WO2023190319A1 - 炭素繊維強化複合材料およびプリプレグ - Google Patents

炭素繊維強化複合材料およびプリプレグ Download PDF

Info

Publication number
WO2023190319A1
WO2023190319A1 PCT/JP2023/012166 JP2023012166W WO2023190319A1 WO 2023190319 A1 WO2023190319 A1 WO 2023190319A1 JP 2023012166 W JP2023012166 W JP 2023012166W WO 2023190319 A1 WO2023190319 A1 WO 2023190319A1
Authority
WO
WIPO (PCT)
Prior art keywords
carbon fiber
particles
prepreg
thermoplastic resin
conductive
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Ceased
Application number
PCT/JP2023/012166
Other languages
English (en)
French (fr)
Japanese (ja)
Inventor
隆一郎 平鍋
隆志 越智
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Toray Industries Inc
Original Assignee
Toray Industries Inc
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Toray Industries Inc filed Critical Toray Industries Inc
Priority to EP23780329.1A priority Critical patent/EP4488320A4/en
Priority to JP2023521748A priority patent/JPWO2023190319A1/ja
Priority to US18/850,303 priority patent/US20250215171A1/en
Publication of WO2023190319A1 publication Critical patent/WO2023190319A1/ja
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

Links

Images

Classifications

    • C—CHEMISTRY; METALLURGY
    • C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08J—WORKING-UP; GENERAL PROCESSES OF COMPOUNDING; AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F, C08G or C08H
    • C08J5/00—Manufacture of articles or shaped materials containing macromolecular substances
    • C08J5/24—Impregnating materials with prepolymers which can be polymerised in situ, e.g. manufacture of prepregs
    • C08J5/241—Impregnating materials with prepolymers which can be polymerised in situ, e.g. manufacture of prepregs using inorganic fibres
    • C08J5/243—Impregnating materials with prepolymers which can be polymerised in situ, e.g. manufacture of prepregs using inorganic fibres using carbon fibres
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B5/00—Layered 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
    • B32B5/02—Layered 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 characterised by structural features of a fibrous or filamentary layer
    • B32B5/024—Woven fabric
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B5/00—Layered 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
    • B32B5/22—Layered 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 characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed
    • B32B5/24—Layered 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 characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer
    • B32B5/26—Layered 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 characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer another layer next to it also being fibrous or filamentary
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B5/00—Layered 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
    • B32B5/22—Layered 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 characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed
    • B32B5/24—Layered 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 characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer
    • B32B5/26—Layered 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 characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer another layer next to it also being fibrous or filamentary
    • B32B5/262—Layered 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 characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer another layer next to it also being fibrous or filamentary characterised by one fibrous or filamentary layer being a woven fabric layer
    • C—CHEMISTRY; METALLURGY
    • C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08J—WORKING-UP; GENERAL PROCESSES OF COMPOUNDING; AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F, C08G or C08H
    • C08J5/00—Manufacture of articles or shaped materials containing macromolecular substances
    • C08J5/04—Reinforcing macromolecular compounds with loose or coherent fibrous material
    • C08J5/0405—Reinforcing macromolecular compounds with loose or coherent fibrous material with inorganic fibres
    • C08J5/042—Reinforcing macromolecular compounds with loose or coherent fibrous material with inorganic fibres with carbon fibres
    • C—CHEMISTRY; METALLURGY
    • C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08J—WORKING-UP; GENERAL PROCESSES OF COMPOUNDING; AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F, C08G or C08H
    • C08J5/00—Manufacture of articles or shaped materials containing macromolecular substances
    • C08J5/24—Impregnating materials with prepolymers which can be polymerised in situ, e.g. manufacture of prepregs
    • C08J5/249—Impregnating materials with prepolymers which can be polymerised in situ, e.g. manufacture of prepregs characterised by the additives used in the prepolymer mixture
    • C—CHEMISTRY; METALLURGY
    • C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08K—Use of inorganic or non-macromolecular organic substances as compounding ingredients
    • C08K3/00—Use of inorganic substances as compounding ingredients
    • C08K3/02—Elements
    • C08K3/04—Carbon
    • C—CHEMISTRY; METALLURGY
    • C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08K—Use of inorganic or non-macromolecular organic substances as compounding ingredients
    • C08K7/00—Use of ingredients characterised by shape
    • C08K7/02—Fibres or whiskers
    • C08K7/04—Fibres or whiskers inorganic
    • C08K7/06—Elements
    • C—CHEMISTRY; METALLURGY
    • C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08L—COMPOSITIONS OF MACROMOLECULAR COMPOUNDS
    • C08L63/00—Compositions of epoxy resins; Compositions of derivatives of epoxy resins
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2250/00—Layers arrangement
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2260/00—Layered product comprising an impregnated, embedded, or bonded layer wherein the layer comprises an impregnation, embedding, or binder material
    • B32B2260/02—Composition of the impregnated, bonded or embedded layer
    • B32B2260/021—Fibrous or filamentary layer
    • B32B2260/023—Two or more layers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2260/00—Layered product comprising an impregnated, embedded, or bonded layer wherein the layer comprises an impregnation, embedding, or binder material
    • B32B2260/04—Impregnation, embedding, or binder material
    • B32B2260/046—Synthetic resin
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
    • B32B2262/10—Inorganic fibres
    • B32B2262/106—Carbon fibres, e.g. graphite fibres
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2264/00—Composition or properties of particles which form a particulate layer or are present as additives
    • B32B2264/10—Inorganic particles
    • B32B2264/107—Ceramic
    • B32B2264/108—Carbon, e.g. graphite particles
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2264/00—Composition or properties of particles which form a particulate layer or are present as additives
    • B32B2264/30—Particles characterised by physical dimension
    • B32B2264/302—Average diameter in the range from 100 nm to 1000 nm
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2307/00—Properties of the layers or laminate
    • B32B2307/20—Properties of the layers or laminate having particular electrical or magnetic properties, e.g. piezoelectric
    • B32B2307/202—Conductive
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2307/00—Properties of the layers or laminate
    • B32B2307/50—Properties of the layers or laminate having particular mechanical properties
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2307/00—Properties of the layers or laminate
    • B32B2307/50—Properties of the layers or laminate having particular mechanical properties
    • B32B2307/54—Yield strength; Tensile strength
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2307/00—Properties of the layers or laminate
    • B32B2307/50—Properties of the layers or laminate having particular mechanical properties
    • B32B2307/558—Impact strength, toughness
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2307/00—Properties of the layers or laminate
    • B32B2307/70—Other properties
    • B32B2307/718—Weight, e.g. weight per square meter
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2307/00—Properties of the layers or laminate
    • B32B2307/70—Other properties
    • B32B2307/732—Dimensional properties
    • B32B2307/737—Dimensions, e.g. volume or area
    • B32B2307/7375—Linear, e.g. length, distance or width
    • B32B2307/7376—Thickness
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2605/00—Vehicles
    • B32B2605/18—Aircraft
    • C—CHEMISTRY; METALLURGY
    • C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08J—WORKING-UP; GENERAL PROCESSES OF COMPOUNDING; AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F, C08G or C08H
    • C08J2363/00—Characterised by the use of epoxy resins; Derivatives of epoxy resins
    • C—CHEMISTRY; METALLURGY
    • C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08J—WORKING-UP; GENERAL PROCESSES OF COMPOUNDING; AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F, C08G or C08H
    • C08J2363/00—Characterised by the use of epoxy resins; Derivatives of epoxy resins
    • C08J2363/02—Polyglycidyl ethers of bis-phenols
    • C—CHEMISTRY; METALLURGY
    • C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08J—WORKING-UP; GENERAL PROCESSES OF COMPOUNDING; AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F, C08G or C08H
    • C08J2477/00—Characterised by the use of polyamides obtained by reactions forming a carboxylic amide link in the main chain; Derivatives of such polymers
    • C08J2477/02—Polyamides derived from omega-amino carboxylic acids or from lactams thereof
    • C—CHEMISTRY; METALLURGY
    • C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08J—WORKING-UP; GENERAL PROCESSES OF COMPOUNDING; AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F, C08G or C08H
    • C08J2477/00—Characterised by the use of polyamides obtained by reactions forming a carboxylic amide link in the main chain; Derivatives of such polymers
    • C08J2477/04—Polyamides derived from alpha-amino carboxylic acids
    • C—CHEMISTRY; METALLURGY
    • C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08J—WORKING-UP; GENERAL PROCESSES OF COMPOUNDING; AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F, C08G or C08H
    • C08J2481/00—Characterised by the use of macromolecular compounds obtained by reactions forming in the main chain of the macromolecule a linkage containing sulfur with or without nitrogen, oxygen, or carbon only; Polysulfones; Derivatives of such polymers
    • C08J2481/06—Polysulfones; Polyethersulfones
    • C—CHEMISTRY; METALLURGY
    • C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08K—Use of inorganic or non-macromolecular organic substances as compounding ingredients
    • C08K2201/00—Specific properties of additives
    • C08K2201/001—Conductive additives
    • C—CHEMISTRY; METALLURGY
    • C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08K—Use of inorganic or non-macromolecular organic substances as compounding ingredients
    • C08K2201/00—Specific properties of additives
    • C08K2201/002—Physical properties
    • C08K2201/005—Additives being defined by their particle size in general
    • C—CHEMISTRY; METALLURGY
    • C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08K—Use of inorganic or non-macromolecular organic substances as compounding ingredients
    • C08K2201/00—Specific properties of additives
    • C08K2201/011—Nanostructured additives
    • C—CHEMISTRY; METALLURGY
    • C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08K—Use of inorganic or non-macromolecular organic substances as compounding ingredients
    • C08K2201/00—Specific properties of additives
    • C08K2201/016—Additives defined by their aspect ratio

