WO2020246440A1 - Fiber reinforced resin molded body - Google Patents

Fiber reinforced resin molded body Download PDF

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Publication number
WO2020246440A1
WO2020246440A1 PCT/JP2020/021663 JP2020021663W WO2020246440A1 WO 2020246440 A1 WO2020246440 A1 WO 2020246440A1 JP 2020021663 W JP2020021663 W JP 2020021663W WO 2020246440 A1 WO2020246440 A1 WO 2020246440A1
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WIPO (PCT)
Prior art keywords
resin
fiber
integrated
fiber sheet
molded product
Prior art date
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PCT/JP2020/021663
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French (fr)
Japanese (ja)
Inventor
田中忠玄
平石陽一
中村崇
中明裕太
駒井優貴
Original Assignee
倉敷紡績株式会社
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Priority to JP2021524839A priority Critical patent/JPWO2020246440A1/ja
Publication of WO2020246440A1 publication Critical patent/WO2020246440A1/en

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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29BPREPARATION OR PRETREATMENT OF THE MATERIAL TO BE SHAPED; MAKING GRANULES OR PREFORMS; RECOVERY OF PLASTICS OR OTHER CONSTITUENTS OF WASTE MATERIAL CONTAINING PLASTICS
    • B29B15/00Pretreatment of the material to be shaped, not covered by groups B29B7/00 - B29B13/00
    • B29B15/08Pretreatment of the material to be shaped, not covered by groups B29B7/00 - B29B13/00 of reinforcements or fillers
    • B29B15/10Coating or impregnating independently of the moulding or shaping step
    • B29B15/12Coating or impregnating independently of the moulding or shaping step of reinforcements of indefinite length
    • 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
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/06Fibrous reinforcements only
    • B29C70/08Fibrous reinforcements only comprising combinations of different forms of fibrous reinforcements incorporated in matrix material, forming one or more layers, and with or without non-reinforced layers
    • 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
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/06Fibrous reinforcements only
    • B29C70/10Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres
    • 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
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/06Fibrous reinforcements only
    • B29C70/10Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres
    • B29C70/16Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length
    • B29C70/20Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in a single direction, e.g. roofing or other parallel 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
    • B32B5/00Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts

Definitions

  • the present invention relates to a fiber-reinforced resin molded body composed of a laminated body in which resin-integrated fiber sheets of different resins are laminated.
  • Fiber reinforced composites made of fiber and matrix resin have excellent mechanical properties, such as building materials, laptop housings, IC trays, sports equipment such as shoes and sticks, windmills, automobiles, railroads, ships, aviation, and space. It is widely used in general industrial applications such as.
  • a fiber-reinforced composite material in which a reinforcing fiber base material sheet having good workability is impregnated with a resin is used in a wide range of applications as a material having both light weight, strength, rigidity and the like.
  • the continuous fiber sheet has extremely high tensile strength as compared with the discontinuous fiber sheet, and is regarded as useful for members requiring strength such as structural members and outer panels of aviation, space, ships, automobiles, and buildings.
  • a fiber-reinforced composite material can be manufactured by laminating and molding a plurality of intermediate materials (prepregs, semipregs) composed of a resin and a fiber sheet as a matrix resin.
  • the fiber-reinforced composite material can be made by laminating a plurality of sheets using carbon fibers arranged in one direction as a reinforcing fiber base material in one direction, an orthogonal direction, or a different direction with respect to the fiber axis direction, and in each direction.
  • physical properties are controlled.
  • Fiber reinforced composites are required to have various properties other than improving strength and moldability.
  • Patent Documents 1 to 4 there is a proposal of laminating a resin or a film on the surface of a fiber-reinforced composite material.
  • the present invention provides a fiber-reinforced resin molded product in which at least one surface layer is provided with functionality, the other layer has high strength, and the overall strength is practically sufficient. provide.
  • the fiber-reinforced resin molded body of the present invention is a fiber-reinforced resin molded body in which a plurality of resin-integrated fiber sheets composed of a continuous fiber sheet and a thermoplastic resin are laminated, and the fiber-reinforced resin molded body is 2 It is characterized in that more than one type of resin-integrated fiber sheet is laminated and integrated, including a surface layer and an inner layer, and the resin-integrated fiber sheet of at least one surface layer is different from the other resin-integrated fiber sheets. To do.
  • a plurality of resin-integrated fiber sheets composed of a continuous fiber sheet and a thermoplastic resin are laminated, and include a surface layer and an inner layer, and the resin-integrated fiber sheet of at least one surface layer and the other resin are integrated.
  • the synthetic fiber sheet at least one surface layer is imparted with functionality, the other layer has high strength, and it is possible to provide a fiber-reinforced resin molded body having practically sufficient strength as a whole. Further, it can be a fiber-reinforced resin molded product that is thin and has strength that can withstand practical use.
  • the matrix resin is a thermoplastic resin, the molding cycle is fast, the shapeability is good, and efficient integral molding is possible.
  • FIG. 1 is a schematic perspective view of a resin-integrated carbon fiber sheet according to an embodiment of the present invention.
  • FIG. 2 is a schematic cross-sectional view of the resin-integrated carbon fiber sheet in the width direction.
  • FIG. 3 is a schematic process diagram showing a method for producing a resin-integrated carbon fiber sheet according to an embodiment of the present invention.
  • FIG. 4A is a schematic perspective view of two types of resin integrated fiber sheets used in one embodiment of the present invention, and FIG. 4B is a schematic explanatory view of laminating the resin integrated fiber sheets.
  • FIG. 5 is a stress-displacement measurement graph of Example 1 of the present invention.
  • FIG. 6 is a stress-displacement measurement graph of Comparative Example 1.
  • FIG. 7 is a stress-displacement measurement graph of Example 2 of the present invention.
  • FIG. 8 is a stress-displacement measurement graph of Comparative Example 2.
  • the present invention is a fiber-reinforced resin molded product in which a plurality of resin-integrated fiber sheets composed of a continuous fiber sheet and a thermoplastic resin are laminated.
  • this fiber-reinforced resin molded body two or more types of resin-integrated fiber sheets are laminated and integrated, and the resin-integrated fiber sheet of at least one surface layer is different from the other resin-integrated fiber sheets.
  • functionality such as adhesiveness can be imparted to at least one surface layer.
  • the resin-integrated fiber sheet of both surface layers is different from the resin-integrated fiber sheet of the inner layer.
  • the resin-integrated fiber sheets of both surface layers may be the same or different. As a result, functionality such as adhesiveness can be imparted to both surface layers, and the balance of strength can be improved.
  • the thickness of the fiber-reinforced resin molded product is preferably 0.1 to 5.0 mm, more preferably 0.25 to 3.0 mm. As a result, a thin and high-strength molded product can be obtained.
  • Reinforcing fibers are used as the fibers of the fiber-reinforced resin molded product.
  • Reinforcing fibers include carbon fibers, glass fibers, aramid fibers, and other thermoplastic fibers (polyethylene, polypropylene, etc.). However, carbon fiber is preferable because it is intended for thin materials.
  • the resins include polyamide-based resin, polycarbonate-based resin, polypropylene-based resin, polyester-based resin, polyethylene-based resin, acrylic-based resin, phenoxy resin, polystyrene-based resin, polyimide-based resin, polyetheretherketone (PEEK) -based resin, and It is preferably selected from polyetherketoneketone (PEKK) -based resins, and the resin of the resin-integrated fiber sheet of at least one surface layer and the resin of the other resin-integrated fiber sheet are preferably different.
  • PEKK polyetherketoneketone
  • the fiber-reinforced resin molded body As an example of the fiber-reinforced resin molded body, two resin-integrated fiber sheets (one on each of the front and back surfaces) made of polyamide (PA) 12 resin and carbon fiber on both surface layers, and phenoxy resin and carbon fiber on the inner layer. Twelve resin-integrated fiber sheets are arranged and laminated and integrated.
  • the PA12 resin has good adhesiveness to rubber and metal, so that it is convenient to integrate with rubber or metal, and rubber can be attached. It is well known in JP-A-2015-145129 and JP-A-2005-111902 that the adhesiveness between PA12 and rubber is good, and that the adhesiveness between PA12 and metal is good is published in JP-A-2004-346255. It is well known in Japanese Patent Application Laid-Open No.
  • unidirectional continuous fibers in which continuous fiber groups are opened and arranged in parallel in one direction and crosslinked fibers in a direction intersecting with the unidirectional continuous fibers are present, and the crosslinked fibers are made of a thermoplastic resin. It is preferably bonded and fixed to the continuous fiber sheet. As a result, the strength in the width direction is high, the cleavage property is low, and the handleability is good even if the thickness is thin.
  • the crosslinked fibers are preferably those generated from the continuous fiber group when the continuous fiber group is opened to form unidirectional continuous fibers arranged in parallel in one direction.
  • the crosslinked fibers generated from the continuous fiber group in a series of steps are interlaced or entangled with the continuous fiber sheet, and have low cleavability.
  • the continuous fiber sheet may be a woven fabric.
  • the crosslinked fibers are preferably 1 to 25% by mass, more preferably 3 to 20% by mass, and further preferably 5 to 15% by mass. ..
  • the crosslinked fibers are present in the above proportions, the strength of the continuous fiber sheet in the width direction is high, the fissure is low, and the handleability can be further improved.
  • the continuous fiber sheet is preferably a semi-preg in which resin powder is adhered to the surface and melted.
  • This semi-preg can be manufactured by a dry method, and the manufacturing efficiency is high.
  • the continuous fiber sheet may be a prepreg impregnated with a resin.
  • the fiber is preferably 30 to 70% by volume and the resin is 70 to 30% by volume, more preferably 35 to 65% by volume of the fiber and 65 to 35% by volume of the resin. is there.
  • the resin component of the resin-integrated fiber sheet can be directly used as the matrix resin component of the molded product. That is, it is possible to eliminate the need to add a new resin when manufacturing the molded product.
  • the mass of the resin-integrated fiber sheet is preferably 10 to 3000 g / m 2 , more preferably 20 to 2000 g / m 2 , and even more preferably 30 to 1000 g / m 2 .
  • the resin adhered state of the resin-integrated fiber sheet of the present invention is that the resin is melt-solidified and adhered near the surface of the opened fiber sheet, and the resin is not impregnated inside the fiber sheet. It is preferably partially impregnated. In the above state, it is preferable to heat and pressurize a plurality of resin-integrated fiber sheets in a laminated state to form a fiber-reinforced resin molded product.
