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有拧紧力矩层合板接头静载损伤失效分析
引用本文:王丹勇,温卫东.有拧紧力矩层合板接头静载损伤失效分析[J].航空动力学报,2008,23(10):1835-1841.
作者姓名:王丹勇  温卫东
作者单位:1. 中国兵器工业集团,第五三研究所,济南,250031
2. 南京航空航天大学,能源与动力学院,南京,210016
摘    要:结合三维有限元分析技术,建立了有拧紧力矩工况下层合板接头静载损伤失效分析方法,模拟了不同尺寸类型层合板接头静载作用过程中损伤状况及内部各铺层损伤起始、发展与结构最终破坏整个累积过程,同时获得其最终破坏强度及破坏模式,并对损伤机理形式及其相互关联作用进行了分析探讨.损伤计算结果与试验试样X光进行了对比分析,结果表明,预测结果与试验结果吻合较好.

关 键 词:损伤失效  拧紧力矩  层合板接头
收稿时间:1/9/2007 12:00:00 AM
修稿时间:2007/12/14 0:00:00

Damage failure analysis for composite bolted joints with tightening torque subjected to static loadings
WANG Dan-yong and WEN Wei-dong.Damage failure analysis for composite bolted joints with tightening torque subjected to static loadings[J].Journal of Aerospace Power,2008,23(10):1835-1841.
Authors:WANG Dan-yong and WEN Wei-dong
Affiliation:WANG Dan-yong1,WEN Wei-dong2(1.Institute 53 of China North Group Corporation,Jinan 250031,China,2.College of Energy , Power Engineering,Nanjing University of Aeronautics , Astronautics,Nanjing 210016,China)
Abstract:A damage failure method was developed to predict the static strength and failure modes of composite bolted joints along with three-dimensional finite element technique.The damage status for different types of joints,the whole process of failure initiation,propagation and catastrophic failure of the structure were also simulated.The predicted results and X-radiographs of specimens were compared.The results of experiments and simulation are very consistent,showing the successful ultimate strength simulation c...
Keywords:damage failure  tightening torque  composites bolted joint  
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