Definitions

  • the present invention relates to a prepreg used to obtain a carbon fiber reinforced composite material, and a carbon fiber reinforced composite material using the prepreg.
  • Reinforced fibers such as carbon fiber and glass fiber are lightweight, yet have excellent mechanical properties such as tensile strength and compressive strength, heat resistance, and corrosion resistance. These reinforcing fibers are impregnated with thermosetting resins such as epoxy resins and phenolic resins to form prepregs, which are then molded and cured to produce carbon fiber reinforced composite materials (hereinafter sometimes referred to as CFRP). It has been applied in numerous fields such as automobiles, railway vehicles, ships, civil engineering and construction, and sporting goods. In particular, in applications that require high performance, fiber-reinforced composite materials using continuous reinforcing fibers are used. The reinforcing fibers are carbon fibers with excellent specific strength and specific modulus, and the matrix resin is thermosetting. Among these resins, epoxy resins are often used because of their excellent adhesion to carbon fibers.
  • thermosetting resins generally have low fracture toughness, so carbon fiber reinforced composite materials have poor impact resistance. Problems such as falling or being hit by hail during operation have arisen.
  • a thermosetting resin layer (hereinafter referred to as an interlayer) in which there are no carbon fibers sandwiched between the carbon fiber layers is an elastic body.
  • Impact resistance is improved by adding particles made of thermoplastic resin and deforming the particles made of thermoplastic resin when subjected to impact, and a carbon fiber reinforced composite made by curing the prepreg obtained by combining these.
  • the material is used in the aerospace field because of its excellent tensile strength, compressive strength, and impact resistance.
  • carbon fiber reinforced composite materials have reached a practical level in this way, carbon fiber reinforced composite materials have low conductivity in a specific direction, so metal mesh or foil is used in aircraft as a lightning protection measure. installed on the surface.
  • Carbon fiber itself has high conductivity, so when it is made into a carbon fiber reinforced composite material, it has high conductivity in the fiber axis direction, but matrix resin has low conductivity, so it does not have high conductivity in the fiber axis direction.
  • the electrical conductivity in the direction tends to be inferior to that of metals, and in particular, since there are almost no carbon fibers between the layers, it becomes an insulating layer, and the electrical conductivity in the thickness direction is low.
  • interlayer reinforcing particles particles made of thermoplastic resin
  • the thickness of the interlayer which is an insulating layer
  • the conductivity in the thickness direction is significantly reduced, which may cause current to stagnate. If the conductivity between the layers can be increased, the current can be dispersed even in the event of a lightning strike, making it possible to obtain a carbon fiber-reinforced composite material with lightning resistance.
  • the first method is to connect the layers by arranging a conductor having a long axis equal to or greater than the thickness between the layers between the layers.
  • Patent Document 1 describes a method of forming a conductive path by arranging conductive particles between layers with a difference in particle size of 10 ⁇ m or less relative to the thickness of the layers
  • Patent Document 2 discloses a method of forming conductive paths with a length of 1 mm. cites a method of forming conductive paths by arranging multi-walled carbon nanotubes between layers with a high aspect ratio of 15 nm in diameter and sufficiently long relative to the thickness between the layers.
  • the second method is to agglomerate nano-sized conductive filler and incorporate it into a resin, etc., form a lump larger than the thickness between the layers, and arrange and connect the layers between the layers, as described in Patent Document 3.
  • Patent Document 3 discloses a method in which a conductive paste containing silver nanofiller at a high concentration is placed between layers by screen printing to a size of approximately 50 ⁇ m
  • Patent Document 4 discloses a method in which conductive paste containing a high concentration of silver nanofiller is placed between layers with a length of 1.5 ⁇ m.
  • a method is mentioned in which carbon nanotubes with a diameter of 10 nm are kneaded into a thermoplastic resin by melt-kneading in a twin-screw extruder, and the resulting mass is made into a diameter of 90 ⁇ m or less and arranged between layers.
  • the third method is to arrange a conductor with a long axis equal to or greater than the interlayer thickness, as in the first method, and to increase the number of conductive paths between the conductor and the carbon fiber layer. be.
  • a conductive path was formed only from carbon fibers that were in direct contact with a conductor or conductive aggregate, but in the third method, a conductive path was formed only from carbon fibers that were in direct contact with a conductor or a conductive aggregate. The feature is that a conductive path is formed even with carbon fibers that are not in contact with each other.
  • Patent Document 5 discloses that carbon particles having a long axis equal to or greater than the interlayer thickness are arranged, and a conductive path between the carbon fiber layer and the carbon particles is increased by a carbon black aggregate having a structure with a structure size of about 400 nm.
  • a method is listed in Patent Document 6, in which a prepreg in which conductive particles having a long axis equivalent to the thickness between the layers are arranged is manufactured, and a bundle of carbon fiber layers is opened by passing the prepreg through an S-wrap roll.
  • One method is to increase the number of contacts between carbon fiber layers and carbon particles by utilizing the phenomenon in which carbon fibers move in the interlayer direction due to springback during curing.
  • a conductor having a major axis (length) equal to or greater than the interlayer thickness is used.
  • the interlayer thickness is determined by the size of thermoplastic resin particles that are insoluble in epoxy, and when imparting lightning resistance to prepreg, the long axis (length) is equal to or larger than the size of the thermoplastic resin particles. It is described that a conductor having the following properties is included.
  • an object of the present invention is to form a conductive path between the layers of a carbon fiber reinforced composite material using a conductive nanofiller, thereby achieving excellent high conductivity as well as high tensile strength and impact resistance. It is an object of the present invention to provide a carbon fiber composite material suitable as a structural material for an aircraft body, and a prepreg that is an intermediate base material for obtaining the carbon fiber composite material. In addition, the prepreg has excellent slit workability, which has been difficult with conventional conductive prepregs using conductive fine particles, and it is possible to obtain narrow prepregs that can be automatically laminated.
  • the present invention has the following configuration. That is, (1) Contains the following components [A], [BCDc], [Ec], and [Fc], and carbon fiber reinforcement in which carbon fiber layers in which carbon fiber [A] is impregnated with matrix resin [BCDc] are laminated.
  • Composite material in a cross section obtained by cutting in the thickness direction at an arbitrary position, the ratio of the major axis to the minor axis is 1.1 or more in 30% or more of the thermoplastic resin particles [Ec] based on the number of particles.
  • a carbon fiber reinforced composite material in which the structure size between carbon fiber layers of conductive nanofiller [Fc] is 0.6 ⁇ m or more.
  • the carbon fibers [A] are present as a bundle, have a basis weight of 250 g/m 2 or more, and have an interlayer thickness of 36 ⁇ m or more between the carbon fiber layers (1) to (3) )
  • Composite material (7)
  • [Gc] Conductive particles with an individual particle size of 1 ⁇ m or more (8) In a cross section obtained by cutting in the thickness direction at an arbitrary position, the conductive particles [Gc] are located between carbon fiber layers.
  • the respective contents (parts by mass) of the compound [Cp], the thermoplastic resin [Dp] composed of a polyarylether skeleton, and the thermoplastic resin particles [Ep] are W [Bp1] , W [Cp1] , and W [Dp1 ] , W [Ep1] , and the constituent elements in the secondary resin are epoxy resin [Bp], aromatic polyamine compound [Cp], thermoplastic resin [Dp] composed of a polyarylether skeleton, and thermoplastic resin particles.
  • thermoplastic resin particles [Ep] are mainly composed of a thermoplastic resin that is insoluble in epoxy resin, and the Tg of the [Ep] is less than 160°C, and the Tm of the [Ep] is less than 185°C or clearly A prepreg which does not exhibit a Tm and further has a D10 in the particle size distribution of [Ep] of 3 ⁇ m or more.
  • an epoxy resin [Bp], an aromatic polyamine compound [Cp], a thermoplastic resin [Dp] composed of a polyarylether skeleton, and a conductive nanofiller [Fp] A primary prepreg impregnated with a mixture of epoxy resin [Bp], an aromatic amine compound [Cp], a thermoplastic resin [Dp] composed of a polyarylether skeleton, and a thermoplastic resin on both sides of the primary prepreg.
  • [Bp], [Cp], [Dp], [Ep], [Fp] and [Gp] are constituent elements contained in the prepreg, and [BCDc], [Ec], [Fc] and [ Gc] is a component contained in the carbon fiber reinforced composite material.
  • FIG. 1 is a schematic cross-sectional view of a carbon fiber reinforced composite material according to the prior art, in which the interlayer thickness is maintained at a certain level or more by thermoplastic resin particles.
  • 1 is a schematic cross-sectional view of a carbon fiber reinforced composite material according to the prior art, in which the interlayer thickness is maintained at a certain level or more by thermoplastic resin particles.
  • 1 is a schematic cross-sectional view of a carbon fiber reinforced composite material according to the prior art, where the location indicated by X has a long distance as a conductive path.
  • FIG. 2 is a schematic cross-sectional view of the carbon fiber reinforced composite material of the present invention, in which a conductive path can be formed in all of Z1, Z2, and Z3.
  • FIG. 1 is a schematic cross-sectional view of a conventional carbon fiber reinforced composite material developed for the purpose of imparting lightning resistance, in which conductive paths between layers are formed by conductive particles having the same or greater interlayer thickness.
  • This is a schematic cross-sectional view of a conventional carbon fiber-reinforced composite material developed for the purpose of imparting lightning resistance, in which conductive paths between layers are formed using conductive fibers or nanotubes that are longer than the interlayer thickness.
  • FIG. 2 is a schematic diagram of a cross-sectional view of a CFRP according to the prior art, showing that particles with small diameters are disturbing and penetrating the carbon fiber layer.
  • Image of structure formation in masterbatch is a schematic cross-sectional view of a carbon fiber reinforced composite material of the present invention, in which conductive paths can be formed;
  • FIG. FIG. 2 is a schematic cross-sectional view of a carbon fiber reinforced composite material with a high basis weight produced by a conventional technique, in which there are locally thick parts between layers and parts where no conductive path is formed.
  • FIG. 2 is a schematic cross-sectional view of a carbon fiber reinforced composite material with a high basis weight produced by a conventional technique, in which there are locally thick parts between layers and parts where no conductive path is formed.
  • thermosetting resin that fixes the carbon fiber bundles
  • carbon fiber layer a layer made of a thermosetting resin that fixes the carbon fiber bundles
  • carbon fiber layer a layer made of a thermosetting resin that fixes the carbon fiber bundles
  • carbon fiber layer a layer made of a thermosetting resin that fixes the carbon fiber bundles
  • carbon fiber layer a layer made of a thermosetting resin that fixes the carbon fiber bundles
  • carbon fiber layer a layer of a thermosetting resin that fixes the carbon fiber bundles
  • Particles made of thermoplastic resin are included.
  • springback and compaction hereinafter referred to as spring
  • springback and compaction hereinafter referred to as spring
  • the technology of the present invention is useful, in which the thermoplastic resin particles insoluble in epoxy are crushed to have a specific aspect ratio and the thickness between the layers is reduced.
  • FIG. 1 is a schematic cross-sectional view of CFRP of Comparative Example 3, in which the thickness between the layers indicated by 3 in the figure is maintained at a certain level or more by the thermoplastic resin particles, and the thickness between the layers is locally maintained by the largest thermoplastic resin particles. The thickness is increased, and this becomes an insulating layer.
  • FIG. 2 is a schematic cross-sectional view of CFRP of Comparative Example 1 according to another embodiment, in which the interlayer thickness indicated by 3 in the figure is maintained at a certain level or more by the thermoplastic resin particles, and the largest thermoplastic resin particles Although the interlayer thickness locally increases to form an insulating layer as in FIG. 1, there are also some thermoplastic resin particles having a specific aspect ratio.
  • FIG. 3 is a schematic cross-sectional view of CFRP of Comparative Example 8 according to yet another form, in which the content of thermoplastic resin particles is reduced, but the location of X is long as a conductive path, and this is a localized It becomes an insulating layer.
  • FIG. 4 is a cross-sectional schematic diagram of the CFRP of the present invention, in which thermoplastic resin particles [Ec] having a specific aspect ratio have a thinner interlayer thickness 3 compared to FIGS. The thickness between the layers is uniform, and all of Z1, Z2, and Z3 can serve as conductive paths.
  • FIG. 5 is a schematic cross-sectional view of CFRP corresponding to the method, in which conductive particles 5 having a particle size equivalent to the thickness of the interlayer 3 are arranged to form a conductive path.
  • FIG. 6 is a schematic cross-sectional view of CFRP corresponding to this method, in which conductive fibers (including carbon nanotubes) 7 that are longer than the thickness between layers are arranged to form conductive paths.
  • FIG. 5 is a schematic cross-sectional view showing that a conductive path is formed between the two. This is common to the present invention in that a conductive path is formed by arranging a conductor with a thickness equal to or greater than the interlayer thickness to provide lightning resistance.
  • CFRP manufactured using prepreg with a high basis weight tends to have a large amount of thermoplastic resin particles per interlayer, and in that case, as shown in FIG.
  • the thickness between the layers expands locally, and there are places where it becomes difficult for the conductor to come into contact with each other, resulting in a much lower lightning resistance than expected simply from the amount of particles contained. found.
  • the present inventors thought that it is important to reduce the thickness between the layers and furthermore, not to create locally thick areas.
  • the thickness of the interlayer 3 largely depends on the particle size of the thermoplastic resin particles 2.
  • thermoplastic resin particles 2 with small particle sizes are simply arranged to reduce the thickness of the interlayer 3, as shown in FIG.
  • particles 8 with small particle diameters invaded the carbon fiber layer, and only CFRP could be obtained, which could result in lower impact resistance and tensile strength.
  • the present inventors have improved impact resistance compared to conventional CFRP by using thermoplastic resin particles present at a specific aspect ratio between carbon fiber layers in which carbon fibers are impregnated with matrix resin. It was possible to reduce the interlayer thickness while maintaining the same level as that of CFRP containing thermoplastic resin particles, and to eliminate locally thick areas.Furthermore, in order to increase the number of conductive paths, it was possible to reduce the interlayer thickness while maintaining the same level as that of CFRP containing thermoplastic resin particles. Considering that the size of the structure is important, we conducted extensive research and found that by mixing conductive nanofiller and epoxy and applying shear, we could obtain conductive nanofiller with a structure of a useful size. Ta.
  • the prepreg of the present invention essentially contains the following components.
  • thermoplastic resin particles [Ec] constituting the CFRP of the present invention have a ratio of the major axis to the minor axis in a cross section obtained by cutting in the thickness direction at an arbitrary position as shown in FIG. (aspect ratio) was observed to be 1.1 or more, and the interlayer thickness is thinner than that of CFRP using thermoplastic resin particles according to the prior art.