  • the width of the spread fiber sheet (hereinafter, also referred to as “spread fiber sheet”) is preferably 0.1 to 5.0 mm per 1000 constituent fibers. Specifically, the width of the spread fiber sheet is about 0.1 to 1.5 mm per 1000 constituent fibers in the case of a large tow such as 50K or 60K, and the constituent fibers in the case of a regular tow such as 12K or 15K. It is about 0.5 to 5.0 mm per 1000 pieces. As the number of constituent fibers of the tow per fiber increases, the twist of the fibers increases and it becomes difficult to open the fibers, so that the width of the opening sheet also becomes narrower.
  • the unopened fiber tow sold by the carbon fiber manufacturer can be expanded to form an easy-to-use spread fiber sheet, which can be supplied to various molded products.
  • the carbon fiber bundle (toe) of the feed yarn is preferably 5,000 to 50,000 / bundle, and 10 to 280 carbon fiber bundles (tow) are preferably supplied.
  • a plurality of carbon fiber bundles (tow) are supplied and opened in this way to form a single sheet, the space between the carbon fiber bundle (toe) and the carbon fiber bundle (toe) is easily cleaved, but in various directions.
  • the crosslinked fibers having properties are adhered and fixed to the sheet with a resin, cleavage between the toes can be prevented.
  • the average length of the crosslinked fibers is preferably 1 mm or more, more preferably 5 mm or more.
  • the carbon fiber sheet has high strength in the width direction and is excellent in handleability.
  • the method for producing a resin-integrated fiber sheet of the present invention includes the following steps.
  • a carbon fiber sheet will be described as a fiber sheet.
  • crosslinked fibers When the carbon fiber filament group is opened by passing through a roll or an opening bar, by applying tension to the carbon fiber filament group, crosslinked fibers can be generated from the carbon fiber filament group at the time of opening.
  • the tension of the carbon fiber filament group can be, for example, in the range of 2.5 to 30 N per 15,000 fibers.
  • air defibration it is preferable to generate crosslinked fibers by a roll or a defibration bar after this.
  • the crosslinked fibers are generated from the carbon fiber filament group, the crosslinked fibers are in a state of being interlaced with the carbon fibers constituting the carbon fiber sheet.
  • crossing includes entanglement.
  • some or all of the crosslinked fibers are present in the carbon fiber sheet and are sterically interlaced with the carbon fibers arranged in one direction.
  • B Powder resin is applied to the opened carbon fiber sheet.
  • C The powder resin is heated and melted in a pressure-free (no pressure) state, cooled, and the resin is partially present on at least a part of the surface of the carbon fiber sheet. At this time, the crosslinked fibers are adhered and fixed to the carbon fiber sheet with the resin on the surface.
  • FIG. 1 is a schematic perspective view of the resin-integrated carbon fiber sheet 1 according to the embodiment of the present invention
  • FIG. 2 is a schematic cross-sectional view of the resin-integrated carbon fiber sheet 1 in the width direction.
  • Crosslinked fibers 3 are arranged in various directions on the surface of the opened carbon fiber sheet 2.
  • the resin 4 is melt-solidified and adhered to the vicinity of the surface of the carbon fiber sheet 2, and the resin 4 is not or partially impregnated inside the carbon fiber sheet 2.
  • the resin 4 adheres and fixes the crosslinked fiber 3 to the surface of the carbon fiber sheet 2.
  • crosslinked fibers 3a and 3b are present on the surface of the carbon fiber sheet 2.
  • the crosslinked fibers 3a are all on the surface of the carbon fiber sheet 2.
  • a part of the crosslinked fiber 3b is on the surface of the carbon fiber sheet 2, and a part of the crosslinked fiber 3b is in a state of entering the inside and interlacing with the carbon fiber.
  • the resin 4 adheres and fixes the crosslinked fiber 3 to the surface of the carbon fiber sheet 2. Further, there is a portion to which the resin 4 is attached and a portion 5 to which the resin is not attached.
  • the portion 5 to which the resin does not adhere is a passage through which the air inside the fiber sheet escapes when the resin-integrated carbon fiber sheet 1 is heated and pressed in a laminated state to form a fiber-reinforced resin molded product. Therefore, the resin on the surface is easily impregnated in the entire fiber sheet by pressurization. As a result, the resin 4 becomes a matrix resin of the fiber-reinforced resin molded product.
  • FIG. 3 is a schematic process diagram showing a method for producing a resin-integrated carbon fiber sheet according to an embodiment of the present invention.
  • the carbon fiber filament group (toe) 8 is pulled out from a large number of supply bobbins 7 and passed between the opening rolls 21a-21j to open the fibers (roll opening step 23). Instead of roll opening, air opening may be used.
  • the spread fiber roll may be fixed or rotated, or may vibrate in the width direction.
  • the opened tow is nipated between the nip rolls 9a and 9b, passed between a plurality of bridge rolls 12a-12b installed between the nip rolls 9a and 9b, and the tension of the toe is applied per 15,000, for example (1).
  • Cross-linked fibers are generated by applying in the range of 2.5 to 30 N (corresponding to the carbon fiber filament group supplied from each supply bobbin) (cross-linked fiber generation step 24).
  • the bridge roll may rotate or oscillate in the width direction.
  • the bridge roll has a satin finish, an uneven surface, a mirror surface, and a plurality of rolls, and the carbon fiber filament group is bent, fixed, rotated, vibrated, or a combination thereof to generate crosslinked fibers.
  • 13a-13g is a guide roll. After that, the dry powder resin 15 is sprinkled on the surface of the spread sheet from the powder supply hopper 14, supplied into the heating device 16 in a pressure-free state and heated to melt the dry powder resin 15, and between the guide rolls 13f-13g. Cooling.
  • the dry powder resin 18 is sprinkled on the back surface of the spread fiber sheet from the powder supply hopper 17, and the dry powder resin 18 is supplied into the heating device 19 in a pressure-free state and heated to melt the dry powder resin 18, cool it, and wind up the roll 20.
  • the dry powder resins 15 and 18 are, for example, phenoxy resins (glass transition point 180 ° C.), the temperatures in the heating devices 16 and 19 are, for example, + 20 to 60 ° C. of the melting point or glass transition point of the resin, and the residence time is, for example, 4 each. Let it be seconds.
  • the carbon fiber spread sheet has high strength in the width direction, and the constituent carbon fibers do not fall apart and can be handled as a sheet.
  • Powder resin can be applied by powder coating method, electrostatic coating method, spraying method, fluid immersion method, etc.
  • a powder coating method in which the powder resin is dropped on the surface of the carbon fiber sheet is preferable.
  • a dry powder-like powder resin is sprinkled on the opened carbon fiber sheet.
  • FIG. 4A is a schematic perspective view of two types of resin integrated fiber sheets used in one embodiment of the present invention
  • FIG. 4B is a schematic explanatory view of laminating the resin integrated fiber sheets.
  • the resin integrated fiber sheet 30 is composed of carbon fibers 32 and resin 33 arranged in one direction, and is arranged on both surface layers.
  • the resin-integrated fiber sheet 31 is composed of carbon fibers 32 and resin 34 arranged in one direction, and is arranged in the inner layer.
  • the crosslinked fibers shown in FIGS. 1 and 2 are present in the resin-integrated fiber sheets 30 and 31, but are omitted in the drawing. As shown in FIG.
  • a plurality of resin-integrated fiber sheets 31 are used as inner layers, resin-integrated fiber sheets 30 are arranged on both surfaces thereof, and the whole is pressurized and heated to be laminated and integrated to form a fiber-reinforced resin molded product.
  • the pressing force for laminating and integrating is preferably 0.2 to 10 MPa, the temperature is preferably + 20 to 60 ° C. of the melting point or flow start temperature of the resin, and the time is preferably 2 to 15 minutes.
  • a preferred example of the present invention can be summarized as follows.
  • the fiber-reinforced resin molded product has a laminated structure of two or more layers.
  • the directionality of the fibers does not matter, but a unidirectional sheet is preferable in consideration of thinness. It is preferable to laminate a sheet with added functionality on at least one surface layer side. Considering warpage after molding, a layer having the same front and back surfaces is preferable. That is, the fiber-reinforced resin molded body is a front surface layer (1 to 2 layers) / inner layer (N layer) / back surface layer (1 to 2 layers), and the number N of inner layers is preferably 1 to 100, and the total number of layers is 3 to 102 is preferable.
  • a molding method a general compression molding method such as press molding or vacuum forming is used. As a result, it is integrally molded. It is meaningless to have the surface layer and the inner layer as separate processes.
  • Others It is preferable to impart functionality to at least one surface layer.
  • the functionality includes adhesiveness, printability, weather resistance, water resistance, chemical resistance, paintability, processability, functionality, thermal conductivity, flame retardancy, surface smoothness and the like. It is also possible to change the fiber volume fraction (Vf) of the resin-integrated fiber sheet to be laminated.
  • Vf fiber volume fraction
  • imparting adhesiveness to the surface layer of the fiber-reinforced resin molded product is useful for integrating with at least one selected from metal, resin and rubber.
  • Example 1 Carbon fiber unopened fiber tow The carbon fiber unopened fiber tow was manufactured by Mitsubishi Chemical Corporation, product number: PYROFILE TR 50S15L, shape: regular tow filament 15K (15,000 fibers,), and a single fiber diameter of 7 ⁇ m was used. An epoxy compound is attached to the carbon fiber of the unopened carbon fiber tow as a sizing agent.
  • Means for opening the unopened fiber tow The fibers were opened using the opening means shown in FIG. In the fiber opening step, the tension of the carbon fiber filament group (toe) was set to 15 N per 15,000 fibers.
  • Mass 132.4g / m 2 (resin: 52.4g / m 2, the fibers: 80g / m 2) was.
  • (3-2) Semi-preg 2 PA12 resin (manufactured by Daicel Evonik, melting point 176 ° C.) was used as the dry powder resin.
  • the average particle size of the dry powder resin was 80 ⁇ m.
  • An average of 24.0 g of this resin was applied to 1 m 2 of carbon fibers on one side and 48.0 g on both sides.
  • the temperature in the heating devices 16 and 19 was 200 ° C., and the residence time was 4 seconds each.
  • the mass was 128.0 g / m 2 (resin: 48 g / m 2 , fiber: 80 g / m 2 ).
  • Example 1 The same experiment as in Example 1 was carried out except that the semi-preg 2 of Example 1 was used for all layers as the resin-integrated fiber sheet (semi-preg).
  • Example 1 A sample was cut out from the molded products of Example 1 and Comparative Example 1 to a length of 80 mm (designated direction) and a width of 15 mm, and allowed to stand at a temperature of 23 ° C. and a relative humidity of 50% for 48 hours or more. Six samples were taken for each of 1 product of Example and 1 product of Comparative Example. The sizes of the obtained samples are summarized in Table 1.
  • FIG. 5 is a stress-displacement measurement graph of Example 1 of the present invention
  • FIG. 6 is a stress-displacement measurement graph of Comparative Example 1.
