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2.5维机织复杂结构件的静强度

刘浩龙 崔海涛 温卫东

刘浩龙, 崔海涛, 温卫东. 2.5维机织复杂结构件的静强度[J]. 航空动力学报, 2015, 30(3): 656-664. doi: 10.13224/j.cnki.jasp.2015.03.016
引用本文: 刘浩龙, 崔海涛, 温卫东. 2.5维机织复杂结构件的静强度[J]. 航空动力学报, 2015, 30(3): 656-664. doi: 10.13224/j.cnki.jasp.2015.03.016
LIU Hao-long, CUI Hai-tao, WEN Wei-dong. Static strength of 2.5 dimensional woven complex structures[J]. Journal of Aerospace Power, 2015, 30(3): 656-664. doi: 10.13224/j.cnki.jasp.2015.03.016
Citation: LIU Hao-long, CUI Hai-tao, WEN Wei-dong. Static strength of 2.5 dimensional woven complex structures[J]. Journal of Aerospace Power, 2015, 30(3): 656-664. doi: 10.13224/j.cnki.jasp.2015.03.016

2.5维机织复杂结构件的静强度

doi: 10.13224/j.cnki.jasp.2015.03.016
基金项目: 

中央高校基本科研业务费专项资金(56XZA13085)

详细信息
    作者简介:

    刘浩龙(1988-),男,山东滨州人,硕士生,主要从事先进复合材料力学性能研究.

  • 中图分类号: V258

Static strength of 2.5 dimensional woven complex structures

  • 摘要: 采用宏细观结合方法,针对经纱和纬纱等材料组分可能发生的多种失效模式,分别建立了基于改进的Hashin准则的系统性的材料失效准则及不同失效模式下的刚度退化模型.引入逐渐损伤的思想,建立了2.5维机织复杂结构件静强度系统性分析方法.模拟并分析了材料经向拉伸和纬向拉伸的应力-应变曲线,与实验得到的材料应力-应变曲线相比,相同应变下应力误差不超过6.5%,具有较好的重合度;对2.5维机织压气机静子连接结构模拟件开展了逐渐损伤模拟,结果表明:结构损伤主要集中在叶根倒角附近,其中吸力面叶根处的基体压缩失效形式会引起结构大幅变形,是结构破坏的主要原因.

     

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出版历程
  • 收稿日期:  2013-10-23
  • 刊出日期:  2015-03-28

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