  • the aspect ratio is preferably 1.25 or more, and more preferably 1.4 or more.
  • this major axis has a direction parallel to the carbon fiber axis.
  • the aspect ratio here refers to the inner diameter of a particle that can be measured through the center of an arbitrarily selected thermoplastic resin particle [Ec] in a cross-sectional image obtained by cutting CFRP in the thickness direction at an arbitrary position.
  • the longest inner diameter is the major axis
  • the inner diameter of the thermoplastic resin particle [Ec] passing through the center of the thermoplastic resin particle [Ec] and perpendicular to the major axis determined above is the short axis, then the major axis ⁇ It is defined as the minor axis, and the individual aspect ratios of 100 particles are averaged as described later in Examples.
  • the aspect ratio is preferably less than 5, more preferably less than 2. Within this preferable range, impact resistance is excellent.
  • the CFRP according to the present invention has high impact resistance by containing thermoplastic resin particles [Ec], and the thickness between the layers can be reduced, so that a conductive path can be formed between the upper and lower carbon fibers, and the tensile strength is Lightning resistance can be improved while maintaining impact resistance.
  • the CFRP of the present invention has thermoplastic resin particles [Ec] in the interlayer 3 of the carbon fiber layers when the basis weight of the carbon fiber [A] is 200 g/m 2 (hereinafter sometimes referred to as gsm) or less. However, it has the characteristic of being thin in the thickness direction.
  • Conventional prepregs are often designed with carbon fiber [A] having a basis weight of around 130 g/m 2 or 190 g/m 2 , and conventionally, thermoplastic resin particles "Ep" with a smaller particle size than the conductor have been used. This allows the conductor to come into contact with the upper and lower carbon fibers [A].
  • the average interlayer thickness of conventional conductive CFRP is 31 to 40 ⁇ m, and this thickness is caused by the particle sizes of the thermoplastic resin particles and the large conductive particles.
  • thermoplastic resin particles have variations in particle size. For example, even particles with an average particle size of about 20 ⁇ m contain a few percent of particles with an individual particle size of 40 ⁇ m or more. Since the thermoplastic resin particles and the conductive particles increase the thickness between the layers, the average thickness between the layers was 31 ⁇ m or more.
  • the thickness of the interlayer 3 of the carbon fiber layer is preferably 30 ⁇ m or less, more preferably less than 20 ⁇ m, and even more preferably less than 12 ⁇ m.
  • thermoplastic resin particles [Ec] having an aspect ratio by crushing individual thermoplastic resin particles having a large particle size during springback, tensile strength and impact resistance can be maintained.
  • the lower limit of the thickness is preferably 3 ⁇ m or more, more preferably 5 ⁇ m or more, and 8 ⁇ m can improve impact resistance.
  • CFRP containing thermoplastic resin particles [Ec] having the aspect ratio of the present invention is more useful when the carbon fiber [A] has a large basis weight as described above.
  • studies have been underway to make CFRP by curing prepregs with a large basis weight of carbon fiber [A] of 250 g/ m2 or more and laminated a small number of times.
  • thermoplastic resin particles [Ep] contained in each interlayer is large, thermoplastic resin particles [Ep] as shown in Figure 11 It was found that multiple layers overlapped in the thickness direction and the interlayers were locally widened, and because the conductor could not connect the upper and lower carbon fibers [A] in the locally widened part, current was likely to stagnate there. I thought so. This problem cannot be solved simply by reducing the particle size of the thermoplastic resin particles [Ep] because the overlap between the particles cannot be controlled, but the CFRP of the present invention spreads locally as shown in Figure 10.
  • thermoplastic resin particles [Ep] are crushed during springback and become thermoplastic resin particles [Ec] with an aspect ratio, allowing the interlayers to have a uniform thickness as designed and forming a conductive path.
  • High lightning resistance can be obtained.
  • thermoplastic resin particles [Ec] contained between one layer is too large, the conductivity in the thickness direction between the layers decreases. It was found that this was because the layers were too dense and the aspect ratio did not reach 1.1 or more, resulting in locally thick areas between the layers, making it impossible to achieve uniformity.
  • the amount of [Ep] contained in the prepreg should be designed so that the amount of thermoplastic resin particles [Ec] contained in one interlayer when it becomes CFRP is below a certain level.
  • the calculation formula for determining the amount of thermoplastic resin particles [Ec] contained between one layer is hereinafter referred to as Formula (1), and a specific example will be described later.
  • the CFRP of the present invention has high lightning resistance even when the carbon fiber [A] has a basis weight of 250 g/m2 or more and a large amount of thermoplastic resin particles [Ec] are included between each layer and the interlayer is thick. It is characterized by having gender.
  • the average thickness between layers that can produce the effects of the present invention is preferably 36 ⁇ m or more, more preferably 41 ⁇ m or more, and even more preferably 45 ⁇ m or more.
  • the upper limit of the average interlayer thickness is preferably 70 ⁇ m or less, more preferably less than 60 ⁇ m, and even more preferably less than 55 ⁇ m. With this preferable upper limit, it becomes easy to form a conductive path.
  • thermoplastic resin particles [Ec] can be made to have the above-mentioned aspect ratio by being crushed so that the thickness of the carbon fiber layer and the interlayer becomes uniform during curing, but the value of the aspect ratio usually varies from particle to particle. have Specifically, when the aspect ratios of 100 particles are measured and the aspect ratio values are arranged in ascending order, the top 30 particles have the above-mentioned aspect ratios. Further, although not particularly limited, the lowest ten aspect ratios may be 1.05 or more and less than 1.1.
  • the range in which the thickness of the carbon fiber layer and the interlayers can be said to be uniform is preferably 85% or more of the average thickness of the carbon fiber layer, more preferably 95% or more, and 97% or more of the average thickness of the carbon fiber layer. It is even more preferable.
  • the maximum thickness is preferably 130% or less, more preferably less than 110%, and even more preferably less than 105%.
  • the carbon fiber layers and the interlayers are adjacent to each other, and if the thickness of the carbon fiber layer is uniform, it can be said that the thickness between the layers is also uniform. Therefore, in order to judge uniformity, either layer may be measured, but carbon fiber layers are usually stacked with the carbon fiber axes in different directions between the layers, such as carbon fibers in the 0 degree direction. Since it is difficult to determine the uniformity of the carbon fiber layer in the +45 degree or -45 degree direction, it is preferable to judge the uniformity.
  • Prepreg is made by pressing and impregnating a thermosetting resin into a carbon fiber bundle.
  • the viscosity of the thermosetting resin decreases, causing the carbon fiber bundle to shrink in the thickness direction.
  • the epoxy resin on the surface of the prepreg moves to the adjacent carbon fiber layer, causing so-called springback.
  • the carbon fiber [A] comes into contact with the structure of the conductive nanofiller [Fp] present on the surface of the prepreg to form a conductive path.
  • the interlayers in CFRP become thinner.
  • the interlayer thickness in CFRP is determined by this springback, and we conceived of using this springback to form the shape of the thermoplastic resin particles [Ec] that constitute the CFRP of the present invention.
  • thermoplastic resin particles [Ep] whose particle size is large enough not to penetrate into the carbon fiber layer are placed between the layers, so that when the interlayer becomes thinner due to springback, the thermoplastic resin particles [Ep] are crushed in the thickness direction.
  • the thermoplastic resin particles can be arranged between the layers without penetrating into the carbon fiber layer, and the thickness between the layers can be made thinner than that of conventional CFRP in which thermoplastic resin particles are inserted, making it easier to form conductive paths. Becomes a form. Therefore, it is preferable to control the particle size and blending amount of the thermoplastic resin particles [Ep] so as to secure a space for the easily crushed thermoplastic resin particles [Ep].
  • thermoplastic resin particles [Ec] constituting the CFRP of the present invention have impact resistance because they exist independently in the matrix resin [BCDc]. Existing independently here means that when observing a cross section of CFRP with a scanning electron microscope or digital microscope, an interface can be observed between the thermoplastic resin particles [Ec] and the matrix resin [BCDc]. , defined as something that can be determined to be a particle.
  • the shape of the thermoplastic resin particles [Ec] includes not only circular shapes but also those with other shapes and those with deformation when observed in cross section. Further, a part of the matrix resin [BCDc] may intrude into the thermoplastic resin particles [Ec], but if the interface can be observed, it is included as an independent thermoplastic resin particle [Ec].
  • thermoplastic resin particles [Ep] are dissolved in the epoxy resin [Bp] at a stage before the resin composition is cured. It is preferable to select thermoplastic resin particles [Ep] that do not dissolve in Bp].
  • thermoplastic resin particles [Ep] thermoplastic resin particles that are candidates for thermoplastic resin particles [Ep] are mixed with epoxy resin [Bp], heated at about 150 ° C., and observed under a microscope. It is preferable to select thermoplastic resin particles [Ep] that do not substantially shrink from their original size and that allow an interface between them and the epoxy resin [Bp] to be observed.
  • thermoplastic resin particles [Ep] exhibit a melting point (hereinafter referred to as Tm), it is preferably 130° C. or higher, since they may not exist independently by being melted and mixed by heat.
  • the temperature is more preferably 140°C or higher, and even more preferably 150°C or higher.
  • Tg glass transition temperature
  • thermoplastic resin particles [Ep] constituting the prepreg of the present invention are so-called interlayer reinforcement particles, and are mainly composed of components insoluble in the epoxy resin [Bp] and aromatic polyamine compound [Cp], and are used to form the prepreg. Even after forming thermoplastic resin particles [Ec] into CFRP by heating and pressurizing, it maintains a predetermined shape, but unlike the shape of thermoplastic resin particles [Ep] before forming, it usually It is shaped like this.
  • the thermoplastic resin particles [Ep] must have a Tg of less than 160°C, more preferably 150°C or less, and even more preferably 140°C or less.
  • thermoplastic resin particles [Ep] when exhibiting Tm, it needs to be less than 185°C, more preferably less than 177°C, and even more preferably less than 174°C. That is fine as long as it does not show a clear Tm.
  • the thermoplastic resin particles [Ep] will be maintained at a higher temperature than the temperature at which the thermoplastic resin particles [Ep] deform during the springback that occurs during heating to cure the prepreg, and the thermoplastic resin particles [Ep] A phenomenon occurs in which the particles are crushed by the springback pressure and become thermoplastic resin particles [Ec].
  • the thermoplastic resin particles [Ec] have a specific aspect ratio, and the interlayer thickness between the carbon fiber layers becomes thin.
  • CFRP for the aerospace field is cured at 170°C to 190°C, which is the normal curing temperature when manufacturing CFRP, if Tg and Tm are within the above range, the thermoplastic resin particles will be cured in the thickness direction of the CFRP.
  • the thickness between the carbon fiber layers can be reduced.
  • materials for particles having such characteristics polyamide 12, polyamide 6/12 copolymer, and grillamide are preferable. More preferred are polyamides (semi-IPN polyamides) having an interstitial network structure.
  • thermoplastic resin particles [Ep] constituting the prepreg of the present invention examples include amorphous, spherical, porous, acicular, whisker-like, and flake-like.
  • it is impregnated into carbon fibers so as not to reduce the flow characteristics of the epoxy resin [Bp], aromatic polyamine compound [Cp], or thermoplastic resin [Dp] composed of a polyarylether skeleton when curing into CFRP.
  • It has excellent properties and can suppress the intrusion of thermoplastic resin particles [Ep] itself into the carbon fiber layer, which prevents defects such as voids and carbon fiber alignment caused by thermoplastic resin particles [Ep] that have penetrated into the carbon fiber layer. This is preferable because it does not cause any deterioration in mechanical properties due to disturbances.
  • Such spherical thermoplastic resin particles [Ep] can become thermoplastic resin particles [Ec] having a specific aspect ratio as described above in the CFRP manufacturing process.
  • thermoplastic resin particles [Ec] constituting the CFRP of the present invention are determined by measuring the total area of the thermoplastic resin particle [Ec] cross sections observed in the cross section of the CFRP obtained by cutting the CFRP at an arbitrary position in the thickness direction. It is preferable that 80 area % or more exists in the resin composition in the interlayer 3 of the carbon fiber layer, more preferably 90 area % or more, and 95 area % or more. is even more preferable.
  • the impact resistance is improved by disposing the thermoplastic resin particles [Ec] in the interlayer 3.
  • thermoplastic resin particles [Ec] enter the inside of the carbon fiber layer the arrangement of the carbon fibers becomes disordered, causing a decrease in tensile strength, impact resistance, and lightning resistance of the carbon fiber layer.
  • thermoplastic resin particles [Ep] are present near the surface.
  • thermoplastic resin particles [Ec] it becomes difficult for the carbon fibers to come into contact with each other near the thermoplastic resin particles [Ec], making it easier for current to stagnate. As a result, the conductivity of the carbon fiber layer decreases.
  • thermoplastic resin particles [Ec] when a large amount of thermoplastic resin particles [Ec] are contained between the layers, it becomes difficult to form a conductive path between the carbon fibers above and below the interlayer, resulting in a decrease in interlayer conductivity.
  • thermoplastic resin particles [Ec] In terms of lightning resistance, it is better to include more thermoplastic resin particles [Ec] in the carbon fiber layer, whichever is easier to maintain lightning resistance between the layers. Slitting of prepreg is difficult because prepreg has poor slitting properties, and CFRP containing thermoplastic resin particles [Ec] in the carbon fiber layer may have reduced tensile strength and impact resistance. In this case, it is preferable to use a prepreg designed so that the thermoplastic resin particles [Ec] are present between the layers, and for this purpose, the thermoplastic resin particles [Ep] are present on the surface.
  • the content of the thermoplastic resin particles [Ep] used in the prepreg of the present invention is preferably 1 part by mass or more, more preferably 2 parts by mass or more based on 100 parts by mass of the epoxy resin [Bp]. , more preferably 3 parts by mass or more. Within this range, impact resistance can be improved.
  • the amount is preferably less than 10 parts by mass, more preferably less than 7 parts by mass, and even more preferably less than 5 parts by mass.
  • the thermoplastic resin particles [Ep] are preferably present near the surface of the prepreg, and specifically, preferably 20% from the surface of the prepreg with respect to 100% of the thickness of the prepreg. %, more preferably up to 10%.
  • the proportion of particles existing in the above depth range is preferably 85 area % or more with respect to the total amount of particles, and 92 area % or more, and even more preferably 97 area % or more. To determine whether the particles are within this range, observe the cross section of the CFRP after hardening it so that the particles do not move, and then take the total area of all observable particles as 100 area%, the total of particles existing up to the above depth. It can be judged based on the area ratio.
  • Thermoplastic resin particles [Ec] can maintain high tensile strength, impact resistance, and lightning resistance of the carbon fiber layer by arranging many of them only between the layers, so it is important to prevent them from penetrating inside the carbon fiber layer as much as possible.
  • thermoplastic resin particles [Ep] and conductive particles [Gp] which will be described later, each having an individual particle size of primary particles of 1 ⁇ m or more in the prepreg stage near the surface.