  • the numerical values in FIGS. 5 to 6 indicate the measurement order.
  • Example 2 since the matrix resin of both surface layers of Example 1 is PA12 resin, it is imparted with the functionality of having high adhesive strength to rubber and metal, and is practically sufficient as a whole. It had strength.
  • Example 2 Carbon fiber unopened fiber tow
  • the carbon fiber unopened fiber tow was manufactured by Mitsubishi Chemical Corporation, product number: PYROFILE TR 50S15L, shape: regular tow filament 15K (15,000 fibers,), and a single fiber diameter of 7 ⁇ m was used.
  • An epoxy compound is attached to the carbon fibers of the unopened carbon fiber tow as a sizing agent.
  • Means for opening the unopened fiber tow The fibers were opened using the opening means shown in FIG. In the fiber opening step, the tension of the carbon fiber filament group (toe) was set to 15 N per 15,000 fibers. In this way, an spread sheet having a carbon fiber filament composition of 50 K, a spread width of 500 mm, and a thickness of 0.08 mm was obtained.
  • the crosslinked fiber was 3.3% by mass.
  • the basis weight was 80 g / m 2 .
  • (3-1) Semi-preg 3 A polycarbonate resin (manufactured by Teijin Limited, melting point 240 ° C. or less) was used as the dry powder resin.
  • the average particle size of the dry powder resin was 180 ⁇ m or less.
  • An average of 26.4 g of this resin was applied to 1 m 2 of carbon fibers on one side and 53 g on both sides.
  • the temperatures in the heating devices 16 and 19 were 260 ° C., and the residence time was 4 seconds each.
  • the mass was 133 g / m 2 (resin: 53 g / m 2 , fiber: 80 g / m 2 ).
  • One semi-preg 4 is installed on the front and back surfaces, 10 semi-pregs 3 are arranged in the inner layer, the base fiber direction is one direction, the base size is 250 mm in length and 250 mm in width, and the press Molding was performed at 300 ° C. and 3 MPa for 5 minutes.
  • Example 2 The same experiment as in Example 2 was carried out except that the semi-preg 3 of Example 2 was used for all layers as the resin-integrated fiber sheet (semi-preg).
  • Example 2 A sample was cut out from the molded products of Example 2 and Comparative Example 2 to a length of 80 mm (designated direction) and a width of 15 mm, and allowed to stand at a temperature of 23 ° C. and a relative humidity of 50% for 48 hours or more. Six samples were taken for each of the two Examples and the two Comparative Examples. The sizes of the obtained samples are summarized in Table 3.
  • FIG. 7 is a stress-displacement measurement graph of Example 2 of the present invention
  • FIG. 8 is a stress-displacement measurement graph of Comparative Example 2.
  • the numerical values in FIGS. 7 to 8 indicate the measurement order.
  • Example 2 since the matrix resin of both surface layers of Example 2 is a phenoxy resin, it is possible to impart a function having excellent moisture resistance, and further, the flexural modulus and bending from Example 2 and Comparative Example 2 The strength was the same, and it had a practically sufficient strength.
  • the fiber-reinforced resin molded product of the present invention is widely applied to building materials, laptop housings, IC trays, sporting goods such as shoes and sticks, and general industrial applications such as windmills, automobiles, railways, ships, aerospace, and the like. it can.

Abstract

A plurality of resin integrated fiber sheets 30, 31 each comprising a continuous fiber sheet and a thermoplastic resin are stacked on one another, at least two types of the resin integrated fiber sheets are stacked and integrated, including a surface layer and an inner layer, and a resin integrated fiber sheet 30 in at least one surface layer and another resin integrated fiber sheet 31 differ from one another. Unidirectional continuous fibers in which continuous fiber groups are opened and are arranged in parallel in one direction, and cross-linking fibers in a direction interleaved with the unidirectional continuous fibers exist in each continuous fiber sheet, and the cross-linking fibers are preferably adhesively fixed to the continuous fiber sheets by means of thermoplastic resin. In this way, functionality is imparted to at least one surface layer, and the other layers have high strength, thereby providing a fiber reinforced resin molded body which also as a whole has adequate strength for practical use.

Description

繊維強化樹脂成形体Fiber reinforced resin molded body
 本発明は、異なる樹脂の樹脂一体化繊維シートを積層した積層体からなる繊維強化樹脂成形体に関する。 The present invention relates to a fiber-reinforced resin molded body composed of a laminated body in which resin-integrated fiber sheets of different resins are laminated.
 繊維とマトリックス樹脂からなる繊維強化複合材は、力学物性に優れており、建築部材、ノートパソコンの筐体、ICトレイ、靴やスティックなどのスポーツ用品、風車、自動車、鉄道、船舶、航空、宇宙などの一般産業用途等において広く用いられている。特に、加工性が良い強化繊維基材シートに樹脂を含浸させた繊維強化複合材は、軽量性と強度、剛性等を兼ね備えた材料として幅広い用途に用いられている。中でも連続繊維シートは不連続繊維シートと比較して引張強度が極めて高く、航空や宇宙、船舶、自動車、建造物の構造部材や外板等の強度が必要な部材においても有用視されている。繊維としては、ガラス繊維や炭素繊維、アラミド繊維を用いたFRPの需要が高く、特に炭素繊維の需要が高まっている。
 繊維強化複合材を製造する方法としては、製品の様態や要求物性に応じて様々な方法が適用可能である。マトリックス樹脂として樹脂と繊維シートからなる中間材料(プリプレグ、セミプレグ)を複数枚積層して成形させることで繊維強化複合材を製造することができる。繊維強化複合材は、一方向に配列した炭素繊維を強化繊維基材とした複数枚のシートを繊維軸方向に対して、一方向や直行方向、異方向に積層することができ、各方向に対して物性の制御が行われる。
Fiber reinforced composites made of fiber and matrix resin have excellent mechanical properties, such as building materials, laptop housings, IC trays, sports equipment such as shoes and sticks, windmills, automobiles, railroads, ships, aviation, and space. It is widely used in general industrial applications such as. In particular, a fiber-reinforced composite material in which a reinforcing fiber base material sheet having good workability is impregnated with a resin is used in a wide range of applications as a material having both light weight, strength, rigidity and the like. Among them, the continuous fiber sheet has extremely high tensile strength as compared with the discontinuous fiber sheet, and is regarded as useful for members requiring strength such as structural members and outer panels of aviation, space, ships, automobiles, and buildings. As the fiber, the demand for FRP using glass fiber, carbon fiber, and aramid fiber is high, and the demand for carbon fiber is particularly increasing.
As a method for producing a fiber-reinforced composite material, various methods can be applied depending on the state of the product and the required physical properties. A fiber-reinforced composite material can be manufactured by laminating and molding a plurality of intermediate materials (prepregs, semipregs) composed of a resin and a fiber sheet as a matrix resin. The fiber-reinforced composite material can be made by laminating a plurality of sheets using carbon fibers arranged in one direction as a reinforcing fiber base material in one direction, an orthogonal direction, or a different direction with respect to the fiber axis direction, and in each direction. On the other hand, physical properties are controlled.
 繊維強化複合材は強度の向上や成形性を上げること以外に、様々な特性が求められる。特に繊維強化複合材の表面性を良くして、難燃性、耐候性、耐水性、耐薬品性、塗装性、加工性、機能性、熱伝導性等機能を向上させることがあげられる。従来技術として、繊維強化複合材の表面に樹脂やフィルムを貼り合せる提案がある(特許文献1~4)。 Fiber reinforced composites are required to have various properties other than improving strength and moldability. In particular, it is possible to improve the surface properties of the fiber-reinforced composite material to improve functions such as flame retardancy, weather resistance, water resistance, chemical resistance, paintability, processability, functionality, and thermal conductivity. As a prior art, there is a proposal of laminating a resin or a film on the surface of a fiber-reinforced composite material (Patent Documents 1 to 4).
WO2017/030190明細書WO2017 / 030190 specification 特開2018-171787号公報JP-A-2018-171787 特開2012-61780号公報Japanese Unexamined Patent Publication No. 2012-61780 特開2011-37150号公報Japanese Unexamined Patent Publication No. 2011-37150
 しかし、従来技術は、薄物の繊維強化複合材の場合、最外層が樹脂フィルムであると、強度が低下する問題がある。構造材となる樹脂が、マトリックス樹脂でない場合は強度等に問題がある。また、熱硬化性樹脂と熱可塑性樹脂の複合材は、熱硬化性樹脂と熱可塑性樹脂は同時に成形することができず、熱硬化性樹脂の強化繊維の成形板に熱可塑性樹脂シートを貼り合せる工程のため、同時に一体化成形することは困難であり、さらに賦形性を求める加工には適さない。
 本発明は、前記従来の問題を解決するため、少なくとも一方の表面層は機能性が付与され、その他の層は強度が高く、全体としても実用的に十分な強度を有する繊維強化樹脂成形体を提供する。
However, in the prior art, in the case of a thin fiber-reinforced composite material, if the outermost layer is a resin film, there is a problem that the strength is lowered. If the resin used as the structural material is not a matrix resin, there is a problem in strength and the like. Further, in the composite material of the thermosetting resin and the thermoplastic resin, the thermosetting resin and the thermoplastic resin cannot be molded at the same time, and the thermoplastic resin sheet is bonded to the molded plate of the reinforcing fiber of the thermosetting resin. Since it is a process, it is difficult to integrally mold it at the same time, and it is not suitable for processing that requires shapeability.
In order to solve the above-mentioned conventional problems, the present invention provides a fiber-reinforced resin molded product in which at least one surface layer is provided with functionality, the other layer has high strength, and the overall strength is practically sufficient. provide.
 本発明の繊維強化樹脂成形体は、連続繊維シートおよび熱可塑性樹脂から構成される樹脂一体化繊維シートが複数枚積層された繊維強化樹脂成形体であって、前記繊維強化樹脂成形体は、2種類以上の樹脂一体化繊維シートが積層一体化されており、表面層と内層を含み、少なくとも一方の表面層の樹脂一体化繊維シートと、その他の樹脂一体化繊維シートとは異なることを特徴とする。 The fiber-reinforced resin molded body of the present invention is a fiber-reinforced resin molded body in which a plurality of resin-integrated fiber sheets composed of a continuous fiber sheet and a thermoplastic resin are laminated, and the fiber-reinforced resin molded body is 2 It is characterized in that more than one type of resin-integrated fiber sheet is laminated and integrated, including a surface layer and an inner layer, and the resin-integrated fiber sheet of at least one surface layer is different from the other resin-integrated fiber sheets. To do.
