WO2017215573A1 - Self-reinforced profiled material, preparation method therefor and use thereof - Google Patents

Self-reinforced profiled material, preparation method therefor and use thereof Download PDF

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Publication number
WO2017215573A1
WO2017215573A1 PCT/CN2017/087966 CN2017087966W WO2017215573A1 WO 2017215573 A1 WO2017215573 A1 WO 2017215573A1 CN 2017087966 W CN2017087966 W CN 2017087966W WO 2017215573 A1 WO2017215573 A1 WO 2017215573A1
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WIPO (PCT)
Prior art keywords
styrene
reinforced
self
profile
copolymer
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PCT/CN2017/087966
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French (fr)
Chinese (zh)
Inventor
魏金刚
陈平绪
叶南飚
肖鹏
李玉虎
官焕祥
何超雄
刘建中
刘波
Original Assignee
金发科技股份有限公司
广东金发科技有限公司
天津金发新材料有限公司
四川金发科技发展有限公司
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Publication of WO2017215573A1 publication Critical patent/WO2017215573A1/en

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    • CCHEMISTRY; METALLURGY
    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08LCOMPOSITIONS OF MACROMOLECULAR COMPOUNDS
    • C08L25/00Compositions of, homopolymers or copolymers of compounds having one or more unsaturated aliphatic radicals, each having only one carbon-to-carbon double bond, and at least one being terminated by an aromatic carbocyclic ring; Compositions of derivatives of such polymers
    • C08L25/02Homopolymers or copolymers of hydrocarbons
    • C08L25/04Homopolymers or copolymers of styrene
    • C08L25/08Copolymers of styrene
    • C08L25/12Copolymers of styrene with unsaturated nitriles
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C48/00Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor
    • B29C48/25Component parts, details or accessories; Auxiliary operations
    • B29C48/92Measuring, controlling or regulating
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B27/00Layered products comprising a layer of synthetic resin
    • B32B27/06Layered products comprising a layer of synthetic resin as the main or only constituent of a layer, which is next to another layer of the same or of a different material
    • B32B27/08Layered products comprising a layer of synthetic resin as the main or only constituent of a layer, which is next to another layer of the same or of a different material of synthetic resin
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B27/00Layered products comprising a layer of synthetic resin
    • B32B27/18Layered products comprising a layer of synthetic resin characterised by the use of special additives
    • B32B27/20Layered products comprising a layer of synthetic resin characterised by the use of special additives using fillers, pigments, thixotroping agents
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B27/00Layered products comprising a layer of synthetic resin
    • B32B27/30Layered products comprising a layer of synthetic resin comprising vinyl (co)polymers; comprising acrylic (co)polymers
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B27/00Layered products comprising a layer of synthetic resin
    • B32B27/30Layered products comprising a layer of synthetic resin comprising vinyl (co)polymers; comprising acrylic (co)polymers
    • B32B27/302Layered products comprising a layer of synthetic resin comprising vinyl (co)polymers; comprising acrylic (co)polymers comprising aromatic vinyl (co)polymers, e.g. styrenic (co)polymers
    • 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
    • C08K13/00Use of mixtures of ingredients not covered by one single of the preceding main groups, each of these compounds being essential
    • C08K13/04Ingredients characterised by their shape and organic or inorganic ingredients
    • 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
    • C08K5/00Use of organic ingredients
    • C08K5/04Oxygen-containing compounds
    • C08K5/13Phenols; Phenolates
    • C08K5/134Phenols containing ester groups
    • 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
    • C08K5/00Use of organic ingredients
    • C08K5/16Nitrogen-containing compounds
    • C08K5/20Carboxylic acid amides
    • 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
    • C08K5/00Use of organic ingredients
    • C08K5/49Phosphorus-containing compounds
    • C08K5/51Phosphorus bound to oxygen
    • C08K5/52Phosphorus bound to oxygen only
    • C08K5/524Esters of phosphorous acids, e.g. of H3PO3
    • C08K5/526Esters of phosphorous acids, e.g. of H3PO3 with hydroxyaryl compounds
    • 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
    • C08K7/14Glass
    • CCHEMISTRY; METALLURGY
    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08LCOMPOSITIONS OF MACROMOLECULAR COMPOUNDS
    • C08L35/00Compositions of homopolymers or copolymers of compounds having one or more unsaturated aliphatic radicals, each having only one carbon-to-carbon double bond, and at least one being terminated by a carboxyl radical, and containing at least one other carboxyl radical in the molecule, or of salts, anhydrides, esters, amides, imides or nitriles thereof; Compositions of derivatives of such polymers
    • C08L35/06Copolymers with vinyl aromatic monomers
    • CCHEMISTRY; METALLURGY
    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08LCOMPOSITIONS OF MACROMOLECULAR COMPOUNDS
    • C08L51/00Compositions of graft polymers in which the grafted component is obtained by reactions only involving carbon-to-carbon unsaturated bonds; Compositions of derivatives of such polymers
    • CCHEMISTRY; METALLURGY
    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08LCOMPOSITIONS OF MACROMOLECULAR COMPOUNDS
    • C08L51/00Compositions of graft polymers in which the grafted component is obtained by reactions only involving carbon-to-carbon unsaturated bonds; Compositions of derivatives of such polymers
    • C08L51/003Compositions of graft polymers in which the grafted component is obtained by reactions only involving carbon-to-carbon unsaturated bonds; Compositions of derivatives of such polymers grafted on to macromolecular compounds obtained by reactions only involving unsaturated carbon-to-carbon bonds
    • CCHEMISTRY; METALLURGY
    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08LCOMPOSITIONS OF MACROMOLECULAR COMPOUNDS
    • C08L55/00Compositions of homopolymers or copolymers, obtained by polymerisation reactions only involving carbon-to-carbon unsaturated bonds, not provided for in groups C08L23/00 - C08L53/00
    • C08L55/02ABS [Acrylonitrile-Butadiene-Styrene] polymers
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C2948/00Indexing scheme relating to extrusion moulding
    • B29C2948/92Measuring, controlling or regulating
    • B29C2948/92504Controlled parameter
    • B29C2948/9258Velocity
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C2948/00Indexing scheme relating to extrusion moulding
    • B29C2948/92Measuring, controlling or regulating
    • B29C2948/92504Controlled parameter
    • B29C2948/92704Temperature
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2250/00Layers arrangement
    • B32B2250/022 layers
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2262/00Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
    • B32B2262/10Inorganic fibres
    • B32B2262/101Glass fibres
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2307/00Properties of the layers or laminate
    • B32B2307/30Properties of the layers or laminate having particular thermal properties
    • B32B2307/302Conductive
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2307/00Properties of the layers or laminate
    • B32B2307/30Properties of the layers or laminate having particular thermal properties
    • B32B2307/304Insulating
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2355/00Specific polymers obtained by polymerisation reactions only involving carbon-to-carbon unsaturated bonds, not provided for in a single one of index codes B32B2323/00 - B32B2333/00
    • B32B2355/02ABS polymers, i.e. acrylonitrile-butadiene-styrene polymers
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2398/00Unspecified macromolecular compounds
    • B32B2398/20Thermoplastics
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2479/00Furniture

Definitions

  • the invention relates to the technical field of plastic profiles, in particular to a self-reinforced profile material and a preparation method and application thereof.
