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"无机粒子-无纺布"协同改性碳纤维复合材料及其增韧机理

康少付 范航天 瞿立 李进 安百俊 李大同

宁夏工程技术2024,Vol.23Issue(1):16-22,7.
宁夏工程技术2024,Vol.23Issue(1):16-22,7.

"无机粒子-无纺布"协同改性碳纤维复合材料及其增韧机理

Carbon Fiber Composite Materials Co-modified by Inorganic Particle and Non-woven Fabric and the Toughening Mechanism

康少付 1范航天 1瞿立 2李进 2安百俊 3李大同4

作者信息

  • 1. 宁夏大学 机械工程学院,宁夏 银川 750021
  • 2. 宁夏大学 材料与新能源学院,宁夏 银川 750021
  • 3. 宁夏银星能源股份有限公司,宁夏 银川 750000
  • 4. 宁夏龙源新能源有限公司,宁夏 银川 750011
  • 折叠

摘要

Abstract

In response to the issues of poor interlaminar properties and susceptibility to delamination damage in carbon fiber composites,a technology for toughening and modifying carbon fiber/epoxy resin matrix composites(CFRP)using SiC particles and thermoplastic copolyamide(PA)non-woven fabric was proposed.It constructed a multi-component and multi-scale toughening system of inorganic particles/thermoplastic fiber/resin matrix within the interlayers.The interlaminar fracture toughness as well as the thermal resistance of the composite materials before and after modification of Mode-Ⅰ and Mode-Ⅱ were compared and analyzed.The mechanisms of toughening and heat resistance were revealed with the help of scanning electron microscopy(SEM)and dynamic thermomechanical analysis.The results showed that compared with the unmodified CFRP materials,when the SiC filling content(by mass fraction)was 1%and the PA non-woven fabric areal density was 25 g/m2,the Mode-Ⅰ interlaminar fracture toughness(GⅠC)and Mode-Ⅱ interlaminar fracture toughness(GⅡC)of the modified CFRP material increased by 52.7%and 222.6%,respectively.The retardation effect of inorganic particles,the bridging effect of fibers and the plastic deformation of matrix resins are the main toughening mechanisms.

关键词

碳纤维复合材料/无机粒子/无纺布/增韧机理/耐热性

Key words

carbon fiber composite composites/inorganic particles/non-woven fabric/toughening mechanism/heat resis-tance

引用本文复制引用

康少付,范航天,瞿立,李进,安百俊,李大同.."无机粒子-无纺布"协同改性碳纤维复合材料及其增韧机理[J].宁夏工程技术,2024,23(1):16-22,7.

基金项目

宁夏自然科学基金项目(2020AAC03006) (2020AAC03006)

宁夏工程技术

1671-7244

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