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Composite material prepreg for restoring ultraviolet light curing structure and preparation method thereof

A composite material and curing structure technology, applied in the field of materials, can solve problems such as limited curing thickness, incomplete curing of thicker products, poor mechanical properties of cured products, etc., and achieve the effect of facilitating promotion and improving light curing efficiency

Inactive Publication Date: 2015-01-28
WUHAN UNIV OF TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The technical problem to be solved by the present invention is: the cured thickness is limited (within about 5mm) in the ultraviolet light curing of composite materials at present, the curing of thicker products is not complete (the curing degree of the shadow and the backlight part is not enough), the curing is uneven and the mechanical properties of the cured product Poor and other problems, provide a composite material prepreg and its preparation method that can be used in some specific fields such as non-excavation light-cured rapid repair of municipal drainage pipes, and solve the problem that large thickness (above 10mm) composite products cannot pass through ultraviolet rays. Technical problems of light one-time fast curing (within 10min)

Method used

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Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0033] The composite material prepreg (about 4mm thick) for UV curing structure repair provided by this embodiment consists of resin mixture (①resin matrix, ②photoinitiator, ③photosensitization accelerator, ④thermal initiator) and reinforcing material (⑤ Alkali-free glass fiber grid cloth) is prepared according to a certain proportion. The proportion of these five raw materials is calculated in parts by weight, which is 100:2:0.5:1:(80-100).

[0034] The above-mentioned composite material prepreg for UV curing structure repair is prepared by the following method, and the steps include:

[0035] (1) Choose TH230 vinyl ester resin as the base material;

[0036] (2) Select Darocur1173 (2-hydroxyl-2-methyl-1-phenylacetone) as photoinitiator;

[0037] (3) Select stannous octoate matched with Darocur1173 as photosensitization accelerator;

[0038] (4) Select BPO (benzoyl peroxide) matched with Darocur1173 as thermal initiator;

[0039] (5) Blend the resin, select the non-alkali g...

Embodiment 2

[0043] The composite material prepreg (about 6 mm thick) for UV curing structure repair provided by this embodiment consists of resin mixture (①resin matrix, ②photoinitiator, ③photosensitization accelerator, ④thermal initiator) and reinforcing material (⑤ Alkali-free glass fiber grid cloth) is prepared according to a certain proportion. The proportion of these five raw materials is calculated in parts by weight, which is 100:2:0.5:1:(80-100).

[0044] The above-mentioned composite material prepreg for UV curing structure repair is prepared by the following method, and the steps include:

[0045] (1) Choose TH230 vinyl ester resin as the base material;

[0046] (2) Select Irgacure184 (1-hydroxycyclohexyl phenyl ketone) photoinitiator;

[0047] (3) Select stannous octoate matching Irgacure184 as photosensitizer;

[0048] (4) AIBN (azobisisobutyronitrile) matching with Irgacure184 is selected as thermal initiator;

[0049] (5) extract approximately 80% styrene in the original ...

Embodiment 3

[0054] The composite material prepreg (about 8mm thick) that this embodiment provides for UV-curable structural repair is made of resin mixture (①resin matrix, ②photoinitiator, ③photosensitization accelerator, ④thermal initiator A, ⑤thermal initiator B) and the reinforcing material (⑥ non-alkali glass fiber grid cloth) are prepared in a certain proportion. The proportions of these six raw materials are calculated in parts by weight, which are 100:2:0.8:1:1 in turn: (80-100).

[0055] The above-mentioned composite material prepreg for UV curing structure repair is prepared by the following method, and the steps include:

[0056] (1) Choose TH230 vinyl ester resin as the base material;

[0057] (2) Select Irgacure184 (1-hydroxycyclohexyl benzophenone) photoinitiator;

[0058] (3) select stannous octoate as photosensitizer;

[0059] (4) BPO (dibenzoyl peroxide) and MEKP (methyl ethyl ketone peroxide) are selected as thermal initiators A and B;

[0060] (5) extract approximate...

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Abstract

The invention provides a composite material prepreg for quickly ultraviolet light curing a resin base structure reinforced by glass fibers with certain thickness and a preparation method thereof. In the method, a common free radical curing resin as a matrix, a proper photoinitiator, a thermal initiator and other assistants are preferably selected to form a light-thermal composite initiation system, a glass fiber textile is used as a reinforcement material, and the composite material prepreg with a certain thickness is prepared by a proper compound process. The prepreg can be cured by irradiating ultraviolet light on a single surface for 10 minutes, and the light curing thickness at one time can be higher than 15 mm. By adopting the invention, the existing technical problem that the ultraviolet light cannot be used for curing composite material structural members with large thicknesses (10-15 mm and larger) at one time is solved, the composite material prepreg is cured more conveniently and efficiently. The light-cured resin and the composite material thereof express huge application prospect and market potential in some special fields, for example, trenchless repair of municipal drainage pipelines.

Description

technical field [0001] The invention relates to the field of materials, in particular to a composite material prepreg with a relatively large thickness (10-15mm) cured by one-time single-sided irradiation of ultraviolet light (within 10 minutes) and using a free radical curable resin as a matrix and its preparation method. Background technique [0002] With the continuous development of the application of polymer composite materials, its curing methods are becoming more and more abundant to meet various actual needs. The rapid UV curing technology of composite resin matrix has developed rapidly in recent years. Compared with traditional thermal polymerization, UV curing has a series of outstanding advantages: ① Fast speed, which can be cured within a few seconds at the fastest, which greatly saves time , which improves production efficiency; ② less pollution, most of the diluents used for UV curing are active monomers, which participate in the curing reaction, and the solid...

Claims

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Application Information

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IPC IPC(8): C08L101/06C08L51/00C08L51/08C08K7/14C08J5/04
Inventor 段华军王钧杨小利唐玉山陈晞胡智枫陈小双
Owner WUHAN UNIV OF TECH
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