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Microwave-assisted efficient construction method for high-strength interface of carbon-based reinforcement/resin composite material

A resin composite material and microwave-assisted technology, which is applied in the field of composite materials, can solve the problems of carbon-based reinforcement mechanical property damage, difficult control of uniformity, low efficiency, etc., to achieve the effect of high efficiency and quick enhancement, and solve the loss of mechanical properties

Active Publication Date: 2020-08-28
BEIJING UNIV OF CHEM TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, the application of microwave in carbon-based reinforcement / resin composites has the disadvantages of low practical application efficiency and poor controllability.
In summary, the main problems in the application of microwave in the construction of carbon-based reinforcement / resin composite material interface are as follows: 1. Carbon-based reinforcement is prone to discharge in the microwave field, and the modification of carbon-based reinforcement can be modified simultaneously. The degree and uniformity are not easy to control, and it is easy to cause detonation. The discharge at the defect and the tip seriously affects the interface strength and mechanical properties of the carbon-based reinforcement / resin composite; 2. Microwave etching has certain effects on the mechanical properties of the carbon-based reinforcement itself damage to the carbon-based reinforcement, its own structure, defects, etc. all affect the degree of microwave absorption, and it is difficult to control the degree of etching when the carbon-based reinforcement is activated; 3. In the traditional construction of the carbon-based reinforcement / resin composite interface , the interface sizing agent mainly enhances the interface through adhesion, and the interface connection is weak, and the sizing agent required for different carbon-based reinforcements is very different; 4. The traditional method of carbon-based reinforcement / resin composite interface construction is too It is cumbersome, requires long-term and multi-process processing, and also has certain damage to the performance of carbon-based reinforcements

Method used

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  • Microwave-assisted efficient construction method for high-strength interface of carbon-based reinforcement/resin composite material
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  • Microwave-assisted efficient construction method for high-strength interface of carbon-based reinforcement/resin composite material

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Experimental program
Comparison scheme
Effect test

Embodiment 1

[0022] The mass parts of epoxy resin, amine curing agent and diluent are prepared according to the ratio of 60:37:40. The epoxy resin adopts 4,5-epoxyhexane-1,2-dicarboxylic acid diglycidyl ester, and the amine curing agent adopts 1,3-bis-(γ-aminopropyl)-5,5-dimethyl For hydantoin, the diluent is ethylene glycol diglycidyl ether. The carbon-based reinforcement is modified into graphene microplatelets, and nickel phthalocyanine nanowires act as both transition metal-type catalysts and nanoparticles. Grind the graphite powder and the nickel phthalocyanine nanowire sheet fully separately, then mix them according to the mass ratio of 50:1.5, and fully mix them with a double-helix conical mixer for 0.5h, so that the appearance of the mixed nanoparticles no longer presents the original nanoparticles The state of the ingredients forms a powdery precursor. Subsequently, 1.5 g of the powdery precursor and 50 mL of deionized water were treated with magnetic stirring at a rate of 3500 ...

Embodiment 2

[0027] Toray T800 carbon fiber was desized by reflux with acetone for 24 hours to prepare desized fiber tow. Grind ferrous chloride, graphite powder ink and zinc oxide nanowires fully separately, then mix them according to the mass ratio of 1:50:0.5, and fully mix them with a double-helix conical mixer for 0.5h, so that the appearance of the mixed nanoparticles The state of the original nanoparticle composition is no longer present, and a powdery precursor is formed. Subsequently, 1.5 g of well-mixed nanoparticles and 50 mL of 1-butyl-3-methylimidazolium tetrafluoroborate were treated with magnetic stirring at a rate of 3500 rpm for 1 h, while removing insufficiently ground nanoparticles to prepare a powder Precursor dispersion. In the resin system, the main resin is a compound of multifunctional cycloaliphatic epoxy resin and triglycidyl isocyanate with a mass fraction of 40:60, and the curing agent is 1-cyanoethyl-2-ethyl- A compound of 4-methylimidazole and 2,2-bis(amino-...

Embodiment 3

[0032] The main resin is a compound of triglycidyl tripolyisocyanate and 1,3-diglycidyl-5,5-dimethylhydantoin epoxy resin with a mass fraction of 50:50, and the curing agent is 2, 2-bis(amino-4-hydroxyphenyl)hexafluoropropane and 1-cyanoethyl-2-ethyl-4-methylimidazole are at a mass fraction of 30:10, and the reactive diluent is diglycidyl adipate The ratio of ester, main resin, curing agent, and reactive diluent in parts by mass is 100:40:20. Nickel phthalocyanine nanowires act as both transition metal-type catalysts and nanoparticles. Grind graphite powder and nickel phthalocyanine nanowires fully separately, then mix them at a mass ratio of 50:1.5, and mix them thoroughly for 0.5 hours, so that the appearance of the mixed nanoparticles no longer shows the state of the original nanoparticle components, and a cage-like interface is prepared Structural precursors. Then, 1.5 g of well-mixed nanoparticles and 50 mL of N,N dimethylformamide were treated with magnetic stirring at...

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Abstract

The invention discloses a microwave-assisted efficient construction method for a high-strength interface of a carbon-based reinforcement / resin composite material, and belongs to the field of compositematerials. The method comprises the following step: modifying a carbon-based reinforcement by nanoparticles through a synergistic effect of physical coating and chemical grafting so as to form an interface (a cage-shaped interface structure) coated with a cage-shaped structure carbon source material shell. Based on the microwave irradiation activation principle, the activation of the carbon-basedreinforcement and the uniform self-assembly of the nanoparticles are realized by adjusting the ratio of the transition metal catalyst to the carbon source material to the nanoparticles. Compared withcomposite material traditional interface enhancement, the method of the invention is more efficient and faster, realizes the nanometer reinforcement of the interface of the carbon-based reinforcement / resin composite material, solves the problem that the structural integrity and strength of the carbon-based reinforcement are damaged by discharging and sparking of the carbon-based reinforcement ina microwave field, and has important significance in preparing the high-performance carbon-based reinforcement / resin composite material; and the high-strength interface can be applied to the high-techfields of composite material pressure containers, aerospace crafts and the like.

Description

technical field [0001] The invention belongs to the field of composite materials, and mainly relates to a microwave-assisted high-efficiency construction method for a carbon-based reinforcement / resin composite material interface. Background technique [0002] Carbon-based reinforcement / resin composites are widely used in the fields of transportation, aerospace and sporting goods due to their excellent properties such as high specific strength, high specific modulus, low density and corrosion resistance. In the field of carbon fiber reinforced resin composites, the carbonization process of carbon fiber production leads to the chemical inertness of the fiber surface, resulting in poor bonding at the fiber and resin interface in carbon matrix reinforcement / resin composites, especially under extreme conditions when it is easily damaged from the interface. It is difficult to control the dispersion of carbon-based nanoparticles in carbon-based nanoparticle-reinforced resin composi...

Claims

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Application Information

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IPC IPC(8): C08L63/00C08K9/10C08K9/00C08K3/04C08K7/06C08J5/06
CPCC08J5/005C08J5/06C08J2363/00C08J2463/00C08K3/04C08K9/00C08K9/10C08K2201/011C08L63/00C08L2205/025C08K7/06C08K3/041
Inventor 贾晓龙史可黎何丰罗锦涛刘聪还献华杨小平
Owner BEIJING UNIV OF CHEM TECH
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