复合材料科学与工程 ›› 2025, Vol. 0 ›› Issue (12): 26-36.DOI: 10.19936/j.cnki.2096-8000.20251228.004

• 基础与力学性能研究 • 上一篇    下一篇

湿热环境对大丝束碳纤维平纹编织复合材料力学性能的影响及其失效机理

杨文涛1, 于宁博2, 王明振1, 张楚哲1, 冀运东2*   

  1. 1.中国特种飞行器研究所,荆门 448035;
    2.武汉理工大学 材料科学与工程学院,武汉 430070
  • 收稿日期:2024-10-21 出版日期:2026-02-06 发布日期:2026-02-06
  • 通讯作者: 冀运东(1972—),男,博士,副教授,研究方向为聚合物基复合材料,jiyundong@whut.edu.cn。
  • 作者简介:杨文涛(1991—),男,硕士,工程师,研究方向为飞行器复合材料与结构设计。
  • 基金资助:
    2023年湖北省重大攻关项目(JD)(2023BAA028)

Influence of hygrothermal environments on the mechanical properties of large tow carbon fiber plain weave composites and their failure mechanism

YANG Wentao1, YU Ningbo2, WANG Mingzhen1, ZHANG Chuzhe1, JI Yundong2*   

  1. 1. China Special Vehicle Research Institute, Jingmen 448035, China;
    2. School of Materials Science and Engineering, Wuhan University of Technology, Wuhan 430070, China
  • Received:2024-10-21 Online:2026-02-06 Published:2026-02-06

摘要: 大丝束碳纤维因其优异的成本效益和卓越的性能在多个领域中展现出巨大的潜力。本文研究了湿热环境对大丝束碳纤维平纹编织增强聚合物拉伸和压缩性能的影响,并对其失效形式和失效机理进行分析。以48K大丝束碳纤维平纹编织预浸料为原料,制备了[0]4和[45/0/-45/90]S两种铺层的层合板,并分别在室温干态和高温湿态环境下处理14 d后进行拉伸和压缩试验。结果表明,湿热处理后,大丝束CFRP的压缩性能严重劣化。使用扫描电子显微镜对断口形貌进行分析,从宏观和微观两个层面分析了材料的失效形式和失效机理。结果表明,湿热处理后树脂基体劣化,减弱了纤维-基体界面和正交编织界面的性能,最终导致大丝束CFRP的失效形式发生改变,同时使力学性能降低。

关键词: 湿热, 大丝束CFRP, 力学性能, 失效机理, 复合材料

Abstract: Large-tow carbon fiber reinforced plastics (CFRP) hold significant promise for various applications, attributed to their exceptional cost-effectiveness and exceptional performance. This study delves into the impact of hygrothermal environments on the tensile and compressive capabilities of plain-woven large-tow CFRP, accompanied by an in-depth analysis of its damage patterns and failure mechanisms. Utilizing 48K plain-woven large-tow carbon fiber prepregs, two types of laminates, namely [0]4 and [45/0/-45/90]S, were crafted. These laminates were subjected to tensile and compressive tests after being exposed to room-temperature dry and elevated temperature wet conditions for 14 days. The findings reveal a substantial decline in the compressive properties of large-tow CFRP following hygrothermal treatment. Scanning electron microscopy (SEM) was utilized to scrutinize the fracture morphologies. A dual-perspective analysis, encompassing both macroscopic and microscopic viewpoints, was conducted to elucidate the failure modes and mechanisms of the material. It was observed that the degradation of the resin matrix after hygrothermal treatment weakened both the fiber-matrix interface and the orthogonal woven interface, ultimately altering the failure modes of large-tow CFRP and compromising its mechanical properties.

Key words: hygrothermal, large tow CFRP, mechanical properties, failure mechanism, composites

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