全部 标题 作者
关键词 摘要

OALib Journal期刊
ISSN: 2333-9721
费用:99美元

查看量下载量

相关文章

更多...
材料工程  2015 

玻璃纤维-铝合金正交层板的拉伸性能研究

DOI: 10.11868/j.issn.1001-4381.2015.09.010, PP. 60-65

Keywords: 玻璃纤维-铝合金正交层板,拉伸实验,损伤演化,失效机理,有限元模拟

Full-Text   Cite this paper   Add to My Lib

Abstract:

通过对两组具有不同铺层次序的玻璃纤维-铝合金正交层板进行拉伸实验,对比研究了铺层次序对材料拉伸力学行为的影响。载荷跌落前两组试件的拉伸力学性能和应力-应变曲线基本一致,说明玻璃纤维-铝合金正交层板的拉伸力学性能与纤维的铺层次序无关。提出了修正后的金属体积分数理论,准确预测了材料的弹性模量、屈服应力及拉伸强度。依据声发射数据和试件损伤失效形貌照片,分析了两组试件的拉伸损伤失效进程。结果表明,铺层次序的不同使得两组材料的损伤进程和破坏模式具有很大差异。最后,利用有限元方法对试件的拉伸力学行为进行了模拟分析,模拟结果与实验值吻合较好。

References

[1]  蒋陵平.Glare层板疲劳性能研究综述[J].材料导报,2012,26(3):113-118. JIANG Ling-ping. Research of Glare laminate fatigue performance comprehensive evaluation[J].Materials Review, 2012,26(3):113-118.
[2]  程晓琳,李文晓,薛元德.单向玻璃纤维-铝合金层板的几种力学性能研究[J].纤维复合材料,2007,18(3):18-20. CHENG Xiao-lin, LI Wen-xiao, XUE Yuan-de. Research on mechanical properties of unidirectional glass fiber-aluminum alloy laminates[J]. Fiber Composites, 2007, 18(3):18-20.
[3]  梁中全,武文静,朱斌,等.GLARE层板与铝合金板在力学性能上的比较及其应用[J].玻璃纤维,2006,(3):11-13. LIANG Zhong-quan, WU Wen-jing, ZHU Bin, et al. Comparison of GLARE laminate with aluminum alloy and its application[J]. Fiber Glass, 2006,(3):11-13.
[4]  SADIGHI M, DARIUSHI S. An experimental study of the fibre orientation and laminate sequencing effects on mechanical properties of Glare[J]. Journal of Aerospace Engineering, 2008, 222(7): 1015-1024.
[5]  PARK S Y, CHOI W J, CHOI H S. Effects of surface pre-treatment and void content on GLARE laminate process characteristics[J]. Journal of Materials Processing Technology, 2010, 210(8): 1008-1016.
[6]  SINMAZ?ELIK T, AVCU E, BORA M ?, et al. A review: fibre metal laminates, background, bonding types and applied test methods[J]. Materials and Design, 2011, 32(7): 3671-3685.
[7]  VOLT A, GUNNINK J W. Fiber Metal Laminates[M]. Netherlands:Kluwer Academic Publishers, 2001.73-75.
[8]  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. MA Hong-yi, LI Xiao-gang, LI Hong-yun. Tension and fatigue properties of glass fiber reinforced aluminum laminates[J]. Journal of Materials Engineering, 2006, (7):61-64.
[9]  SOLTANI P, KEIKHOSRAVY M, OSKOUEI R H, et al. Studying the tensile behaviour of GLARE laminates: a finite element modelling approach[J]. Applied Composite Materials, 2011, 18(4): 271-282.
[10]  IBARRA-CASTANEDO C, AVDEIDIS N P, GRINZATO E G, et al. Delamination detection and impact damage assessment of GLARE by active thermography[J]. International Journal of Materials and Product Technology, 2011, 41(1-4):5-16.
[11]  YAGHOUBI A S, LIU Y X, LIAW B M. Drop-weight impact studies of GLARE 5 fiber-metal laminates[A].PROULX T. Experimental and Applied Mechanics[C].New York: Springer,2011.267-279.
[12]  刘怀喜,马润香,张恒.芳纶纤维/ 环氧树脂复合材料损伤与断裂过程的声发射特性[J].材料导报,2004,18(6):93-95. LIU Huai-xi, MA Run-xiang, ZHANG Heng. The feature of acoustic emission on the damage and fracture in composite of Kevlar-fiber/epoxy[J]. Materials Review, 2004,18(6):93-95.
[13]  王世明,吴中庆,张振军,等.大飞机用Glare层板的性能综合评价研究[J].材料导报,2010, 24(9):88-94. WANG Shi-ming, WU Zhong-qing, ZHANG Zhen-jun, et al. Research of Glare laminates performance comprehensive evaluation applied to large aircraft[J]. Materials Review, 2010, 24(9):88-94.
[14]  潘文革,矫桂琼,王波,等.声发射技术在三维编织C/SiC复合材料拉伸损伤分析中的应用[J].无机材料学报,2004,19(4):871-875. PAN Wen-ge,JIAO Gui-qiong,WANG Bo,et al.Characterizing damage evolution of three-dimensional braid C/SiC composite with AE technology[J].Journal of Inorganic Materials, 2004,19(4):871-875.
[15]  沈观林,胡更开.复合材料力学[M].北京:清华大学出版社,2006.91.

Full-Text

Contact Us

service@oalib.com

QQ:3279437679

WhatsApp +8615387084133