Sandwich structure composite material and preparation method thereof

A composite material and sandwich structure technology, applied in chemical instruments and methods, layered products, electronic equipment, etc., can solve problems such as low production efficiency, difficult quality assurance, and inability to form thin-walled structures.

Active Publication Date: 2019-01-04
GUANGDONG XINXIU NEW MATERIAL CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, as an alternative material, it also has its disadvantages. The skin and foam core material need to be molded separately, and then they are bonded or co-cured into a whole
If you need an intermediate core material with a thin wall thickness such as 0.3mm thickness and a certain curved surface shape, you need to use complex mechanical equipment to cut the foam sheet into a sheet of about 0.3mm, and then heat it above the softening point and pre-bend it so that the foam core material and the shape of the mold The disadvantage is that the production efficiency is low and the quality is not easy to guarantee. In addition, the high price of foams that can withstand high temperatures, such as PMI and PPSU, is also a major factor that limits the application of high-performance foam core sandwich structure composite materials. factor
3. As a core material, balsa wood also has disadvantages. It cannot form thin-walled and thick structures, nor can it form complex curved surface structural parts.

Method used

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Examples

Experimental program
Comparison scheme
Effect test

preparation example Construction

[0027] The preparation method of sandwich structure composite material of the present invention, comprises the steps:

[0028] Provide carbon fiber unidirectional yarn or carbon fiber woven cloth and a first resin matrix, draw carbon fiber unidirectional yarn or carbon fiber woven cloth under preset tension, and compound the first resin matrix on carbon fiber unidirectional yarn or carbon fiber woven cloth On both sides, a sandwich layer is formed, and the first resin matrix is ​​melted and impregnated in carbon fiber unidirectional yarn or carbon fiber woven cloth by a hot pressing roller to form a carbon fiber prepreg;

[0029]Provide glass fiber cloth, hollow glass microspheres, and a second resin matrix, add the hollow glass microspheres into the second resin matrix, mix thoroughly, draw out the glass fiber cloth under preset tension, and place the first The mixture of the second resin matrix and hollow glass microspheres is compounded on both sides of the glass fiber clot...

Embodiment 1

[0051] The preparation method of the sandwich structure composite material described in this embodiment comprises the following steps:

[0052] Provide the following components by weight: the median particle diameter D50 is 40 μm, and the true density is 0.1 g / cm 3 ~0.5g / cm 3 100 parts by weight of hollow glass microspheres, 100 parts by weight of alcohol, 4 parts by weight of silane coupling agent, and 0.8 parts by weight of fluorocarbon surfactant were added to a high-speed disperser and stirred at a high speed at a speed of 1500 rpm to obtain a mixed solution ; Dry the treated hollow glass microspheres in an oven at 100°C.

[0053] Provide the following components by weight: 70 parts of bisphenol A glycidyl ether epoxy resin E51, 20 parts of bisphenol F glycidyl ether epoxy resin CYDF-170, 10 parts of novolac epoxy resin F51, bisphenol 7 parts of cyanamide curing agent, 3 parts of accelerator DCMU (N-(3,4-dichlorophenyl)-N', N'-dimethylurea), mix the above components and ...

Embodiment 2

[0060] The preparation method of the sandwich structure composite material described in this embodiment comprises the following steps:

[0061] Provide the following components by weight: the median particle diameter D50 is 50 μm, and the true density is 0.1 g / cm 3 ~0.5g / cm 3 100 parts by weight of hollow glass microspheres, 100 parts by weight of alcohol, 4 parts by weight of silane coupling agent, and 0.8 parts by weight of fluorocarbon surfactant were added to a high-speed disperser and stirred at a high speed at a speed of 1500 rpm to obtain a mixed solution ; Dry the treated hollow glass microspheres in an oven at 100°C.

[0062] Provide the following components by weight: 70 parts of bisphenol A glycidyl ether epoxy resin E51, 30 parts of E20, 8 parts of dicyandiamide curing agent, 1 part of 2-ethyl-4-methylimidazole, the above The components are mixed and heated to a temperature of 90°C, stirred at a high speed and mixed evenly to obtain a resin matrix, the first resi...

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Abstract

The invention discloses an interlayer structure composite material and a preparation method thereof. The composite material comprises a hollow glass microbead sandwiched layer and carbon fiber covering layers disposed on two opposite surfaces of the hollow glass microbead sandwiched layer; and the hollow glass microbead sandwiched layer is formed by hot pressing and curing glass fiber preimpregnated cloth made by virtue of a hot melt method and capable of being laid in a flat or curved mold, and the carbon fiber covering layer is formed by hot pressing and curing carbon fiber preimpregnated cloth made by virtue of a hot melt method and a preimpregnating process and capable of being laid in a flat or curved mold. The method comprises the following steps: first preparing carbon fiber preimpregnated cloth, then preparing glass fiber preimpregnated cloth, and covering two surfaces of the glass fiber preimpregnated cloth with the carbon fiber preimpregnated cloth, and hot pressing and molding. The method is simple in process, convenient to operate and low in cost; and the prepared interlayer composite material is low in density, light in weight, high in pressure resistance, excellent in bending performance and good in appearance quality.

Description

technical field [0001] The invention relates to the technical field of sandwich structure composite materials, in particular to a sandwich structure composite material containing a hollow glass bead core and a carbon fiber skin and a preparation method thereof. Background technique [0002] A structural member made of two rigid, strong skins separated by a lightweight core, increasing the moment of inertia of the structure to obtain an efficient structure resistant to bending and buckling loads, called a sandwich structure. The skin is generally a continuous fiber reinforced composite material, which mainly bears the in-plane tensile stress, compressive stress and shear stress caused by the bending moment, and the core body is honeycomb, polymer foam, balsa wood, etc. Stress and support the skin without losing its stability. After optimizing the structural design, the sandwich structure can reduce the structural weight, increase the structural rigidity, and improve the stru...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B32B9/00B32B9/04B32B17/04B32B17/06B32B27/04
CPCB32B9/007B32B9/047B32B17/04B32B17/067B32B2260/021B32B2260/025B32B2260/046B32B2262/101B32B2262/106B32B2307/546B32B2307/718B32B2307/72B32B2457/00B32B2605/08
Inventor 巫俊斌文峰汪应山
Owner GUANGDONG XINXIU NEW MATERIAL CO LTD
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