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Modification method of interface between carbon fiber and non-polar resin

A non-polar resin and carbon fiber technology, applied in the field of interface modification of composite materials, can solve the problems of lack of surface activation method and low shear strength, and achieve the effects of enhanced adhesion, improved interface performance and good interface performance.

Active Publication Date: 2007-06-06
HARBIN INST OF TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0005] The purpose of the present invention is to solve the problem of low interlaminar shear strength of the composite material composed of carbon fiber and non-polar resin due to the lack of surface activation method in the treatment of existing composite material interface, thereby providing a method for carbon fiber and non-polar resin Modification Method of Polar Resin Binding Interface

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  • Modification method of interface between carbon fiber and non-polar resin
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  • Modification method of interface between carbon fiber and non-polar resin

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specific Embodiment approach 1

[0010] Specific embodiment one: this specific embodiment is carried out according to the following steps: one, pretreatment: use acetone or ethanol to remove the original coating on carbon fiber surface; two, prepare coating solution: coating solution is made of vinyl silsesquisil Oxygen and tetrahydrofuran, the quality of the vinyl silsesquioxane accounts for 1% to 2% of the total mass of the coating solution; 3. Activated carbon fiber: use air-cooled plasma at a power of 150-200W Activating the carbon fiber, so that a large amount of active species is produced on the surface of the carbon fiber; 4. Introducing the coating solution: under the condition of maintaining a vacuum, the coating solution is introduced, and the carbon fiber is soaked in the coating solution for 5 to 35 minutes, so that the surface is activated. The carbon fiber reacts with the vinyl silsesquioxane; 5. Post-treatment: take out the carbon fiber from the plasma device, and dry it in a vacuum to obtain th...

specific Embodiment approach 2

[0012] Embodiment 2: The difference between this embodiment and Embodiment 1 is: the coating solution prepared in the second step contains 2 g of vinyl silsesquioxane, and 198 g of tetrahydrofuran; the third step uses air-cooled plasma in The carbon fiber is activated for 10 minutes at a power of 175W; the fourth step is to soak the carbon fiber in the coating solution for 15 minutes; the fifth step is to dry the carbon fiber at 50°C. Other steps are the same as in the first embodiment. This specific embodiment makes a large number of unsaturated double bonds matching the polyarylene with non-polar structure appear on the surface of the fiber. The interlaminar shear strength of the composite material prepared by the silsesquioxane modified carbon fiber and polyarylacetylene silicone resin prepared by this specific embodiment by molding can reach 49.2MPa at room temperature, which is different from that of untreated carbon fiber Compared with the composite material formed, the...

specific Embodiment approach 3

[0013] Specific embodiment three: the difference between this specific embodiment and specific embodiment two is: vinyl silsesquioxane contains 4g in the coating solution prepared in the second step, and tetrahydrofuran contains 196g; Soak in the coating solution for 20min. Other steps are the same as in the second embodiment. The interlaminar shear strength of the composite material prepared by molding the silsesquioxane modified carbon fiber and polyarylacetylene silicone resin prepared in this specific embodiment at room temperature can reach 41.7MPa, which is different from that of untreated carbon fiber Compared with the composite material formed, the interlaminar shear strength increased by 22%. As shown in Figure 2, the broken line with dots represents the increase rate of the interlaminar shear strength of the composite material treated with the coating solution containing 2% (mass ratio) of vinyl silsesquioxane compared with that in the coating solution Correspondin...

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Abstract

The present invention is modification method for the combination interface between carbon fiber and non-polar resin, relates to the interface modification method for polymer-base composite material, and aims at raising the intralaminar shearing strength of composite comprising carbon fiber and non-polar resin through surface activation. The method of the present invention includes the following steps: pre-treatment, preparing coating solution; activating carbon fiber; introducing coating solution; and post-treatment. The carbon fiber and polyaryl acetylene silicon resin thus treated may be molded into composite material with resin content of 35 wt%, and this composite material has intralaminar shearing strength at room temperature up to 38-52 MPa and lowered to 32.5-37.5 MPa after high temperature oxidation.

Description

Technical field: [0001] The invention relates to composite material interface modification technology, in particular to a method for polymer-based composite material interface modification. Background technique: [0002] Advanced polymer matrix composites play an important role in aviation, aerospace, military, construction and other fields, and the interface is a unique and extremely important component of composite materials, which plays an important and even decisive role in the performance of materials , has been recognized as a basic and common research topic throughout the development of composite materials. The interface directly affects the stress transfer and dispersion between the composite fiber and the matrix, thereby affecting the off-axis performance of the composite material; the interface characteristics also affect the damage accumulation and crack propagation process inside the composite material, thereby affecting the fracture toughness of the composite ma...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): D01F11/10D06M10/00
Inventor 黄玉东张学忠刘丽刘立洵王天玉胡立江
Owner HARBIN INST OF TECH