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混杂复合材料层合板抗冲击性能研究

张超锋 韩超超 朱佳佳

宇航材料工艺2023,Vol.53Issue(6):48-53,6.
宇航材料工艺2023,Vol.53Issue(6):48-53,6.DOI:10.12044/j.issn.1007-2330.2023.06.007

混杂复合材料层合板抗冲击性能研究

Research on Impact Resistance of Hybrid Composite Laminates

张超锋 1韩超超 1朱佳佳2

作者信息

  • 1. 江南大学机械工程学院,无锡 214122
  • 2. 江南航天机电工业有限公司,苏州 215300
  • 折叠

摘要

Abstract

In order to investigate the structural safety of composite laminates due to impact loads in practical applications,the influence of the impactor shape on the damage mechanism of composite laminate was analyzed simultaneously by experiment and simulation.Subsequently,the variation pattern of the load-bearing capacity and energy absorption of the laminate was further revealed considering different impact energy.The results show that under same impact energy,the damage range and bearing capacity of laminates present incremental change when impacted by conical,hemispherical and flat impactors.The critical penetration energy of laminates increases along using conical,hemispherical and flat impactors.The impactor shape and the impact energy have a greater influence on the energy absorption capacity of laminates.

关键词

混杂复合材料/层合板/低速重载冲击/冲头形状/冲击性能

Key words

Hybrid composite material/Laminate/Low-velocity heavy mass impact/Impactor shape/Impact resistance

分类

通用工业技术

引用本文复制引用

张超锋,韩超超,朱佳佳..混杂复合材料层合板抗冲击性能研究[J].宇航材料工艺,2023,53(6):48-53,6.

基金项目

国家自然科学基金(51408263) (51408263)

宇航材料工艺

OA北大核心CSCDCSTPCD

1007-2330

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