 本発明は、連続繊維シートおよび熱可塑性樹脂から構成される樹脂一体化繊維シートが複数枚積層され、表面層と内層を含み、少なくとも一方の表面層の樹脂一体化繊維シートと、その他の樹脂一体化繊維シートとは異なることにより、少なくとも一方の表面層は機能性が付与され、その他の層は強度が高く、全体としても実用的に十分な強度を有する繊維強化樹脂成形体を提供できる。また、薄物で実用に耐えうる強度を有する繊維強化樹脂成形体とすることもできる。さらに、マトリックス樹脂は熱可塑性樹脂であるため、成形サイクルが早く、賦形性が良く、効率の良い一体成形が可能となる。 In the present invention, a plurality of resin-integrated fiber sheets composed of a continuous fiber sheet and a thermoplastic resin are laminated, and include a surface layer and an inner layer, and the resin-integrated fiber sheet of at least one surface layer and the other resin are integrated. By being different from the synthetic fiber sheet, at least one surface layer is imparted with functionality, the other layer has high strength, and it is possible to provide a fiber-reinforced resin molded body having practically sufficient strength as a whole. Further, it can be a fiber-reinforced resin molded product that is thin and has strength that can withstand practical use. Further, since the matrix resin is a thermoplastic resin, the molding cycle is fast, the shapeability is good, and efficient integral molding is possible.
図1は本発明の一実施形態の樹脂一体化炭素繊維シートの模式的斜視図である。FIG. 1 is a schematic perspective view of a resin-integrated carbon fiber sheet according to an embodiment of the present invention. 図2は同、樹脂一体化炭素繊維シートの幅方向の模式的断面図である。FIG. 2 is a schematic cross-sectional view of the resin-integrated carbon fiber sheet in the width direction. 図3は本発明の一実施形態の樹脂一体化炭素繊維シートの製造方法を示す模式的工程図である。FIG. 3 is a schematic process diagram showing a method for producing a resin-integrated carbon fiber sheet according to an embodiment of the present invention. 図4Aは本発明の一実施形態で使用する2種類の樹脂一体化繊維シートの模式的斜視図、図4Bは同樹脂一体化繊維シートを積層する模式的説明図である。FIG. 4A is a schematic perspective view of two types of resin integrated fiber sheets used in one embodiment of the present invention, and FIG. 4B is a schematic explanatory view of laminating the resin integrated fiber sheets. 図5は本発明の実施例1の応力-変位測定グラフである。FIG. 5 is a stress-displacement measurement graph of Example 1 of the present invention. 図6は比較例1の応力-変位測定グラフである。FIG. 6 is a stress-displacement measurement graph of Comparative Example 1. 図7は本発明の実施例2の応力-変位測定グラフである。FIG. 7 is a stress-displacement measurement graph of Example 2 of the present invention. 図8は比較例2の応力-変位測定グラフである。FIG. 8 is a stress-displacement measurement graph of Comparative Example 2.
 本発明は、連続繊維シートおよび熱可塑性樹脂から構成される樹脂一体化繊維シートが複数枚積層された繊維強化樹脂成形体である。この繊維強化樹脂成形体は、2種類以上の樹脂一体化繊維シートが積層一体化されており、少なくとも一方の表面層の樹脂一体化繊維シートと、その他の樹脂一体化繊維シートとは異なる。これにより、少なくとも一方の表面層に接着性等の機能性を付与できる。両表面層の樹脂一体化繊維シートと、内層の樹脂一体化繊維シートとは異なることが好ましい。また、両表面層の樹脂一体化繊維シートは、同一のものでもよく、異なるものでもよい。これにより、両表面層に接着性等の機能性を付与できるとともに、強度のバランスを良好にできる。 The present invention is a fiber-reinforced resin molded product in which a plurality of resin-integrated fiber sheets composed of a continuous fiber sheet and a thermoplastic resin are laminated. In this fiber-reinforced resin molded body, two or more types of resin-integrated fiber sheets are laminated and integrated, and the resin-integrated fiber sheet of at least one surface layer is different from the other resin-integrated fiber sheets. As a result, functionality such as adhesiveness can be imparted to at least one surface layer. It is preferable that the resin-integrated fiber sheet of both surface layers is different from the resin-integrated fiber sheet of the inner layer. Further, the resin-integrated fiber sheets of both surface layers may be the same or different. As a result, functionality such as adhesiveness can be imparted to both surface layers, and the balance of strength can be improved.
 前記繊維強化樹脂成形体の厚みは0.1~5.0mmが好ましく、より好ましくは0.25~3.0mmである。これにより、薄くて強度の高い成形体とすることができる。 The thickness of the fiber-reinforced resin molded product is preferably 0.1 to 5.0 mm, more preferably 0.25 to 3.0 mm. As a result, a thin and high-strength molded product can be obtained.
 前記繊維強化樹脂成形体の繊維は、強化繊維を用いる。強化繊維は、炭素繊維、ガラス繊維、アラミド繊維、その他の熱可塑性繊維(ポリエチレン、ポリプロピレン等)がある。ただし、薄物を目的としているため、炭素繊維が好ましい。 Reinforcing fibers are used as the fibers of the fiber-reinforced resin molded product. Reinforcing fibers include carbon fibers, glass fibers, aramid fibers, and other thermoplastic fibers (polyethylene, polypropylene, etc.). However, carbon fiber is preferable because it is intended for thin materials.
 前記樹脂は、ポリアミド系樹脂、ポリカーボネート系樹脂、ポリプロピレン系樹脂、ポリエステル系樹脂、ポリエチレン系樹脂、アクリル系樹脂、フェノキシ樹脂、ポリスチレン系樹脂、ポリイミド系樹脂、ポリエーテルエーテルケトン(PEEK)系樹脂、及びポリエーテルケトンケトン(PEKK)系樹脂から選ばれ、少なくとも一方の表面層の樹脂一体化繊維シートの樹脂と、その他の樹脂一体化繊維シートの樹脂は異なることが好ましい。 The resins include polyamide-based resin, polycarbonate-based resin, polypropylene-based resin, polyester-based resin, polyethylene-based resin, acrylic-based resin, phenoxy resin, polystyrene-based resin, polyimide-based resin, polyetheretherketone (PEEK) -based resin, and It is preferably selected from polyetherketoneketone (PEKK) -based resins, and the resin of the resin-integrated fiber sheet of at least one surface layer and the resin of the other resin-integrated fiber sheet are preferably different.
 前記繊維強化樹脂成形体の一例として、両表面層にポリアミド(PA)12樹脂と炭素繊維からなる樹脂一体化繊維シート2枚(表裏面1枚ずつ)と、内層にフェノキシ樹脂と炭素繊維からなる樹脂一体化繊維シート12枚を配置して積層一体化する。これにより、PA12樹脂はゴム、金属との接着性が良好なため、ゴム又は金属と一体化するのに都合よく、さらにゴムの取付加工も可能となる。PA12とゴムとの接着性が良いことは特開2015-145129号公報、同2005-111902号公報等で周知であり、PA12と金属との接着性が良いことは特開2004-346255号公報、同2003-089773号公報、特開平10-330651等で周知である。他の例として、両表面層にフェノキシ樹脂と炭素繊維からなる樹脂一体化繊維シート2枚(表裏面1枚ずつ)と、内層にポリカーボネート(PC)樹脂と炭素繊維からなる樹脂一体化繊維シート12枚を配置して積層一体化する。これにより、フェノキシ樹脂は耐水性が高い樹脂のため、耐水性を向上させることができる。 As an example of the fiber-reinforced resin molded body, two resin-integrated fiber sheets (one on each of the front and back surfaces) made of polyamide (PA) 12 resin and carbon fiber on both surface layers, and phenoxy resin and carbon fiber on the inner layer. Twelve resin-integrated fiber sheets are arranged and laminated and integrated. As a result, the PA12 resin has good adhesiveness to rubber and metal, so that it is convenient to integrate with rubber or metal, and rubber can be attached. It is well known in JP-A-2015-145129 and JP-A-2005-111902 that the adhesiveness between PA12 and rubber is good, and that the adhesiveness between PA12 and metal is good is published in JP-A-2004-346255. It is well known in Japanese Patent Application Laid-Open No. 2003-089773 and JP-A-10-330651. As another example, two resin-integrated fiber sheets (one on each of the front and back surfaces) made of phenoxy resin and carbon fiber on both surface layers, and a resin-integrated fiber sheet 12 made of polycarbonate (PC) resin and carbon fiber on the inner layer. The sheets are arranged and laminated and integrated. As a result, since the phenoxy resin is a resin having high water resistance, the water resistance can be improved.
 前記連続繊維シートは、連続繊維群が開繊され一方向に並列状に配列された一方向連続繊維と、一方向連続繊維と交錯する方向に架橋繊維が存在し、架橋繊維は熱可塑性樹脂により連続繊維シートに接着固定されていることが好ましい。これにより、幅方向の強度が高く、低開裂性であり、厚みが薄くても取り扱い性が良好となる。前記架橋繊維は、連続繊維群が開繊され一方向に並列状に配列された一方向連続繊維を作る際に、連続繊維群から発生したものが好ましい。一連の工程で連続繊維群から発生した架橋繊維は、連続繊維シートと交錯ないしは交絡しており、低開裂性となる。前記連続繊維シートは、織物であってもよい。 In the continuous fiber sheet, unidirectional continuous fibers in which continuous fiber groups are opened and arranged in parallel in one direction and crosslinked fibers in a direction intersecting with the unidirectional continuous fibers are present, and the crosslinked fibers are made of a thermoplastic resin. It is preferably bonded and fixed to the continuous fiber sheet. As a result, the strength in the width direction is high, the cleavage property is low, and the handleability is good even if the thickness is thin. The crosslinked fibers are preferably those generated from the continuous fiber group when the continuous fiber group is opened to form unidirectional continuous fibers arranged in parallel in one direction. The crosslinked fibers generated from the continuous fiber group in a series of steps are interlaced or entangled with the continuous fiber sheet, and have low cleavability. The continuous fiber sheet may be a woven fabric.
 前記一方向連続繊維及び架橋繊維の合計を母数としたとき、前記架橋繊維は1~25質量%が好ましく、より好ましくは3~20質量%であり、さらに好ましくは5~15質量%である。架橋繊維が前記の割合で存在すれば、連続繊維シートの幅方向の強度が高く、低開裂性であり、取り扱い性がより改善できる。 When the total of the unidirectional continuous fibers and the crosslinked fibers is used as a parameter, the crosslinked fibers are preferably 1 to 25% by mass, more preferably 3 to 20% by mass, and further preferably 5 to 15% by mass. .. When the crosslinked fibers are present in the above proportions, the strength of the continuous fiber sheet in the width direction is high, the fissure is low, and the handleability can be further improved.