  • the main board of the wardrobe, cabinet, and desk uses melamine board, MDF or particle board.
  • the main board needs to be sawed according to different sizes during the manufacturing process, so the sawed part is bare.
  • the core of the board seriously affects the appearance of the product, so it is necessary to wrap the bare core part of the edging material.
  • the quality of the edging is also an important criterion for measuring the quality of the wardrobe.
  • the edging material also plays an important role in the deformation of the cabinet, so the edging material of the wardrobe also requires a certain strength, rigidity and the like.
  • aluminum alloy edging strips in the wardrobe, cabinets, desks and so on.
  • aluminum alloy has the advantages of light material, high strength, good sealing performance, good corrosion resistance and small deformation during installation.
  • the aluminum alloy edging material also has the following shortcomings: the production of aluminum alloy edging material High energy consumption, poor thermal insulation, poor sound insulation, high material density, single color, and complicated process during installation.
  • Another object of the present invention is to provide a process for the preparation of the above self-reinforced profile.
  • a self-reinforcing profile comprising a core layer and a skin layer disposed outside the core layer, the skin layer being a thermoplastic resin profile, the core layer being a reinforced styrene-based composition material, the parts by weight of which are as follows:
  • the reinforcing styrene-based composition material is in parts by weight, and comprises the following components:
  • the self-reinforced profiled material is tested according to the GB/T 10297 standard, and the test equipment is a Xiangtan Xiangke DRX-II thermal conductivity tester with a thermal conductivity of 0.20-0.30 W/mK.
  • the self-reinforcing profile is tested according to the ISO 2813 standard.
  • the test equipment is WG60G of Weifu Optoelectronics, and the gloss of the angle tested by 60° is greater than 90°.
  • the thermoplastic resin profile is a polyvinyl chloride PVC profile, an acrylonitrile-styrene-acrylate copolymer ASA profile, an acrylonitrile-ethylene propylene diene monomer-styrene copolymer AES profile, acrylonitrile-butadiene-styrene Copolymer ABS profile, styrene-acrylonitrile copolymer AS profile or acrylonitrile-silicone rubber-styrene copolymer SAS.
  • the styrene-based copolymer resin has a melt flow rate of from 1 g/10 min to 80 g/10 min at 220 ° C under a load of 10 kg, which is more easily extruded, preferably from 5 g/10 min to 20 g/10 min, more preferably 10 g/ 10min-15g/10min.
  • the styrene-based copolymer is selected from the group consisting of styrene-acrylonitrile copolymer AS, styrene-butadiene-acrylonitrile copolymer ABS, methyl methacrylate-styrene-butadiene-acrylonitrile copolymer MABS, Acrylonitrile-styrene-acrylate copolymer ASA, acrylonitrile-ethylene propylene diene monomer-styrene copolymer AES, acrylonitrile-silicone rubber-styrene copolymer SAS, methyl methacrylate-styrene copolymer One or several of the MS.
  • the reinforcing agent is selected from one or more of glass fiber, carbon fiber, basalt fiber, talc powder, wollastonite, whisker, glass microbead, preferably glass fiber, and the glass fiber has a diameter of 6-20 ⁇ m.
  • the styrene-based composition material of the present invention further comprises, by weight, 0.5-10 parts of a compatibilizing agent, 0.1-5.0 parts of a coupling agent, and 0.1-5.0 parts of a processing aid.
  • the compatibilizer is selected from the group consisting of styrene-butadiene-acrylonitrile-maleic anhydride copolymer, styrene-butadiene-acrylonitrile-glycidyl methacrylate copolymer, styrene-acrylonitrile-Malay One or more of an acid anhydride copolymer, a styrene-acrylonitrile-glycidyl methacrylate copolymer, an acrylate resin, a methyl methacrylate-styrene copolymer resin, a styrene-maleic anhydride copolymer ;
  • the coupling agent is selected from one or more of a silane coupling agent, a titanate coupling agent, an aluminate coupling agent, and a zirconate coupling agent; the processing aid includes a lubricant or an anti- One or several of the oxygen agents.
  • the lubricant is selected from the group consisting of a fatty acid salt, a fatty acid amide, pentaerythritol stearate, a solid paraffin, a liquid paraffin, a stearate, a silicone, an N, N'-ethylene bis stearic acid amide or Several.
  • the antioxidant is tetrakis[ ⁇ -(3,5-di-tert-butyl-4-hydroxyphenyl)propionic acid] quaternary tetraol and tris[2,4-di-tert-butylphenyl]phosphite a mixture of esters.
  • the method for preparing a self-reinforced profile according to the present invention comprises the following steps:
  • (1) Preparation of reinforced styrene-based composition material in addition to the reinforcing agent, the raw materials of the reinforced styrene-based composition are added to a high-mixing machine to be uniformly mixed according to the ratio; and the above mixture is fed into a twin-screw extruder. , wherein the reinforcing agent is added through the first venting hole or the side feeding system, melt extrusion granulation, that is, the reinforced styrene-based composition material is enhanced;
  • Co-extrusion preparation is carried out by using a host machine and an auxiliary machine vertically designed by the host, and the host is used for extruding reinforced benzene.
  • the alkenyl composition material is used for extruding a thermoplastic resin profile, and the main machine and the auxiliary machine are simultaneously extruded, and the shape is cooled and shaped to obtain a self-reinforced profile.
  • the mixing temperature is 20-50 ° C, the rotation speed is 100-800 rpm, and the mixing time is 2-5 minutes; the temperature of each section of the twin-screw extruder is 200-240 ° C, double The screw extruder has a length to diameter ratio of 36-48 and a screw speed of 300-500 rpm.
  • the main machine is a single-screw extruder, and the temperature of each section of the single-screw extruder is 160-215 ° C;
  • the auxiliary machine is a twin-screw extruder, and the temperature of each section of the twin-screw extruder is 150-200 ° C.
  • the main machine is a single-screw extruder
  • the head temperature is 175-195 ° C
  • the temperature of the fuselage one zone is 160-165 ° C
  • the temperature of the fuselage two zone is 160-175 ° C
  • the temperature of the fuselage three zones is 175-185 ° C
  • the temperature of the four zones of the fuselage is 175-185 ° C
  • the screw speed is 18-22 rpm.
  • the auxiliary machine is a twin-screw extruder, the head temperature is 175-195 ° C, the temperature of the fuselage one zone is 155-165 ° C, the temperature of the fuselage two zone is 165-175 ° C, and the temperature of the fuselage three zones is 175- 185 ° C, the temperature of the fuselage four zones is 175-185 ° C, the screw speed is 18-22 rpm;
  • the invention also provides the use of the above self-reinforced profile in a desk edging, a wardrobe edging or a cabinet edging.
  • the present invention has the following advantages:
  • the invention replaces the aluminum alloy edging material by using a thermoplastic resin profile and a self-reinforced profile prepared by co-extruding the styrene-based composition material, wherein the skin layer is a thermoplastic resin profile, which provides an excellent appearance effect, and the core layer is highly rigid and reinforced.
  • a styrene-based composition material that provides the strength, rigidity, and the like properties required for the edging material.
  • the self-reinforced profile of the invention has excellent thermal insulation performance, low density and excellent appearance, and the co-extrusion process is simple, and can be applied to the wardrobe edging, the desk edging, the cabinet edging material, and has better. Application prospects.