  • heat is applied to impregnate a bundle of carbon fibers [A] with a thermoplastic resin [Dp] composed of an epoxy resin [Bp], an aromatic polyamine compound [Cp], and a polyarylether skeleton.
  • thermoplastic resin particles [Ep] and conductive particles [Gp] When pressed, a portion of the thermoplastic resin particles [Ep] and conductive particles [Gp] become a thermoplastic resin [Bp] composed of an epoxy resin [Bp], an aromatic polyamine compound [Cp], and a polyarylether skeleton. Dp], as shown in FIG. 7, the arrangement will be disturbed along the way. This disorder remains even when the prepreg is cured to form CFRP, which is not preferable. Furthermore, as will be described later, prepregs in which conductive particles [Gp] or conductive nanofillers [Fp] are present in the carbon fiber layer also have poor slit workability.
  • thermoplastic resin particles [Ep] As a means for arranging the thermoplastic resin particles [Ep] near the surface, it is possible to control the range of D10 in the particle size distribution of the thermoplastic resin particles [Ep] and the conductive nanofiller [Fp], and to arrange the thermoplastic resin particles [Ep] in the vicinity of the surface.
  • One example is the use of a two-stage impregnation hot melt method, which will be described later.
  • D10 in the particle size distribution of the thermoplastic resin particles [Ep] is It is preferably 3 ⁇ m or more, preferably 6 ⁇ m or more, and even more preferably 10 ⁇ m or more.
  • D10 in the particle size distribution is within the above range, it is possible to suppress particles from entering the spaces between bundles of carbon fibers [A] during the manufacturing stage of prepreg obtained using general carbon fibers, so that particles can be prevented from entering into the prepreg. It can be present within a range of 20% depth from the surface.
  • Particles generally have a particle size distribution, and even if the average particle size is large, it may contain many small particles, so it is preferable that D10 in the particle size distribution is within the above range.
  • the particles have the effect of improving impact resistance when made into CFRP, and it is preferable to leave room for deformation when subjected to impact. For example, if particles of 30 ⁇ m are crushed to 10 ⁇ m during springback, there is little room for deformation in the crushed state, and the amount of impact that can be absorbed decreases, which tends to lower impact resistance. Therefore, D90 in the volume average particle size distribution is preferably 50 ⁇ m or less, more preferably less than 30 ⁇ m.
  • D10 and D90 in the particle size distribution refer to the particle diameter when the cumulative frequency of individual particle sizes on a volume basis is 10% and 90%, respectively, and D50 in the particle size distribution described below is: This is the particle size when the cumulative frequency is 50%. Further, D10, D50, and D90 in the particle size distribution are calculated only for particles with individual particle diameters of 1 ⁇ m or more. Particles with a particle size of less than 1 ⁇ m are excluded because they do not disturb the arrangement of carbon fibers, but among these, particles with an individual particle size of less than 1 ⁇ m are defined as nanofillers in the present invention and will be described later.
  • the method for producing the prepreg of the present invention is not particularly limited, but preferably a hot melt method.
  • the hot melt method is a method in which the viscosity is lowered by heating and impregnated into reinforcing fibers without using a solvent.
  • the prepreg of the present invention may be produced by a hot melt method, such as a single-stage impregnation hot-melt method, a multi-stage impregnation hot-melt method, etc.;
  • a hot melt method such as a single-stage impregnation hot-melt method, a multi-stage impregnation hot-melt method, etc.
  • the particles easily penetrate into the carbon fiber layer compared to the multi-stage impregnation hot melt method, so it is better to manufacture with this manufacturing method which uses thermoplastic resin particles [Ep] that have a D10 in the above range and are crushed during springback. Effective.
  • the one-stage impregnation hot melt method refers to the constituent elements of the present invention, such as epoxy resin [Bp], aromatic polyamine compound [Cp], thermoplastic resin [Dp] composed of a polyarylether skeleton, and thermoplastic resin particles [ Ep] and conductive nanofiller [Fp], and if necessary, conductive particles of 1 ⁇ m or more [Gp], etc., are heated and pressed from both sides or one side of the carbon fiber [A]. This is a one-step impregnation method.
  • the conductor that penetrates into the carbon fiber layer becomes a starting point for cracks, which tends to reduce tensile strength and impact resistance.
  • the present invention controls the D10 of the thermoplastic resin particles so that they do not invade the carbon fiber layer, and the thermoplastic resin particles are crushed by springback during pressurization and heating to adjust the interlayer thickness.
  • the manufacturing method can be said to be a more useful method even when a one-stage impregnation hot melt method is used.
  • the CFRP of the present invention In order for the CFRP of the present invention to have high lightning resistance, it is necessary to form a conductive path in the thickness direction between the layers, and it is important to control the thickness between the layers. For this purpose, it is preferable to determine the blending amount per interlayer so as to secure a space for the thermoplastic resin particles [Ep] having a large individual particle size to collapse during springback.
  • the content can be determined by the thermoplastic resin particle [Ec] content relative to the matrix resin [BCDc] content, but for each interlayer, as the basis weight of the carbon fiber [A] layer increases, the number of interlayers increases.
  • the content (fabric weight) of carbon fiber [A] is added to the calculation formula. Therefore, in the prepreg design for the CFRP of the present invention, the content (fabric weight) of the carbon fiber [A], which is a component, is W [A] , and the epoxy component, which is a component in the resin for the primary prepreg, is set to W [A].
  • thermoplastic resin [Dp] composed of a polyarylether skeleton
  • thermoplastic resin particles [Ep] are W [Bp1] , W [Cp1] , W [Dp1] , W [Ep1] are composed of epoxy resin [Bp], aromatic polyamine compound [Cp], and polyarylether skeleton, which are constituent elements in the resin film for secondary prepreg.
  • thermoplastic resin [Dp] and thermoplastic resin particles [Ep] are respectively W [Bp2] , W [Cp2], W [Dp2] , and W [Ep2] .
  • conductive particles [Gp] with an individual particle size of 1 ⁇ m or more and inorganic particles such as flame retardants may be included in the prepreg.
  • inorganic particles such as Gp] or flame retardants.
  • the value of formula (1) is preferably less than 60, more preferably less than 45, and even more preferably less than 30. On the other hand, from the viewpoint of maintaining the post-impact compression ratio within an excellent range, the value of formula (1) is preferably 5 or more, more preferably 10 or more, and even more preferably 20 or more.
  • the multi-stage impregnation hot melt method is a method in which the raw material that will become the matrix resin is divided into multiple stages and impregnated by heating and pressurizing the carbon fiber [A], which is a constituent element, from both sides or one side.
  • the multi-stage impregnation hot-melt method a prepreg in which different types of matrix resins are laminated can be manufactured by performing multi-stage hot melting, but the more the number of laminations, the higher the manufacturing cost. Therefore, when considering both the lamination of multiple types of resin and the manufacturing cost, the raw material that will become the matrix resin is divided into two stages, and the carbon fiber [A] that is the component is heated and pressurized from both sides or one side.
  • a more preferred method is the so-called two-stage impregnation hot melt method.
  • the constituent elements of the primary prepreg resin are epoxy resin [Bp], aromatic polyamine compound [Cp], thermoplastic resin [Dp] composed of a polyarylether skeleton, and, if necessary, a prepreg precursor (hereinafter referred to as primary prepreg) in which carbon fiber [A], which is a component, is impregnated from both sides or one side with a primary resin film made of conductive nanofiller [Fp].
  • the constituent elements of the resin for secondary prepreg are epoxy resin [Bp], aromatic polyamine compound [Cp], thermoplastic resin [Dp] composed of a polyarylether skeleton, and thermoplastic resin particles [Ep]. It is more preferable to obtain a prepreg by attaching a resin film for a secondary prepreg containing a conductive nanofiller [Fp] and a conductive nanofiller [Fp] to both sides or one side of the prepreg precursor.
  • the primary resin film is made to have a relatively low viscosity so that it can be easily impregnated into the carbon fiber bundle, and thermoplastic resin particles [Ep] and conductive particles of 1 ⁇ m or more [Gp], which are the constituent elements of the resin for the primary prepreg, are added.
  • thermoplastic resin particles [Ep] and conductive particles of 1 ⁇ m or more [Gp] which are the constituent elements of the resin for the primary prepreg
  • thermoplastic resin particles [Ep] and conductive particles [Gp] of 1 ⁇ m or more are arranged only on the surface.
  • the content of each component contained in the raw material included in the resin for the primary prepreg and the resin for the secondary prepreg is the content in the resin for the primary prepreg, or the content in the resin for the secondary prepreg.
  • the respective contents (parts by mass) of resin [Dp] and thermoplastic resin particles [Ep] are expressed as W[Bp1], W[Cp1], W[Dp1], and W[Ep1], respectively.
  • thermoplastic resin particles [Ep] are respectively written as W[Bp2], W[Cp2], W[Dp2], and W[Ep2].
  • the viscosity of the resin composition impregnated into the carbon fiber bundle is preferably 0.1 Pa ⁇ s or more and 100 Pa ⁇ s or less at 50°C.
  • the viscosity of the resin composition to be impregnated here refers to the viscosity of the resin composition corresponding to the primary resin in the case of a multi-stage impregnation hot melt method including two-stage impregnation.
  • the viscosity of the resin composition to be impregnated into the carbon fiber bundle to preferably 100 Pa ⁇ s or less, more preferably less than 50 Pa ⁇ s, and even less than 10 Pa ⁇ s, the carbon fibers can be transported in a prepreg state. It is possible to obtain a prepreg in which the arrangement of the bundles is not disordered and furthermore, when it is made into CFRP, the generation of voids can be suppressed.
  • the CFRP of the present invention has thermoplastic resin particles [Ec] in the interlayer 3, it has a thin aspect ratio in the thickness direction.
  • the thickness of the interlayer 3 is preferably 30 ⁇ m or less, more preferably less than 20 ⁇ m, and even more preferably less than 12 ⁇ m. With this thickness range, it is relatively easy to form a conductive path with just the conductive nanofiller, and it maintains higher conductivity and tensile strength than when using a conductor with a large diameter. Can be done.
  • the lower limit of the thickness is preferably 3 ⁇ m or more, more preferably 5 ⁇ m or more, and even more preferably 8 ⁇ m or more. When the thickness is greater than this, it can be said that the thermoplastic resin particles [Ec] exist without being dissolved, and the impact resistance can be increased.
  • the CFRP of the present invention is characterized in that a conductive path is formed between the carbon fibers above and below the interlayer by conductive nanofiller [Fc].
  • Conductive nanofiller [Fc] forms a structure in resin films and prepregs, and when they become CFRP, the structures are further connected in multiple pieces (hereinafter, a structure in which multiple structures are connected is referred to as an aggregate). ). This is thought to be because when the prepreg flows together with the epoxy during curing, the structure collides with the carbon fibers and collects there. In order to form a conductive path between the carbon fiber layers above and below the interlayer, it is preferable to increase the structure size per one.
  • the structure of conductive nanofillers [Fc] and [Fp] between the layers is preferably increased. It is important that the size is 0.6 ⁇ m or more, preferably 0.8 ⁇ m or more, and more preferably 1.1 ⁇ m or more. The large size of the structure makes it easier to aggregate and connect to form conductive paths, improving lightning resistance.
  • the structure size of the conductive nanofillers [Fc] and [Fp] is preferably less than 10 ⁇ m, more preferably less than 5 ⁇ m, and even more preferably less than 3 ⁇ m. Within this preferable range, the structure of the conductive nanofillers [Fc] and [Fp] is unlikely to become a starting point of fracture, and a decrease in tensile strength and impact resistance can be prevented.
  • the size of the structure of the conductive nanofillers [Fc] and [Fp] in the carbon fiber layer is important for the effect of forming a conductive path between the carbon fibers [A] and the carbon fibers [A]. It may be shorter than the structure size between the layers described above.
  • the structure size of the conductive nanofillers [Fp] and [Fc] in the carbon fiber layer is preferably 0.1 ⁇ m or more, more preferably 0.15 ⁇ m or more, and 0.2 ⁇ m or more. It is more preferable that The upper limit is preferably less than 0.8 ⁇ m, more preferably less than 0.6 ⁇ m, and even more preferably less than 0.4 ⁇ m.
  • the sizes of the structures of the conductive nanofillers [Fc] and [Fp] are those observed using a transmission electron microscope (TEM).
  • TEM transmission electron microscope
  • the value is the average value of 100 structures observed in the image, starting from the largest structure, and the distance in the longest direction for each one measured.
  • a method for adjusting the conductive nanofillers [Fc] and [Fp], which are the constituent elements, to a size range of such a structure will be exemplified below, but is not limited to the following method.
  • a part of the epoxy resin [Bp] and the conductive nanofiller [Fp] are mixed to obtain a mixture [BFp] (so-called masterbatch) containing the conductive nanofiller [Fp] at a high concentration.
  • masterbatch mixture
  • the epoxy resin [Bp] and the conductive nanofiller are diluted with the remaining epoxy resin [Bp].
  • a masterbatch [BFp] containing nanofiller [Fp] in a designed ratio can be obtained.
  • the ratio of epoxy resin [Bp] and conductive nanofiller [Fp] in the masterbatch it is preferable to increase the concentration of conductive nanofiller [Fp] in order to easily apply shearing, and the mass ratio is 80: It is better to set the ratio to be about 20:60 to 40:60, more preferably about 70:30 to 50:50.
  • the conductive nanofiller [Fp] forms aggregates as shown in FIG.
  • the conductive nanofiller [Fp] was made into a structured state by stirring it (Preparation Example 2 in Figure 8), but by applying shear to this, the conductive nanofiller [Fp] became structured. It turns out that the size is larger than before. This is thought to be due to the fact that by applying shear to transform the agglomerates into a dispersed state, reaggregation occurs due to surface tension after standing, resulting in a larger structure size than when simply stirring (as shown in Figure 8).
  • Example 1 Possible means for applying shear include a planetary or rotational mixer such as a planetary mixer, a single screw extruder, or a multi-screw extruder with two or more screws. A plurality of these methods may be performed, or one method may be performed multiple times. In order to maintain a large structure size of the conductive nanofiller [Fp], it is preferable to apply shearing only once using a mixer.
  • the average particle size of the primary particles of the conductive nanofiller [Fp] is a factor that controls the structure size of the conductive nanofiller [Fp], and depending on the desired structure size of the conductive nanofiller [Fp], the conductivity It is preferable to select the average particle size of the primary particles of the nanofiller [Fp].
  • the average particle size of the primary particles of the conductive nanofiller [Fp] is preferably 50 nm or less, preferably less than 30 nm, and more preferably less than 20 nm.
  • the structure size of the conductive nanofiller [Fp] can be increased.
  • the lower limit of the average particle size of the primary particles of the conductive nanofiller [Fp] is preferably 5 nm or more, more preferably 10 nm or more, and even more preferably 15 nm or more. Within this preferable lower limit range, good handling properties can be maintained.
  • the average particle size of the primary particles of the conductive nanofiller is defined as the average particle size obtained by measuring the individual particle sizes of 100 or more primary particles using a transmission electron microscope.
  • nanofillers are defined as those having individual particle diameters of less than 1 ⁇ m, and nanofillers of 1 ⁇ m or more are not included in the calculation of the average particle diameter of primary particles.
  • both conductive particles with individual particle diameters of 1 ⁇ m or more and less than 1 ⁇ m it is designated as [FGc] or [FGp].
  • [FGp] has the effects of both [Fp] and [Gp]
  • [FGc] has the effects of both [Fc] and [Gc].
  • the structure of the conductive nanofiller [Fp] flows together with the thermoplastic resin [Dp] composed of an epoxy resin [Bp], an aromatic polyamine compound [Cp], and a polyarylether skeleton. Then, it connects the gaps between carbon fibers [A] and carbon fibers [A], or connects the gaps between carbon fibers [A] and conductive particles [Gp] with a particle size of 1 ⁇ m or more (symbol 6 in FIG. 5).
  • structures may be combined to form an aggregate. It is known that structures tend to be bonded in the longitudinal direction rather than in a spherical shape, and an image of the aggregated structures of conductive nanofiller [Fp] is shown in FIG. By increasing the structure size, the size of this aggregate also increases, making it possible to connect the upper and lower carbon fibers across the layers, and the CFRP that has been cured is considered to have high lightning resistance.
  • the material of the conductive nanofiller [Fp] constituting the prepreg of the present invention includes, but is not limited to, carbon, graphite, nickel, gold, platinum, palladium, silver, copper, or cobalt. is preferable, and carbon materials include carbon nanofibers, carbon nanohorns, carbon nanocones, carbon nanotubes, carbon nanocoils, carbon microcoils, carbon nanowalls, carbon nanochaplets, fullerenes, carbon black, and graphite. , graphene, carbon nanoflakes, and derivatives thereof. Nanofillers made of these carbon materials may be used alone or in combination of two or more.
  • the shape preferably has a small aspect ratio, preferably 100 or less, more preferably less than 10, and even more preferably less than 2.
  • Carbon black is good in this respect, and examples of such carbon black include furnace black, hollow furnace black, acetylene black, channel black, etc. Furnace black is preferred.
  • [Fc] contained in CFRP made by curing prepreg containing [Fp] can be basically considered to have the same shape as [Fp] in terms of particle size, aspect ratio, etc., but [Fc] is in the curing stage. form a cohesive structure.
  • the primary resin film contains conductive nanofiller [Fp], and the secondary resin film also contains conductive nanofiller [Fp]. As shown in FIG. Nanofiller [Fp] may also be included.
  • the structure size of the conductive nanofiller [Fp] to be contained in the secondary resin film is 0.6 ⁇ m or more, and 1 Next, it is preferable that the structure size of the conductive nanofiller [Fp] contained in the resin film is 0.1 ⁇ m or more and less than 0.5 ⁇ m.
  • the structure size of the conductive nanofiller [Fp] contained in the primary resin film is more preferably 0.12 ⁇ m or more and less than 0.4 ⁇ m, and even more preferably 0.15 ⁇ m or more and less than 0.3 ⁇ m.
  • the conductive nanofiller [Fp] contained in the secondary resin film has a large effect of forming vertical conductive paths between layers, while the conductive nanofiller [Fp] contained in the primary resin film has a large effect on forming vertical conductive paths between layers.
  • the conductivity contained in the primary resin film has the effect of penetrating into the inside of the layer and forming a conductive path between carbon fibers [A] and carbon fibers [A] within the same carbon fiber layer.
  • the nanofiller [Fp] preferably has a smaller structure size than the conductive nanofiller [Fp] contained in the secondary resin film so that it can penetrate into the carbon fiber layer. By doing so, conductive paths are formed between the carbon fiber layers, and the number of conductive paths in the carbon fiber layers increases, thereby improving conductivity and increasing lightning resistance.
  • the structure size of the conductive nanofiller [Fp] to be included in the primary resin film is preferably less than 0.5 ⁇ m.
  • the conductive nanofiller [Fp] may be dispersed throughout the secondary resin film, or the conductive nanofiller [Fp] may be contained in a master batch of the conductive nanofiller [Fp].
  • [BCFp] may be locally arranged as a lump.
  • the masterbatch [BCFp] is made into a lump, the masterbatch is shaped into dots by stencil printing or screen printing, and then heat-treated to form the epoxy resin [Bp] of the secondary resin film. It is better to semi-cure the aromatic polyamine compound [Cp] to the extent that it is solidified at room temperature because the masterbatch [BCFp] will be easier to handle.
  • the advantage of making the masterbatch [BCFp] into a lump is that the conductive nanofiller [Fp] is present only in the lump part compared to the case where the conductive nanofiller [Fp] is dispersed throughout the secondary resin film. , the cost is reduced by reducing the content of conductive nanofiller [Fp], which is expensive, and slitting processability is improved by creating areas that contain conductive nanofiller [Fp] and areas that do not, as described below.
  • the goal is to improve As a method for locally disposing a lumped masterbatch [BCFp], other secondary resin films such as epoxy resin [Bp], aromatic polyamine compound [Cp], and thermoplastic resin [Dp] composed of a polyarylether skeleton can be used.
  • thermoplastic resin particles [Ep], etc. may be kneaded with other secondary resin films such as epoxy resin [Bp], aromatic polyamine compound [Cp], and thermoplastic resin composed of polyarylether skeleton.
  • resin [Dp], thermoplastic resin particles [Ep], etc. are made into a resin film and then a masterbatch [BCFp] is sprayed, or a method is used in which dots are printed on release paper, etc. and then the release paper is placed on the resin film. A possible method is to transfer them at the same time.
  • the content of the conductive nanofiller [Fp] constituting the prepreg of the present invention is preferably in the range of 0.5 to 15.0 parts by mass, more preferably from 0.5 to 15.0 parts by mass based on 100 parts by mass of the epoxy resin [Bp]. is in the range of 2.0 to 10.0 parts by weight, more preferably in the range of 4.0 to 7.0 parts by weight.
  • By setting the blending amount of the conductive nanofiller [Fp] within this range it is possible to balance the conductivity and mechanical properties of the obtained CFRP.
  • the content of the conductive nanofiller [Fp] is preferably 1 part by mass or more, and 3 parts by mass or more based on 100 parts by mass of the epoxy resin [Bp] of the secondary resin film. It is more preferably at least 5 parts by mass, and even more preferably at least 5 parts by mass.
  • the upper limit is preferably 20 parts by mass or less, more preferably less than 15 parts by mass, and even more preferably less than 10 parts by mass.
  • the CFRP and prepreg of the present invention contain particles having an individual particle size of 1 ⁇ m or more, particularly conductive particles [Gc] and [Gp] having an individual particle size equivalent to the interlayer thickness, within a range that does not impede the effects of the present invention. It can also be included.
  • the materials constituting [Gc] and [Gp] include, but are not limited to, carbon, graphite, nickel, gold, platinum, palladium, silver, copper, or cobalt, and the above materials are added to the thermoplastic resin particles. It is also possible to use particles that have been made into particles by coating them.
  • the individual particle size of the conductive particles [Gc] and [Gp] is preferably equal to or greater than the interlayer thickness in terms of forming a conductive path, but specifically, D50 in the particle size distribution is 11 ⁇ m or more. It is preferable that it is, it is preferable that it is 15 micrometers or more, and it is more preferable that it is 20 micrometers or more.
  • the upper limit of D50 in the particle size distribution is preferably 50 ⁇ m or less, preferably less than 30 ⁇ m, and more preferably less than 25 ⁇ m.
  • Conductive particles [Gc] and [Gp] basically do not form a structure, and [Gc] contained in CFRP made from a cured prepreg containing [Gp] basically has the same particle size and aspect as [Gp].
  • the shapes such as ratios may be considered to be the same.
  • conductive particles [Gc] and [Gp] can be a factor in reducing tensile strength and impact resistance, but they are relatively large in volume compared to conductive nanofillers [Fc] and [Fp]. A large amount of current can flow through it. Therefore, when disposing between layers, a submicron structure consisting of conductive nanofillers [Fc] and [Fp] contained in the secondary resin film is used to form fine conductive paths like spokes without gaps.
  • the upper limit of the content of conductive particles [Gp] is preferably less than 5 parts by mass, more preferably less than 3 parts by mass, and less than 2 parts by mass. More preferred. In this case, it is preferable to prepare a master batch [BCFGp] in which both [Fp] and [Gp] are mixed together, and even if [Fp] and [Gp] are prepared separately as conductive particles, the individual particle size is 1 ⁇ m. Particles [FGp] containing a mixture of conductive particles with a diameter of less than 1 ⁇ m and conductive particles with a diameter of 1 ⁇ m or more may be prepared.
  • the master batch for the secondary resin film [BCFGp] may be locally placed in the form of a lump.
  • the width accuracy when cutting the prepreg can be increased, and CFRP with high conductivity when cured can be obtained.
  • conductive particles [Gp] are present in the carbon fiber layer, fuzz will easily occur when the carbon fiber is cut as shown in FIG. It is preferable that there is no (described later). Therefore, it is preferable that the so-called primary resin does not contain conductive particles [Gp], and even when conductive particles [Gp] are added to the secondary resin, the conductive particles [Gp] do not enter the carbon fiber layer.
  • D50 in the particle size distribution of the conductive particles [Gp] is preferably 11 ⁇ m or more.
  • D50 in the particle size distribution of the conductive particles [Gp] is preferably set to 11 ⁇ m or more.
  • particles [FGp] in which conductive particles having individual particle diameters of less than 1 ⁇ m and those of 1 ⁇ m or more are mixed are preferably prevented from entering the carbon fiber layer.
  • the CFRP of the present invention is characterized by high lightning resistance, but the volume resistivity in the thickness direction is preferably 50 ⁇ cm or less, more preferably 30 ⁇ cm or less, and 15 ⁇ cm or less. It is even more preferable. By keeping the volume resistivity below this range, it can be said that it has high conductivity, and when a current is applied due to a lightning strike, etc., the layer does not become an insulating layer, and the structure is such that the current does not flow and stagnate. I can say it.
  • the CFRP of the present invention is conductive due to the aggregate of submicron structures in which the conductive nanofillers [Fc] and [Fp] are connected. Because the distance between the conductive paths is short in the planar direction, compared to CFRP that uses conductors of 11 ⁇ m or more that have been developed in the past, the distance between the conductive paths is short, causing the current to accumulate locally. There are no spots, and even with the same volume resistivity, the lightning resistance tends to be higher than that of CFRP that uses a conductor of 11 ⁇ m or more. On the other hand, when locally arranged as a lump, the width accuracy when cutting the prepreg tends to be high.
  • the carbon fiber [A] used in the CFRP and prepreg of the present invention preferably has a higher tensile modulus because the tensile strength of the CFRP can be increased.
  • the tensile modulus of carbon fiber is preferably 200 GPa or more, more preferably 230 GPa or more, and even more preferably 250 GPa or more.
  • the tensile modulus it is preferably 440 GPa or less, more preferably 400 GPa or less. This preferable upper limit can prevent a decrease in tensile elongation.
  • Other reinforcing fibers include glass fibers, aramid fibers, boron fibers, PBO fibers, high strength polyethylene fibers, alumina fibers, and silicon carbide fibers.
  • the tensile elongation of the carbon fiber [A] used in the CFRP and prepreg of the present invention is preferably 0.8% or more, more preferably 1.0% or more, and further preferably 1.2% or more. preferable. Since carbon fiber [A] has a high tensile elongation and is difficult to break, the tensile strength of CFRP becomes high. When tensile stress is applied to CFRP using the conventional conductor mentioned above, interfacial peeling occurs between the conductor and the matrix resin [BCDc], regardless of the tensile elongation of the carbon fiber, and this becomes the starting point for fracture.
  • the CFRP of the present invention it is also possible to use no conductor in addition to the conductive nanofiller, and in that case, the tensile elongation of the carbon fiber [A] can be effectively utilized. .
  • impact resistance can also be improved due to the high tensile elongation.
  • the tensile modulus tends to decrease, so it is preferably in the range of 3.0% or less, more preferably less than 2.5%.
  • the tensile modulus and tensile elongation of the carbon fiber [A] are values measured according to JIS R 7601 (2006).
  • the carbon fiber [A] used in the CFRP and prepreg of the present invention preferably has a number of filaments in the range of 1,000 to 50,000 in one carbon fiber [A] bundle. If the number of filaments is less than 1,000, the fiber arrangement tends to meander, which tends to cause a decrease in strength. The number of filaments is more preferably in the range of 2,500 to 40,000, which is particularly suitable for aerospace applications.
  • the mass proportion of carbon fiber [A] in the CFRP and prepreg of the present invention is preferably 60 mass% or more in order to utilize the specific strength and specific modulus of carbon fiber and obtain high tensile strength, and is preferably 62 mass% or more. % or more, and even more preferably 65% by mass or more. Furthermore, if the mass percentage of carbon fiber [A] is too large, voids tend to occur between the bundles of carbon fibers [A], so in order to suppress voids, it is preferably 80% by mass or less, and 75% by mass or less. It is more preferably less than 70% by mass, even more preferably less than 70% by mass.
  • the CFRP of the present invention can utilize the tensile strength of the carbon fiber [A] at a high utilization rate, but when the carbon fibers are arranged in one direction, such tensile strength characteristics are determined by 0° tensile strength measurement. It can be evaluated.
  • the 0° tensile strength of CFRP varies depending on the tensile strength of the carbon fiber [A], and if the carbon fiber [A] at the time of the present invention is used, it is 2,850 MPa or more, further 2,950 MPa or more, and even 3,050 MPa. It is possible to manufacture products with the above-mentioned high performance. Such tensile strength characteristics can be evaluated by measuring 0° tensile strength.
  • the 0° tensile strength of CFRP is defined as the fiber direction of unidirectional CFRP being the axial direction, that direction being defined as the 0° axis, and the direction perpendicular to the axis being 90°. Define. A 0° tensile test is conducted at room temperature (23°C) according to the standard of JIS K 7073 (1988).
  • the prepreg of the present invention includes an epoxy resin [Bp], an aromatic polyamine compound [Cp], and a thermoplastic resin [Dp] composed of a polyarylether skeleton, and these are blended and then pressurized and heated. This results in a cured product in which the thermoplastic resin [Dp] composed of a polyarylether skeleton is dissolved in the polymerization of the epoxy resin [Bp] and the aromatic polyamine compound [Cp], which is a suitable matrix resin [BCDc]. can do.
  • the composition examples will be mainly explained with a focus on preferred composition examples that allow the CFRP of the present invention to be obtained under curing conditions used in current aerospace applications, but are not limited to the following compositions.
  • the epoxy resin [Bp] constituting the prepreg of the present invention preferably contains a tetrafunctional epoxy resin.
  • the tetrafunctional epoxy resin is an epoxy resin containing four or more epoxy groups in one molecule, and is preferably liquid at 23°C. Specifically, tetraglycidyldiaminodiphenylmethane (TGDDM), halogen-substituted products, alkyl-substituted products, aralkyl-substituted products, hydrogenated products, etc. thereof can be used.
  • TGDDM tetraglycidyldiaminodiphenylmethane
  • halogen-substituted products alkyl-substituted products
  • aralkyl-substituted products hydrogenated products, etc. thereof
  • High CFRP can be obtained.
  • the epoxy resin [Bp] contains a component that tends to cause the difference between the maximum and minimum free volume pore radii to be 0.09 nm or more when molded and cured to form CFRP.
  • Some bifunctional epoxies tend to have nonuniform three-dimensional network structures, such as fluorene-type epoxy resins, phenol novolac-type epoxy resins, cresol novolac-type epoxy resins, resorcinol-type epoxy resins, and phenol aralkyl-type epoxy resins.
  • N,N-diglycidylaniline, N,N-diglycidyltoluidine, or derivatives thereof are preferred because they have higher effects.
  • the epoxy resin [Bp] constituting the prepreg of the present invention may contain epoxy resins other than those mentioned above.
  • Bifunctional epoxy resins are added according to the required properties, and preferred bifunctional epoxy resins include bisphenol-type epoxy resins, amine-type epoxy resins, phenol novolac-type epoxy resins, cresol novolac-type epoxy resins, and resorcinol-type epoxy resins. , phenol aralkyl type epoxy resin, naphthol aralkyl type epoxy resin, dicyclopentadiene type epoxy resin, epoxy resin having a biphenyl skeleton, isocyanate modified epoxy resin, tetraphenylethane type epoxy resin, triphenylmethane type epoxy resin, etc. More than one species can be selected and used.
  • aromatic polyamine compound [Cp] constituting the prepreg of the present invention include diaminodiphenylsulfone, diaminodiphenylmethane, phenylenediamine, and various derivatives and positional isomers thereof. 4,4'-diaminodiphenylsulfone and 3,3'-diaminodiphenylsulfone are preferred. Since 3,3'-diaminodiphenylsulfone has a bent structure and is asymmetric, the maximum and minimum free volume pore radii obtained by positron annihilation lifetime measurement are smaller than those of 4,4'-diaminodiphenylsulfone.
  • 4,4'-diaminodiphenylsulfone is superior in moldability. Therefore, in the prepreg of the present invention, it is more preferable to use 4,4'-diaminodiphenylsulfone with emphasis on moldability.If higher compressive strength is required, 4,4'-diaminodiphenyl It is preferable to use a mixture of sulfone as the main component and 3,3'-diaminodiphenylsulfone in an appropriate proportion.
  • the prepreg of the present invention may contain an auxiliary curing agent such as a curing accelerator within a range that does not impair the heat resistance and thermal stability of the resin composition.
  • an auxiliary curing agent such as a curing accelerator within a range that does not impair the heat resistance and thermal stability of the resin composition.
  • the secondary curing agent include tertiary amines, Lewis acid complexes, onium salts, imidazole compounds, urea compounds, hydrazide compounds, and sulfonium salts.
  • the content of the sub-curing agent needs to be adjusted appropriately depending on the type used, it is preferably 10 parts by mass or less, more preferably 5 parts by mass or less, based on 100 parts by mass of the total amount of epoxy resin [Bp].
  • the curing accelerator is contained within this range, it is preferable because temperature unevenness is less likely to occur when molding CFRP.
  • thermoplastic resin [Dp] composed of a polyarylether skeleton that constitutes the prepreg of the present invention improves mechanical properties such as resin toughness, microcrack resistance, and further solvent resistance, depending on the amount contained. be able to.
  • Thermoplastic resins composed of a polyarylether skeleton suitable as the thermoplastic resin [Dp] composed of a polyarylether skeleton include, for example, polysulfone, polyphenylsulfone, polyethersulfone, polyetherimide, polyphenylene ether, Examples include polyetheretherketone and polyetherethersulfone, which dissolve in the epoxy resin [Bp] and the aromatic polyamine compound [Cp] at high temperatures.
  • thermoplastic resins constituted by a polyarylether skeleton may be used alone or in combination.
  • polyether sulfone can be preferably used because it can impart toughness to the resulting CFRP without deteriorating its heat resistance or mechanical properties.
  • Commercial products of polyether sulfone that can be suitably used as the thermoplastic resin [Dp] composed of a polyarylether skeleton include "Sumika Excel” (registered trademark) PES 5003P (manufactured by Sumitomo Chemical Co., Ltd.) and "VIRANTAGE”. (registered trademark) VW-10700RFP, etc.
  • the amount of [Dp] may be adjusted as necessary depending on the viscosity of the matrix resin, the tack of the prepreg, the mechanical properties of the CFRP, etc., but the preferred range is:
  • the amount is preferably from 5 to 40 parts by weight, more preferably from 10 to 35 parts by weight, and even more preferably from 15 to 30 parts by weight.
  • CFRP of the present invention can have high impact resistance.
  • CFRP according to the prior art also contains thermoplastic resin particles to improve impact resistance, and these particles are mainly composed of thermoplastic resin that is insoluble in epoxy resin, so they do not maintain their shape. It has high impact resistance because the shape of these particles deforms when an impact is applied.
  • the thermoplastic resin particles [Ec] in order to utilize the tensile strength of carbon fibers at a high utilization rate, the thermoplastic resin particles [Ec] have the above-described specific aspect ratio. These particles are blended primarily for the effect of improving tensile strength, but by adjusting the blending amount, etc., it is possible to provide impact resistance required for current aerospace applications.
  • the CAI of CFRP is the CAI after applying impact energy of 6.7 J per mm of thickness of the test piece according to JIS K 7089 (1996).
  • the CFRP of the present invention can have high 0° compressive strength.
  • the 0° compressive strength of CFRP is preferably 250 MPa or more, more preferably 280 MPa or more, and even more preferably 300 MPa or more.
  • the average pore radius is preferably 0.270 nm or less, less than 0.255 nm, or less than 0.248 nm in a distribution curve obtained from the free volume radius obtained by positron annihilation lifetime measurement and its existence probability. When the average pore radius is 0.270 nm or less, it becomes difficult to deform under compressive stress, and compressive strength improves.
  • the lower limit of the average pore radius is preferably 0.230 nm or more, more preferably 0.240 nm or more, and even more preferably 0.245 nm or more. With this preferable lower limit, it is possible to prevent an increase in the number of parts that cannot be initially deformed when tensile stress is applied, and to increase the tensile strength.
  • the form of the prepreg of the present invention may be either a unidirectional prepreg or a woven prepreg.
  • the carbon fibers [A] constituting the prepreg of the present invention usually exist as a bundle, preferably arranged in one direction, and preferably have a mass per unit area of 120 g/m 2 or more, and 250 g/m It is more preferably 2 or more, and even more preferably 350/m 2 or more.
  • CFRP can be obtained by laminating a plurality of prepregs and then curing them, but if the amount of carbon fiber per prepreg is large, the number of laminations can be reduced, and the cost during molding can be lowered.
  • the thickness per layer between carbon fiber layers will be affected by voids etc. Therefore, the latter tends to be thicker. In that case, thickness variations are likely to occur due to particles between the layers, so the configuration of the present invention can be said to be more useful when using such prepregs in which the mass of carbon fiber bundles is large.
  • the weight per unit area of the carbon fiber [A] there is a tendency that the smaller the bundle amount of carbon fiber, the better the drape property (ease of bending during lamination or slitting).
  • 200 g/m 2 or less more preferably less than 600 g/m 2 , even more preferably less than 400 g/m 2 .
  • the prepreg of the present invention can be used in the form of a tape or thread by cutting it into predetermined widths using a known method.
  • These tapes and filamentous prepregs (hereinafter sometimes referred to as slit tapes) are suitably used in automatic lamination devices.
  • the prepreg can be cut (hereinafter sometimes referred to as slitting) using a commonly used cutter. Examples include a carbide blade cutter, an ultrasonic cutter, and a round blade cutter.
  • the ATL (Automated Tape Layup) method and AFP (Automated Fiber Placement) method using automatic lamination equipment have been used to manufacture large composite materials such as aircraft and automobiles.
  • the conductive particles [Gp] that are the constituent elements are selectively arranged at a depth corresponding to 20% from the prepreg surface with respect to the average thickness of the prepreg. It is preferable that 85% by area or more is arranged between the layers, more preferably 92% by area or more is arranged between the layers.
  • slitting prepreg it is possible to obtain a narrow prepreg (slit tape) with less fuzz and good quality, and this narrow prepreg with less fuzz can be laminated using ATL or AFP.
  • By curing it is also possible to make a carbon fiber composite material with high designability that has both high impact resistance and high conductivity in the thickness direction.
  • thermoplastic resin particles [Ep] perhaps because they are adhered to the surrounding epoxy resin, even if they exist in the carbon fiber layer, compared to the case where conductive particles [Gp] with a particle size of 1 ⁇ m or more are present.
  • the conductive nanofiller [Fp] is less likely to generate fluff, probably because it is smaller in size than the conductive particles [Gp] with a particle size of 1 ⁇ m or more, although it depends on the structure size.
  • the conductive particles [Gc] are arranged between the layers with high resin toughness, and the impact and tensile stress This is advantageous because when such stress occurs, the high toughness resin around [Gc] can absorb the stress.
  • 80 area% or more of the conductive particles [Gc] are arranged between carbon fiber layers. It is preferable that 85% by area or more of the material is located between the layers, more preferably 85% by area or more is located between the layers, and even more preferably 92% by area or more is located between the layers.
  • the thermoplastic resin particles [Ec] are arranged in an area of 80% or more between the layers because the impact resistance and tensile strength are increased. It is preferable to place
  • fuzzing can be suppressed on the prepreg surface by creating a part made of thermoplastic resin containing filler and a part made of thermoplastic resin not containing particles or fillers.
  • conductive nanofiller [Fp] it has been found that it is effective to suppress fluffing when kneaded and semi-cured as a masterbatch [BCFp] or [BCFGp] and placed on the surface. Ta.
  • the conductive nanofiller [Fp] on the surface of the prepreg scatters when it rubs against a slitting blade, guide roll, etc., but at that time, the surrounding epoxy resin remains attached.
  • the prepreg of the present invention is a prepreg that has lightning resistance, has high slitting processability, and can obtain a narrow prepreg with little fuzz and high quality.
  • the prepreg has a width of 5 inches or less, and A diameter of 0.1 inch to 3 inches, or even 0.2 inch to 1 inch, can be usefully obtained.
  • the CFRP of the present invention can be obtained by laminating the prepregs of the present invention in a predetermined form and then heating to cure the resin. From the viewpoint of suppressing voids and obtaining a uniform cured product, it is preferable to apply pressure during molding.
  • a method for applying heat and pressure known methods such as an autoclave molding method, a press molding method, a bagging molding method, a wrapping tape method, and an internal pressure molding method can be used.
  • a lightning-resistant prepreg the width accuracy when slit is high, and prepreg with a width of 5 inches or less has little fuzz, so it can be suitably used to obtain CFRP molded using ATL or AFP. Can be done.
  • the CFRP and prepreg of the present invention have excellent tensile strength and impact resistance, and can obtain lightning resistance higher than conventional ones, so they can contribute to reducing the weight of aircraft in the aerospace field, as well as sporting goods and automobile applications. .
  • Carbon fiber [A] ⁇ “Trading Card” (registered trademark) T800S-24K-10E (24,000 fibers, tensile modulus: 294 GPa, density 1.8 g/cm 3 , manufactured by Toray Industries, Inc.)
  • Epoxy resin [Bp] ⁇ “Araldite” (registered trademark) GY282 (component: bisphenol F type epoxy resin [BisF]) manufactured by Huntsman Advanced Materials Co., Ltd.
  • ⁇ “Araldite” registered trademark) MY721 (tetraglycidyldiaminodiphenylmethane [TGDDM]) Huntsman ⁇ Advanced Materials Co., Ltd.
  • [Fp] - Conductive carbon black #3230B [CB] (ingredients: furnace black, average particle diameter of primary particles 23 nm, aspect ratio 1, manufactured by Mitsubishi Chemical Corporation).
  • Conductive particles with an individual particle size of 1 ⁇ m or more [Gp] - Conductive particles [CP26] obtained by firing phenolic resin particles (Marilyn HF type, manufactured by Gunei Chemical Industry Co., Ltd.) at 2000°C and classifying them (component: carbon, D50 in particle size distribution: 26 ⁇ m) ).
  • An A4-sized piece of black film X30 manufactured by Toray Industries, Inc. was irradiated with an infrared laser with a wavelength of 1,069 nm and an output of 2 W at equal intervals, and the black film was perforated in circles at equal intervals with the laser.
  • a film was created. This was used as a stencil, the FEP film and the stencil were stacked on an iron plate, the edges were fixed, and the paste was extruded through the stencil with a squeegee to create a paste sheet in which lumps of paste were formed at equal intervals.
  • thermoplastic resin particles [Ep], conductive particles [Gp] with an individual particle size of 1 ⁇ m or more, and a masterbatch [BFp] were added and stirred while cooling, until the temperature reached about 60°C.
  • a secondary resin was obtained by adding an aromatic polyamine compound [Cp] and stirring.
  • the input ratio of each raw material was set as shown in the table. In each table, conductive particles [Gp] with an individual particle diameter of 1 ⁇ m or more and masterbatch [BFp] in the case of 0 part by mass indicate that they were not added.
  • the secondary resin two secondary resin films each having a resin amount of 20 g/m 2 were produced in the same manner.
  • the primary resin is 42g/m 2 and the secondary resin is 28g/m 2
  • the bundle of carbon fibers [A] is 380g/m 2 .
  • the primary resin was 60 g/m 2 and the secondary resin was 40 g/m 2 .
  • the FEP film on which the paste lump is placed is attached to the second resin film so that the paste lump is in contact with the resin film, and then the FEP film is applied so that the paste lump is transferred to the resin film. I peeled off the film.
  • a secondary resin film is layered on both sides of the carbon fibers arranged in one direction in a sheet shape with the basis weight listed in Table 1, and the carbon fibers are impregnated with the second resin by heating and pressurizing.
  • a single-stage impregnated prepreg with a ratio of 35.4% was prepared.
  • (1) Post-impact compressive strength measurement of CFRP The prepreg manufactured in each example was cut into a predetermined size, and the longitudinal direction of the carbon fiber was defined as 0°, [+45°/0°/-45°/90° ] was repeated three times and laminated symmetrically to form a quasi-isotropic preliminary laminate with a total of 24 plies.
  • the two laminates that were repeated twice were laminated symmetrically to form a quasi-isotropic preliminary laminate with a total of 16 plies.
  • the obtained preliminary laminate was placed in an autoclave and cured under the conditions shown in Table 1 to obtain CFRP.
  • a sample measuring 40 mm long x 40 mm wide was cut out from the obtained CFRP, and after polishing off the resin layer on both surfaces, conductive paste N-2057 (manufactured by Shoei Chemical Industry Co., Ltd.) was applied to both sides using a bar coater. It was applied to a thickness of about 70 ⁇ m and cured in a hot air oven adjusted to a temperature of 180° C. for 30 minutes to obtain a sample for conductivity evaluation.
  • the resistance in the thickness direction of the obtained sample was measured by a four-terminal method using an R6581 digital multimeter manufactured by Advantest Co., Ltd. The measurement was performed six times, and the average value was taken as the volume resistivity ( ⁇ cm) in the thickness direction of the CFRP.
  • (3) Individual particle size, average particle size, and structure size of primary particles of conductive nanofiller [Fc] The CFRP obtained in (2) above was processed into thin sections using a microtome, and then subjected to transmission electron microscopy (TEM). ), and after measuring the distance in the longest direction of the conductive nanofiller [Fc] as the individual particle size of the primary particles, the average value of 100 particles was determined as the conductive nanofiller [Fc] primary particle.
  • thermoplastic resin particles For the five CFRP sheets obtained in each example, a cross section in the thickness direction obtained by selecting an arbitrary position was measured using a scanning electron microscope. Cross-sectional images were obtained one by one by observing at a magnification of about 1,000 times. In the cross-sectional image of 1, for the thermoplastic resin particles that exist between the layers and are located near the center, use the length measurement tool attached to the microscope to determine the length of the longest diagonal line that passes through the center of the particle as the major axis.
  • the length of a diagonal line drawn perpendicularly through the center of the particle to the straight line indicating the major axis was defined as the minor axis.
  • 19 particles that exist in the same layer as the particle near the center of the measurement and are located close to that particle are measured in the same way, and the remaining 4 cross sections are also measured in the same way to obtain 100 particles. Obtained the long axis and short axis.
  • thermoplastic resin particles [Ec] particles with an aspect ratio of 1.1 or more was calculated. did. (5) D10, D50, D90 in the particle size distribution of thermoplastic resin particles [Ep] and conductive particles [Gp] particles with an individual particle size of 1 ⁇ m or more Thermoplastic resin particles [Ep] or conductive particles [Gp] having an individual particle size of 1 ⁇ m or more were added to distilled water and dispersed by ultrasonication so that the particle concentration was about 0.1% by mass.
  • the volume-based particle size distribution of this dispersion liquid was measured using a laser diffraction particle size distribution analyzer (SALD-2100: manufactured by Shimadzu Corporation).
  • SALD-2100 manufactured by Shimadzu Corporation
  • the particle size detection range was set to 1 to 100 ⁇ m, and this range was set to be divided into 50.
  • a particle size distribution chart was obtained by plotting the relative particle amount in terms of volume on the vertical axis and the logarithm of the particle size on the horizontal axis, connecting each plot with a straight line. In this particle size distribution chart, the particle sizes when the frequency of individual particle sizes reached 10%, 50%, and 90% were defined as D10, D50, and D90 in the particle size distribution.
  • Thickness uniformity of carbon fiber layer Regarding the scanning electron microscope image obtained in (4), measure the distance from the top edge of the image of the carbon fiber layer in the +45 degree direction or -45 degree direction to the bottom edge using the length measurement tool attached to the microscope. 50 lines were drawn at 20 ⁇ m intervals using a 20 ⁇ m interval, and the lengths were measured. At this time, it was decided that the carbon fiber layer would not include those that were separated from the carbon fiber layer and moved between the layers. The average value was calculated by summing up the four lines excluding the longest one among the five lines from the rightmost end of the obtained image and dividing by four. The reason for excluding the longest one is to reduce the possibility of including carbon fibers released from the carbon fiber layer.
  • Example 1 The resin composition described in Example 1 of Table 1-1 was made into a masterbatch by the method of Preparation Example 1, and a prepreg was produced by a two-stage impregnation method. After cutting the obtained prepreg to a predetermined size and laminating the number of sheets described in each measurement method, vacuum bagging is performed, and using an autoclave, a temperature of 180 ° C. and a pressure of 6 kg/cm 2 are maintained for 2 hours. By doing so, we obtained CFRP.
  • the prepreg had excellent slit workability, and the cured CFRP had excellent compressive strength after impact and electrical conductivity in the thickness direction.
  • Comparative example 1 Prepreg and CFRP were obtained in the same manner as in Example 1, except that the resin composition described in Comparative Example 1 in Table 1-1 was made into a masterbatch by the method in Preparation Example 1.
  • the CFRP obtained by curing has a large value of formula (1), the thermoplastic resin particles [Ec] are densely packed, there are few particles with an aspect ratio, and as shown in Figure 2, the thermoplastic resin particles are interlayered. An insulating layer was formed, and the conductivity in the thickness direction was poor. The large thermoplastic resin particles [Ec] spread the thickness between the layers, making the thickness non-uniform, and the average thickness between the layers was 56 ⁇ m.
  • Example 2 Prepreg and CFRP were obtained in the same manner as in Example 1, except that the resin composition described in Example 2 in Table 1-1 was made into a masterbatch by the method in Preparation Example 1.
  • the prepreg had excellent slit workability, and the cured CFRP had excellent compressive strength after impact and electrical conductivity in the thickness direction.
  • Comparative example 2 Prepreg and CFRP were obtained in the same manner as in Example 1, except that the resin composition was as described in Comparative Example 2 in Table 1-1.
  • Example 3 Prepreg and CFRP were obtained in the same manner as in Example 1, except that the resin composition was as described in Example 3 in Table 1-1.
  • the prepreg had excellent slit workability, and the CFRP obtained by curing had a small amount of thermoplastic resin particles [Ec], so although the compressive strength after impact was not high, it had excellent conductivity in the thickness direction.
  • Comparative example 3 Prepreg and CFRP were obtained in the same manner as in Example 1, except that the resin composition was as described in Comparative Example 3 in Table 1-1.
  • Prepreg has excellent slit processability, and as shown in Figure 1, the thermoplastic resin particles in the cured CFRP have a high melting point and do not collapse, so there are few particles with an aspect ratio, and large thermoplastic resin particles [Ec]. The thickness between the layers was widened, the thickness of the carbon fiber layer was uneven, and the conductivity in the thickness direction was poor.
  • Comparative example 4 Prepreg and CFRP were obtained in the same manner as in Example 2, except that a masterbatch was prepared by the method in Preparation Example 2.
  • Example 4 The resin composition described in Example 4 in Table 1-2 was made into a masterbatch by the method of Preparation Example 1, and a prepreg was produced by a one-step impregnation method. The obtained prepreg was cured by the method of Example 1 to obtain CFRP.
  • thermoplastic resin particles [Ep1] and conductive nanofiller [Fp1] are contained in the carbon fiber layer, some fuzz occurs during the slitting process of the prepreg, and the hardened CFRP does not have any fuzz after impact. Although the compressive strength was not higher than other standards, the conductivity in the thickness direction was excellent. The reason why the conductivity in the thickness direction is excellent is that the thermoplastic resin particles [Ec] are included in the inner layer of the carbon fiber layer, making the interlayer thickness 36 ⁇ m thinner than other examples. This seems to be because the conductive paths between the fiber layers became easier to connect.
  • Example 5 The same method as Example 1 except that the primary resin composition described in Example 5 in Table 1-2 was made into a masterbatch by the method of Preparation Example 2, and the secondary resin composition was made into a masterbatch by the method of Preparation Example 1. prepreg and CFRP were obtained. The prepreg had excellent slit workability, and the cured CFRP had excellent compressive strength after impact and electrical conductivity in the thickness direction. (Example 6) Prepreg and CFRP were obtained in the same manner as in Example 1, except that the resin composition was as described in Example 6 in Table 1-2.
  • Prepreg has excellent slitting properties, and the cured CFRP contains conductive particles [Gc], so the compressive strength after impact is not high, but it can be improved by adding a small amount of conductive particles [Gc]. It had excellent conductivity in the thickness direction.
  • Example 7 Prepreg and CFRP were prepared in the same manner as in Example 1, except that the epoxy-modified polyamide particles of the thermoplastic resin particles [Ep] to be included in the secondary resin were classified to remove small-sized particles before use. Obtained. The prepreg had excellent slit workability, and the cured CFRP had the same conductivity in the thickness direction as Example 1, and had an even higher compressive strength after impact.
  • Comparative example 5 Prepreg and CFRP were obtained in the same manner as in Example 1, except that the resin composition was as described in Comparative Example 5 in Table 1-2.
  • thermoplastic resin particles [Ep] included in the secondary resin D10 in the particle size distribution of the thermoplastic resin particles [Ep] included in the secondary resin is small, and a large number of thermoplastic resin particles [Ep] invade the carbon fiber layer, so some fuzz occurs during prepreg slitting.
  • the CFRP obtained by curing had poor compressive strength after impact, the thickness of the carbon fiber layer was uneven, and the conductivity in the thickness direction was also poor.
  • Prepreg and CFRP were obtained in the same manner as in Example 1, except that the resin composition was as described in Example 8 in Table 2-1.
  • thermoplastic resin particles [Ep] and the conductive nanofiller [Fp] contained in the primary resin are contained in the carbon fiber layer, some fuzz occurred during the prepreg slitting process, but this was at an acceptable level. Moreover, the CFRP obtained by curing was inferior to other standards in compressive strength after impact, but excellent in conductivity in the thickness direction. (Example 9) Using particles [CP02] in which both conductive nanofiller [Fp] with an individual particle size of less than 1 ⁇ m and conductive particles [Gp] with a particle size of 1 ⁇ m or more are mixed in the secondary resin, as in the production example. A dot-like mass of conductive paste was stencil-printed on an FEP film.
  • Example 10 After semi-curing, it was peeled off from the FEP film, and the second resin was prepared by kneading the resin to have the resin composition described in Example 8 of Table 2-1. Made into a resin film. Other than that, prepreg and CFRP were obtained in the same manner as in Example 1. The prepreg had excellent slit workability, and the cured CFRP had excellent compressive strength after impact and electrical conductivity in the thickness direction. (Example 10) A prepreg and CFRP were obtained in the same manner as in Example 9, except that the conductive nanofiller [Fp] was not added to the primary resin.
  • Example 11 In Example 9, instead of adding conductive nanofiller [Fp] to the primary resin, [CP02] was added as particles [FGp] in which individual particle sizes were both less than 1 ⁇ m and 1 ⁇ m or more, Prepreg and CFRP were obtained in the same manner as in Example 1. A large amount of fuzz was generated during the prepreg slitting process. The cured CFRP had excellent post-impact compressibility and conductivity in the thickness direction.
  • Example 12 A dot-like mass of conductive paste was produced on an FEP film in the same manner as described in Example 9. Next, a secondary resin film was prepared so as to have the final resin composition as described in Example 11 in Table 2-1, and an FEP film was pasted onto it so that the dot-shaped lumps of conductive paste overlapped. A secondary resin film was prepared by peeling off the FEP film so that the lump of conductive paste was transferred to the resin film side. A prepreg and CFRP were obtained in the same manner as in Example 1 except for the secondary film.
  • the prepreg had even better slit workability than Example 9, and the cured CFRP had excellent compressive strength after impact and electrical conductivity in the thickness direction.
  • Comparative example 6 Prepreg and CFRP were obtained in the same manner as in Example 12, except that the basis weight of carbon fiber [A] was 380 g/m 2 .
  • the CFRP obtained by curing had a large value of (Formula 1), the thermoplastic resin particles [Ec] were densely packed, and there were few particles with an aspect ratio. As shown in the figure, the thickness uniformity of the carbon fiber layer was poor, the thermoplastic resin particles formed an insulating layer between the layers, and the conductivity in the thickness direction was poor.
  • Example 13 A prepreg and CFRP were obtained in the same manner as in Comparative Example 6, except that the content of thermoplastic resin particles [Ep] contained in the secondary resin was reduced so that the value of (Formula 1) was 50.7.
  • the prepreg had excellent slit workability, and the cured CFRP contained many thermoplastic resin particles [Ec] having an aspect ratio, and had excellent compressive strength after impact and electrical conductivity in the thickness direction.
  • Prepreg and CFRP were produced in the same manner as in Example 13, except that particles [FGp] in which individual particle diameters were both less than 1 ⁇ m and 1 ⁇ m or more were added to the primary resin. A large amount of fuzz was generated during the prepreg slitting process.
  • Example 15 A prepreg and CFRP were obtained in the same manner as in Example 13, except that the thermoplastic resin particles [Ep] were added to the primary resin instead of the secondary resin. Because the prepreg contains thermoplastic resin particles [Ep] contained in the primary resin and conductive nanofiller [Fp] in the carbon fiber layer, some fluffing occurred during slitting, but it was at an acceptable level and hardened. Although the obtained CFRP had a slightly lower post-impact compressive strength and thickness direction conductivity than other examples, it was excellent.
  • Example 16 Prepreg and CFRP were obtained in the same manner as in Example 2, except that the basis weight of the carbon fiber [A] was 380 g/m 2 and the resin composition was as described in Example 16 in Table 2-2.
  • the prepreg had excellent slit workability, and the CFRP obtained by curing had excellent conductivity in the thickness direction, although it was slightly lower than the example with a basis weight of 270 g/m 2 .
  • Example 17 Prepreg and CFRP were obtained in the same manner as in Example 6 except that the basis weight of carbon fiber [A] was 380 g/m 2 .
  • the prepreg had excellent slit workability, and the CFRP obtained by curing had excellent conductivity in the thickness direction, although it was slightly lower than the example with a basis weight of 270 gsm.
  • Prepreg and CFRP were obtained in the same manner as in Example 1, except that the basis weight of carbon fiber [A] was 190 g/m 2 and the resin composition was as described in Example 18 in Table 2-2.
  • the prepreg had excellent slit workability, and although the CFRP obtained by curing had somewhat low compressive strength after impact, it had excellent conductivity in the thickness direction because the interlayer thickness was as thin as 23 ⁇ m.
  • Example 7 Prepreg and CFRP were obtained in the same manner as in Example 18, except that the resin composition was as described in Comparative Example 7 in Table 3. As shown in Figure 3, the hardened CFRP has thermoplastic resin particles with a high melting point with a wide interlayer spacing of 32 ⁇ m, and has inferior conductivity in the thickness direction compared to other examples of 190 g/ m2 . there were.
  • Example 19 Prepreg was produced in the same manner as in Example 12, except that the basis weight of the carbon fiber [A] was 190 g/ m2 , and the type and content of the thermoplastic resin particles [Ep] contained in the secondary resin were as shown in Table 3. and obtained CFRP.
  • the prepreg had excellent slit workability, and the cured CFRP contained many thermoplastic resin particles [Ec] having an aspect ratio, and had excellent compressive strength after impact and electrical conductivity in the thickness direction.
  • Prepreg and CFRP were obtained in the same manner as in Example 13, except that the resin composition was as described in Example 20 in Table 3. A large amount of fuzz was generated in the prepreg during slitting.
  • the cured CFRP had an acceptable post-impact compression ratio, although it was inferior to other examples because the thermoplastic resin particles [Ec] penetrated into the carbon fiber layer and disturbed the carbon fiber bundles. The conductivity in the thickness direction was excellent.
  • Example 21 Prepreg and CFRP were obtained in the same manner as in Example 20, except that the resin composition was as described in Example 21 in Table 3.
  • Prepreg has excellent slitting processability, and the thermoplastic resin particles [Ec] infiltrate the carbon fiber layer and disturb the carbon fiber bundles of the cured CFRP, so the post-impact compression ratio is lower than that of other examples. Although it was inferior to , it was within an acceptable range and had excellent conductivity in the thickness direction.
  • Comparative example 8 CFRP was obtained in the same manner as in Example 20, except that the resin composition was as described in Comparative Example 8 in Table 3. The slitting processability of the prepreg resulted in a lot of fuzz.
  • the cured CFRP had poor conductivity in the thickness direction because the thermoplastic resin particles formed an insulating layer between the layers.
  • Prepreg and CFRP were obtained in the same manner as in Example 17, except that the resin composition was as described in Example 22 in Table 3.
  • the cured CFRP had excellent compressive strength after impact and electrical conductivity in the thickness direction.
  • Carbon fiber [A] 2 Particles with a ratio of major axis to minor axis of less than 1.1 3... Interlayer between carbon fiber layers 4... Thermoplastic resin particles with a ratio of major axis to minor axis of 1.1 or more [ Ec] 5... Conductive particles having a long axis equal to or greater than the interlayer thickness 6... Conductive nanofiller [Fc] forming a conductive path between the carbon fiber and the conductive particles 7... Conductive fiber 8... Particles with small particle size moving to the carbon fiber layer 9... Conductive nano filler [Fp] mixed with epoxy resin [Bp] 10... Structure of conductive nano filler [Fp] mixed with epoxy resin [Bp] 11...

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Polymers & Plastics (AREA)
  • Health & Medical Sciences (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Medicinal Chemistry (AREA)
  • Organic Chemistry (AREA)
  • Materials Engineering (AREA)
  • Manufacturing & Machinery (AREA)
  • Inorganic Chemistry (AREA)
  • Textile Engineering (AREA)
  • Reinforced Plastic Materials (AREA)
  • Laminated Bodies (AREA)
PCT/JP2023/012166 2022-03-30 2023-03-27 炭素繊維強化複合材料およびプリプレグ Ceased WO2023190319A1 (ja)

Priority Applications (3)

Application Number Priority Date Filing Date Title
EP23780329.1A EP4488320A4 (en) 2022-03-30 2023-03-27 CARBON FIBER REINFORCED PREPREG COMPOSITE MATERIAL
JP2023521748A JPWO2023190319A1 (https=) 2022-03-30 2023-03-27
US18/850,303 US20250215171A1 (en) 2022-03-30 2023-03-27 Carbon fiber reinforced composite material and prepreg

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
JP2022-055767 2022-03-30
JP2022055767 2022-03-30

Publications (1)

Publication Number Publication Date
WO2023190319A1 true WO2023190319A1 (ja) 2023-10-05

Family

ID=88202259

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/JP2023/012166 Ceased WO2023190319A1 (ja) 2022-03-30 2023-03-27 炭素繊維強化複合材料およびプリプレグ

Country Status (4)

Country Link
US (1) US20250215171A1 (https=)
EP (1) EP4488320A4 (https=)
JP (1) JPWO2023190319A1 (https=)
WO (1) WO2023190319A1 (https=)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN118711467A (zh) * 2024-08-28 2024-09-27 武汉华星光电半导体显示技术有限公司 显示模组及显示设备

Citations (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH01104624A (ja) 1987-10-16 1989-04-21 Toray Ind Inc 樹脂微粒子を用いたプリプレグ
WO2008018421A1 (fr) 2006-08-07 2008-02-14 Toray Industries, Inc. Préimprégné et matériau composite renforcé avec des fibres de carbone
WO2012084197A1 (en) 2010-12-21 2012-06-28 Hexcel Composites Limited Improvements in composite materials
WO2012124450A1 (ja) * 2011-03-17 2012-09-20 東レ株式会社 プリプレグ、プリプレグの製造方法および炭素繊維強化複合材料
WO2013141916A2 (en) 2011-12-23 2013-09-26 Cytec Technology Corp. Composite materials comprising conductive nano-fillers
WO2014115844A1 (ja) * 2013-01-28 2014-07-31 東レ株式会社 プリプレグ、繊維強化複合材料および熱可塑性樹脂粒子
WO2015130368A2 (en) 2013-12-13 2015-09-03 Cytec Industries Inc. Composite materials with electrically conductive and delamination resistant properties
WO2015146781A1 (ja) 2014-03-24 2015-10-01 東レ株式会社 プリプレグおよび繊維強化複合材料
WO2016017553A1 (ja) 2014-07-28 2016-02-04 東邦テナックス株式会社 プリプレグおよび繊維強化複合材料
JP2017132932A (ja) * 2016-01-29 2017-08-03 東レ株式会社 プリプレグおよび繊維強化複合材料
JP2021172694A (ja) * 2020-04-21 2021-11-01 帝人株式会社 プリプレグ
WO2022230800A1 (ja) * 2021-04-26 2022-11-03 東レ株式会社 プリプレグ

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2473226A (en) * 2009-09-04 2011-03-09 Hexcel Composites Ltd Composite materials
JP2012193322A (ja) * 2011-03-18 2012-10-11 Toray Ind Inc プリプレグ、および炭素繊維強化複合材料
JP6833679B2 (ja) * 2014-09-22 2021-02-24 サイテック インダストリーズ インコーポレイテッド 高いｚ方向電気伝導率をもつ複合材料
JP7524904B2 (ja) * 2020-06-30 2024-07-30 東レ株式会社 繊維強化複合材料およびプリプレグの製造方法

Patent Citations (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH01104624A (ja) 1987-10-16 1989-04-21 Toray Ind Inc 樹脂微粒子を用いたプリプレグ
WO2008018421A1 (fr) 2006-08-07 2008-02-14 Toray Industries, Inc. Préimprégné et matériau composite renforcé avec des fibres de carbone
WO2012084197A1 (en) 2010-12-21 2012-06-28 Hexcel Composites Limited Improvements in composite materials
WO2012124450A1 (ja) * 2011-03-17 2012-09-20 東レ株式会社 プリプレグ、プリプレグの製造方法および炭素繊維強化複合材料
WO2013141916A2 (en) 2011-12-23 2013-09-26 Cytec Technology Corp. Composite materials comprising conductive nano-fillers
WO2014115844A1 (ja) * 2013-01-28 2014-07-31 東レ株式会社 プリプレグ、繊維強化複合材料および熱可塑性樹脂粒子
WO2015130368A2 (en) 2013-12-13 2015-09-03 Cytec Industries Inc. Composite materials with electrically conductive and delamination resistant properties
JP2017501904A (ja) * 2013-12-13 2017-01-19 サイテック インダストリーズ インコーポレイテッド 導電特性及び耐層間剥離特性を有する複合材料
WO2015146781A1 (ja) 2014-03-24 2015-10-01 東レ株式会社 プリプレグおよび繊維強化複合材料
WO2016017553A1 (ja) 2014-07-28 2016-02-04 東邦テナックス株式会社 プリプレグおよび繊維強化複合材料
JP2017132932A (ja) * 2016-01-29 2017-08-03 東レ株式会社 プリプレグおよび繊維強化複合材料
JP2021172694A (ja) * 2020-04-21 2021-11-01 帝人株式会社 プリプレグ
WO2022230800A1 (ja) * 2021-04-26 2022-11-03 東レ株式会社 プリプレグ

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See also references of EP4488320A4

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN118711467A (zh) * 2024-08-28 2024-09-27 武汉华星光电半导体显示技术有限公司 显示模组及显示设备
CN118711467B (zh) * 2024-08-28 2024-12-24 武汉华星光电半导体显示技术有限公司 显示模组及显示设备
WO2026044915A1 (zh) * 2024-08-28 2026-03-05 武汉华星光电半导体显示技术有限公司 显示模组及显示设备

Also Published As

Publication number Publication date
EP4488320A1 (en) 2025-01-08
JPWO2023190319A1 (https=) 2023-10-05
US20250215171A1 (en) 2025-07-03
EP4488320A4 (en) 2025-10-15

Similar Documents

Publication Publication Date Title
US10549499B2 (en) Composite materials with high Z-direction electrical conductivity
JP5900327B2 (ja) プリプレグ、プリプレグの製造方法および炭素繊維強化複合材料の製造方法
US11745439B2 (en) Hybrid veil as interlayer in composite materials
EP3707208B1 (en) Composites with interlaminar toughening particles and method of making the same
KR20150003800A (ko) 복합 재료들
JP7524904B2 (ja) 繊維強化複合材料およびプリプレグの製造方法
CN106133036A (zh) 预浸料坯及纤维增强复合材料
JP2009286895A (ja) プリプレグおよび繊維強化複合材料の成形方法
JP2011213991A (ja) 炭素繊維強化複合材料
JP2009242459A (ja) 樹脂組成物、プリプレグ、及びそれらの製造方法
JP6213225B2 (ja) プリプレグおよび繊維強化複合材料
JP6854591B2 (ja) プリプレグ、強化繊維、繊維強化複合材料、およびプリプレグの製造方法
WO2023190319A1 (ja) 炭素繊維強化複合材料およびプリプレグ
WO2023074733A1 (ja) 炭素繊維強化複合材料
JP2023147961A (ja) 炭素繊維強化複合材料およびプリプレグ
JP2023147962A (ja) 炭素繊維強化複合材料、プリプレグおよびエポキシ樹脂組成物
US12617161B2 (en) Hybrid veil as interlayer in composite materials
WO2025033448A1 (ja) プリプレグ、炭素繊維強化複合材料および構造体
WO2023008357A1 (ja) 炭素繊維強化複合材料
JP2023157425A (ja) 強化繊維基材およびそれを用いた繊維強化複合材料
CN119798747A (zh) 一种热固性聚合物复合材料层间增韧的方法

Legal Events

Date Code Title Description
WWE Wipo information: entry into national phase

Ref document number: 2023521748

Country of ref document: JP

121 Ep: the epo has been informed by wipo that ep was designated in this application

Ref document number: 23780329

Country of ref document: EP

Kind code of ref document: A1

WWE Wipo information: entry into national phase

Ref document number: 18850303

Country of ref document: US

WWE Wipo information: entry into national phase

Ref document number: 2023780329

Country of ref document: EP

ENP Entry into the national phase

Ref document number: 2023780329

Country of ref document: EP

Effective date: 20240930

NENP Non-entry into the national phase

Ref country code: DE

WWP Wipo information: published in national office

Ref document number: 18850303

Country of ref document: US