 前記連続繊維シートは、表面に樹脂粉体が付着され溶融したセミプレグが好ましい。このセミプレグは乾式法で製造でき、製造効率は高い。また、前記連続繊維シートは、樹脂を含浸したプリプレグであってもよい。 The continuous fiber sheet is preferably a semi-preg in which resin powder is adhered to the surface and melted. This semi-preg can be manufactured by a dry method, and the manufacturing efficiency is high. Further, the continuous fiber sheet may be a prepreg impregnated with a resin.
 前記樹脂一体化繊維シートを100体積%としたとき、繊維30~70体積%、樹脂70~30体積%であるのが好ましく、より好ましくは繊維35~65体積%、樹脂65~35体積%である。これにより、前記樹脂一体化繊維シートの樹脂成分を、そのまま成形体のマトリックス樹脂成分にすることができる。すなわち、成形体を製造する際に、新たな樹脂の追加は不要にできる。樹脂一体化繊維シートの質量は10~3000g/m2が好ましく、より好ましくは20~2000g/m2であり、さらに好ましくは30~1000g/m2である。 When the resin-integrated fiber sheet is 100% by volume, the fiber is preferably 30 to 70% by volume and the resin is 70 to 30% by volume, more preferably 35 to 65% by volume of the fiber and 65 to 35% by volume of the resin. is there. As a result, the resin component of the resin-integrated fiber sheet can be directly used as the matrix resin component of the molded product. That is, it is possible to eliminate the need to add a new resin when manufacturing the molded product. The mass of the resin-integrated fiber sheet is preferably 10 to 3000 g / m 2 , more preferably 20 to 2000 g / m 2 , and even more preferably 30 to 1000 g / m 2 .
 本発明の樹脂一体化繊維シートの樹脂の付着状態は、開繊された繊維シートの表面付近に樹脂が溶融固化して付着しており、樹脂は繊維シート内部には含浸していないか又は一部含浸しているのが好ましい。前記状態であると、樹脂一体化繊維シートを複数枚積層状態で加熱・加圧して繊維強化樹脂成形品に成形するために好ましい。 The resin adhered state of the resin-integrated fiber sheet of the present invention is that the resin is melt-solidified and adhered near the surface of the opened fiber sheet, and the resin is not impregnated inside the fiber sheet. It is preferably partially impregnated. In the above state, it is preferable to heat and pressurize a plurality of resin-integrated fiber sheets in a laminated state to form a fiber-reinforced resin molded product.
 開繊された繊維シート(以下、「開繊シート」ともいう)の幅は、炭素繊維の場合、構成繊維本数1000本当たり0.1~5.0mmが好ましい。具体的には、開繊シートの幅は、50Kまたは60Kなどのラージトウの場合は構成繊維本数1000本当たり0.1~1.5mm程度であり、12Kまたは15Kなどのレギュラートウの場合は構成繊維本数1000本当たり0.5~5.0mm程度である。1本当たりのトウの構成繊維本数が増加するほど、繊維の捩れが大きくなり開繊しにくくなるので、開繊シートの幅も狭くなる。これにより、炭素繊維メーカーの販売する未開繊トウを拡開し、使用し易い開繊シートとし、様々な成形物に供給できる。供給糸の炭素繊維束(トウ)は5,000~50,000本/束が好ましく、この炭素繊維束(トウ)を10~280本供給するのが好ましい。このように炭素繊維束(トウ)を複数本供給して開繊し、1枚のシートにすると、炭素繊維束(トウ)と炭素繊維束(トウ)の間が開裂しやすいが、様々な方向性を有する架橋繊維が樹脂によりシートに接着固定されていると、トウ間の開裂も防止できる。 In the case of carbon fibers, the width of the spread fiber sheet (hereinafter, also referred to as “spread fiber sheet”) is preferably 0.1 to 5.0 mm per 1000 constituent fibers. Specifically, the width of the spread fiber sheet is about 0.1 to 1.5 mm per 1000 constituent fibers in the case of a large tow such as 50K or 60K, and the constituent fibers in the case of a regular tow such as 12K or 15K. It is about 0.5 to 5.0 mm per 1000 pieces. As the number of constituent fibers of the tow per fiber increases, the twist of the fibers increases and it becomes difficult to open the fibers, so that the width of the opening sheet also becomes narrower. As a result, the unopened fiber tow sold by the carbon fiber manufacturer can be expanded to form an easy-to-use spread fiber sheet, which can be supplied to various molded products. The carbon fiber bundle (toe) of the feed yarn is preferably 5,000 to 50,000 / bundle, and 10 to 280 carbon fiber bundles (tow) are preferably supplied. When a plurality of carbon fiber bundles (tow) are supplied and opened in this way to form a single sheet, the space between the carbon fiber bundle (toe) and the carbon fiber bundle (toe) is easily cleaved, but in various directions. When the crosslinked fibers having properties are adhered and fixed to the sheet with a resin, cleavage between the toes can be prevented.
 架橋繊維の平均長さは、1mm以上が好ましく、さらに好ましくは5mm以上である。架橋繊維の平均長さが前記の範囲であれば、幅方向の強度が高く、取り扱い性に優れた炭素繊維シートとなる。 The average length of the crosslinked fibers is preferably 1 mm or more, more preferably 5 mm or more. When the average length of the crosslinked fibers is within the above range, the carbon fiber sheet has high strength in the width direction and is excellent in handleability.
 本発明の樹脂一体化繊維シートの製造方法は、次の工程を含む。繊維シートとして炭素繊維シートを挙げて説明する。
A 炭素繊維フィラメント群を複数のロールを通過、開繊バーを通過、及びエアー開繊から選ばれる少なくとも一つの手段により開繊させ、一方向に並列状に配列させるに際し、開繊時もしくは開繊後に架橋繊維を炭素繊維フィラメント群から発生させるか、又は開繊時もしくは開繊後に架橋繊維を炭素繊維シートに落下させ、前記架橋繊維は炭素繊維シートの面積10mm2あたり平均1本以上とする。ロール又は開繊バーを通過させて炭素繊維フィラメント群を開繊する場合、炭素繊維フィラメント群に張力をかけることで、開繊時に炭素繊維フィラメント群から架橋繊維を発生させることができる。炭素繊維フィラメント群の張力は、例えば、15,000本あたり2.5~30Nの範囲とすることができる。エアー開繊を採用する場合は、この後にロール又は開繊バーにより架橋繊維を発生させるのが好ましい。架橋繊維を炭素繊維フィラメント群から発生させた場合は、架橋繊維は、炭素繊維シートを構成する炭素繊維と交錯した状態となる。ここで交錯とは、絡み合いを含む。例えば、架橋繊維の一部または全部は炭素繊維シート内に存在し、一方向に配列されている炭素繊維と立体的に交錯している。
B 開繊された炭素繊維シートに粉体樹脂を付与する。
C 加圧フリー(加圧なし)状態で粉体樹脂を加熱溶融し、冷却し、炭素繊維シートの少なくとも表面の一部に部分的に樹脂を存在させる。この際に、架橋繊維を表面の樹脂により炭素繊維シートに接着固定させる。
The method for producing a resin-integrated fiber sheet of the present invention includes the following steps. A carbon fiber sheet will be described as a fiber sheet.
A When the carbon fiber filament group is opened by at least one means selected from passing through a plurality of rolls, passing through a fiber opening bar, and air fiber opening and arranging in parallel in one direction, the fiber is opened or opened. Later, the crosslinked fibers are generated from the carbon fiber filament group, or the crosslinked fibers are dropped onto the carbon fiber sheet at the time of opening or after opening, and the average number of the crosslinked fibers is one or more per 10 mm 2 of the carbon fiber sheet. When the carbon fiber filament group is opened by passing through a roll or an opening bar, by applying tension to the carbon fiber filament group, crosslinked fibers can be generated from the carbon fiber filament group at the time of opening. The tension of the carbon fiber filament group can be, for example, in the range of 2.5 to 30 N per 15,000 fibers. When air defibration is adopted, it is preferable to generate crosslinked fibers by a roll or a defibration bar after this. When the crosslinked fibers are generated from the carbon fiber filament group, the crosslinked fibers are in a state of being interlaced with the carbon fibers constituting the carbon fiber sheet. Here, crossing includes entanglement. For example, some or all of the crosslinked fibers are present in the carbon fiber sheet and are sterically interlaced with the carbon fibers arranged in one direction.
B Powder resin is applied to the opened carbon fiber sheet.
C The powder resin is heated and melted in a pressure-free (no pressure) state, cooled, and the resin is partially present on at least a part of the surface of the carbon fiber sheet. At this time, the crosslinked fibers are adhered and fixed to the carbon fiber sheet with the resin on the surface.
 以下図面を用いて説明する。以下の図面において、同一符号は同一物を示す。図1は本発明の一実施形態の樹脂一体化炭素繊維シート1の模式的斜視図、図2は同、樹脂一体化炭素繊維シート1の幅方向の模式的断面図である。開繊された炭素繊維シート2の表面には架橋繊維3が様々な方向に配置している。また炭素繊維シート2の表面付近に樹脂4が溶融固化して付着しており、樹脂4は炭素繊維シート2内部には含浸していないか又は一部含浸している程度である。樹脂4は架橋繊維3を炭素繊維シート2の表面に接着固定している。図2に示すように、炭素繊維シート2の表面には架橋繊維3a,3bが存在する。架橋繊維3aは全部が炭素繊維シート2の表面にある。架橋繊維3bは一部が炭素繊維シート2の表面にあり、一部は内部に入って炭素繊維と交錯した状態である。樹脂4は架橋繊維3を炭素繊維シート2の表面に接着固定している。また、樹脂4が付着している部分と、樹脂が付着していない部分5がある。樹脂が付着していない部分5は、樹脂一体化炭素繊維シート1を複数枚積層状態で加熱・加圧して繊維強化樹脂成形品に成形する際に、繊維シート内部の空気がこの部分から抜ける通路となり、加圧により表面の樹脂が繊維シート内全体に含浸しやすくなる。これにより樹脂4は繊維強化樹脂成形体のマトリックス樹脂となる。 The following will be explained using drawings. In the drawings below, the same reference numerals indicate the same products. FIG. 1 is a schematic perspective view of the resin-integrated carbon fiber sheet 1 according to the embodiment of the present invention, and FIG. 2 is a schematic cross-sectional view of the resin-integrated carbon fiber sheet 1 in the width direction. Crosslinked fibers 3 are arranged in various directions on the surface of the opened carbon fiber sheet 2. Further, the resin 4 is melt-solidified and adhered to the vicinity of the surface of the carbon fiber sheet 2, and the resin 4 is not or partially impregnated inside the carbon fiber sheet 2. The resin 4 adheres and fixes the crosslinked fiber 3 to the surface of the carbon fiber sheet 2. As shown in FIG. 2, crosslinked fibers 3a and 3b are present on the surface of the carbon fiber sheet 2. The crosslinked fibers 3a are all on the surface of the carbon fiber sheet 2. A part of the crosslinked fiber 3b is on the surface of the carbon fiber sheet 2, and a part of the crosslinked fiber 3b is in a state of entering the inside and interlacing with the carbon fiber. The resin 4 adheres and fixes the crosslinked fiber 3 to the surface of the carbon fiber sheet 2. Further, there is a portion to which the resin 4 is attached and a portion 5 to which the resin is not attached. The portion 5 to which the resin does not adhere is a passage through which the air inside the fiber sheet escapes when the resin-integrated carbon fiber sheet 1 is heated and pressed in a laminated state to form a fiber-reinforced resin molded product. Therefore, the resin on the surface is easily impregnated in the entire fiber sheet by pressurization. As a result, the resin 4 becomes a matrix resin of the fiber-reinforced resin molded product.
