyl methacrylate, the weight ratio of itaconic acid ammonium are 95.3:2.8:1.9, total polymerization monomer Input concentration be 23wt%, while add initiator ammonium persulfate, initiator amount is calculated as with all polymerized monomer total amounts 0.53wt%, 63 DEG C of polymeric reaction temperature, reaction time are 110 minutes.Then obtained condensate is dissolved in concentration is In the dense sodium thiocyanate solution of 52wt%, dissolving is stirred, spinning is made after deaeration is filtered in dissolved thick stoste Polyacrylonitrile matrix.
Step 2:Spinning.
Using sodium sulfocyanate (NaSCN) wet spinning production method, by polyacrylonitrile matrix by solidification forming, cold lead Stretch, wash, hot gas spring, oil, dry, steam drafting, sizing, be made precursor.The hole diameter of spinneret 0.062mm, solidification forming temperature When 0 DEG C of degree, coagulating bath flow 1500L/ are small, solidify bath concentration 14.2%;1.93 times of the drafting multiple of cold drawing-off;Washing temperature 50 DEG C, when washing flow 1400L/ is small;92 DEG C of hot gas spring temperature, 5.2 times of the drafting multiple of hot gas spring;Oil oil concentration 2%;It is dry Dry 125 DEG C of temperature;2.0 times of steam drafting multiple, steam pressure 100KPa;110 DEG C of setting temperature.
Step 3:Pre-oxidation.
Precursor sequentially passes through No. 1 oxidation furnace, No. 2 oxidation furnaces, No. 3 oxidation furnaces, No. 4 oxidation furnaces, No. 5 oxidation furnaces, No. 6 oxidations Stove carries out pre-oxidation treatment.No. 1 oxidation furnace, No. 2 oxidation furnaces, No. 3 oxidation furnaces, No. 4 oxidation furnaces, No. 5 oxidation furnaces, No. 6 oxidation furnaces Stove area temperature is respectively 215 DEG C, 226 DEG C, 232 DEG C, 240 DEG C, 250 DEG C, 260 DEG C.Drafting multiple between each warm area of oxidation furnace Respectively -0.1%, -1.2%, -4%, -4%, -0.5%, -0.5%.Each 14 minutes oxidation furnace residence times, pre-oxidation are total Time is 84min.
Step 4:Low-temperature carbonization
The oxidization fiber of No. 6 oxidation outlet of stills enters low temperature carbonization furnace by draw-gear, using nitrogen as medium, carries out low temperature Carbonization, is made low-temperature carbonization silk.The 1st area of low temperature carbonization furnace, the 2nd area, the 3rd area, the 4th area, the 5th area, the 6th area's temperature control difference For 440 DEG C, 510 DEG C, 560 DEG C, 630 DEG C, 700 DEG C, 750 DEG C.It is 3.5% to control drafting multiple, is always stopped in low temperature carbonization furnace It is 1.6min to stay the time.
Step 5::High temperature cabonization
The tow of low-temperature carbonization outlet of still enters high temperature carbonization furnace by draw-gear, using nitrogen as medium, carries out high temperature Carbonization, is made high temperature cabonization silk.The 1st area of high temperature carbonization furnace, the 2nd area, the 3rd area, the 4th area, the 5th area, the 6th area's temperature control difference For 810 DEG C, 900 DEG C, 1150 DEG C, 1200 DEG C, 1250 DEG C, 1320 DEG C.It is -3.0% to control drafting multiple, in high temperature carbonization furnace Total residence time is 1.6min.
Step 6:Surface treatment
The tow of high temperature cabonization outlet of still enters surface processing trough by draw-gear, using ammonium bicarbonate aqueous solution as electrolysis Liquid, voltage 20V, concentration of electrolyte 12%, the residence time is 3min to tow in the electrolytic solution.
Step 7:Starching and drying, winding receive silk
Quantitative polyamide resin powders, polyacrylamide are uniformly mixed spare;Quantitative water is added in reaction kettle A And mechanical agitation is opened, keep under certain rotating speed, be gradually added into said mixture, continue the timing of stirring one after being added completely into Between;Above-mentioned aqueous mixture is transferred in reaction kettle B by dosing pump, adds quantitative fatty alcohol polyoxyethylene ether, is opened High-speed emulsifying machine, suspension sizing agent is prepared with the emulsification of certain rotating speed after a certain period of time.Then by charging pump by starching Agent is transferred in sizing groove, is opened sizing groove circulating pump, sizing agent is slowly flowed in sizing groove.
The tow for being surface-treated outlet is impregnated by sizing agent first in the first live-roller in sizing groove, sizing groove successively Roller, the second live-roller, the second dip roll, steam hot-rolling, the 3rd live-roller, pressure roller.Wherein lead at the steam inlet of steam hot-rolling It is 40kgf/cm to enter absolute pressure2Saturated vapor, 250 DEG C of temperature controlling range on steam hot-rolling roll surface.Carbon after starching Fiber is dried into vertical hot air drier, and 4 warm area temperature controls are respectively 330 DEG C, 280 DEG C, 180 DEG C, 120 DEG C. The dried carbon fiber of starching enters carbon fiber wound machine, and winding is received silk and is made suitable for polyamides under 1000~1350cN tension force The 3K carbon fibers of polyimide resin based composites.
Embodiment 5~8
The present embodiment is a kind of manufacture method of the 6K carbon fibers suitable for polyamide resin resin-based composite, detailed process Silk production process is received including polymerization, spinning, pre-oxidation, low-temperature carbonization, high temperature cabonization, surface treatment, starching, drying, winding.This The detailed process of embodiment is identical with the detailed process of embodiment 1~4, wherein polymerization, spinning, pre-oxidation, low-temperature carbonization, high temperature Carbonization, the parameter of starching are different.