  • the raw materials used are as follows:
  • ABS profile ABS AG10NP, Taihua
  • AES profile AES HW500E, Kumho, South Korea;
  • ABS resin ABS AG10NP, Taiwan; melt flow rate 6g/10min;
  • ASA styrene-acrylonitrile-acrylate copolymer ASA PW-997, Taiwan Chi Mei; melt flow rate 5g/10min;
  • Glass fiber ECS13-4.5-534A, Tongxiang boulders, diameter 6 ⁇ 20 ⁇ m.
  • the raw materials of the reinforced styrene-based composition are uniformly mixed in a high-mixing machine according to the ratio of Table 1; the above mixed material is fed into a twin-screw extruder, wherein the reinforcing agent passes through the first venting opening Or the side feed system is added, melt extrusion granulation, that is, the styrene-based composition material is reinforced.
  • the mixing temperature is 20-50 ° C
  • the rotation speed is 100-800 rpm
  • the mixing time is 2-5 minutes
  • the temperature of each section of the twin-screw extruder is 200-240 ° C
  • the twin-screw extruder The aspect ratio is 36-48 and the screw speed is 300-500 rpm.
  • the obtained reinforced styrene-based composition material was dried in a blast oven at 90 ° C for 4 hours, and then sampled by a Ningbo Haitian injection molding machine BS650-III, and the injection temperature was set to 230-240-240-250 ° C.
  • the properties of the physical properties of the styrene-based composition materials are shown in Table 1.
  • the tensile strength was tested according to the ISO 527 standard.
  • the sample was a type I specimen and the test equipment was a tensile tester Z020 from Zwick, Germany.
  • the flexural modulus was tested according to the ISO 178 standard.
  • the sample size was 4 mm ⁇ 10 mm ⁇ 80 mm.
  • the test equipment was a bending tester Z005 from Zwick Roell, Germany.
  • the IZOD notched impact strength was tested in accordance with the ISO 180 standard, and the sample size was 4 mm ⁇ 10 mm ⁇ 80 mm, and the notch depth was 2 mm.
  • the test equipment is the impact tester HIT5.5P from Zwick Roell, Germany.
  • the density was tested according to the ISO 1183 standard, and the test equipment was a digital liquid density meter MD-300S of Japan ALFA MIRAGE.
  • the gloss was tested according to the ISO 2813 standard.
  • the test equipment was WG60G from Weifu Optoelectronics and the angle was tested at 60°.
  • the thermal conductivity is tested according to GB/T 10297 standard.
  • the test equipment is Xiangtan Xiangke DRX-II thermal conductivity tester.
  • the reinforced styrene-based composition material of the present invention has excellent mechanical properties such as strength and rigidity as the core layer, and has a low density of only about half of the aluminum alloy material.
  • the main machine and the auxiliary machine vertically designed by the main machine are used for co-extrusion preparation.
  • the main machine is used for extruding and reinforced styrene-based composition materials
  • the auxiliary machine is used for extruding thermoplastic resin profiles, and the main machine and auxiliary machine are simultaneously extruded.
  • Out after forming, cooling and setting to obtain self-reinforced profile;
  • the main machine is a single-screw extruder
  • the head temperature is 175-195 ° C
  • the temperature of the fuselage one zone is 160-165 ° C
  • the temperature of the fuselage two zone is 160-175 ° C
  • the temperature of the fuselage three zones is 175.
  • the temperature of the fuselage four zones is 175-185 ° C, the screw speed is 18-22 rpm; the auxiliary machine is a twin-screw extruder, the head temperature is 175-195 ° C, the temperature of the fuselage zone is 155 -165 ° C, the fuselage two zone temperature is 165-175 ° C, the fuselage three zone temperature is 175-185 ° C, the fuselage four zone temperature is 175-185 ° C, the screw speed is 18-22rpm.
  • the present invention utilizes a thermoplastic resin profile as a skin layer, and its glossiness is above 90°, which is significantly improved compared with the glossiness of the aluminum alloy (about 70°), and can provide an excellent appearance effect and high rigidity to enhance benzene.
  • the vinyl composition material serves as a core layer, which can provide the strength, rigidity and the like properties required for the edging material, and the self-reinforced profile obtained by co-extrusion has a thermal conductivity of 0.20-0.30 W/mK, which is significantly low.
  • the thermal conductivity of the aluminum alloy (about 200 W/mK) therefore, the self-reinforced profile of the present invention has a lower thermal conductivity and is more advantageous in terms of thermal insulation and appearance.
  • the profile prepared by the invention can replace the aluminum alloy edging material, and has good application prospects in the desk, the cabinet and the wardrobe edging.

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  • Chemical & Material Sciences (AREA)
  • Health & Medical Sciences (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Medicinal Chemistry (AREA)
  • Polymers & Plastics (AREA)
  • Organic Chemistry (AREA)
  • Extrusion Moulding Of Plastics Or The Like (AREA)
  • Compositions Of Macromolecular Compounds (AREA)
  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)

Abstract

Provided are a self-reinforced profiled material, a preparation method therefor and the use thereof. The self-reinforced profiled material comprises a core layer and a skin layer arranged outside the core layer, wherein the skin layer is made of a thermoplastic resin profile, and the core layer is made of a reinforced styryl composition material, with the parts by weight thereof being: 100 parts of a reinforced styryl composition material, and 5-100 parts of the thermoplastic resin profile; and the reinforced styryl composition material comprises the following components: 25-65 parts of a styryl copolymer, and 30-65 parts of a reinforcing agent. The preparation method therefor involves firstly preparing the reinforced styryl composition material; then performing co-extrusion using a main machine and an auxiliary machine perpendicular to the main machine, wherein the main machine is used for extruding the reinforced styryl composition material, the auxiliary machine is used for extruding the thermoplastic resin profile, and the main machine and the auxiliary machine simultaneously perform extrusion; and cooling and shaping after moulding to obtain the self-reinforced profiled material. The self-reinforced profiled material has excellent thermal insulation properties, a lower density, an excellent appearance, and a simple co-extrusion process, can be used as a material for wardrobe edging, office table edging and kitchen cabinet edging, and has a better application prospect.

Description

一种自增强异型材及其制备方法和应用Self-reinforced profiled material and preparation method and application thereof
技术领域Technical field
本发明涉及塑料型材技术领域,具体涉及一种自增强异型材及其制备方法和应用。The invention relates to the technical field of plastic profiles, in particular to a self-reinforced profile material and a preparation method and application thereof.
背景技术Background technique
衣柜,橱柜,办公桌的主体板材使用三聚氰胺板,密度板或刨花板,但由于不同型号产品的尺寸不一样,在制作过程中都需要按照不同尺寸把主体板材锯开,那么锯开的部分就是裸露的板芯,严重影响产品的外观,所以就需要包边材料把裸露的板芯部分包住,包边的好坏也是衡量衣柜质量的一个重要标准。另外,包边材料还对柜体的变形起着重要的作用,所以衣柜的包边材料还需要一定的强度,刚性等要求。The main board of the wardrobe, cabinet, and desk uses melamine board, MDF or particle board. However, due to the different sizes of different models, the main board needs to be sawed according to different sizes during the manufacturing process, so the sawed part is bare. The core of the board seriously affects the appearance of the product, so it is necessary to wrap the bare core part of the edging material. The quality of the edging is also an important criterion for measuring the quality of the wardrobe. In addition, the edging material also plays an important role in the deformation of the cabinet, so the edging material of the wardrobe also requires a certain strength, rigidity and the like.