 図3は本発明の一実施形態の樹脂一体化炭素繊維シートの製造方法を示す模式的工程図である。多数個の供給ボビン7から炭素繊維フィラメント群(トウ)8を引き出し、開繊ロール21a-21jの間を通過させることで、開繊させる(ロール開繊工程23)。ロール開繊に代えて、エアー開繊としてもよい。開繊ロールは固定又は回転してもよく、幅方向に振動してもよい。
 開繊工程の後、開繊されたトウをニップロール9a,9b間でニップし、この間に設置した複数のブリッジロール12a-12bの間を通過させ、トウの張力を例えば15,000本あたり(1個の供給ボビンから供給される炭素繊維フィラメント群に相当)2.5~30Nの範囲でかけることで、架橋繊維を発生させる(架橋繊維発生工程24)。ブリッジロールは回転してもよく、幅方向に振動してもよい。ブリッジロールは、例えば表面が梨地、凹凸、鏡面、複数ロールで炭素繊維フィラメント群を屈曲、固定、回転、振動又はこれらの組み合わせにより架橋繊維を発生させる。13a-13gはガイドロールである。
 その後、粉体供給ホッパー14からドライパウダー樹脂15を開繊シートの表面に振りかけ、圧力フリー状態で加熱装置16内に供給し加熱し、ドライパウダー樹脂15を溶融し、ガイドロール13f-13g間で冷却する。その後、開繊シートの裏面にも粉体供給ホッパー17からドライパウダー樹脂18を振りかけ、圧力フリー状態で加熱装置19内に供給し加熱し、ドライパウダー樹脂18を溶融し、冷却し、巻き上げロール20に巻き上げられる(粉体樹脂付与工程25)。ドライパウダー樹脂15、18は、例えばフェノキシ樹脂(ガラス転移点180℃)とし、加熱装置16,19内の各温度は例えば樹脂の融点又はガラス転移点の+20~60℃、滞留時間は例えば各4秒とする。これにより、炭素繊維開繊シートは幅方向の強度が高くなり、構成炭素繊維がバラバラになることはなく、シートとして扱えるようになる。
FIG. 3 is a schematic process diagram showing a method for producing a resin-integrated carbon fiber sheet according to an embodiment of the present invention. The carbon fiber filament group (toe) 8 is pulled out from a large number of supply bobbins 7 and passed between the opening rolls 21a-21j to open the fibers (roll opening step 23). Instead of roll opening, air opening may be used. The spread fiber roll may be fixed or rotated, or may vibrate in the width direction.
After the fiber-spreading step, the opened tow is nipated between the nip rolls 9a and 9b, passed between a plurality of bridge rolls 12a-12b installed between the nip rolls 9a and 9b, and the tension of the toe is applied per 15,000, for example (1). Cross-linked fibers are generated by applying in the range of 2.5 to 30 N (corresponding to the carbon fiber filament group supplied from each supply bobbin) (cross-linked fiber generation step 24). The bridge roll may rotate or oscillate in the width direction. The bridge roll has a satin finish, an uneven surface, a mirror surface, and a plurality of rolls, and the carbon fiber filament group is bent, fixed, rotated, vibrated, or a combination thereof to generate crosslinked fibers. 13a-13g is a guide roll.
After that, the dry powder resin 15 is sprinkled on the surface of the spread sheet from the powder supply hopper 14, supplied into the heating device 16 in a pressure-free state and heated to melt the dry powder resin 15, and between the guide rolls 13f-13g. Cooling. After that, the dry powder resin 18 is sprinkled on the back surface of the spread fiber sheet from the powder supply hopper 17, and the dry powder resin 18 is supplied into the heating device 19 in a pressure-free state and heated to melt the dry powder resin 18, cool it, and wind up the roll 20. (Powder resin applying step 25). The dry powder resins 15 and 18 are, for example, phenoxy resins (glass transition point 180 ° C.), the temperatures in the heating devices 16 and 19 are, for example, + 20 to 60 ° C. of the melting point or glass transition point of the resin, and the residence time is, for example, 4 each. Let it be seconds. As a result, the carbon fiber spread sheet has high strength in the width direction, and the constituent carbon fibers do not fall apart and can be handled as a sheet.
 粉体樹脂の付与は、粉体塗布法、静電塗装法、吹付法、流動浸漬法などが採用できる。炭素繊維シート表面に粉体樹脂を落下させる粉体塗布法が好ましい。例えばドライパウダー状の粉体樹脂を開繊された炭素繊維シートに振りかける。 Powder resin can be applied by powder coating method, electrostatic coating method, spraying method, fluid immersion method, etc. A powder coating method in which the powder resin is dropped on the surface of the carbon fiber sheet is preferable. For example, a dry powder-like powder resin is sprinkled on the opened carbon fiber sheet.
 図4Aは本発明の一実施形態で使用する2種類の樹脂一体化繊維シートの模式的斜視図、図4Bは同樹脂一体化繊維シートを積層する模式的説明図である。図4Aに示すように、樹脂一体化繊維シート30は一方向に配列する炭素繊維32と樹脂33で構成され、両表面層に配置する。樹脂一体化繊維シート31は一方向に配列する炭素繊維32と樹脂34で構成され、内層に配置する。樹脂一体化繊維シート30,31には図1~2に示す架橋繊維が存在するが、作図上省略している。図4Bに示すように、複数枚の樹脂一体化繊維シート31を内層とし、その両表面に樹脂一体化繊維シート30を配置し、全体を加圧加熱して積層一体化し、繊維強化樹脂成形体35とする。積層一体化する際の加圧力は0.2~10MPaが好ましく、温度は樹脂の融点又は流動開始温度の+20~60℃、時間は2~15分が好ましい。 FIG. 4A is a schematic perspective view of two types of resin integrated fiber sheets used in one embodiment of the present invention, and FIG. 4B is a schematic explanatory view of laminating the resin integrated fiber sheets. As shown in FIG. 4A, the resin integrated fiber sheet 30 is composed of carbon fibers 32 and resin 33 arranged in one direction, and is arranged on both surface layers. The resin-integrated fiber sheet 31 is composed of carbon fibers 32 and resin 34 arranged in one direction, and is arranged in the inner layer. The crosslinked fibers shown in FIGS. 1 and 2 are present in the resin-integrated fiber sheets 30 and 31, but are omitted in the drawing. As shown in FIG. 4B, a plurality of resin-integrated fiber sheets 31 are used as inner layers, resin-integrated fiber sheets 30 are arranged on both surfaces thereof, and the whole is pressurized and heated to be laminated and integrated to form a fiber-reinforced resin molded product. Let it be 35. The pressing force for laminating and integrating is preferably 0.2 to 10 MPa, the temperature is preferably + 20 to 60 ° C. of the melting point or flow start temperature of the resin, and the time is preferably 2 to 15 minutes.
 本発明の好ましい例をまとめると次のようになる。
(1)繊維強化樹脂成形体について
 繊維強化樹脂成形体は2層以上の積層構造である。繊維の方向性は問わないが、薄さを考慮すると一方向性のシートが好ましい。少なくとも一方の表面層側には機能性を付与したシートを積層することが好ましい。成形後の反り等を考慮すると、表裏面が同じ層が好ましい。すなわち、繊維強化樹脂成形体は、表面層(1~2層)/内層(N層)/裏面層(1~2層)であり、内層の枚数Nは1~100が好ましく、合計層数は3~102が好ましい。
(2)成形について
 成形方法は、プレス成形や真空成形等、一般的な圧縮成形方法が用いられる。これにより一体成形する。表面層と内層を別工程とすることは意味が無い。
(3)その他
 少なくとも一方の表面層には機能性を付与することが好ましい。機能性とは、接着性、印刷性、耐候性、耐水性、耐薬品性、塗装性、加工性、機能性、熱伝導性、難燃性、表面平滑性等である。積層させる樹脂一体化繊維シートの繊維体積率(Vf)を変更することもできる。とくに前記繊維強化樹脂成形体の表層に接着性を付与すると、金属、樹脂及びゴムから選ばれる少なくとも一つと一体化するのに有用である。
A preferred example of the present invention can be summarized as follows.
(1) Fiber-reinforced resin molded product The fiber-reinforced resin molded product has a laminated structure of two or more layers. The directionality of the fibers does not matter, but a unidirectional sheet is preferable in consideration of thinness. It is preferable to laminate a sheet with added functionality on at least one surface layer side. Considering warpage after molding, a layer having the same front and back surfaces is preferable. That is, the fiber-reinforced resin molded body is a front surface layer (1 to 2 layers) / inner layer (N layer) / back surface layer (1 to 2 layers), and the number N of inner layers is preferably 1 to 100, and the total number of layers is 3 to 102 is preferable.
(2) Molding As a molding method, a general compression molding method such as press molding or vacuum forming is used. As a result, it is integrally molded. It is meaningless to have the surface layer and the inner layer as separate processes.
(3) Others It is preferable to impart functionality to at least one surface layer. The functionality includes adhesiveness, printability, weather resistance, water resistance, chemical resistance, paintability, processability, functionality, thermal conductivity, flame retardancy, surface smoothness and the like. It is also possible to change the fiber volume fraction (Vf) of the resin-integrated fiber sheet to be laminated. In particular, imparting adhesiveness to the surface layer of the fiber-reinforced resin molded product is useful for integrating with at least one selected from metal, resin and rubber.
