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大厚度L形复合材料层合板残余应变监测和失效行为研究

王伟伦 曹子荷 俞星辰 卢弈先 曹东风 胡海晓 冀运东 李书欣

复合材料科学与工程Issue(4):1-10,46,11.
复合材料科学与工程Issue(4):1-10,46,11.DOI:10.19936/j.cnki.2096-8000.20250428.001

大厚度L形复合材料层合板残余应变监测和失效行为研究

Research on residual strain monitoring and failure behavior of thick L-shaped composite laminates

王伟伦 1曹子荷 1俞星辰 2卢弈先 1曹东风 1胡海晓 3冀运东 1李书欣3

作者信息

  • 1. 武汉理工大学 材料复合新技术国家重点实验室,武汉 430070
  • 2. 国家能源氢能及氨氢融合新能源技术重点实验室 佛山仙湖实验室,佛山 528200
  • 3. 武汉理工大学 材料复合新技术国家重点实验室,武汉 430070||国家能源氢能及氨氢融合新能源技术重点实验室 佛山仙湖实验室,佛山 528200||武汉理工大学 新材料力学理论与应用湖北省重点实验室,武汉 430070
  • 折叠

摘要

Abstract

The study involves monitoring residual strains and investigating failure behavior in thick L-shaped composite laminates.It aims to explore how the stacking sequence under high thickness conditions affects the struc-tural load-bearing capacity and failure modes.Utilizing embedded fiber bragg grating(FBG),the study monitors the evolution and distribution characteristics of the temperature field and strain field within the curved region of the L-shaped composite laminate during the curing process.It aims to investigate how thickness and ply orientation an-gle influence the thermal residual strain and spring-in angle in L-shaped composite laminates.Conducting bending tests,utilizing DIC(digital image correlation)to observe the strain field and failure modes in the lateral cross-sec-tion.And comparing the results with empirical formulas,exploring the influence of thermal residual stress under dif-ferent ply orientations on the load-carrying capacity and failure modes.The results indicate that the large-thickness L-shaped laminates exhibit a certain temperature gradient,but the temperature difference between the upper and lower layers and the middle layer is relatively small.Due to the mold effect,L-shaped laminates with angles are more likely to generate pre-loaded regions on the inner side of the corner compared to pure 0°ply.The results of the bending test indicate that the ultimate load obtained for pure 0° ply is essentially consistent with the theoretical pre-diction.However,for quasi-isotropic ply,the ultimate load is 25%smaller than the theoretical prediction.The pre-load region has a certain influence on the subsequent load-carrying capacity and failure mode.

关键词

L形复合材料/固化监测/前负载/失效模式/残余应力

Key words

L-shaped composite/curing monitoring/pre-loaded/failure mode/residual stress

引用本文复制引用

王伟伦,曹子荷,俞星辰,卢弈先,曹东风,胡海晓,冀运东,李书欣..大厚度L形复合材料层合板残余应变监测和失效行为研究[J].复合材料科学与工程,2025,(4):1-10,46,11.

基金项目

国家自然科学基金(52273080,12302481,12172265) (52273080,12302481,12172265)

湖北省自然科学基金(20231j0223) (20231j0223)

2023年湖北省重大攻关项目(JD2023BAA028) (JD2023BAA028)

复合材料科学与工程

OA北大核心

2096-8000

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