目前,主要是采用铝合金包边条应用在衣柜,橱柜,办公桌等方面。与钢材相比,铝合金具有材料轻,强度高,密闭性能好,耐腐蚀效果好,安装时变形小等优点,但是铝合金包边材料也存在以下不足之处:铝合金包边材料的生产能耗高,保温隔热、隔音效果差,材料密度大,颜色单一,而且在安装时,工艺复杂。At present, the main use of aluminum alloy edging strips in the wardrobe, cabinets, desks and so on. Compared with steel, aluminum alloy has the advantages of light material, high strength, good sealing performance, good corrosion resistance and small deformation during installation. However, the aluminum alloy edging material also has the following shortcomings: the production of aluminum alloy edging material High energy consumption, poor thermal insulation, poor sound insulation, high material density, single color, and complicated process during installation.
发明内容Summary of the invention
为了克服上述现有技术的不足,本发明的目的在于提供一种自增强异型材,该自增强异型材具有优异的保温隔热性能,较低的密度和优异的外观等优点,可作为包边材料代替铝合金应用于衣柜、橱柜、办公桌包边等。In order to overcome the above deficiencies of the prior art, it is an object of the present invention to provide a self-reinforcing profile which has excellent thermal insulation properties, low density and excellent appearance, and can be used as a edging. The material replaces the aluminum alloy for use in wardrobes, cabinets, desk edging, and the like.
本发明的另一个目的是在于提供上述自增强异型材的制备方法。Another object of the present invention is to provide a process for the preparation of the above self-reinforced profile.
本发明通过下述技术方案来实现:The invention is achieved by the following technical solutions:
一种自增强异型材,包括芯层以及设置在芯层外的皮层,所述皮层为热塑性树脂型材,所述芯层为增强苯乙烯基组合物材料,其重量份数如下:A self-reinforcing profile comprising a core layer and a skin layer disposed outside the core layer, the skin layer being a thermoplastic resin profile, the core layer being a reinforced styrene-based composition material, the parts by weight of which are as follows:
增强苯乙烯基组合物材料  100份Reinforced styrene based composition material 100 parts
热塑性树脂型材  5-100份;Thermoplastic resin profile 5-100 parts;
其中,所述增强苯乙烯基组合物材料按重量份数计,包括如下组分:Wherein the reinforcing styrene-based composition material is in parts by weight, and comprises the following components:
苯乙烯基共聚物  25-65份;Styrene-based copolymer 25-65 parts;
增强剂  30-65份。Enhancer 30-65 parts.
所述自增强异型材的按GB/T 10297标准进行测试,测试设备为湘潭湘科DRX-Ⅱ导热系数测试仪,热导率为0.20-0.30W/mK。 The self-reinforced profiled material is tested according to the GB/T 10297 standard, and the test equipment is a Xiangtan Xiangke DRX-II thermal conductivity tester with a thermal conductivity of 0.20-0.30 W/mK.
所述自增强异型材按ISO 2813标准进行测试,测试设备为威福光电的WG60G,角度按60°进行测试的光泽度大于90°The self-reinforcing profile is tested according to the ISO 2813 standard. The test equipment is WG60G of Weifu Optoelectronics, and the gloss of the angle tested by 60° is greater than 90°.
所述热塑性树脂型材为聚氯乙烯PVC型材、丙烯腈-苯乙烯-丙烯酸酯共聚物ASA型材、丙烯腈-三元乙丙橡胶-苯乙烯共聚物AES型材、丙烯腈-丁二烯-苯乙烯共聚物ABS型材、苯乙烯-丙烯腈共聚物AS型材或丙烯腈-硅丙橡胶-苯乙烯共聚物SAS。The thermoplastic resin profile is a polyvinyl chloride PVC profile, an acrylonitrile-styrene-acrylate copolymer ASA profile, an acrylonitrile-ethylene propylene diene monomer-styrene copolymer AES profile, acrylonitrile-butadiene-styrene Copolymer ABS profile, styrene-acrylonitrile copolymer AS profile or acrylonitrile-silicone rubber-styrene copolymer SAS.
所述苯乙烯基共聚物树脂在220℃,10kg载荷条件下的熔体流动速率为1g/10min-80g/10min,为更易挤出成型,优选5g/10min-20g/10min,更优选为10g/10min-15g/10min。The styrene-based copolymer resin has a melt flow rate of from 1 g/10 min to 80 g/10 min at 220 ° C under a load of 10 kg, which is more easily extruded, preferably from 5 g/10 min to 20 g/10 min, more preferably 10 g/ 10min-15g/10min.
所述苯乙烯基共聚物选自苯乙烯-丙烯腈共聚物AS、苯乙烯-丁二烯-丙烯腈共聚物ABS、甲基丙烯酸甲酯-苯乙烯-丁二烯-丙烯腈共聚物MABS、丙烯腈-苯乙烯-丙烯酸酯共聚物ASA、丙烯腈-三元乙丙橡胶-苯乙烯共聚物AES、丙烯腈-硅丙橡胶-苯乙烯共聚物SAS、甲基丙烯酸甲酯-苯乙烯共聚物MS中的一种或几种。The styrene-based copolymer is selected from the group consisting of styrene-acrylonitrile copolymer AS, styrene-butadiene-acrylonitrile copolymer ABS, methyl methacrylate-styrene-butadiene-acrylonitrile copolymer MABS, Acrylonitrile-styrene-acrylate copolymer ASA, acrylonitrile-ethylene propylene diene monomer-styrene copolymer AES, acrylonitrile-silicone rubber-styrene copolymer SAS, methyl methacrylate-styrene copolymer One or several of the MS.
所述增强剂选自玻璃纤维、碳纤维,玄武岩纤维、滑石粉、硅灰石、晶须、玻璃微珠中的一种或几种,优选玻璃纤维,所述玻璃纤维的直径为6-20μm。The reinforcing agent is selected from one or more of glass fiber, carbon fiber, basalt fiber, talc powder, wollastonite, whisker, glass microbead, preferably glass fiber, and the glass fiber has a diameter of 6-20 μm.
本发明所述增强苯乙烯基组合物材料,按重量份数计,还包括相容剂0.5-10份、偶联剂0.1-5.0份、加工助剂0.1-5.0份。The styrene-based composition material of the present invention further comprises, by weight, 0.5-10 parts of a compatibilizing agent, 0.1-5.0 parts of a coupling agent, and 0.1-5.0 parts of a processing aid.