Step 1, it polymerize.The polymerization process is identical with the described method of 1~4 step 1 of embodiment, wherein polymerizeing The parameter that production process changes is that the comonomer proportioning of ternary aqueous polymerization reaction is different, acrylonitrile, methyl methacrylate, The weight ratio of itaconic acid ammonium is 95.0:3.3:1.7, the input concentration of total polymerization monomer is 21wt%, and initiator ammonium persulfate is used Amount is calculated as 0.51wt%, 61 DEG C of polymeric reaction temperature with all polymerized monomer total amounts, and the reaction time is 100 minutes.
Step 2, spinning.The spinning production process is identical with the described method of 1~4 step 2 of embodiment, solidification forming When 0.5 DEG C of temperature, coagulating bath flow 2000L/ are small, solidify bath concentration 14%;1.9 times of the drafting multiple of cold drawing-off;Washing temperature 52 DEG C, when washing flow 1800L/ is small;95 DEG C of hot gas spring temperature, 5.0 times of the drafting multiple of hot gas spring;Oil oil concentration 2.2%;130 DEG C of drying temperature;1.88 times of steam drafting multiple, steam pressure 105KPa;115 DEG C of setting temperature.
Step 3, pre-oxidize.The pre-oxidation production process is identical with the described method of 1~4 step 3 of embodiment.Wherein It is No. 1 oxidation furnace, No. 2 oxidation furnaces, No. 3 oxidation furnaces, No. 4 oxidation furnaces, No. 5 oxidation furnaces, 6 to pre-oxidize the parameter that production process changes Number oxidation furnace stove area temperature is respectively 220 DEG C, 230 DEG C, 240 DEG C, 248 DEG C, 254 DEG C, 262 DEG C.Between each warm area of oxidation furnace Drafting multiple is respectively -0.1%, -1.2%, -4%, -4%, -0.5%, -0.5%.Each 15 minutes oxidation furnace residence times, Pre-oxidation total time is 90min.
Step 4, low-temperature carbonization.The low-temperature carbonization production process is identical with the described method of 1~4 step 4 of embodiment. The parameter that wherein low-temperature carbonization production process changes is the 1st area of low temperature carbonization furnace, the 2nd area, the 3rd area, the 4th area, the 5th area, the 6th area Temperature control is respectively 455 DEG C, 530 DEG C, 590 DEG C, 670 DEG C, 710 DEG C, 760 DEG C.It is 3.2% to control drafting multiple.In low temperature Total residence time is 1.7min in carbide furnace.
Step 5, high temperature cabonization.The high temperature cabonization production process is identical with the described method of 1~4 step 5 of embodiment. The parameter that wherein high temperature cabonization production process changes is the 1st area of high temperature carbonization furnace, the 2nd area, the 3rd area, the 4th area, the 5th area, the 6th area Temperature control is respectively 826 DEG C, 930 DEG C, 1250 DEG C, 1280 DEG C, 1320 DEG C, 1360 DEG C.It is -3.5% to control drafting multiple. Total residence time is 1.7min in high temperature carbonization furnace.
Step 6, it is surface-treated.The surface treatment production process is identical with the described method of 1~4 step 6 of embodiment.
Step 7, starching and drying, winding receive silk.
Suspension sizing agent preparation method, method for sizing, drying means, winding receipts silk method and the embodiment 1~4 The described method of step 7 is identical.It is 48kgf/cm that absolute pressure is wherein passed through at the steam inlet of steam hot-rolling2Saturated water Steam, 260 DEG C of temperature on steam hot-rolling roll surface.Vertical 4 warm area temperature controls of hot air drier are respectively 320 DEG C, 275 DEG C, 175℃、120℃.It is 1400~1650cN to control winding tension, the final 6K being made suitable for polyamide resin resin-based composite Carbon fiber.
Suspension sizing agent solid constituent prepared by above-described embodiment 1~8 is shown in Table 1, and sizing agent forms dosage and concentration 2 are shown in Table, sizing agent preparation technology parameter is shown in Table 3, and gained carbon fiber Evaluation results are shown in Table 4.The present invention uses SP10 high temperature Starching amount of the starching tester to starching carbon fiber is tested;The breadth of starching carbon fiber is tested using ruler; Using OCA20 contact angle measurements test polyamide drop from contact carbon fiber is started to being totally submerged inside carbon fiber The complete wetting time;Polyamide is tested using Japanese Dong Rong industry companies MODEL HM410 interface performances evaluating apparatus With the interface shear strength of carbon fiber.
By the test result of 3K carbon fibers in embodiment 1~4 as it can be seen that with comparative example 1 (using on epoxy resin-matrix sizing agent The carbon fiber of slurry) to compare, the starching carbon fiber starching amount higher being prepared using suspension sizing agent, breadth is substantially increased, Starching amount coefficient of dispersion is low, shows that fiber surface is uniformly coated with more polyamide sizing agent and fiber has been obtained sufficiently Expanding effect.Polyamide is less to starching carbon fiber infiltrating time, better technological properties, interface shear strength higher, fine Dimension has more preferable effect of impregnation and binding ability with polyamide substrate interlaminar resin.6K carbon fibers obtain together in embodiment 5~8 The improvement of sample.
1 sizing agent solid constituent of table
2 sizing agent of table forms dosage and concentration
3 sizing agent preparation technology parameter of table
4 carbon fiber Evaluation results of table
Although the present invention discloses preferred embodiment as above, so it is not limited to present disclosure, any ripe Know this those skilled in the art, do not departing from the present invention main spirits and context in, when can make it is various change and retouch, because of the invention Protection domain should be subject to the actual claim scope applied for a patent.

