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先进树脂基复合材料固化过程的铺放缺陷演变规律研究

李树健 湛利华 周源琦 蒲永伟

宇航材料工艺2018,Vol.48Issue(2):20-24,5.
宇航材料工艺2018,Vol.48Issue(2):20-24,5.DOI:10.12044/j.issn.1007-2330.2018.02.004

先进树脂基复合材料固化过程的铺放缺陷演变规律研究

Evolution of Paving Defects During Curing Process of Advanced Resin Matrix Composites

李树健 1湛利华 2周源琦 2蒲永伟3

作者信息

  • 1. 湖南科技大学机电工程学院,湘潭 411201
  • 2. 中南大学机电学院,长沙410081
  • 3. 光启技术股份有限公司,深圳518000
  • 折叠

摘要

Abstract

Taking the paving defects such as fiber wrinkling as the studying targets,the evolution of paving defects of composites during prepreg-autoclave process was studied,and the forming quality and mechanical properties after curing were compared and analyzed.The results showed that using a shorter prepreg during paving and a moderate curing pressure during curing was advantageous to improve the compliance of fibers and the smoothness of specimen,and the paving defects of fiber wrinkling can be effectively reduced.Under the conditions of this experiment,with the composite specimen length of 70mm and the curing pressure of0.4MPa,the improvement effect of fiber wrinkling was relatively remarkable.In addition,the relatively high mechanical properties can be obtained after curing.

关键词

复合材料/缺陷/纤维皱曲/固化过程/演变规律

Key words

Composites/Defects/Fiber wrinkling/Curing process/Evolution law

分类

通用工业技术

引用本文复制引用

李树健,湛利华,周源琦,蒲永伟..先进树脂基复合材料固化过程的铺放缺陷演变规律研究[J].宇航材料工艺,2018,48(2):20-24,5.

基金项目

国家重点基础研究规划(973)课题(2014CB046502) (973)

湖南科技大学博士科研启动资金(E51782)资助 (E51782)

宇航材料工艺

OA北大核心CSCDCSTPCD

1007-2330

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