所述相容剂选自苯乙烯-丁二烯-丙烯腈-马来酸酐共聚物、苯乙烯-丁二烯-丙烯腈-甲基丙烯酸缩水甘油酯共聚物、苯乙烯-丙烯腈-马来酸酐共聚物、苯乙烯-丙烯腈-甲基丙烯酸缩水甘油酯共聚物、丙烯酸酯树脂、甲基丙烯酸甲酯-苯乙烯共聚物树脂、苯乙烯-马来酸酐共聚物中的一种或几种;The compatibilizer is selected from the group consisting of styrene-butadiene-acrylonitrile-maleic anhydride copolymer, styrene-butadiene-acrylonitrile-glycidyl methacrylate copolymer, styrene-acrylonitrile-Malay One or more of an acid anhydride copolymer, a styrene-acrylonitrile-glycidyl methacrylate copolymer, an acrylate resin, a methyl methacrylate-styrene copolymer resin, a styrene-maleic anhydride copolymer ;
所述偶联剂选自硅烷偶联剂、钛酸酯偶联剂、铝酸酯偶联剂、锆酸酯偶联剂中的一种或几种;所述加工助剂包括润滑剂或抗氧剂中的一种或几种。The coupling agent is selected from one or more of a silane coupling agent, a titanate coupling agent, an aluminate coupling agent, and a zirconate coupling agent; the processing aid includes a lubricant or an anti- One or several of the oxygen agents.
所述润滑剂选自脂肪酸盐、脂肪酸酰胺、季戊四醇硬脂酸酯、固体石蜡、液体石蜡、硬脂酸盐、硅酮、N,N'-乙撑双硬脂酸酰胺中的一种或几种。The lubricant is selected from the group consisting of a fatty acid salt, a fatty acid amide, pentaerythritol stearate, a solid paraffin, a liquid paraffin, a stearate, a silicone, an N, N'-ethylene bis stearic acid amide or Several.
所述抗氧剂为四[β-(3,5-二叔丁基-4-羟基苯基)丙酸]季茂四醇脂和三[2,4-二叔丁基苯基]亚磷酸酯的混合物。The antioxidant is tetrakis[β-(3,5-di-tert-butyl-4-hydroxyphenyl)propionic acid] quaternary tetraol and tris[2,4-di-tert-butylphenyl]phosphite a mixture of esters.
本发明所述的自增强异型材的制备方法,包括以下步骤:The method for preparing a self-reinforced profile according to the present invention comprises the following steps:
(1)增强苯乙烯基组合物材料的制备:除增强剂外,按配比将增强苯乙烯基组合物的各原料加入高混机中混合均匀;将上述混合物料送入双螺杆挤出机中,其中增强剂通过第一排气孔或侧喂***加入,熔融挤出造粒,即得增强增强苯乙烯基组合物材料;(1) Preparation of reinforced styrene-based composition material: in addition to the reinforcing agent, the raw materials of the reinforced styrene-based composition are added to a high-mixing machine to be uniformly mixed according to the ratio; and the above mixture is fed into a twin-screw extruder. , wherein the reinforcing agent is added through the first venting hole or the side feeding system, melt extrusion granulation, that is, the reinforced styrene-based composition material is enhanced;
(2)共挤成型:采用主机与该主机垂直设计的辅机进行共挤制备,主机用于挤出增强苯乙 烯基组合物材料,辅机用于挤出热塑性树脂型材,主机、辅机同时挤出,成型后冷却定型得到自增强异型材。(2) Co-extrusion: co-extrusion preparation is carried out by using a host machine and an auxiliary machine vertically designed by the host, and the host is used for extruding reinforced benzene. The alkenyl composition material is used for extruding a thermoplastic resin profile, and the main machine and the auxiliary machine are simultaneously extruded, and the shape is cooled and shaped to obtain a self-reinforced profile.
步骤(1)中,所述混合温度为20-50℃,转速为100-800转/分钟,混合时间为2-5分钟;所述双螺杆挤出机各段温度为200-240℃,双螺杆挤出机的长径比为36-48,螺杆转速为300-500转/分钟。In the step (1), the mixing temperature is 20-50 ° C, the rotation speed is 100-800 rpm, and the mixing time is 2-5 minutes; the temperature of each section of the twin-screw extruder is 200-240 ° C, double The screw extruder has a length to diameter ratio of 36-48 and a screw speed of 300-500 rpm.
步骤(2)中,所述主机为单螺杆挤出机,单螺杆挤出机各段温度为160-215℃;所述辅机为双螺杆挤出机,双螺杆挤出机各段温度为150-200℃。In the step (2), the main machine is a single-screw extruder, and the temperature of each section of the single-screw extruder is 160-215 ° C; the auxiliary machine is a twin-screw extruder, and the temperature of each section of the twin-screw extruder is 150-200 ° C.
优选的,所述主机为单螺杆挤出机,机头温度为175-195℃,机身一区温度为160-165℃,机身二区温度为160-175℃,机身三区温度为175-185℃,机身四区温度为175-185℃,螺杆转速为18-22rpm。所述辅机为双螺杆挤出机,机头温度为175-195℃,机身一区温度为155-165℃,机身二区温度为165-175℃,机身三区温度为175-185℃,机身四区温度为175-185℃,螺杆转速为18-22rpm;Preferably, the main machine is a single-screw extruder, the head temperature is 175-195 ° C, the temperature of the fuselage one zone is 160-165 ° C, the temperature of the fuselage two zone is 160-175 ° C, and the temperature of the fuselage three zones is 175-185 ° C, the temperature of the four zones of the fuselage is 175-185 ° C, the screw speed is 18-22 rpm. The auxiliary machine is a twin-screw extruder, the head temperature is 175-195 ° C, the temperature of the fuselage one zone is 155-165 ° C, the temperature of the fuselage two zone is 165-175 ° C, and the temperature of the fuselage three zones is 175- 185 ° C, the temperature of the fuselage four zones is 175-185 ° C, the screw speed is 18-22 rpm;
本发明还提供了上述自增强异型材在办公桌包边、衣柜包边或橱柜包边中的应用。The invention also provides the use of the above self-reinforced profile in a desk edging, a wardrobe edging or a cabinet edging.
相对于现有技术,本发明具有如下优点:Compared with the prior art, the present invention has the following advantages:
本发明利用热塑性树脂型材和增强苯乙烯基组合物材料共挤制备的自增强异型材来代替铝合金包边材料,其中皮层为热塑性树脂型材,其提供优异的外观效果,芯层为高刚性增强苯乙烯基组合物材料,其提供包边材料所需要的强度,刚性等使用性能。本发明的自增强异型材具有优异的保温隔热性能,较低的密度和优异的外观,且共挤工艺简单,可应用于衣柜包边、办公桌包边、橱柜包边材料,具有较好的应用前景。The invention replaces the aluminum alloy edging material by using a thermoplastic resin profile and a self-reinforced profile prepared by co-extruding the styrene-based composition material, wherein the skin layer is a thermoplastic resin profile, which provides an excellent appearance effect, and the core layer is highly rigid and reinforced. A styrene-based composition material that provides the strength, rigidity, and the like properties required for the edging material. The self-reinforced profile of the invention has excellent thermal insulation performance, low density and excellent appearance, and the co-extrusion process is simple, and can be applied to the wardrobe edging, the desk edging, the cabinet edging material, and has better. Application prospects.
具体实施方式detailed description
为更好地理解本发明,下面通过实施例对本发明作进一步的说明,需要说明的是实施例并不构成对本发明保护范围的限制。The invention is further described by the following examples in order to provide a better understanding of the invention.