Claims (10)

1. a kind of preparation method of polyamide resin resin-based composite carbon fiber, it is characterised in that the preparation process includes poly- The step of conjunction, spinning, pre-oxidation, low-temperature carbonization, high temperature cabonization, surface treatment, starching, drying and winding receive silk;Wherein:Starching When by infusion process using polyamide resin aliphatic radical suspension sizing agent carry out;The polyamide resin aliphatic radical suspension sizing agent is by gathering Amide resin, dispersant, stabilizer and deionized water composition;Counted according to the gross mass of solid constituent for 100%, polyamide 60~80% are accounted for, dispersant accounts for 5~15%, and stabilizer accounts for 15~25%.
2. preparation method according to claim 1, it is characterised in that low-temperature carbonization carries out in low temperature carbonization furnace, low temperature Carbide furnace has 6 warm areas, and temperature control is respectively 0~650 DEG C, 0~650 DEG C, 0~750 DEG C, 0~900 DEG C, 0~900 DEG C and 0 ~900 DEG C.
3. preparation method according to claim 1, it is characterised in that high temperature cabonization carries out in high temperature carbonization furnace, high temperature Carbide furnace has 6 warm areas, temperature control is respectively 0~1250 DEG C, 0~1350 DEG C, 0~1600 DEG C, 0~1800 DEG C, 0~2000 DEG C and 0~2000 DEG C.
4. preparation method according to claim 1, it is characterised in that the system of the polyamide resin aliphatic radical suspension sizing agent Preparation Method is as follows:First polyamide, dispersant are uniformly mixed in deionized water, add stabilizer, is emulsified in high speed Suspension sizing agent is obtained after emulsifying 10~25min in machine with 2000~10000rpm rotating speeds.
5. preparation method according to claim 1, it is characterised in that the polyamide is selected from polyamide 6, polyamide 11st, any one in polyamide 12, polyamide 66, polyamide 610, polyamide 612, polyamide 1010 or polyamide 1012 or It is several.
6. preparation method according to claim 1, it is characterised in that the dispersant is polyacrylamide, and number is divided equally Son amount is between 1.0 ten thousand~3.0 ten thousand;The stabilizer is fatty alcohol polyoxyethylene ether.
7. preparation method according to claim 1, it is characterised in that in polyamide resin aliphatic radical suspension sizing agent, solid The content of component is 5%~30%;Starching amount during starching is controlled 1%~20%.
8. preparation method according to claim 1, it is characterised in that when carbon fiber carries out sizing process, introduce steam heat Roller heats.
9. preparation method according to claim 1, it is characterised in that dry to be carried out using vertical hot air drier;It is described The warm area of vertical drying case is 4, and each area's temperature control is respectively 0~350 DEG C, 0~300 DEG C, 0~200 DEG C and 0~150 DEG C.
10. the polyamide resin resin-based composite carbon that a kind of preparation method according to one of claim 1-9 obtains is fine Dimension.
CN201610968544.6A 2016-10-28 2016-10-28 Carbon fiber for polyamide resin matrix composite material and preparation method thereof Active CN108004621B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201610968544.6A CN108004621B (en) 2016-10-28 2016-10-28 Carbon fiber for polyamide resin matrix composite material and preparation method thereof

