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Preparation method of ZIF-67 nondestructive modified carbon fiber reinforced composite material

A technology of ZIF-67, 1. ZIF-67 is applied in the fields of carbon fiber, fiber treatment, textile and paper making, and can solve problems such as poor wettability, poor bonding performance, and damage to the inherent strength of carbon fiber.

Inactive Publication Date: 2020-10-23
XIAN AERONAUTICAL POLYTECHNIC INST
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

However, the surface of carbon fiber has a turbostratic graphite structure, and its surface contains almost no active functional groups, showing chemical inertness and liquid repellency. The poor bonding performance between carbon fiber and resin matrix becomes its bottleneck.
The use of strong oxidation or high-energy radiation will damage the inherent strength of carbon fibers, and the grafting of hydrophobic nanomaterials will result in poor wettability between the fibers and the matrix. Chinese patent (application number CN201810429653.X) discloses "electrochemical polymerization modification The method of surface treatment of carbon fiber and carbon fiber composite material", using carbon fiber as anode and graphite plate as cathode, the surface of carbon fiber is treated under the action of electric current to change the surface state of carbon fiber, but this method will damage the inherent strength of carbon fiber; Chinese patent (The application number is CN201811544172.X) discloses "an isocyanate surface modified carbon fiber-polypropylene composite material and its preparation method", using polyurethane or epoxy resin sized chopped carbon fiber, and grafting on the carbon fiber by surface grafting The introduction of long-chain alkyl groups on the surface improves the interfacial binding force between the carbon fiber surface and the polypropylene matrix, but grafting macromolecular substances on the carbon fiber surface will have a large steric hindrance effect, which is not conducive to the subsequent resin impregnation process
Chinese patent (Application No. CN201210544213.1) discloses "a method for surface treatment of carbon fibers". The high-energy plasma emitted at low temperature hits the surface of carbon fibers, causing a series of physical and chemical changes on the surface of carbon fibers and obtaining a large amount of activated activated carbon. atoms to improve the bonding strength between carbon fiber and resin matrix, but this method requires high experimental techniques

Method used

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  • Preparation method of ZIF-67 nondestructive modified carbon fiber reinforced composite material

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Experimental program
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Effect test

Embodiment 1

[0050] The preparation method of the ZIF-67 non-destructively modified carbon fiber reinforced composite material of the present invention is specifically implemented according to the following steps:

[0051] Step 1, using acetone to remove pollutants on the carbon fiber surface;

[0052] Specifically: under oil bath conditions, acetone and a mixture of acetone and water are used in a Soxhlet extractor to treat carbon fibers in a supercritical state;

[0053] When using acetone for treatment, the treatment temperature is 80°C and the treatment time is 2h;

[0054] When using a mixture of acetone and water for treatment, the treatment temperature is 110°C and the treatment time is 30 minutes; the volume ratio of acetone and water in the mixture of acetone and water is 5:1;

[0055] The diameter of carbon fiber is 7-10μm;

[0056] Step 2, immersing the carbon fibers obtained in step 1 in nitric acid for treatment to obtain functionalized carbon fibers;

[0057] The treatment...

Embodiment 2

[0063] The preparation method of the ZIF-67 non-destructively modified carbon fiber reinforced composite material of the present invention is specifically implemented according to the following steps:

[0064] Step 1, using acetone to remove pollutants on the carbon fiber surface;

[0065] Specifically: under oil bath conditions, acetone and a mixture of acetone and water are used in a Soxhlet extractor to treat carbon fibers in a supercritical state;

[0066] When using acetone for treatment, the treatment temperature is 80°C and the treatment time is 2h;

[0067] When using a mixture of acetone and water for treatment, the treatment temperature is 110°C and the treatment time is 30 minutes; the volume ratio of acetone and water in the mixture of acetone and water is 5:1;

[0068] The diameter of carbon fiber is 7-10μm;

[0069] Step 2, immersing the carbon fibers obtained in step 1 in nitric acid for treatment to obtain functionalized carbon fibers;

[0070] The treatment...

Embodiment 3

[0075] The preparation method of the ZIF-67 non-destructively modified carbon fiber reinforced composite material of the present invention is specifically implemented according to the following steps:

[0076] Step 1, using acetone to remove pollutants on the carbon fiber surface;

[0077] Specifically: under oil bath conditions, acetone and a mixture of acetone and water are used in a Soxhlet extractor to treat carbon fibers in a supercritical state;

[0078] When using acetone for treatment, the treatment temperature is 80°C and the treatment time is 2h;

[0079] When using a mixture of acetone and water for treatment, the treatment temperature is 110°C and the treatment time is 30 minutes; the volume ratio of acetone and water in the mixture of acetone and water is 5:1;

[0080] The diameter of carbon fiber is 7-10μm;

[0081] Step 2, immersing the carbon fibers obtained in step 1 in nitric acid for treatment to obtain functionalized carbon fibers;

[0082] Step 3, disso...

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Abstract

The invention discloses a preparation method of a ZIF-67 nondestructive modified carbon fiber reinforced composite material, which comprises the following steps: removing pollutants on the carbon fiber surface, and immersing in nitric acid; dissolving cobalt nitrate hexahydrate into an alcoholic solution a to form a solution A, dissolving functionalized carbon fibers and 2-methylimidazole into analcoholic solution b to form a solution B, and adding the solution A into the solution B for hydrothermal reaction to obtain ZIF-67 modified carbon fibers; mixing the ZIF-67 modified carbon fibers, aramid fibers and paper fibers, and preparing a composite material prefabricated body by adopting a suction filtration molding process; and then dipping in a modified phenolic resin ethanol solution, and carrying out hot-pressing curing to obtain the ZIF-67 nondestructive modified carbon fiber reinforced composite material. ZIF-67 is grafted to carbon fibers under the hydrothermal condition, so thatthe inert smooth environment of the surfaces of the carbon fibers is improved, and the mechanical property of the composite material is improved. The method is simple in process and low in material preparation cost.

Description

technical field [0001] The invention belongs to the technical field of composite material preparation, and in particular relates to a preparation method of ZIF-67 nondestructively modified carbon fiber reinforced composite material. Background technique [0002] Carbon fiber not only has the inherent intrinsic characteristics of carbon materials, but also has the softness and processability of textile fibers, and has high specific strength, high specific modulus, high temperature resistance, chemical corrosion resistance, radiation resistance, fatigue resistance, creep resistance, etc. The series has excellent performance, so it can be used as a very important structural component. However, the surface of carbon fiber has a turbostratic graphite structure, and its surface contains almost no active functional groups, showing chemical inertness and liquid repellency. The poor bonding performance between carbon fiber and resin matrix becomes its bottleneck. The use of strong o...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): C08L61/14C08L77/10C08L97/02C08K9/04C08K7/06C08K9/02D06M11/64D06M15/37D06M101/40
CPCC08L61/14D06M11/64D06M15/37D06M2101/40C08L2205/03C08L2205/16C08L77/10C08L97/02C08K9/08C08K7/06C08K9/02Y02P20/54
Inventor 段笑杨春宋攀
Owner XIAN AERONAUTICAL POLYTECHNIC INST
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