所用原材料如下:The raw materials used are as follows:
PVC型材,PVC-EX23,金发科技自制;PVC profiles, PVC-EX23, blonde technology homemade;
ASA型材,ASA PW-997,台湾奇美;ASA profile, ASA PW-997, Taiwan Chi Mei;
AS型材,SAN PN-137H,台湾奇美;AS profile, SAN PN-137H, Taiwan Chi Mei;
ABS型材,ABS AG10NP,台化;ABS profile, ABS AG10NP, Taihua;
AES型材,AES HW500E,韩国锦湖;AES profile, AES HW500E, Kumho, South Korea;
SAS型材,DIALAC E259B,日本UMG;SAS profile, DIALAC E259B, UMG Japan;
AS苯乙烯-丙烯腈树脂,SAN PN-137H,台湾奇美,熔体流动速率12g/10min; AS styrene-acrylonitrile resin, SAN PN-137H, Taiwan Chi Mei, melt flow rate 12g/10min;
AS苯乙烯-丙烯腈树脂,SAN NF-5台化定制;熔体流动速率5g/10min;AS styrene-acrylonitrile resin, SAN NF-5 Taihua custom; melt flow rate 5g/10min;
AS苯乙烯-丙烯腈树脂,SAN NF2200,台化,熔体流动速率35g/10min;AS styrene-acrylonitrile resin, SAN NF2200, Taiwan, melt flow rate 35g/10min;
ABS树脂,ABS AG10NP,台化;熔体流动速率6g/10min;ABS resin, ABS AG10NP, Taiwan; melt flow rate 6g/10min;
ASA苯乙烯-丙烯腈-丙烯酸酯共聚物,ASA PW-997,台湾奇美;熔体流动速率5g/10min;ASA styrene-acrylonitrile-acrylate copolymer, ASA PW-997, Taiwan Chi Mei; melt flow rate 5g/10min;
玻璃纤维,ECS13-4.5-534A,桐乡巨石,直径为6~20μm。Glass fiber, ECS13-4.5-534A, Tongxiang boulders, diameter 6~20μm.
马来酸酐苯乙烯共聚物,SMA-700,上海华雯公司;Maleic anhydride styrene copolymer, SMA-700, Shanghai Huawen Company;
偶联剂,KH560,沸点化工;Coupling agent, KH560, boiling point chemical industry;
润滑剂,N,N'-亚乙基双硬脂酰胺,上海宁成;Lubricant, N, N'-ethylene bis stearamide, Shanghai Ningcheng;
抗氧剂,168和1010,瑞士汽巴精化公司。Antioxidants, 168 and 1010, Swiss Ciba Specialty Chemicals.
增强苯乙烯基组合物材料的制备:Preparation of reinforced styrene-based composition materials:
除增强剂外,按表1配比将增强苯乙烯基组合物的各原料加入高混机中混合均匀;将上述混合物料送入双螺杆挤出机中,其中增强剂通过第一排气孔或侧喂***加入,熔融挤出造粒,即得增强苯乙烯基组合物材料。其中,所述混合温度为20-50℃,转速为100-800转/分钟,混合时间为2-5分钟;所述双螺杆挤出机各段温度为200-240℃,双螺杆挤出机的长径比为36-48,螺杆转速为300-500转/分钟。In addition to the reinforcing agent, the raw materials of the reinforced styrene-based composition are uniformly mixed in a high-mixing machine according to the ratio of Table 1; the above mixed material is fed into a twin-screw extruder, wherein the reinforcing agent passes through the first venting opening Or the side feed system is added, melt extrusion granulation, that is, the styrene-based composition material is reinforced. Wherein, the mixing temperature is 20-50 ° C, the rotation speed is 100-800 rpm, the mixing time is 2-5 minutes; the temperature of each section of the twin-screw extruder is 200-240 ° C, the twin-screw extruder The aspect ratio is 36-48 and the screw speed is 300-500 rpm.
将得到的增强苯乙烯基组合物材料在90℃的鼓风烘箱中干燥4小时后,用宁波海天注射成型机BS650-Ⅲ制样,注塑温度设定为230-240-240-250℃,所得增强苯乙烯基组合物材料的物性测试结果性能见表1。The obtained reinforced styrene-based composition material was dried in a blast oven at 90 ° C for 4 hours, and then sampled by a Ningbo Haitian injection molding machine BS650-III, and the injection temperature was set to 230-240-240-250 ° C. The properties of the physical properties of the styrene-based composition materials are shown in Table 1.
拉伸强度按ISO 527标准进行测试,试样为Ⅰ型试样,测试设备为德国Zwick公司的拉伸试验机Z020。The tensile strength was tested according to the ISO 527 standard. The sample was a type I specimen and the test equipment was a tensile tester Z020 from Zwick, Germany.
弯曲模量按ISO 178标准进行测试,试样尺寸为4mm×10mm×80mm,测试设备为德国Zwick Roell公司的弯曲试验机Z005。The flexural modulus was tested according to the ISO 178 standard. The sample size was 4 mm × 10 mm × 80 mm. The test equipment was a bending tester Z005 from Zwick Roell, Germany.
IZOD缺口冲击强度按照ISO 180标准进行测试,试样尺寸为4mm×10mm×80mm,缺口深度为2mm。测试设备为德国Zwick Roell公司的冲击试验机HIT5.5P。The IZOD notched impact strength was tested in accordance with the ISO 180 standard, and the sample size was 4 mm × 10 mm × 80 mm, and the notch depth was 2 mm. The test equipment is the impact tester HIT5.5P from Zwick Roell, Germany.
密度按ISO 1183标准进行测试,测试设备为日本ALFA MIRAGE的数显液体密度计MD-300S。The density was tested according to the ISO 1183 standard, and the test equipment was a digital liquid density meter MD-300S of Japan ALFA MIRAGE.
光泽度按ISO 2813标准进行测试,测试设备为威福光电的WG60G,角度按60°进行测试。The gloss was tested according to the ISO 2813 standard. The test equipment was WG60G from Weifu Optoelectronics and the angle was tested at 60°.
热导率按GB/T 10297标准进行测试,测试设备为湘潭湘科DRX-Ⅱ导热系数测试仪。The thermal conductivity is tested according to GB/T 10297 standard. The test equipment is Xiangtan Xiangke DRX-II thermal conductivity tester.
表1增强苯乙烯基组合物各组分配比(重量份)及物性 Table 1 Reinforced styrene based composition group distribution ratio (parts by weight) and physical properties
[根据细则26改正03.07.2017] 
Figure WO-DOC-FIGURE-63
[Correct according to Rule 26 03.07.2017]
Figure WO-DOC-FIGURE-63
从表1可以看出,本发明的增强苯乙烯基组合物材料作为芯层,具有优异的强度、刚性等力学性能,且密度较低,只有铝合金材料的一半左右。As can be seen from Table 1, the reinforced styrene-based composition material of the present invention has excellent mechanical properties such as strength and rigidity as the core layer, and has a low density of only about half of the aluminum alloy material.