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201610968544.6A CN108004621B (en) 2016-10-28 2016-10-28 Carbon fiber for polyamide resin matrix composite material and preparation method thereof

Publications (2)

Publication Number Publication Date
CN108004621A true CN108004621A (en) 2018-05-08
CN108004621B CN108004621B (en) 2022-01-21

Family

ID=62047669

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201610968544.6A Active CN108004621B (en) 2016-10-28 2016-10-28 Carbon fiber for polyamide resin matrix composite material and preparation method thereof

Country Status (1)

Country Link
CN (1) CN108004621B (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112877950A (en) * 2021-01-12 2021-06-01 中国科学院苏州纳米技术与纳米仿生研究所南昌研究院 Preparation system and method of filament carbon fiber 3D printing wire
CN113529242A (en) * 2021-07-29 2021-10-22 吉祥三宝高科纺织有限公司 Method for preparing anti-cutting gloves by using carbon fiber composite material

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103290527A (en) * 2013-05-22 2013-09-11 西安康本材料有限公司 Method for lowering ash content of polyacrylonitrile-based carbon fiber
CN103774284A (en) * 2012-10-18 2014-05-07 西安交大京盛科技发展有限公司 Carbon fiber production process
CN104195766A (en) * 2014-09-05 2014-12-10 中复神鹰碳纤维有限责任公司 Drying method for carbon fiber having been subjected to sizing
CN104204342A (en) * 2012-03-09 2014-12-10 帝人株式会社 Carbon fiber bundle and process for producing same
CN105624874A (en) * 2016-03-23 2016-06-01 江苏澳盛复合材料科技有限公司 Carbon fiber widening equipment and process
CN105734721A (en) * 2014-12-09 2016-07-06 重庆市鸿腾无纺机械有限公司 Carbon fiber making technology

