Numerical Analysis of Exfoliation Corroded Holed Aluminum Plates Repaired with Adhesively Bonded Composite Patches

摘要：

　　A 3D FE model of exfoliation corroded holed aluminum plates repaired with adhesively bonded composite patches was established in this paper,and then the stress distribution in the repaired aluminum plate was analyzed.The result shows after repairing σ3,max in the exfoliation corroded holed aluminum plate gets reduced for 33.62%,and the repaired aluminum plates undergoes bending deformations due to the offset between load axis and centroidal axis of the repaired structure.

关键词： Composite Patch Adhesively Bonded Repair 3D FE Model Exfoliation Corrosion

作者: Xiaohua YANG Ding ZHANG Lin KUANG Yong ZHANG Wenyong Ding

作者单位: Department of Aeronautical Mechanism, Naval Aeronautical Engineering Academy Qingdao Branch, Qingdao postgraduate team, Naval Aeronautical Engineering Academy Qingdao Branch, Qingdao,Shandong, 266041, The 91685th Unit of PLA, Lingshui, Hainan, 572425, China

会议类型: 国际会议

会议名称: the 2010 International Conference on Frontiers of Manufacturing and Design Science(第一届制造与设计科学国际会议(ICFMD 2010))

会议地点: 重庆

会议语种:英文

页码: 2847-2851

在线出版日期: 2010-12-11（万方平台首次上网日期，不代表论文的发表时间）