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  4. 碳纤维/环氧树脂层压板疲劳性能研究进展

玻璃钢/复合材料, 2010, (6): 70-74. doi: 10.3969/j.issn.1003-0999.2010.06.017

碳纤维/环氧树脂层压板疲劳性能研究进展

张阿樱 1, , 张东兴 2, , 李地红 3, , 杨蕤 4, , 肖海英 5, , 贾近 6,

1.哈尔滨工业大学,哈尔滨,150001;哈尔滨学院,哈尔滨,150086

2.哈尔滨工业大学,哈尔滨,150001

3.哈尔滨工业大学,哈尔滨,150001

4.哈尔滨工业大学,哈尔滨,150001

5.

6.

关键词： 碳纤维 , 复合材料 , 疲劳性能 , 数值模拟

ADVANCES OF STUDY ON FATIGUE PROPERTIES OF CARBON FIBER REINFORCED EPOXY LAMINATES

介绍了碳纤维/环氧树脂层压板的疲劳机理、复合材料界面的疲劳研究及疲劳性能的影响因素,总结了疲劳寿命预测研究及有限元数值模拟等方面的研究进展,并对复合材料疲劳性能方面进一步的研究进行了展望.

参考文献

[1] 杜善义.先进复合材料与航空航天[J].复合材料学报,2007(01):1-12.
[2] 沈军,谢怀勤.航空用复合材料的研究与应用进展[J].玻璃钢/复合材料,2006(05):48-54.
[3] Rebecca A. Atadero;Vistasp M. Karbhari .Calibration of resistance factors for reliability based design of externally-bonded FRP composites[J].Composites, Part B. Engineering,2008(4):665-679.
[4] Marouani s;Curtil L;Hamelin P.Composites realized by hand lay-up precess in a civil engineering environment:initial properties and durability[J].Materials and Structures,2008(06):831-851.
[5] F.L.Matthews;R.D.Bawlings.Composite materials:Engineering and science[M].London:Chapman and Hall Press,1994
[6] 齐红宇,温卫东.先进纤维增强复合材料疲劳寿命的预测[J].玻璃钢复合材料,2000(05):6-9,13.
[7] 胡静,冯振宇,徐建新.不同层板复合材料疲劳性能试验研究[J].航空维修与工程,2005(3):38-39.
[8] R F Dickson;J C Jones;B Harris .Environmental Fatigue Behavior of Carbon Fiber/PEEK Composites[J].Journal of Materials Science,1985,20(01):60-70.
[9] Curtis P.T.An investigation of the tensile fatigue behaviour of improved carbon fibre composite materials[A].,1987:54-64.
[10] Walls DP;zok FW .Interfacial fatigue in a fiber reinforced metal matrix composites[J].Acta Metathrgica et materialia,1994,42(08):2675-2681.
[11] 刘宇艳,黄玉东,刘立洵,陶少辉.界面性能对单向碳纤维/环氧复合材料弯曲疲劳性能的影响[J].物理测试,2003(01):5-8.
[12] 张志民.复合材料结构力学[M].北京:北京航空航天大学出版社,1993:7-9.
[13] 罗祖道;王震鸣.复合材料力学进展[M].北京:北京大学出版社,1992:1-5.
[14] 王放,魏玉卿,吕世金,曾祥国.纤维增强复合材料疲劳渐进破坏过程的Monte-Carlo模拟[J].船舶力学,2009(04):587-592.
[15] s.F.M.Almeida;z.S.N.Net0 .Effects of Void Content on theStrength of Composite Laminates[J].Computers & Structures,1994,28(02):139-148.
[16] W. Van Paepegem;J. Degrieck .Coupled residual stiffness and strength model for fatigue of fibre-reinforced composite materials[J].Composites science and technology,2002(5):687-696.
[17] M.M. Shokrieh;F. Taheri-Behrooz .A unified fatigue life model based on energy method[J].Composite structures,2006(1/4):444-450.
[18] Atsushi Hosoi;Hiroyuki Kaweda;Hiromichi Yoshino .Fatigue characteristies of quasi-isotropic CFRP laminates subjected To variable amplitude cyclic two-stage loading[J].International Journal of Faague,2006,28(10):1284-1289.
[19] A.R. Chambers;J.S. Earl;C.A. Squires .The effect of voids on the flexural fatigue performance of unidirectional carbon fibre composites developed for wind turbine applications[J].International Journal of Fatigue,2006(10):1389-1398.
[20] 姚卫星.飞机结构疲劳寿命分析的一些特殊问题[J].南京航空航天大学学报,2008(04):433-441.
[21] 杨坚,李亚智,张开达.层压复合材料剪切疲劳寿命预估[J].机械强度,2009(01):113-116.
[22] 潘应雄,童小燕,李斌.复合材料疲劳性能的能量耗散试验研究[J].强度与环境,2009(01):51-56.
[23] G.M. Candido;M.L. Costa;M.C. Rezende;S.F.M. Almeida .Hygrothermal effects on quasi-isotropic carbon epoxy laminates with machined and molded edges[J].Composites, Part B. Engineering,2008(3):490-496.