自增强异型材的制备:Preparation of self-reinforced profiles:
采用主机与该主机垂直设计的辅机进行共挤制备,按表2配比,主机用于挤出增强苯乙烯基组合物材料,辅机用于挤出热塑性树脂型材,主机、辅机同时挤出,成型后冷却定型得到自增强异型材;The main machine and the auxiliary machine vertically designed by the main machine are used for co-extrusion preparation. According to the ratio of Table 2, the main machine is used for extruding and reinforced styrene-based composition materials, and the auxiliary machine is used for extruding thermoplastic resin profiles, and the main machine and auxiliary machine are simultaneously extruded. Out, after forming, cooling and setting to obtain self-reinforced profile;
其中,所述主机为单螺杆挤出机,机头温度为175-195℃,机身一区温度为160-165℃,机身二区温度为160-175℃,机身三区温度为175-185℃,机身四区温度为175-185℃,螺杆转速为18-22rpm;所述辅机为为双螺杆挤出机,机头温度为175-195℃,机身一区温度为155-165℃,机身二区温度为165-175℃,机身三区温度为175-185℃,机身四区温度为175-185℃,螺杆转速为18-22rpm。Wherein, the main machine is a single-screw extruder, the head temperature is 175-195 ° C, the temperature of the fuselage one zone is 160-165 ° C, the temperature of the fuselage two zone is 160-175 ° C, and the temperature of the fuselage three zones is 175. -185 ° C, the temperature of the fuselage four zones is 175-185 ° C, the screw speed is 18-22 rpm; the auxiliary machine is a twin-screw extruder, the head temperature is 175-195 ° C, the temperature of the fuselage zone is 155 -165 ° C, the fuselage two zone temperature is 165-175 ° C, the fuselage three zone temperature is 175-185 ° C, the fuselage four zone temperature is 175-185 ° C, the screw speed is 18-22rpm.
表2自增强异型材的各组分配比及性能结果(重量份) Table 2 Distribution ratios and performance results of each group of self-reinforced profiles (parts by weight)
[根据细则26改正03.07.2017] 
Figure WO-DOC-FIGURE-69
[Correct according to Rule 26 03.07.2017]
Figure WO-DOC-FIGURE-69
由表2可以看出,本发明利用热塑性树脂型材作为皮层,其光泽度达到90°以上,较铝合金的光泽度(70°左右)有明显提高,可提供优异的外观效果,高刚性增强苯乙烯基组合物材料作为芯层,其可提供包边材料所需要的强度,刚性等使用性能,此外二者共挤制备得到的自增强异型材的导热率为0.20-0.30W/mK,显著低于铝合金的热导率(200W/mK左右),因此,本发明的自增强型材具有更低的热导率,在保温隔热,外观效果方面更加具有优势。本发明制备的异型材可代替铝合金包边材料,在办公桌、橱柜、衣柜包边等具有较好的应用前景。 It can be seen from Table 2 that the present invention utilizes a thermoplastic resin profile as a skin layer, and its glossiness is above 90°, which is significantly improved compared with the glossiness of the aluminum alloy (about 70°), and can provide an excellent appearance effect and high rigidity to enhance benzene. The vinyl composition material serves as a core layer, which can provide the strength, rigidity and the like properties required for the edging material, and the self-reinforced profile obtained by co-extrusion has a thermal conductivity of 0.20-0.30 W/mK, which is significantly low. The thermal conductivity of the aluminum alloy (about 200 W/mK), therefore, the self-reinforced profile of the present invention has a lower thermal conductivity and is more advantageous in terms of thermal insulation and appearance. The profile prepared by the invention can replace the aluminum alloy edging material, and has good application prospects in the desk, the cabinet and the wardrobe edging.

Claims (14)

  1. 一种自增强异型材,其特征在于,包括芯层以及设置在芯层外的皮层,所述皮层为热塑性树脂型材,所述芯层为增强苯乙烯基组合物材料,其重量份数如下:A self-reinforcing profile characterized by comprising a core layer and a skin layer disposed outside the core layer, the skin layer being a thermoplastic resin profile, the core layer being a reinforced styrene-based composition material, the parts by weight of which are as follows:
    增强苯乙烯基组合物材料  100份Reinforced styrene based composition material 100 parts
    热塑性树脂型材          5-100份;Thermoplastic resin profile 5-100 parts;
    其中,所述增强苯乙烯基组合物材料按重量份数计,包括如下组分:Wherein the reinforcing styrene-based composition material is in parts by weight, and comprises the following components:
    苯乙烯基共聚物  25-65份;Styrene-based copolymer 25-65 parts;
    增强剂          30-65份。Enhancer 30-65 parts.
  2. 根据权利要求1所述的自增强异型材,其特征在于,所述自增强异型材按GB/T 10297标准进行测试,测试设备为湘潭湘科DRX-Ⅱ导热系数测试仪,热导率为0.20-0.30W/mK。The self-reinforcing profile according to claim 1, wherein the self-reinforced profile material is tested according to the GB/T 10297 standard, and the test device is a Xiangtan Xiangke DRX-II thermal conductivity tester, and the thermal conductivity is 0.20. -0.30W/mK.
  3. 根据权利要求1所述的自增强异型材,其特征在于,所述自增强异型材按ISO 2813标准进行测试,测试设备为威福光电的WG60G,角度按60°进行测试的光泽度大于90°。The self-reinforced profile according to claim 1, wherein the self-reinforced profile is tested according to the ISO 2813 standard, and the test device is WG60G of Weifu Optoelectronics, and the gloss of the angle tested by 60° is greater than 90°. .
  4. 根据权利要求1所述的自增强异型材,其特征在于,所述热塑性树脂型材为聚氯乙烯PVC型材、丙烯腈-苯乙烯-丙烯酸酯共聚物ASA型材、丙烯腈-三元乙丙橡胶-苯乙烯共聚物AES型材、丙烯腈-丁二烯-苯乙烯共聚物ABS型材、苯乙烯-丙烯腈共聚物AS型材或丙烯腈-硅丙橡胶-苯乙烯共聚物SAS型材。The self-reinforcing profile according to claim 1, wherein the thermoplastic resin profile is a polyvinyl chloride PVC profile, an acrylonitrile-styrene-acrylate copolymer ASA profile, acrylonitrile-ethylene propylene diene monomer- Styrene copolymer AES profile, acrylonitrile-butadiene-styrene copolymer ABS profile, styrene-acrylonitrile copolymer AS profile or acrylonitrile-silicone rubber-styrene copolymer SAS profile.
  5. 根据权利要求1所述的自增强异型材,其特征在于,所述苯乙烯基共聚物在220℃,10kg载荷条件下的熔体流动速率为1g/10min-80g/10min,优选为5g/10min-20g/10min,更优选为10g/10min-15g/10min。The self-reinforcing profile according to claim 1, wherein the styrene-based copolymer has a melt flow rate of from 1 g/10 min to 80 g/10 min, preferably 5 g/10 min at 220 ° C under a load of 10 kg. -20 g/10 min, more preferably 10 g/10 min-15 g/10 min.
  6. 根据权利要求5所述的自增强异型材,其特征在于,所述苯乙烯基共聚物选自苯乙烯-丙烯腈共聚物AS、丙烯腈-丁二烯-苯乙烯共聚物ABS、甲基丙烯酸甲酯-丙烯腈-丁二烯-苯乙烯共聚物MABS、丙烯腈-苯乙烯-丙烯酸酯共聚物ASA、丙烯腈-三元乙丙橡胶-苯乙烯共聚物AES、丙烯腈-硅丙橡胶-苯乙烯共聚物SAS、甲基丙烯酸甲酯-苯乙烯共聚物MS中的一种或几种。The self-reinforced profile according to claim 5, wherein the styrene-based copolymer is selected from the group consisting of styrene-acrylonitrile copolymer AS, acrylonitrile-butadiene-styrene copolymer ABS, methacrylic acid. Methyl ester-acrylonitrile-butadiene-styrene copolymer MABS, acrylonitrile-styrene-acrylate copolymer ASA, acrylonitrile-ethylene propylene diene monomer-styrene copolymer AES, acrylonitrile-silicone rubber One or more of styrene copolymer SAS, methyl methacrylate-styrene copolymer MS.
