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A composite material sandwich structure and its preparation method and application

A technology of composite materials and structures, applied in the field of composite materials, can solve problems such as low degree of production automation, long molding cycle, and insufficient rigidity, and achieve the effect of improving market competitiveness, light weight, and good rigidity

Active Publication Date: 2018-08-31
GUANGZHOU KINGFA CARBON FIBER NEW MATERIALS DEV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, the sandwich structure is a carbon fiber composite material plate formed by ordinary resin into a sandwich structure. It is a common manufacturing scheme on the market at present, and has problems such as low strength, insufficient rigidity, long molding cycle, low degree of production automation, and high cost.

Method used

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  • A composite material sandwich structure and its preparation method and application

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0039] Taking epoxy resin as the matrix, adding 10wt% lightweight filler (composed of 60wt% hollow glass microspheres and 40wt% mixture composed of talcum powder, aluminum powder, silicon carbide powder and silicon nitride) to the epoxy resin matrix, and 40wt% carbon fiber (size 3-5mm), heated to 120°C in the mold, maintained at a pressure of 50kg, and mixed for 30 minutes to form a core material, the specific gravity of the core material is 1.1g / cm 3, the thickness is 1.0mm, the elastic modulus is 23000 MPa according to ASTM D 638 test, and the shear modulus is 80 MPa according to ASTMD 638 test;

[0040] In a mold with a smooth surface, the upper and lower sides of the above-mentioned core material are covered with a transition film adhesive layer (thickness 0.05mm) composed of 40wt% thermosetting epoxy resin and glass fiber woven cloth (50gsm), and then A resin-based fiber reinforcement composed of epoxy resin and carbon fiber is pasted on the adhesive layer of the transiti...

Embodiment 2

[0042] Based on epoxy resin, by adding 30wt% lightweight filler (consisting of 70wt% hollow glass microspheres and 30wt% mixture composed of talcum powder, aluminum powder, silicon carbide powder and silicon nitride) in the epoxy resin matrix and 20wt% carbon fiber (size 50mm), heated to 130°C in the mold, maintained at a pressure of 80kg, and molded for 40 minutes to form a core material. The specific gravity of the core material is 0.8g / cm 3 , the thickness is 1.0mm, the elastic modulus is 12000 MPa according to ASTM D 638 test, and the shear modulus is 60 MPa according to ASTM D 638 test;

[0043] The resin-based fiber reinforcement composed of epoxy resin and carbon fiber 3K woven cloth, the transition adhesive film bonding layer (thickness 0.1mm) composed of 50wt% thermosetting epoxy resin and carbon fiber 3K woven cloth, and the above-mentioned core material were placed on a smooth surface. Composite heating and curing in the surface plate mold, the heating pressure is c...

Embodiment 3

[0045] Based on epoxy resin, by adding 50wt% lightweight filler (consisting of 80wt% hollow glass microspheres and 20wt% mixture composed of talcum powder, aluminum powder, silicon carbide powder and silicon nitride) in the epoxy resin matrix and 10wt% basalt fiber (size 20mm) are heated to 140°C in the mold, the pressure is maintained at 30kg, and the molding time is 50min to form a core material. The specific gravity of the core material is 0.6g / cm 3 , the thickness is 1.0mm, the elastic modulus is 6500 MPa according to ASTM D 638 test, and the shear modulus is 30 MPa according to ASTM D 638 test;

[0046] The resin-based fiber reinforcement composed of epoxy resin and basalt fiber woven cloth, the transition adhesive film bonding layer (thickness 0.06mm) composed of 60wt% thermosetting epoxy resin and glass fiber woven cloth (specification 100gsm), and the above core The material is compositely heated and solidified in a flat mold with a smooth surface, the heating pressure...

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Abstract

The invention discloses a composite material sandwich structure and its preparation method and application, comprising a core material (I), a resin-based fiber reinforcement (II) arranged on the upper and lower surfaces of the core material (I), and a The transition film bonding layer (III) between the material (I) and the resin-based fiber reinforcement (II), the resin-based fiber reinforcement (II) is composed of a resin matrix and a fiber reinforcement, and the core material (I ) is composed of epoxy resin, lightweight fillers and fibers, the specific gravity of the core material (I) is 0.3g / cm3~1.2g / cm3, and the thickness is 0.1mm~5.0mm. The composite sandwich structure prepared by the present invention not only has the advantages of light weight, high strength and good rigidity, but also can significantly reduce the cost of products and improve market competitiveness; the preparation process is simple, and can be applied to 3C consumer electronics industry, Surface structural panels such as home appliance industry, automobile industry, aviation, rail transit industry and related chassis.

Description

technical field [0001] The invention relates to the field of composite materials, in particular to a sandwich structure of composite materials and its preparation method and application. Background technique [0002] In recent years, light-weight, thin-walled and high-rigidity components have been widely used in computers, communication industries, home appliance industries, and automotive parts, building parts, and panel parts. As a member that can ensure mechanical properties and improve lightness, a sandwich structure formed by arranging fiber-reinforced resin (FRP) reinforced by continuous reinforcing fiber groups on the skin of a lightweight core material is known. In order to reduce the weight, a lighter core material is selected. Balsa wood core, honeycomb core or polyurethane foam core are frequently used as core materials. However, the existing known balsa cores, honeycomb cores or polyurethane foam cores are difficult to prepare thinner core materials. Even if thi...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B32B27/08B32B27/04B32B27/20B32B27/36B32B27/38B32B27/40B32B27/42B32B7/12B32B37/06B32B37/10B32B37/12
Inventor 黄险波陈大华蒋新范欣愉卢勇高雄
Owner GUANGZHOU KINGFA CARBON FIBER NEW MATERIALS DEV