基于集成CT、3D- dic和AE分析的三维编织碳纤维复合材料轴扭转破坏机制的多尺度研究

IF 9.8 1区 材料科学 Q1 MATERIALS SCIENCE, COMPOSITES
Jikang Li , Zheng Liu , Xuecheng Liu , Zhe Zhang , Xu Chen
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引用次数: 0

摘要

本研究通过静态扭转力学测试、计算机断层扫描(CT)损伤分析、三维数字图像相关(3D- dic)和声发射(AE)监测相结合的综合多尺度方法,系统地研究了三维编织碳纤维/环氧树脂复合材料的扭转损伤演化和破坏机制。实验结果表明,三维编织碳纤维增强复合材料试件在扭转过程中表现出近似的线弹性行为。增加编织角(15°~ 45°)可使剪切模量和强度提高67%,但破坏应变降低至0.61%,破坏模式由延性基体变形为主转变为脆性纤维断裂。CT分析表明,压缩纤维束破坏控制着力学性能,损伤进程始于界面剥离(在60%载荷下),通过裂纹分岔(在80%载荷下),最终以纤维屈曲破坏告终。3D-DIC定量表征了编织拓扑调节下的应变非均匀性,结果表明,随着编织角度的增加,最大剪切应变降低了67%。值得注意的是,45°试样呈现网格状应变分布模式,揭示了空间纤维缠结对载荷传递路径的定向调节。将Hilbert-Huang变换与频域校准技术相结合的声发射信号处理框架成功识别出三种特征损伤模式:基体开裂(100-200 kHz)、界面剥离(200-320 kHz)和纤维断裂(320-420 kHz)。统计分析表明,基体损伤主导了破坏过程(占75.5 - 80%),发生在加载早期阶段,而纤维破坏发生在最终破裂附近。较高的编织角度可以通过增强纤维互锁效应来抑制基体损伤。
本文章由计算机程序翻译,如有差异,请以英文原文为准。

Multiscale investigation of torsional failure mechanisms in 3D braided carbon fiber composite shafts via integrated CT, 3D-DIC, and AE analysis

Multiscale investigation of torsional failure mechanisms in 3D braided carbon fiber composite shafts via integrated CT, 3D-DIC, and AE analysis
This study systematically investigated the torsional damage evolution and failure mechanisms of 3D braided carbon fiber/epoxy resin composites through an integrated multiscale methodology combining static torsion mechanical testing, computed tomography (CT) damage analysis, three-dimensional digital image correlation (3D-DIC), and acoustic emission (AE) monitoring. Experimental results revealed that the 3D braided carbon fiber-reinforced composite specimens exhibited approximately linear elastic behavior during torsion. An increase in braiding angle (15°–45°) enhanced shear modulus and strength by 67 %, but reduced failure strain to 0.61 % while shifting the failure mode dominance from ductile matrix deformation to brittle fiber fracture. CT analysis demonstrated that compressive fiber bundle failure governed mechanical performance, with damage progression initiating as interfacial debonding (at 60 % load), progressing through crack bifurcation (at 80 % load), and culminating in fiber buckling failure. 3D-DIC quantitatively characterized the strain heterogeneity regulated by braiding topology, showing that maximum shear strain decreased by 67 % with increasing braiding angles. Notably, 45° specimens developed mesh-like strain distribution pattern, revealing the directional regulation of load transfer paths through spatial fiber entanglement. The proposed AE signal processing framework integrating Hilbert-Huang transform with frequency-domain calibration techniques successfully identified three characteristic damage modes: matrix cracking (100–200 kHz), interface debonding (200–320 kHz), and fiber fracture (320–420 kHz). Statistical analysis indicated matrix damage dominated the failure process (75.5–80 % contribution), occurring during early loading stages, whereas fiber failure emerged near final rupture. Higher braiding angles were found to suppress matrix damage through enhanced fiber interlocking effects.
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来源期刊
Composites Science and Technology
Composites Science and Technology 工程技术-材料科学:复合
CiteScore
16.20
自引率
9.90%
发文量
611
审稿时长
33 days
期刊介绍: Composites Science and Technology publishes refereed original articles on the fundamental and applied science of engineering composites. The focus of this journal is on polymeric matrix composites with reinforcements/fillers ranging from nano- to macro-scale. CSTE encourages manuscripts reporting unique, innovative contributions to the physics, chemistry, materials science and applied mechanics aspects of advanced composites. Besides traditional fiber reinforced composites, novel composites with significant potential for engineering applications are encouraged.
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