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104204342A (en) * 2012-03-09 2014-12-10 帝人株式会社 Carbon fiber bundle and process for producing same
CN103774284A (en) * 2012-10-18 2014-05-07 西安交大京盛科技发展有限公司 Carbon fiber production process
CN103290527A (en) * 2013-05-22 2013-09-11 西安康本材料有限公司 Method for lowering ash content of polyacrylonitrile-based carbon fiber
CN104195766A (en) * 2014-09-05 2014-12-10 中复神鹰碳纤维有限责任公司 Drying method for carbon fiber having been subjected to sizing
CN105734721A (en) * 2014-12-09 2016-07-06 重庆市鸿腾无纺机械有限公司 Carbon fiber making technology
CN105624874A (en) * 2016-03-23 2016-06-01 江苏澳盛复合材料科技有限公司 Carbon fiber widening equipment and process

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112877950A (en) * 2021-01-12 2021-06-01 中国科学院苏州纳米技术与纳米仿生研究所南昌研究院 Preparation system and method of filament carbon fiber 3D printing wire
CN113529242A (en) * 2021-07-29 2021-10-22 吉祥三宝高科纺织有限公司 Method for preparing anti-cutting gloves by using carbon fiber composite material

Also Published As

Publication number Publication date
CN108004621B (en) 2022-01-21

Similar Documents

Publication Publication Date Title
CN103290527A (en) Method for lowering ash content of polyacrylonitrile-based carbon fiber
CN102733009A (en) High strength polyacrylonitrile-base carbon fibers having structured surface grooves, and preparation method thereof
CN109322006B (en) Colored high-strength polyethylene fiber and preparation method thereof
CN108004621A (en) A kind of polyamide resin resin-based composite carbon fiber and preparation method thereof
CN102212965B (en) Sizing agent of liquid polyacrylonitrile oligomer and application thereof to carbon fibre
CN110499559A (en) A kind of preparation method of high-strength complex yarns and fabric
CN103952797A (en) Preparation method of wet-process high-strength polyacrylonitrile-based carbon fiber
CN109252251A (en) Major diameter wet-dry change polyacrylonitrile-based carbon fibre and preparation method thereof
CN109082730A (en) Major diameter polyacrylonitrile-based carbon fibre and preparation method thereof
CN109722743B (en) Carbon fiber for polyolefin resin matrix composite material and preparation method thereof
CN104231159B (en) A kind of preparation method of carbon fiber PAN polymer
JP2007039866A (en) Oil agent for carbon fiber precursor and carbon fiber precursor
CN109722745A (en) A kind of polyetherimide resin based composites carbon fiber and preparation method thereof
CN101984154B (en) Method for preparing water-repellent polyester fibers
CN108004620A (en) A kind of polyester resin based composites carbon fiber and preparation method thereof
CN108004781B (en) Polyamide resin-based suspension sizing agent for carbon fibers and preparation method thereof
CN103184592B (en) Ternary ammoniation modified T400 level 12K carbon fiber production method
Can et al. A Novel Carbon Nanofiber Precursor: Poly (acrylonitrile-co-vinylacetate-co-itaconic acid) Terpolymer
CN109722903B (en) Carbon fiber for polysulfone resin-based composite material and preparation method thereof
CN111621863A (en) Processing technology of functional nano regenerated fiber
CN110373729A (en) As-spun fibre, polyacrylonitrile fibre, polyacrylonitrile-based carbon fibre and preparation method
CN107338652A (en) Wastewater recycling process in treasured island matte micro fiber leather dyeing and its preparation process
CN107164969A (en) Aqueous treasured island matte micro fiber leather and its preparation technology
CN206352177U (en) A kind of high-strength high-accuracy utter misery conductive monofilament of polyamide fibre 66
CN109722742B (en) Carbon fiber for polyphenylene sulfide resin-based composite material and preparation method thereof

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant