摘要:
Carbon fibers having a high tensile strength satisfy the relationship represented by formula (1) and one of the relationships represented by formulas (2) to (5): La ≥ 1 La ≤ − 0.5 + 0.01 × TM when 170 ≤ TM ≤ 230 La ≤ − 37.3 + 0.17 × TM when 230 TM ≤ 240 La ≤ − 2.5 + 0.025 × TM when 240 TM ≤ 300 and La ≤ 2 + 0.01 × TM when 300 TM where La is a crystal size in nm in a direction parallel to an axis of the fibers measured with by X-ray diffraction, and TM is a tensile modulus in GPa.
摘要:
An object of the present invention is to provide a prepreg capable of giving a fiber-reinforced composite material having both excellent mechanical characteristics and conductivity in the thickness direction thereof. The prepreg of the present invention is a prepreg including conductive fibers impregnated with a matrix resin, the prepreg being a prepreg having a conductive region where a conductive material is dispersed in the resin. In the present invention, it is preferred that a resin layer composed of at least the matrix resin is present on one or both surfaces of a conductive fiber layer composed of at least the conductive fibers, and the conductive region is present at least in the resin layer. In addition, it is preferred that the above-described conductive region is present continuously in the thickness direction. It is also preferred that the conductive region is a conductive region where the conductive material is dispersed in the matrix resin, and that the resin in the conductive region forms a continuous phase with the matrix resin in other regions. In the present invention, it is preferred that a volume resistivity of the conductive region is 1/1,000 or less of that of other regions of the matrix resin.
摘要:
The present invention provides a prepreg comprising: a primary pre-pregnant made of a reinforced fiber substrate and an epoxy resin composition containing at least epoxy resin and thermoplastic resin impregnated into the reinforcing fiber that forms the reinforced fiber substrate; and a surface layer made of epoxy resin composition containing at least an epoxy resin and an epoxy resin-soluble thermoplastic resin that dissolves in the epoxy resin, the surface layer being formed on one or both surfaces of the primary prepreg; the prepreg being characterized in that only one of either the epoxy resin composition of the primary prepreg or the epoxy resin composition of the surface layer contains a hardening agent for an epoxy resin.
摘要:
The present invention provides a heat-curable resin composition, which comprises (1) a heat-curable resin mixture comprising a heat-curable resin (a) and thickener particles (b) and exhibiting a viscosity (150°C) after having been held at a temperature of 150°C for 30 seconds that is a viscosity (S), and (2) a curing agent, and is characterized in that the heat-curable resin composition exhibits a lowest viscosity (R) at 80-120°C, the lowest viscosity (R) is 0.1-10 Pa·s, and the viscosity (S) and lowest viscosity (R) satisfy the relationship of formula (1): 5
摘要:
A method of opening or spreading a woven fabric, in which while leaving the fabric weaving process unchanged, the warp and weft yarns can be uniformly opened or spread through simple processing. There is provided a method of opening or spreading a woven fabric (4) produced by weaving weft yarns (3) and warp yarns (2) each obtained by bundling multiple fiber filaments (1). In the method, an abutting member (6) is disposed on the surface of the woven fabric (4) with a protective film (5) interposed therebetween. A relative displacement of the abutting member (6) to the woven fabric (4) is effected obliquely in the longitudinal direction of the warp yarns (2) or weft yarns (3) to thereby attain the opening or spreading of the warp yarns (2) or weft yarns (3).
摘要:
A carbon fiber strand which is produced by obtaining a solidified-yarn strand by spinning with a spinneret having 20,000-30,000 spinning holes, passing the strand through an interlacing nozzle having an air blowing pressure of 20-60 kPa to obtain precursor fibers, oxidizing them in heated air having a temperature of 200-280 °C to obtain oxidized fibers, subjecting these oxidized fibers to a first carbonization treatment in an inert-gas atmosphere at a temperature of 300-900 °C in which the fibers are firstly stretched in a stretch ratio of 1.03-1.06 and then secondarily stretched in a stretch ratio of 0.9-1.01, subsequently conducting a second carbonization treatment in an inert-gas atmosphere at 1,360.2,100 °C, and then conducting a surface oxidization treatment in an aqueous solution of an inorganic acid salt in a quantity of electricity of 20-100 C per g of the carbon fibers. This carbon fiber strand has a strand tensile strength of 5,650 MPa or higher, strand tensile modulus of 300 GPa or higher, and strand width of 5.5 mm or larger. No strand crack is observed in an examination by a strand crack evaluation method.
摘要:
According to the present invention there is provided a method for opening a fabric, in which warp and weft yarns can be uniformly opened using a simple method without having to alter the fabric weaving procedure. The method is a method for opening a fabric (4) produced by weaving a warp yarn (2) and a weft yarn (3), each of which having a bundled plurality of fiber filaments (1). A contact body (6) is provided to a surface of the fabric (4) with a protective film (5) interposed therebetween, and the contact body (6) is caused to move over the fabric (4) obliquely, and in a relative manner, with respect to the longitudinal direction of the warp yarn (2) or the weft yarn (3), whereby the warp yarn (2) or the weft yarn (3) is spread.
摘要:
The present invention discloses: a resin composition comprising, as essential components, 100 parts by mass of a component (A) which is an epoxy resin, 41 to 80 parts by mass of a component (B) which is thermoplastic resin particles, and 20 to 50 parts by mass (in terms of diaminodiphenylsulfone) of a component (C) which is diaminodiphenylsulfone microencapsulated with a coating agent, in which resin composition the thermoplastic resin particles (B) comprise at least thermoplastic resin particles (B 1 ) having an average particle diameter of 1 to 50 µm and thermoplastic resin particles (B 2 ) having an average particle diameter of 2 to 100 µm at a mass ratio of 3:1 to 1:3 and the average particle diameter ratio D 2 /D 1 of the average particle diameter D 2 of the thermoplastic resin particles (B 2 ) to the average particle diameter D 1 of the thermoplastic resin particles (B 1 ) is 2 or more, and a prepreg produced using the resin composition.
摘要:
A radiation-curing resin composition that includes a resin component that includes an epoxy resin and/or oxetane resin having a naphthalene structure or a biphenyl structure, a boron-based diaryliodonium salt polymerization initiator represented by a specific formula at 0.005 to 0.5 mol per kg of the resin component, and a viscosity adjusting agent, the resin composition having a viscosity at 50°C of at least 50 Pa·s, and a prepreg obtained by impregnating a fiber reinforcement with such a resin composition. This resin composition has excellent reactivity, and a prepreg formed from this resin composition and a fiber reinforcement is used for producing a composite material/member suitable for the aerospace field in particular.