 以下実施例を用いて本発明を具体的に説明する。なお、本発明は下記の実施例に限定されるものではない。
 (実施例1)
(1)炭素繊維未開繊トウ
 炭素繊維未開繊トウは三菱ケミカル社製、品番:PYROFILE TR 50S15L、形状:レギュラートウ フィラメント15K(15,000本,)、単繊維直径7μmを使用した。この炭素繊維未開繊トウの炭素繊維にはエポキシ系化合物がサイジング剤として付着されている。
(2)未開繊トウの開繊手段
 図3の開繊手段を使用して開繊した。開繊工程において、炭素繊維フィラメント群(トウ)の張力は15,000本あたり15Nとした。このようにして炭素繊維フィラメント構成本数50K、開繊幅500mm、厚み0.08mmの開繊シートとした。架橋繊維は3.3質量%であった。目付量は80g/m2であった。
(3-1)セミプレグ1
 ドライパウダー樹脂としてフェノキシ樹脂(ガブリエル社製,ガラス転移点180℃)を使用した。ドライパウダー樹脂の平均粒子径は80μmであった。この樹脂は、炭素繊維1m2に対して平均片面26.2g、両面で52.4g付与した。加熱装置16,19内の温度は各220℃、滞留時間は各4秒とした。質量は132.4g/m2(樹脂:52.4g/m2、繊維:80g/m2)であった。
(3-2)セミプレグ2
 ドライパウダー樹脂としてPA12樹脂(ダイセルエボニック社製,融点176℃)を使用した。ドライパウダー樹脂の平均粒子径は80μmであった。この樹脂は、炭素繊維1m2に対して平均片面24.0g、両面で48.0g付与した。加熱装置16,19内の温度は各200℃、滞留時間は各4秒とした。質量は128.0g/m2(樹脂:48g/m2、繊維:80g/m2)であった。
(4)成形体の成形
 表裏面にセミプレグ2を1枚ずつ設置し、内層にセミプレグ1を10枚配置し、基材繊維方向は一方向とし、基材サイズはタテ250mm、ヨコ250mmとし、プレス成形は260℃、3MPaにて5分間プレスした。
Hereinafter, the present invention will be specifically described with reference to Examples. The present invention is not limited to the following examples.
(Example 1)
(1) Carbon fiber unopened fiber tow The carbon fiber unopened fiber tow was manufactured by Mitsubishi Chemical Corporation, product number: PYROFILE TR 50S15L, shape: regular tow filament 15K (15,000 fibers,), and a single fiber diameter of 7 μm was used. An epoxy compound is attached to the carbon fiber of the unopened carbon fiber tow as a sizing agent.
(2) Means for opening the unopened fiber tow The fibers were opened using the opening means shown in FIG. In the fiber opening step, the tension of the carbon fiber filament group (toe) was set to 15 N per 15,000 fibers. In this way, an spread sheet having a carbon fiber filament composition of 50 K, a spread width of 500 mm, and a thickness of 0.08 mm was obtained. The crosslinked fiber was 3.3% by mass. The basis weight was 80 g / m 2 .
(3-1) Semi-preg 1
A phenoxy resin (manufactured by Gabriel, glass transition point 180 ° C.) was used as the dry powder resin. The average particle size of the dry powder resin was 80 μm. An average of 26.2 g of this resin was applied to 1 m 2 of carbon fibers on one side and 52.4 g on both sides. The temperatures in the heating devices 16 and 19 were 220 ° C., and the residence time was 4 seconds each. Mass 132.4g / m 2 (resin: 52.4g / m 2, the fibers: 80g / m 2) was.
(3-2) Semi-preg 2
PA12 resin (manufactured by Daicel Evonik, melting point 176 ° C.) was used as the dry powder resin. The average particle size of the dry powder resin was 80 μm. An average of 24.0 g of this resin was applied to 1 m 2 of carbon fibers on one side and 48.0 g on both sides. The temperature in the heating devices 16 and 19 was 200 ° C., and the residence time was 4 seconds each. The mass was 128.0 g / m 2 (resin: 48 g / m 2 , fiber: 80 g / m 2 ).
(4) Molding of molded body One semi-preg 2 is installed on the front and back surfaces, 10 semi-pregs 1 are arranged in the inner layer, the base fiber direction is one direction, the base size is 250 mm in length and 250 mm in width, and a press is used. Molding was performed at 260 ° C. and 3 MPa for 5 minutes.
 (比較例1)
 樹脂一体化繊維シート(セミプレグ)として、全層とも実施例1のセミプレグ2を使用した以外は実施例1と同様に実験した。
(Comparative Example 1)
The same experiment as in Example 1 was carried out except that the semi-preg 2 of Example 1 was used for all layers as the resin-integrated fiber sheet (semi-preg).
 実施例1及び比較例1の成形品から長さ80mm(指定方向)、幅15mmにサンプルを切り出し、温度23℃、相対湿度50%で48時間以上静置した。実施例1品及び比較例1品それぞれにつき6サンプルずつ行った。得られた各サンプルのサイズを表1にまとめて示す。 A sample was cut out from the molded products of Example 1 and Comparative Example 1 to a length of 80 mm (designated direction) and a width of 15 mm, and allowed to stand at a temperature of 23 ° C. and a relative humidity of 50% for 48 hours or more. Six samples were taken for each of 1 product of Example and 1 product of Comparative Example. The sizes of the obtained samples are summarized in Table 1.
Figure JPOXMLDOC01-appb-T000001
Figure JPOXMLDOC01-appb-T000001
 次に、作製したサンプルをJIS K7074に準拠の3点曲げ試験を行った。条件は下記の通りであった。
・治具:圧子=R5、支点=R2
・下部支持間隔:60mm
・試験速度:5mm/min
・試験回数:6回
Next, the prepared sample was subjected to a three-point bending test in accordance with JIS K7074. The conditions were as follows.
・ Jig: Indenter = R5, fulcrum = R2
・ Lower support interval: 60 mm
・ Test speed: 5mm / min
・ Number of tests: 6 times
 3点曲げ試験の結果を表2及び図5~6に示す。図5は本発明の実施例1の応力-変位測定グラフ、図6は比較例1の応力-変位測定グラフである。図5~6の数値は測定順を示す。 The results of the 3-point bending test are shown in Table 2 and FIGS. 5 to 6. FIG. 5 is a stress-displacement measurement graph of Example 1 of the present invention, and FIG. 6 is a stress-displacement measurement graph of Comparative Example 1. The numerical values in FIGS. 5 to 6 indicate the measurement order.
Figure JPOXMLDOC01-appb-T000002
Figure JPOXMLDOC01-appb-T000002
 表2から明らかなとおり、実施例1の両表面層のマトリックス樹脂はPA12樹脂であることから、ゴムや金属に対して接着力が高いという機能性が付与され、全体としても実用的に十分な強度を有していた。 As is clear from Table 2, since the matrix resin of both surface layers of Example 1 is PA12 resin, it is imparted with the functionality of having high adhesive strength to rubber and metal, and is practically sufficient as a whole. It had strength.
 (実施例2)
(1)炭素繊維未開繊トウ
 炭素繊維未開繊トウは三菱ケミカル社製、品番:PYROFILE TR 50S15L、形状:レギュラートウ フィラメント15K(15,000本,)、単繊維直径7μmを使用した。この炭素繊維未開繊トウの炭素繊維にはエポキシ系化合物がサイジング剤として付着されている。
(2)未開繊トウの開繊手段
 図3の開繊手段を使用して開繊した。開繊工程において、炭素繊維フィラメント群(トウ)の張力は15,000本あたり15Nとした。このようにして炭素繊維フィラメント構成本数50K、開繊幅500mm、厚み0.08mmの開繊シートとした。架橋繊維は3.3質量%であった。目付量は80g/m2であった。
(3-1)セミプレグ3
 ドライパウダー樹脂としてポリカーボネート樹脂(帝人社製,融点240℃以下)を使用した。ドライパウダー樹脂の平均粒子径は180μm以下であった。この樹脂は、炭素繊維1m2に対して平均片面26.4g、両面で53g付与した。加熱装置16,19内の温度は各260℃、滞留時間は各4秒とした。質量は133g/m2(樹脂:53g/m2、繊維:80g/m2)であった。
(3-2)セミプレグ4
 ドライパウダー樹脂としてフェノキシ樹脂(ガブリエル社製,ガラス転移点180℃)を使用した。ドライパウダー樹脂の平均粒子径は80μmであった。この樹脂は、炭素繊維1m2に対して平均片面26.2g、両面で52.4g付与した。加熱装置16,19内の温度は各220℃、滞留時間は各4秒とした。質量は132.4g/m2(樹脂:52.4g/m2、繊維:80g/m2)であった。
(4)成形体の成形
 表裏面にセミプレグ4を1枚ずつ設置し、内層にセミプレグ3を10枚配置し、基材繊維方向は一方向とし、基材サイズはタテ250mm、ヨコ250mmとし、プレス成形は300℃、3MPaにて5分間プレスした。
(Example 2)
(1) Carbon fiber unopened fiber tow The carbon fiber unopened fiber tow was manufactured by Mitsubishi Chemical Corporation, product number: PYROFILE TR 50S15L, shape: regular tow filament 15K (15,000 fibers,), and a single fiber diameter of 7 μm was used. An epoxy compound is attached to the carbon fibers of the unopened carbon fiber tow as a sizing agent.
(2) Means for opening the unopened fiber tow The fibers were opened using the opening means shown in FIG. In the fiber opening step, the tension of the carbon fiber filament group (toe) was set to 15 N per 15,000 fibers. In this way, an spread sheet having a carbon fiber filament composition of 50 K, a spread width of 500 mm, and a thickness of 0.08 mm was obtained. The crosslinked fiber was 3.3% by mass. The basis weight was 80 g / m 2 .
(3-1) Semi-preg 3
A polycarbonate resin (manufactured by Teijin Limited, melting point 240 ° C. or less) was used as the dry powder resin. The average particle size of the dry powder resin was 180 μm or less. An average of 26.4 g of this resin was applied to 1 m 2 of carbon fibers on one side and 53 g on both sides. The temperatures in the heating devices 16 and 19 were 260 ° C., and the residence time was 4 seconds each. The mass was 133 g / m 2 (resin: 53 g / m 2 , fiber: 80 g / m 2 ).
(3-2) Semi-preg 4
A phenoxy resin (manufactured by Gabriel, glass transition point 180 ° C.) was used as the dry powder resin. The average particle size of the dry powder resin was 80 μm. An average of 26.2 g of this resin was applied to 1 m 2 of carbon fibers on one side and 52.4 g on both sides. The temperatures in the heating devices 16 and 19 were 220 ° C., and the residence time was 4 seconds each. Mass 132.4g / m 2 (resin: 52.4g / m 2, the fibers: 80g / m 2) was.
(4) Molding of molded body One semi-preg 4 is installed on the front and back surfaces, 10 semi-pregs 3 are arranged in the inner layer, the base fiber direction is one direction, the base size is 250 mm in length and 250 mm in width, and the press Molding was performed at 300 ° C. and 3 MPa for 5 minutes.
