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Method for constructing multi-scale flexible-rigid interface layers on surfaces of carbon fibers for synchronous reinforcement and toughening

A technology of strengthening and toughening, carbon fiber, applied in the direction of carbon fiber, fiber processing, textiles and papermaking, etc., can solve the problem that the structural strength and toughness of the interface layer are difficult to improve at the same time, and achieve the effect of increasing the number, roughness and surface energy.

Active Publication Date: 2021-07-20
HARBIN INST OF TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0006] The purpose of the present invention is to solve the problem that the structural strength and toughness of the interface layer between carbon fiber and resin are difficult to improve at the same time, and to provide a method for constructing a multi-scale soft-rigid interface layer on the surface of carbon fiber to simultaneously strengthen and toughen. Based on the respective advantages of polyethyleneimine and metal-organic framework compounds, the interfacial bonding performance between carbon fiber and resin is effectively strengthened through the chemical reaction between the multi-scale "flexible-rigid" interface layer structure and the carbon fiber and resin matrix. At the same time, the use of branched polyethyleneimine can produce large plastic deformation and the metal-organic framework compound’s own energy absorption effect simultaneously improves the interfacial fracture toughness of the composite material, which has a certain effect on the construction of the interface layer of carbon fiber reinforced resin matrix composites. Its guiding significance further expands its application in high-speed transportation and other fields

Method used

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  • Method for constructing multi-scale flexible-rigid interface layers on surfaces of carbon fibers for synchronous reinforcement and toughening
  • Method for constructing multi-scale flexible-rigid interface layers on surfaces of carbon fibers for synchronous reinforcement and toughening

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specific Embodiment approach 1

[0021] Specific Embodiment 1: This embodiment describes a method for constructing a multi-scale flexible-rigid interface layer on the surface of carbon fibers to simultaneously strengthen and toughen. The method includes the following steps:

[0022] Step 1, cleaning and drying the carbon fiber; the purpose is to remove the sizing agent, coating, etc. on the surface of the fiber product, so as to facilitate the modification of the fiber fibril;

[0023] Step 2, putting the cleaned and dried carbon fibers and excess nitric acid into a reaction vessel for oxidation treatment to obtain carbon fibers with a large amount of carboxyl groups on the surface;

[0024] Step 3. Use the aqueous solution of branched polyethyleneimine and the suspension of metal-organic framework compound to jointly build a multi-scale "flexible-rigid" interface layer structure on the surface of the fiber, that is, the aqueous solution of branched polyethyleneimine, the metal-organic framework compound The ...

specific Embodiment approach 2

[0026] Specific embodiment 2: A method for constructing a multi-scale soft-rigid interface layer on the surface of carbon fibers described in specific embodiment 1 to simultaneously strengthen and toughen. In step 1, the cleaning liquid is acetone, and the cleaning temperature is 50-80 ° C. The cleaning time is 12-60 hours, the drying temperature is 40-90°C, and the drying time is 3-10 hours. Acetone has a low boiling point, and when using acetone, it needs to be below 80°C. Since the carbon fiber is coated with a sizing agent when it leaves the factory, in order to clean the sizing agent, the cleaning time is limited to more than 12 hours, and the cleaning time is 60 hours is enough to clean it. In order to remove acetone, it is sufficient to dry at 40-90°C for 3-10 hours, and the drying time is shortened when the temperature is high.

specific Embodiment approach 3

[0027] Specific embodiment three: a method for constructing a multi-scale flexible-rigid interface layer on the surface of carbon fibers to simultaneously strengthen and toughen the method described in specific embodiment one. In step two, the temperature of the oxidation treatment is 60-80 ° C, and the It is 60min~240min. When the temperature is higher than 80 ℃, the experimental operation will be very dangerous. When the reaction time is less than 60 minutes, the degree of oxidation is not enough, and it is difficult to carry out the next reaction. When the reaction time is more than 240 minutes, the oxidation will bring serious physical defects to the fiber, thus destroying the bulk strength of the fiber to a large extent.

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Abstract

The invention discloses a method for constructing multi-scale flexible-rigid interface layers on the surfaces of carbon fibers for synchronous reinforcement and toughening. The method comprises the following steps: cleaning and drying the carbon fibers; putting the cleaned and dried carbon fibers and excessive nitric acid into a reaction container for oxidation treatment to obtain the carbon fibers with a large number of carboxyl groups on the surfaces; jointly constructing multi-scale flexible-rigid interface layer structures on the surfaces of the fibers by using an aqueous solution of branched polyethyleneimine and a suspension of a metal-organic framework compound; and cleaning and drying the modified carbon fibers. According to the method, the advantages of the branched polyethyleneimine and the metal-organic framework compound are combined, and the interface bonding performance between the carbon fibers and resin matrices is effectively enhanced through the multi-scale flexible-rigid interface layer structures and chemical reactions between the carbon fibers and the resin matrices.

Description

technical field [0001] The invention belongs to the technical field of carbon fiber surface modification, and in particular relates to a method for constructing a multi-scale soft-rigid interface layer on the surface of carbon fiber to simultaneously strengthen and toughen. Background technique [0002] In view of the fact that carbon fiber has high strength, high modulus, low weight and excellent environmental stability, its reinforced epoxy resin-based composites are widely used in aviation, ships, automotive energy and other fields. On the basis of meeting the requirements of mechanical properties Significantly reduced weight. [0003] However, due to the smooth, non-polar and chemically inert surface of carbon fiber, the interface compatibility with the resin matrix is ​​poor, and the existence of a weak interface can easily cause irreversible damage to the material; at the same time, the modulus of carbon fiber is high, and the toughness of epoxy resin is insufficient, ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): D06M11/65D06M15/61D06M15/37D06M101/40
CPCD06M11/65D06M15/61D06M15/37D06M2101/40
Inventor 刘丽普饮川马震宇白永平
Owner HARBIN INST OF TECH
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