| 混杂铺层层板穿透挖补修理后拉伸性能 |
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| 引用本文： | 刘遂,关志东,郭霞,席国芬,蔡婧.混杂铺层层板穿透挖补修理后拉伸性能[J].复合材料学报,2013,30(1):223-229. |
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| 作者姓名： | 刘遂 关志东 郭霞 席国芬 蔡婧 |
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| 作者单位： | 1. 北京航空航天大学 航空科学与工程学院, 北京 100191;2. 中国商用飞机有限责任公司 设计研发中心, 上海 200232 |
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| 摘 要： | 对经穿透挖补修理后的平面编织混杂铺层层板的拉伸性能进行了试验研究, 结果表明初始损伤相同时, 挖补斜度为1∶30的试件的拉伸强度最高, 可以达到完好板强度的97.8%, 并且不同挖补斜度的试件表现出不同的破坏模式。此外挖补斜度相同时增大初始损伤会导致拉伸强度降低。在试验基础上建立渐进损伤有限元模型, 并对修理试件的拉伸强度及破坏过程进行研究, 数值模型得到的极限强度和破坏模式与试验结果吻合良好。
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| 关 键 词： | 挖补修理 平面织物 混杂铺层 渐进损伤 拉伸强度 |
| 收稿时间： | 2011-12-01 |
| 修稿时间： | 2012-03-21 |
Tensile behavior of hybrid laminates repaired by full depth scarfing |
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| LIU Sui,GUAN Zhidong,GUO Xia,XI Guofen,CAI Jing.Tensile behavior of hybrid laminates repaired by full depth scarfing[J].Acta Materiae Compositae Sinica,2013,30(1):223-229. |
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| Authors: | LIU Sui GUAN Zhidong GUO Xia XI Guofen CAI Jing |
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| Affiliation: | 1. School of Aeronautic Science and Engineering, Beihang University, Beijing 100191, China;2. Design and Research Center, Commercial Aircraft Corporation of China, Ltd., Shanghai 200232, China |
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| Abstract: | Experimental study on tensile behavior of hybrid plain woven fabric laminate repaired by scarfing method was conducted. The results show under the same initial damage dimension, the specimen with scarf ratio of 1∶30 has the highest tensile strength which can reach 97.8% of the intact laminate strength and the failure mode changes upon the scarf ratio. Besides, when the scarf ratio is fixed, extending the dimension of initial damage can decrease the tensile strength of specimen. Based on test results, a finite element model is adopted to research tensile strength and progressive damage process of repaired specimen. The calculated strength and failure mode are in good agreement with test results. |
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| Keywords: | scarfing repair plain woven hybrid laminate progressive damage tensile strength |
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