 (比較例2)
 樹脂一体化繊維シート(セミプレグ)として、全層とも実施例2のセミプレグ3を使用した以外は実施例2と同様に実験した。
(Comparative Example 2)
The same experiment as in Example 2 was carried out except that the semi-preg 3 of Example 2 was used for all layers as the resin-integrated fiber sheet (semi-preg).
 実施例2及び比較例2の成形品から長さ80mm(指定方向)、幅15mmにサンプルを切り出し、温度23℃、相対湿度50%で48時間以上静置した。実施例2品及び比較例2品それぞれにつき6サンプルずつ行った。得られた各サンプルのサイズを表3にまとめて示す。 A sample was cut out from the molded products of Example 2 and Comparative Example 2 to a length of 80 mm (designated direction) and a width of 15 mm, and allowed to stand at a temperature of 23 ° C. and a relative humidity of 50% for 48 hours or more. Six samples were taken for each of the two Examples and the two Comparative Examples. The sizes of the obtained samples are summarized in Table 3.
Figure JPOXMLDOC01-appb-T000003
Figure JPOXMLDOC01-appb-T000003
 次に、作製したサンプルをJIS K7074に準拠の3点曲げ試験を行った。条件は下記の通りであった。
・治具:圧子=R5、支点=R2
・下部支持間隔:60mm
・試験速度:5mm/min
・試験回数:6回
Next, the prepared sample was subjected to a three-point bending test in accordance with JIS K7074. The conditions were as follows.
・ Jig: Indenter = R5, fulcrum = R2
・ Lower support interval: 60 mm
・ Test speed: 5mm / min
・ Number of tests: 6 times
 3点曲げ試験の結果を表4及び図7~8に示す。図7は本発明の実施例2の応力-変位測定グラフ、図8は比較例2の応力-変位測定グラフである。図7~8の数値は測定順を示す。 The results of the 3-point bending test are shown in Table 4 and FIGS. 7 to 8. FIG. 7 is a stress-displacement measurement graph of Example 2 of the present invention, and FIG. 8 is a stress-displacement measurement graph of Comparative Example 2. The numerical values in FIGS. 7 to 8 indicate the measurement order.
Figure JPOXMLDOC01-appb-T000004
Figure JPOXMLDOC01-appb-T000004
 表4から明らかなとおり、実施例2の両表面層のマトリックス樹脂はフェノキシ樹脂であることから、耐湿性に優れた機能を付与でき、さらには実施例2と比較例2から曲げ弾性率及び曲げ強度は同等であり、実用的に十分な強度を有していた。 As is clear from Table 4, since the matrix resin of both surface layers of Example 2 is a phenoxy resin, it is possible to impart a function having excellent moisture resistance, and further, the flexural modulus and bending from Example 2 and Comparative Example 2 The strength was the same, and it had a practically sufficient strength.
 本発明の繊維強化樹脂成形体は、建築部材、ノートパソコンの筐体、ICトレイ、靴やスティックなどのスポーツ用品、風車、自動車、鉄道、船舶、航空、宇宙などの一般産業用途等において広く応用できる。 The fiber-reinforced resin molded product of the present invention is widely applied to building materials, laptop housings, IC trays, sporting goods such as shoes and sticks, and general industrial applications such as windmills, automobiles, railways, ships, aerospace, and the like. it can.
1 樹脂一体化炭素繊維シート
2 炭素繊維シート
3,3a,3b 架橋繊維
4 樹脂
5 樹脂が付着していない部分
6 開繊装置
7 供給ボビン
8 炭素繊維フィラメント群(炭素繊維未開繊トウ)
9a,9b ニップロール
12a-12b ブリッジロール
13a-13g ガイドロール
14,17 粉体供給ホッパー
15,18 ドライパウダー樹脂
16,19 加熱装置
20 巻き上げロール
21a-21j 開繊ロール
23 ロール開繊工程
24 架橋繊維発生工程
25 粉体樹脂付与工程
30,31 樹脂一体化繊維シート
32 炭素繊維
33,34 樹脂
35 繊維強化樹脂成形体
1 Resin-integrated carbon fiber sheet 2 Carbon fiber sheet 3,3a, 3b Cross-linked fiber 4 Resin 5 Part where resin is not attached 6 Fiber opening device 7 Supply bobbin 8 Carbon fiber filament group (carbon fiber unopened fiber toe)
9a, 9b Nip roll 12a-12b Bridge roll 13a- 13g Guide roll 14,17 Powder supply hopper 15, 18 Dry powder resin 16, 19 Heating device 20 Winding roll 21a-21j Spreading roll 23 Roll opening process 24 Cross-linked fiber generation Step 25 Powder resin applying step 30, 31 Resin integrated fiber sheet 32 Carbon fiber 33, 34 Resin 35 Fiber reinforced resin molded product

Claims (12)

  1.  連続繊維シート及び熱可塑性樹脂から構成される樹脂一体化繊維シートが複数枚積層された繊維強化樹脂成形体であって、
     前記繊維強化樹脂成形体は、2種類以上の樹脂一体化繊維シートが積層一体化されており、表面層と内層を含み、
     少なくとも一方の表面層の樹脂一体化繊維シートと、その他の樹脂一体化繊維シートとは異なることを特徴とする繊維強化樹脂成形体。
    A fiber-reinforced resin molded product in which a plurality of resin-integrated fiber sheets composed of a continuous fiber sheet and a thermoplastic resin are laminated.
    The fiber-reinforced resin molded body is formed by laminating and integrating two or more types of resin-integrated fiber sheets, and includes a surface layer and an inner layer.
    A fiber-reinforced resin molded product characterized in that the resin-integrated fiber sheet of at least one surface layer is different from the other resin-integrated fiber sheet.
  2.  前記繊維強化樹脂成形体は、両表面層の樹脂一体化繊維シートと、内層の樹脂一体化繊維シートとは異なる請求項1に記載の繊維強化樹脂成形体。 The fiber-reinforced resin molded body according to claim 1, which is different from the resin-integrated fiber sheet of both surface layers and the resin-integrated fiber sheet of the inner layer.
  3.  前記繊維強化樹脂成形体の厚みが0.1~5.0mmである請求項1又は2に記載の繊維強化樹脂成形体。 The fiber-reinforced resin molded product according to claim 1 or 2, wherein the thickness of the fiber-reinforced resin molded product is 0.1 to 5.0 mm.
  4.  前記樹脂は、ポリアミド系樹脂、ポリカーボネート系樹脂、ポリプロピレン系樹脂、ポリエステル系樹脂、ポリエチレン系樹脂、アクリル系樹脂、フェノキシ樹脂、ポリスチレン系樹脂、ポリイミド系樹脂、ポリエーテルエーテルケトン系樹脂、及びポリエーテルケトンケトン(PEKK)系樹脂から選ばれ、少なくとも一方の表面層の樹脂一体化繊維シートの樹脂と、その他の樹脂一体化繊維シートの樹脂は異なる請求項1~3のいずれかに記載の繊維強化樹脂成形体。 The resins include polyamide-based resin, polycarbonate-based resin, polypropylene-based resin, polyester-based resin, polyethylene-based resin, acrylic-based resin, phenoxy resin, polystyrene-based resin, polyimide-based resin, polyetheretherketone-based resin, and polyetherketone. The fiber-reinforced resin according to any one of claims 1 to 3, wherein the resin of the resin-integrated fiber sheet of at least one surface layer selected from the ketone (PEKK) -based resin and the resin of the other resin-integrated fiber sheet are different. Molded body.
  5.  前記連続繊維シートは、連続繊維群が開繊され一方向に並列状に配列された一方向連続繊維と、前記一方向連続繊維と交錯する方向に架橋繊維が存在し、前記架橋繊維は、前記熱可塑性樹脂により前記連続繊維シートに接着固定されている請求項1~4のいずれかに記載の繊維強化樹脂成形体。 The continuous fiber sheet includes unidirectional continuous fibers in which continuous fiber groups are opened and arranged in parallel in one direction, and crosslinked fibers in a direction intersecting the unidirectional continuous fibers. The fiber-reinforced resin molded body according to any one of claims 1 to 4, which is adhered and fixed to the continuous fiber sheet with a thermoplastic resin.
  6.  前記一方向連続繊維及び架橋繊維の合計を母数としたとき、前記架橋繊維は1~25質量%である請求項5に記載の繊維強化樹脂成形体。 The fiber-reinforced resin molded product according to claim 5, wherein the crosslinked fibers are 1 to 25% by mass when the total of the unidirectional continuous fibers and the crosslinked fibers is used as a population.
  7.  前記連続繊維シートは、織物である請求項1~6のいずれかに記載の繊維強化樹脂成形体。 The fiber-reinforced resin molded product according to any one of claims 1 to 6, wherein the continuous fiber sheet is a woven fabric.
  8.  前記連続繊維シートは、表面に熱可塑性樹脂粉体が付着され溶融したセミプレグである請求項1~6のいずれかに記載の繊維強化樹脂成形体。 The fiber-reinforced resin molded product according to any one of claims 1 to 6, wherein the continuous fiber sheet is a semi-preg in which thermoplastic resin powder is adhered to the surface and melted.
  9.  前記連続繊維シートは、樹脂を含浸したプリプレグである請求項1~7のいずれかに記載の繊維強化樹脂成形体。 The fiber-reinforced resin molded product according to any one of claims 1 to 7, wherein the continuous fiber sheet is a prepreg impregnated with a resin.
  10.  前記樹脂一体化繊維シートを100体積%としたとき、繊維30~70体積%、樹脂70~30体積%である請求項1~9のいずれかに記載の繊維強化樹脂成形体。 The fiber-reinforced resin molded product according to any one of claims 1 to 9, wherein the resin-integrated fiber sheet is 100% by volume, the fiber is 30 to 70% by volume, and the resin is 70 to 30% by volume.
  11.  前記樹脂は、前記繊維強化樹脂成形体のマトリックス樹脂となる樹脂である請求項1~10のいずれかに記載の繊維強化樹脂成形体。 The fiber-reinforced resin molded product according to any one of claims 1 to 10, wherein the resin is a resin that serves as a matrix resin for the fiber-reinforced resin molded product.
  12.  前記繊維強化樹脂成形体は、金属、樹脂及びゴムから選ばれる少なくとも一つと一体化するための繊維強化樹脂成形体である請求項1~11のいずれかに記載の繊維強化樹脂成形体。 The fiber-reinforced resin molded product according to any one of claims 1 to 11, wherein the fiber-reinforced resin molded product is a fiber-reinforced resin molded product for integrating with at least one selected from metal, resin, and rubber.
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JPH071625A (en) * 1993-06-16 1995-01-06 Asics Corp Hybrid frp laminate
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