Carbon Fiber Sizing Composition for Humidity-Stable Resin Adhesion

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Solution Overview

Problem

Conventional sizing agents for carbon fibers fail to achieve sufficient interfacial adhesion with thermoplastic resins, leading to poor mechanical properties, especially under humid conditions, due to inadequate interaction between the carbon fibers and the matrix resin.

Innovation Solution

A carbon fiber-reinforced resin composition is developed, where carbon fibers are coated with a sizing agent containing a specific ratio of aliphatic and aromatic epoxy compounds, optimizing the surface chemistry to enhance interfacial adhesion by creating a gradient structure that improves interaction with both the carbon fibers and the thermoplastic resin.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If conventional sizing agents with single epoxy compound are used, then carbon fibers gain basic adhesion and bindability, but interfacial adhesion with thermoplastic resins remains insufficient especially under humid conditions

Engineering Contradiction:
Improveinterfacial adhesionVSAvoidcompatibility with thermoplastic resin
Core Design Contradiction:
ReliabilityVSAdaptability or versatility

Solution Approach 1:

The sizing agent uses a composite composition of multiple epoxy compounds (aliphatic epoxy compound, aromatic epoxy compound, and glycidyl ether compound) rather than a single compound. This composite approach enables the sizing agent to provide both adhesion to carbon fibers and compatibility with thermoplastic resins, resolving the contradiction between reliability and adaptability.

Inventive Principle:
Principle #40Composite materials

Solution Approach 2:

The invention creates a gradient structure in the sizing agent where different epoxy compounds are distributed at different concentrations. The aliphatic epoxy compound provides adhesion at the carbon fiber interface, while the aromatic epoxy compound ensures compatibility with the thermoplastic resin matrix. This local differentiation of chemical properties allows the single sizing agent to fulfill multiple functional requirements.

Inventive Principle:
Principle #3Local quality

2Reliability

If oxidation process is applied to carbon fibers to improve interfacial adhesion, then oxygen-containing functional groups are introduced to carbon fiber surface, but adhesion to thermoplastic resins remains inadequate

Engineering Contradiction:
Improveinterfacial adhesionVSAvoidprocessing complexity
Core Design Contradiction:
ReliabilityVSEase of manufacture

Solution Approach 1:

The sizing agent acts as an intermediary substance between the oxidized carbon fiber surface and the thermoplastic resin. The multiple epoxy compounds in the sizing agent bridge the gap by providing chemical groups that interact with both the oxygen-containing functional groups on carbon fibers and the thermoplastic resin matrix, thereby achieving adequate adhesion without requiring complex multi-step surface treatments.

Inventive Principle:
Principle #24Intermediary (Mediator)

3Ease of operation

If carbon fibers are coated with sizing agent to improve bindability and abrasion resistance, then fluffs and broken threads are reduced, but interfacial adhesion with matrix resin becomes insufficient

Engineering Contradiction:
ImprovebindabilityVSAvoidinterfacial adhesion
Core Design Contradiction:
Ease of operationVSReliability

Solution Approach 1:

The invention changes the chemical composition parameters of the sizing agent by incorporating multiple epoxy compounds with different molecular structures and properties. The aliphatic epoxy compound (with flexible chain structure) provides bindability and abrasion resistance, while the aromatic epoxy compound (with rigid ring structure) enhances interfacial adhesion to thermoplastic resins. This parameter optimization allows simultaneous achievement of ease of operation and reliability.

Inventive Principle:
Principle #35Parameter changes

Applied Scientific Principles

This section explains which scientific principles are used to turn an abstract innovation direction into a practical engineering solution.

Function Achieved in This Case

The composition achieves excellent interfacial adhesion and maintains high mechanical properties under humid conditions, suitable for applications in aircraft, spacecraft, and automotive components.

Implementation Method 1

excellent interfacial adhesion between the carbon fibers and a matrix resin is important in order to impart excellent characteristics of the carbon fiber

Methodology Applied
Scientific EffectInterfacial adhesion: Adhesive

Implementation Method 2

the sizing agent comprises at least an aliphatic epoxy compound (A) and an aromatic epoxy compound (B1) as an aromatic compound (B)

Methodology Applied
Scientific EffectEpoxy compound interaction: Chemical Bonding

Data Source

PatentUS10501605B2Carbon fiber-reinforced resin composition, method for manufacturing carbon fiber-reinforced resin composition, molding material, method for manufacturing molding material, and carbon fiber-reinforced resin molded article
Publication Date: 2019.12.10 TORAY INDUSTRIES INC
  • US10501605B2 patent drawing

AI summary

A carbon fiber-reinforced resin composition of the present invention includes: sizing agent-coated carbon fibers in which carbon fibers are coated with a sizing agent; and a matrix resin. The sizing agent includes at least an aliphatic epoxy compound (A) and an aromatic epoxy compound (B1) as an aromatic compound (B). The sizing agent-coated carbon fibers have a ratio (a)/(b) of 0.50 to 0.90 where (a) is the height (cps) of a component having a binding energy (284.6 eV) attributed to CHx, C—C, and C═C and (b) is the height (cps) of a component having binding energy (286.1 eV) attributed to C—O in a C1s core spectrum of the surface of the sizing agent measured by X-ray photoelectron spectroscopy at a photoelectron takeoff angle of 15°.