碳纤维增强铝合金层合板拉伸性能研究

玻璃钢/复合材料 ›› 2017, Vol. 0 ›› Issue (11): 89-94.

碳纤维增强铝合金层合板拉伸性能研究

袁斌,黄亚新^*,林渊,徐若航

中国人民解放军理工大学,南京210007

收稿日期:2017-05-12 出版日期:2017-11-28 发布日期:2017-11-28
通讯作者: 黄亚新(1962-),男,教授,博士生导师,主要从事军用浮桥方面的研究,10946786821@qq.com。
作者简介:袁斌(1992-),男,硕士研究生,主要从事玻璃钢浮箱基础研究。

EXPLORATION OF TENSILE PERFORMANCE OF CARBON FIBERREINFORCED ALUMINUM LAMINATES

YUAN Bin, HUANG Ya-xin^*, LIN Yuan, XU Ruo-hang

PLA University of Science & Technology, Nanjing 210007, China

Received:2017-05-12 Online:2017-11-28 Published:2017-11-28

摘要/Abstract

摘要： 采用试验方法与理论分析相结合,对两种不同纤维铺层结构的碳纤维增强铝合金层合板(CARALL)开孔前后的拉伸性能进行了比较研究,得出了开孔前后不同纤维铺层结构的层合板拉伸性能变化规律,并给出了作为拉伸构件的碳纤维铺层结构建议,提出了应用金属体积分数理论和点应力准则预测层合板开孔前后拉伸性能的方法。

关键词: 碳纤维铝合金层压板, 开孔拉伸, 金属体积分数, 点应力准则

Abstract: The tensile performance of carbon fiber reinforced aluminum laminates (CARALL) of two different fiber orientations with hole and without hole were studied experimentally and theoretically. Tensile properties of CARALL were obtained. Meanwhile, the theory of metal volume fraction and the point stress criterion to predict the strength of unbroken laminated plates and that were punched a hole have been proved.

Key words: carbon fiber reinforced aluminum laminates, open-hole tension, metal volume fraction, point stress criterion

中图分类号:

TB332

袁斌,黄亚新,林渊,徐若航. 碳纤维增强铝合金层合板拉伸性能研究[J]. 玻璃钢/复合材料, 2017, 0(11): 89-94.

YUAN Bin, HUANG Ya-xin, LIN Yuan, XU Ruo-hang. EXPLORATION OF TENSILE PERFORMANCE OF CARBON FIBERREINFORCED ALUMINUM LAMINATES[J]. Fiber Reinforced Plastics/Composites, 2017, 0(11): 89-94.

参考文献

[1] 郑兴伟, 何雪婷, 刘红兵, 等. 纤维铝合金层合板的研究进展[J] . 材料导报, 2013, 27(S1): 347-350.
[2] Wu G, Yang J M. The mechanical behavior of GLARE laminates for aircraft structures[J] . JOM, 2005, 57(1): 72-79.
[3] Sadighi M, Dariushi S. An experimental study of the fibre orientation and laminate sequencing effects on mechanical properties of Glare[J] . Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering, 2008, 222(7): 1015-1024.
[4] Wu H F, Wu L L, Slagter W J, et al. Use of rule of mixtures and metal volume fraction for mechanical property predictions of fiber-reinforced aluminium laminates[J] . Journal of Materials Science, 1994, 29(17): 4583-4591.
[5] Pinho S, Vyas G, Robinson P. Material and structural response of polymer-matrix fiber-reinforced composites: Part B[J] . Journal of Composite Materials, 2012, 47(19-20): 679-696.
[6] Takao Y, Matsubara T. Development of carbon fiber reinforced aluminum laminates[C] . 复合材料表征与应用的新进展, 2006.
[7] Botelho, Cocchierisilva E, Almeidapardini R, et al. A review on the development and properties of continuous fiber/epoxy/aluminum hybrid composites for aircraft structures[J] . Materials Research, 2006, 9(3): 247-256.
[8] 蔺晓红, 张涛, 张小波,等. 碳纤维增强铝合金板的抗冲击性能[J] . 爆炸与冲击, 2013, 33(3): 303-310.
[9] 鲍宏琛, 刘广彦. 准各向同性纤维增强复合材料层合板的开孔拉伸破坏模拟[J] . 复合材料学报, 2016, 33(5): 1026-1032.
[10] 崔海涛, 郝勇, 温卫东. 含孔复合材料层合板逐渐损伤破坏分析[J] . 理化检验-物理分册, 2002, 38(4): 150-153.
[11] Lessard L B, Chang F K. Damage Tolerance of Laminated Composites Containing an Open Hole and Subjected to Compressive Loadings[J] . Journal of Composite Materials, 1991, 25(1): 44-64.
[12] 邱家波, 熊征, 朱锡. 开孔复合材料层合板的拉伸强度和失效模式分析[J] . 海军工程大学学报, 2014(6): 12-16.
[13] Publications S. Journal of Reinforced Plastics and Composites[M] . Technomic Publishing Co, 1982.
[14] 马宏毅, 李小刚, 李宏运. 玻璃纤维-铝合金层板的拉伸和疲劳性能研究[J] . 材料工程, 2006(7): 61-64.
[15] Awerbuch J, Madhukar M S. Notched Strength of Composite Laminates: Predictions and Experiments--A Review[J] . Journal of Reinforced Plastics & Composites, 1985, 4(1): 3-159.
[16] 林渊. 碳纤维铝合金层板(CARALL)的制备及力学性能研究[D] . 江苏: 中国人民解放军理工大学, 2015.