Preparation of carbon fiber/epoxy resin prepreg sprayed with aminated carbon nanotubes

A carbon nanotube and epoxy resin technology, applied in the field of carbon fiber composite material preparation, can solve the problems of limited carbon nanotube addition, high preparation cost, and difficulty in large-scale application, and achieve modulus and interlayer shear Increased strength, improved compressive strength and modulus, and easy promotion and application

Inactive Publication Date: 2015-04-29
BEIJING UNIV OF CHEM TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The published patents US8187703 B2 and CN102140230 A use mechanical stirring to blend functionalized carbon nanotubes with epoxy resin to improve the performance of composite materials by strengthening the resin matrix. The effect of material interface properties is not obvious
Although there have been reports on the use of thermoplastic polymer fibers containing carbon nanotubes to reinforce and toughen carbon fiber composites, for example, the disclosed patent CN102794952 A uses the fiber film containing oriented carbon nanotubes prepared by electros

Method used

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Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0019] Component 1 is multi-walled carbon nanotubes grafted on the surface of ethylenediamine, which is obtained by TNMC3 carboxylated multi-walled carbon nanotubes produced by Chengdu Zhongke Times Nano Co., Ltd. through acyl chloride and amination treatment. The surface grafting ratio of amino groups is 2.5wt%, the outer diameter of carbon nanotubes is 10~30nm, and the average length is 1μm; component 2 is N,N-dimethylformamide, with a purity of ≥99%, produced by Yangzhou Yaguan Chemical Co., Ltd.; component 3 is Homemade Toray ? Unidirectional prepreg of T700-12K carbon fiber / 4,4′diaminodiphenylmethane tetraglycidylamine epoxy resin, the curing agent is 4,4′diaminodiphenylsulfone, and the thickness of the prepreg is 0.15 mm, surface density is 220g / m 2 . Step 1: Add multi-walled carbon nanotubes grafted on the surface of ethylenediamine into N,N-dimethylformamide, the mixing amount of carbon nanotubes is 3 wt%, and ultrasonically oscillate for 1 hour to form a uniform mi...

Embodiment 2

[0022] Component 1 is multi-walled carbon nanotubes grafted on the surface of ethylenediamine, which is obtained by TNMC3 carboxylated multi-walled carbon nanotubes produced by Chengdu Zhongke Times Nano Co., Ltd. through acyl chloride and amination treatment. The surface grafting ratio of amino groups is 2.1wt%, the outer diameter of carbon nanotubes is 10-30nm, and the average length is 1μm; component 2 is tetrahydrofuran, with a purity ≥ 99%, produced by Shanghai Nanze Chemical Co., Ltd.; component 3 is self-made Toray ? T700-12K carbon fiber / 4,4′diaminodiphenylmethane tetraglycidylamine epoxy resin unidirectional prepreg, the curing agent is 4,4′diaminodiphenylsulfone, the thickness is 0.15mm, the surface The density is 220g / m 2 . Step I: adding multi-walled carbon nanotubes grafted on the surface of ethylenediamine into tetrahydrofuran, the mixing amount of carbon nanotubes is 10wt%, and ultrasonically oscillating for 1 hour to form a uniform mixed solution. Put the ul...

Embodiment 3

[0025] Component 1 is multi-walled carbon nanotubes grafted on the surface of ethylenediamine, which is obtained by TNMC3 carboxylated multi-walled carbon nanotubes produced by Chengdu Zhongke Times Nano Co., Ltd. through acyl chloride and amination treatment. The surface grafting ratio of amino groups is 1.5wt%, the outer diameter of carbon nanotubes is 10~30nm, and the average length is 1μm; component 2 is N,N-dimethylformamide, with a purity of ≥99%, produced by Yangzhou Yaguan Chemical Co., Ltd.; component 3 is Homemade Toray ?T700-12K carbon fiber / 4,4'diaminodiphenylmethane tetraglycidylamine epoxy resin plain fabric prepreg, the curing agent is 4,4'diaminodiphenylsulfone, the thickness is 0.15mm, the surface The density is 350g / m 2 . Step I: Add multi-walled carbon nanotubes grafted on the surface of ethylenediamine into N,N-dimethylformamide, the mixing amount of carbon nanotubes is 20wt%, and ultrasonically oscillate for 1 hour to form a uniform mixed solution. Pu...

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Abstract

The invention belongs to the field of preparation of composite materials, and particularly relates to a preparing method of a carbon fiber prepreg sprayed with carbon nanotubes in an electrostatic manner. The method is characterized in that: the surface of a carbon fiber/epoxy resin prepreg is rapidly sprayed with the amino-grafted carbon nanotubes by adoption of an electrostatic spraying technology, thus obviously improving compression strength and modulus and interlaminar shear strength of a carbon fiber composite material. The method comprises following technical steps of: I) grinding the amino-grafted carbon nanotubes and a preferred electrostatic spraying agent in a ball mill according to a certain ratio to obtain a uniform and stable suspension; II) putting the suspension obtained in the step I) into an electrostatic spraying device, and uniformly spraying the surface of the carbon fiber/epoxy resin prepreg with the carbon nanotubes; and III) controlling the thickness of a carbon nanotube coating on the surface of the carbon fiber prepreg to be 10-80 [mu]m. The interlaminar content of the carbon nanotubes in the composite material is controllable. A processing process of the composite material is not influenced. The method is simple and convenient in operation and prone to popularization and application in practical production.

Description

technical field [0001] The invention belongs to the field of preparation of carbon fiber composite materials, in particular to a preparation method of amino-grafted carbon nanotube electrostatically sprayed carbon fiber / epoxy resin unidirectional prepreg or fabric prepreg. Background technique [0002] Carbon fiber / epoxy resin composites have a series of excellent properties such as high strength, high modulus, low density, and dimensional stability, and have been widely used in aerospace, energy transportation, sports equipment, and military industries. However, the current carbon fiber / epoxy resin composites still have problems such as easy delamination between layers, poor impact resistance, and low mechanical properties perpendicular to the fiber direction, which make it difficult to meet the application requirements of some advanced composite materials. These properties are mainly affected by the interface properties between the resin matrix and carbon fibers. Improving...

Claims

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Application Information

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IPC IPC(8): C08J7/06C08L63/00C08K9/04C08K7/06B32B27/04
Inventor 隋刚张清杰杨小平李刚杨青
Owner BEIJING UNIV OF CHEM TECH
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