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基于动态高分子基复合材料的一体化T型加筋壁板力学性能仿真研究

张勋 刘翔 方梅 郭攀 冯跃战 黄明 刘春太

中国塑料2025,Vol.39Issue(3):53-59,7.
中国塑料2025,Vol.39Issue(3):53-59,7.DOI:10.19491/j.issn.1001-9278.2025.03.010

基于动态高分子基复合材料的一体化T型加筋壁板力学性能仿真研究

Simulation on mechanical performance of integrated T-shaped reinforced wall panel based on carbon fiber reinforced dynamic polymer composites

张勋 1刘翔 1方梅 1郭攀 1冯跃战 1黄明 1刘春太1

作者信息

  • 1. 郑州大学橡塑模具国家工程研究中心,工业装备结构分析优化与CAE软件全国重点实验室,郑州 450002
  • 折叠

摘要

Abstract

The prepreg tape with dynamic reversibility and excellent mechanical properties were prepared by using bi-sphenol-A diglycidyl ether as a resin matrix,glutaric anhydride as a curing agent,carbon fiber as a reinforcement.The tensile,compressive,bending,stress relaxation,and creep properties of the composites after hot pressing were investi-gated.According to The mechanical test results,the solid modeling was conducted for the secondary bonding forming and integrated forming structure panel,and a finite element simulation analysis was carried out.The results indicated that compared to the traditional secondary bonding forming structure panel,the maximum deformation of the integrated forming structure panel decreased by 28.57%,28.57%,28.04%and 8.27%under tension,compression,bending,and impact conditions,respectively,at the same external load.When buckling instability occurred,the critical load of the integrated structure panel increased by 84.69%,and its longitudinal strain at the maximum deformation at each an-gle was greatly improved,demonstrating excellent anti-buckling performance.

关键词

碳纤维增强复合材料/动态高分子/飞机壁板/力学性能/有限元仿真

Key words

carbon fiber reinforced composites/dynamic polymer/aircraft panel/mechanical property/finite element simulation

分类

化学化工

引用本文复制引用

张勋,刘翔,方梅,郭攀,冯跃战,黄明,刘春太..基于动态高分子基复合材料的一体化T型加筋壁板力学性能仿真研究[J].中国塑料,2025,39(3):53-59,7.

基金项目

国家重点研发计划(2019YFA0706802) (2019YFA0706802)

中国塑料

OA北大核心

1001-9278

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