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Carbon fiber coated with sizing agent, method for producing carbon fiber coated with sizing agent, prepreg, and carbon fiber-reinforced composite material

A manufacturing method and technology of prepregs, which are applied in the fields of carbon fiber manufacturing methods, carbon fiber reinforced composite materials, prepregs and carbon fibers, can solve problems such as low reactivity and difficulty in achieving high adhesion of matrix resins, and achieve Less change over time, excellent adhesion, excellent heat resistance and strength properties

Active Publication Date: 2016-11-02
TORAY IND INC
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0016] In addition, Patent Document 19 discloses that a polyfunctional aliphatic compound exists in the inner layer of the sizing agent, and a low-reactivity aromatic epoxy resin and aromatic-based reactant exist in the outer layer, and it can be expected that the prepreg can be maintained for a long period of time. However, since there is no polyfunctional aliphatic compound with high adhesiveness on the surface layer of the sizing agent, it is difficult to achieve high adhesiveness with the matrix resin

Method used

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  • Carbon fiber coated with sizing agent, method for producing carbon fiber coated with sizing agent, prepreg, and carbon fiber-reinforced composite material
  • Carbon fiber coated with sizing agent, method for producing carbon fiber coated with sizing agent, prepreg, and carbon fiber-reinforced composite material
  • Carbon fiber coated with sizing agent, method for producing carbon fiber coated with sizing agent, prepreg, and carbon fiber-reinforced composite material

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0439] This embodiment includes the following I process, II process and III process.

[0440] ・Step I: A step of manufacturing carbon fiber used as a raw material

[0441] A copolymer composed of 99 mol% of acrylonitrile and 1 mol% of itaconic acid was dry-wet spun and fired to obtain a total number of filaments of 24,000, a total fineness of 1,000Tex, a specific gravity of 1.8, and a strand tensile strength of 5.9GPa. Carbon fibers with a tensile modulus of elasticity of 295GPa. Next, the carbon fiber was subjected to electrolytic surface treatment under the condition that an aqueous solution of ammonium bicarbonate with a concentration of 0.1 mol / l was used as an electrolytic solution and the electric quantity was 80 coulombs per 1 g of carbon fiber. The carbon fibers subjected to the electrolytic surface treatment were then washed with water and dried in heated air at a temperature of 150° C. to obtain carbon fibers as raw materials. At this time, the surface oxygen conce...

Embodiment 2~8

[0448] ・Step I: A step of producing carbon fiber used as a raw material

[0449] It carried out similarly to Example 1.

[0450] ・The second step: the step of attaching the sizing agent to the carbon fiber

[0451] Carbon fibers coated with a sizing agent were obtained in the same manner as in Example 1 except that the component (B1) shown in Table 1 was used as the sizing agent. Next, measure the epoxy equivalent of the sizing agent, measure the surface of the sizing agent by X-ray photoelectron spectroscopy, interfacial shear strength (IFSS) of the carbon fiber coated with the sizing agent, and the mixture of the sizing agent and latent curing agent (E) The rising temperature (ΔTg) of the glass transition temperature, the amount of aliphatic epoxy compound (A) eluted from the carbon fiber coated with the sizing agent. It can be seen that the epoxy equivalent of the sizing agent, the chemical composition of the sizing agent surface, ΔTg, and the elution amount of the alipha...

Embodiment 9~13

[0457] ・Step I: A step of producing carbon fiber used as a raw material

[0458] It carried out similarly to Example 1.

[0459] ・The second step: the step of attaching the sizing agent to the carbon fiber

[0460] Carbon fibers coated with a sizing agent were obtained in the same manner as in Example 1 except that the component (A) shown in Table 2 was used as the sizing agent. Next, measure the epoxy equivalent of the sizing agent, measure the surface of the sizing agent by X-ray photoelectron spectroscopy, interfacial shear strength (IFSS) of the carbon fiber coated with the sizing agent, and the mixture of the sizing agent and latent curing agent (E) The rising temperature (ΔTg) of the glass transition temperature, the amount of aliphatic epoxy compound (A) eluted from the carbon fiber coated with the sizing agent. It can be seen that the epoxy equivalent of the sizing agent, the chemical composition of the sizing agent surface, ΔTg, and the elution amount of the aliphat...

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Abstract

The present invention provides sizing agent-coated carbon fibers excellent in adhesion between carbon fibers and matrix resins, stability of composite properties in the case of long-term storage of prepregs, and high-order processability, and methods of the sizing agent-coated carbon fibers Manufacturing methods, prepregs and carbon fiber reinforced composites. The present invention is a carbon fiber coated with a sizing agent containing at least an aliphatic epoxy compound (A) and an aromatic epoxy compound (B1) as an aromatic compound (B) on the carbon fiber, and is characterized in that AlKα1,2 is used as X-ray source, using X-ray photoelectron spectroscopy to measure the surface of the sizing agent at a photoelectron take-off angle of 15°, the C1s core level energy spectrum (a) is assigned to the bonds of CHx, C-C, and C=C The ratio (a) / (b) of the height (cps) of the component with energy (284.6eV) and (b) the height (cps) of the component attributable to the bond energy (286.1eV) of C-O is 0.50 to 0.90.

Description

technical field [0001] The present invention relates to a carbon fiber coated with a sizing agent suitable for sports applications such as golf clubs, fishing rods, and other general industrial applications represented by aircraft components, spacecraft components, automobile components, and ship components, and the carbon fiber coated with a sizing agent. A method for manufacturing carbon fibers of a sizing agent, a prepreg, and a carbon fiber-reinforced composite material. More specifically, the present invention relates to excellent mechanical properties in severe environments such as low temperatures, and when an epoxy resin suitable as a structural material is used as a matrix resin, the matrix resin has excellent adhesion to carbon fibers and can suppress long-term A sizing agent-coated carbon fiber having reduced physical properties during storage, a method for producing the sizing agent-coated carbon fiber, a prepreg, and a carbon fiber-reinforced composite material. ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): D06M13/11D06M15/55D06M101/40
CPCD06M13/11D06M2101/40C08J5/06C08J2363/00Y10T428/2918Y10T428/249944D06M15/55C08J5/248D01F11/14
Inventor 市川智子远藤真大皷宽小林正信荒井信之三角润
Owner TORAY IND INC