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Z-pins增强陶瓷基复合材料层间Ⅰ型开裂性能预测

陶永强 李晶 宋月娥

陶永强, 李晶, 宋月娥. Z-pins增强陶瓷基复合材料层间Ⅰ型开裂性能预测[J]. 航空动力学报, 2017, 32(5): 1099-1104. doi: 10.13224/j.cnki.jasp.2017.05.010
引用本文: 陶永强, 李晶, 宋月娥. Z-pins增强陶瓷基复合材料层间Ⅰ型开裂性能预测[J]. 航空动力学报, 2017, 32(5): 1099-1104. doi: 10.13224/j.cnki.jasp.2017.05.010
Prediction of model Ⅰ interlaminar fracture performance for Z-pins reinforced ceramic matrix composites[J]. Journal of Aerospace Power, 2017, 32(5): 1099-1104. doi: 10.13224/j.cnki.jasp.2017.05.010
Citation: Prediction of model Ⅰ interlaminar fracture performance for Z-pins reinforced ceramic matrix composites[J]. Journal of Aerospace Power, 2017, 32(5): 1099-1104. doi: 10.13224/j.cnki.jasp.2017.05.010

Z-pins增强陶瓷基复合材料层间Ⅰ型开裂性能预测

doi: 10.13224/j.cnki.jasp.2017.05.010

Prediction of model Ⅰ interlaminar fracture performance for Z-pins reinforced ceramic matrix composites

  • 摘要: 基于Z-pins增强陶瓷基复合材料层间Ⅰ型断裂韧性的试验结果、Z-pins增强机理,提出了Z-pins拔出的单线性软化模型.重点考虑了Z-pins直径范围内拔出位移的不一致性,在简单双悬臂梁(DCB)理论的基础上,获得了Z-pins增强陶瓷基复合材料层间Ⅰ型开裂性能的分析预测模型,预测结果与试验结果吻合较好.在此基础上,采用预测模型获得了不同Z-pins直径、裂纹长度下的裂尖能量释放率,并与理想弹簧元法进行了比较.结果表明:当裂尖靠近Z-pins时,随着Z-pins直径增大,两种方法所得的裂尖能释放率的差异逐渐增大,但总体来说差异的量级很小;随着裂纹长度的增加,裂尖逐渐远离Z-pins,两种方法所得的裂尖能释放率的存在较大的差异,不能忽略Z-pins直径范围内拔出位移不一的影响.

     

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出版历程
  • 收稿日期:  2015-08-19
  • 刊出日期:  2017-05-28

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