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复合材料裙级间连接结构强度预测
引用本文:李书良,刘勇琼,甘晓松,刘建超.复合材料裙级间连接结构强度预测[J].固体火箭技术,2007,30(6):494-497.
作者姓名:李书良  刘勇琼  甘晓松  刘建超
作者单位:1. 中国航天科技集团公司四院四十一所,西安,710025
2. 西安航天复合材料研究所,西安,710025
3. 西北工业大学,航天学院,西安,710072
摘    要:针对复合材料裙级间螺栓-柱销连接结构试件,建立了三维有限元逐渐损伤模型。该模型可模拟试件损伤起始、发展及最终破坏的整个过程,并能较好预测试件破坏的模式和强度。该模型包括应力分析、失效判定准则和材料性能退化3个步骤,采用该模型对试件进行了损伤扩展分析和强度预测,计算结果与实验结果较吻合。

关 键 词:连接结构  逐渐损伤破坏  破坏准则  强度预测  有限元分析
文章编号:1006-2793(2007)06-0494-04
收稿时间:2006-11-23
修稿时间:2007-04-05

Prediction on strength of fastened joint of composite skirts
LI Shu-liang,LIU Yong-qiong,GAN Xiao-song,LIU Jian-chao.Prediction on strength of fastened joint of composite skirts[J].Journal of Solid Rocket Technology,2007,30(6):494-497.
Authors:LI Shu-liang  LIU Yong-qiong  GAN Xiao-song  LIU Jian-chao
Abstract:Aiming at bolt-plug connecting pieces of composite skirts,a 3D finite element gradual damaging model was derived.The model can be used for simulating the overall process of sample damaging,such as initiation,development and final failure,and perfectly predicting failure mode and strength of sample.The model includes three stages,such as stress analysis,failure criteria,material property degradation.The model was used for damaging analysis and strength prediction,and the calculated results agreed well with the experimental results.
Keywords:joint structure  gradual damaging failure  failure criteria  strength prediction  finite element analysis
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