  7. 根据权利要求1所述的自增强异型材,其特征在于,所述增强剂选自玻璃纤维、碳纤维、玄武岩纤维、滑石粉、硅灰石、晶须、玻璃微珠中的一种或几种,优选玻璃纤维。The self-reinforced profile according to claim 1, wherein the reinforcing agent is one or more selected from the group consisting of glass fiber, carbon fiber, basalt fiber, talc powder, wollastonite, whisker, and glass microbead. Preferred is glass fiber.
  8. 根据权利要求7所述的自增强异型材,其特征在于,所述玻璃纤维的直径为6-20μm。The self-reinforced profile according to claim 7, wherein the glass fibers have a diameter of 6 to 20 μm.
  9. 根据权利要求1所述的自增强异型材,其特征在于,按重量份数计,所述增强苯乙烯基组合物材料还包括相容剂0.5-10份、偶联剂0.1-5.0份、加工助剂0.1-5.0份。The self-reinforcing profile according to claim 1, wherein the reinforced styrene-based composition material further comprises 0.5-10 parts of a compatibilizing agent, 0.1-5.0 parts of a coupling agent, and processing, in parts by weight. Auxiliary 0.1-5.0 parts.
  10. 根据权利要求9所述的自增强异型材,其特征在于,所述相容剂选自苯乙烯-丁二烯-丙烯腈-马来酸酐共聚物、苯乙烯-丁二烯-丙烯腈-甲基丙烯酸缩水甘油酯共聚物、苯乙烯-丙烯 腈-马来酸酐共聚物、苯乙烯-丙烯腈-甲基丙烯酸缩水甘油酯共聚物、丙烯酸酯树脂、甲基丙烯酸甲酯-苯乙烯共聚物、苯乙烯-马来酸酐共聚物中的一种或几种;所述偶联剂选自硅烷偶联剂、钛酸酯偶联剂、铝酸酯偶联剂、锆酸酯偶联剂中的一种或几种;所述加工助剂包括润滑剂或抗氧剂中的一种或几种。The self-reinforced profile according to claim 9, wherein the compatibilizing agent is selected from the group consisting of styrene-butadiene-acrylonitrile-maleic anhydride copolymer, styrene-butadiene-acrylonitrile-A Glycidyl acrylate copolymer, styrene-propylene Nitrile-maleic anhydride copolymer, styrene-acrylonitrile-glycidyl methacrylate copolymer, acrylate resin, methyl methacrylate-styrene copolymer, styrene-maleic anhydride copolymer Or a plurality of; the coupling agent is selected from one or more of a silane coupling agent, a titanate coupling agent, an aluminate coupling agent, and a zirconate coupling agent; and the processing aid includes One or more of a lubricant or an antioxidant.
  11. 根据权利要求1-10任一项所述的自增强异型材的制备方法,其特征在于,包括以下步骤:The method for preparing a self-reinforced profile according to any one of claims 1 to 10, comprising the steps of:
    (1)增强苯乙烯基组合物材料的制备:除增强剂外,按配比将增强苯乙烯基组合物材料的各原料加入高混机中混合均匀;将上述混合物料送入双螺杆挤出机中,其中增强剂通过第一排气孔或侧喂***加入,熔融挤出造粒,即得增强苯乙烯基组合物材料;(1) Preparation of reinforced styrene-based composition material: in addition to the reinforcing agent, each raw material of the styrene-based composition material is added to a high-mixing machine to be uniformly mixed according to a ratio; and the above mixture is fed into a twin-screw extruder Wherein the reinforcing agent is added through the first venting hole or the side feeding system, melt extrusion granulation, that is, the styrene-based composition material is reinforced;
    (2)共挤成型:采用主机与该主机垂直设计的辅机进行共挤制备,主机用于挤出增强苯乙烯基组合物材料,辅机用于挤出热塑性树脂型材,主机、辅机同时挤出,成型后冷却定型得到自增强异型材。(2) Co-extrusion: co-extrusion preparation is carried out by using a main machine and a vertical machine designed by the main machine. The main machine is used for extruding and reinforced styrene-based composition materials, and the auxiliary machine is used for extruding thermoplastic resin profiles, and the main machine and auxiliary machine are simultaneously Extrusion, cooling and shaping after forming to obtain a self-reinforced profile.
  12. 根据权利要求11所述的增强异型材的制备方法,其特征在于,步骤(1)中,所述混合温度为20-50℃,转速为100-800转/分钟,混合时间为2-5分钟;所述双螺杆挤出机各段温度为200-240℃,双螺杆挤出机的长径比为36-48,螺杆转速为300-500转/分钟。The method for preparing a reinforced profile according to claim 11, wherein in the step (1), the mixing temperature is 20-50 ° C, the rotation speed is 100-800 rpm, and the mixing time is 2-5 minutes. The temperature of each section of the twin-screw extruder is 200-240 ° C, the length-to-diameter ratio of the twin-screw extruder is 36-48, and the screw rotation speed is 300-500 rpm.
  13. 根据权利要求11所述的自增强异型材的制备方法,其特征在于,步骤(2)中,所述主机为单螺杆挤出机,单螺杆挤出机各段温度为160-215℃,所述辅机为双螺杆挤出机,双螺杆挤出机各段温度为150-200℃;优选的,所述主机为单螺杆挤出机,机头温度为175-195℃,机身一区温度为160-165℃,机身二区温度为160-175℃,机身三区温度为175-185℃,机身四区温度为175-185℃,螺杆转速为18-22rpm;所述辅机为双螺杆挤出机,机头温度为175-195℃,机身一区温度为155-165℃,机身二区温度为165-175℃,机身三区温度为175-185℃,机身四区温度为175-185℃,螺杆转速为18-22rpm。The method for preparing a self-reinforcing profile according to claim 11, wherein in the step (2), the main machine is a single-screw extruder, and the temperature of each section of the single-screw extruder is 160-215 ° C. The auxiliary machine is a twin-screw extruder, and the temperature of each section of the twin-screw extruder is 150-200 ° C; preferably, the main machine is a single-screw extruder, the head temperature is 175-195 ° C, and the fuselage area is The temperature is 160-165 ° C, the temperature of the second zone of the fuselage is 160-175 ° C, the temperature of the fuselage three zones is 175-185 ° C, the temperature of the fuselage four zones is 175-185 ° C, and the screw rotation speed is 18-22 rpm; The machine is a twin-screw extruder with a head temperature of 175-195°C, a temperature of 155-165°C in the fuselage area, a temperature of 165-175°C in the second zone, and a temperature of 175-185°C in the fuselage. The temperature of the four zones of the fuselage is 175-185 ° C, and the screw speed is 18-22 rpm.
  14. 权利要求1-10任一项所述的自增强异型材在办公桌包边、衣柜包边或橱柜包边中的应用。 Use of the self-reinforced profile of any of claims 1-10 in a desk edging, a wardrobe edging or a cabinet edging.
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