[24] 张立鹏,沈真.复合材料吸湿试验的若干问题[J].航空制造技术,2009(z1):85-88.
[25] Komai K;Minoshima K;Tanaka K et al.Effects of stress waveform and water absorption on the fatigue suength of angleply aramid fiher/epoxy composites[J].International Journal of Fatigue,2002(24):339-348.
[26] Yang JN;Lee LJ;Sheu DY.Modulus reduction and fatigue damage of Matrix dominated composite laminates[J].Computers & Structures,1992(21):91-100.
[27] Samirkumar M. Soni;Ronald F. Gibson;Emmanuel O. Ayorinde .The influence of subzero temperatures on fatigue behavior of composite sandwich structures[J].Composites science and technology,2009(6):829-838.
[28] Yasuhiro NISHIKAWA;Kazuya OKUBO;Toru FUJII .Effect of Moisture Absorption at Fabrication Stage on Static and Fatigue Properties for Plain-Woven CF/Epoxy Composites[J].JSME International Journal, Series A. Solid mechanics and material engineering,2005(2):73-78.
[29] Y.Zhang;A.P.Vassilopoulos;T.Keller .Environmental effects on fatigue behavior of adhesively-bonded pultrudod structural joints[J].Composites Science and Technology,2009,69(7-8):1022-1028.
[30] 吴富强,姚卫星.一种复合材料层合板的S-N曲线模型[J].机械强度,2004(z1):127-129.
[31] T.P. Philippidis;V.A. Passipoularidis .Residual strength after fatigue in composites: Theory vs. experiment[J].International Journal of Fatigue,2007(12):2104-2116.
[32] Philippidis T.P.;Vassilopoulos A.P. .Fatigue design allowables for GRP laminates based to stiffness degradation measurements[J].Composites science and technology,2000(15):2819-2828.
[33] Hwang W;Han K S .Fatigue of composites-fatigue modulus concept and life prediction[J].Journal of Composite Materials,1986,20(02):154-165.
[34] A. Varvani-Farahani;H. Haftchenari;M. Panbechi .An energy-based fatigue damage parameter for off-axis unidirectional FRP composites[J].Composite Structures,2007(3):381-389.
[35] Yang JN .Residual strength dcgradationmodeland theory ofperiodical proof tests for graphite/epoxy laminates[J].Journal of Composite Materials,1977,11(04):176-179.
[36] Yang JN;Jones DL;Yang sH .A stiffness degradation model for graphite/epoxy lam inates[J].Journal of Composite Materials,1987,24(07):753-796.
[37] 李亚智,张开达,张博平.一种FRP累积损伤模型及其在结构疲劳寿命估算中的应用[J].应用力学学报,2003(01):54-58.
[38] 陈群志,关志东,王进,朱珊,王逾涯,陈小东.分层缺陷对复合材料结构疲劳寿命影响研究[J].机械强度,2004(z1):121-123.
[39] 贾宝惠,李顶河,李伟,徐建新.基于疲劳损伤两段论的复合材料刚度降模型研究[J].玻璃钢/复合材料,2010(01):16-19.
[40] Mathmood M. Shokrieh;Larry B. Lessard .Progressive fatigue damage modeling of composite materials, Part I: modeling[J].Journal of Composite Materials,2000(13):1056-1080.
[41] M.M. Shokrieh;F. Taheri-Behrooz .A unified fatigue life model based on energy method[J].Composite structures,2006(1/4):444-450.
[42] 董兴建,李亚智,孟光.复合材料层压板疲劳寿命预测方法[J].上海交通大学学报,2004(10):1748-1752.
[43] SmojverI;Seric J .Finite element modeling of the damage and failure in fiber reinforced composites(overview)Computers[J].Materials and Continua,2006,3(01):13-23.
[44] 杨忠清,姚卫星,胡伟峰.复合材料层合板疲劳寿命分析的系列单元失效模型[J].南京航空航天大学学报,2007(01):6-10.
[45] 徐颖,温卫东,崔海涛.复合材料层合板疲劳逐渐累积损伤寿命预测方法[J].航空动力学报,2007(04):602-607.
[46] 廉伟,姚卫星.复合材料层压板剩余刚度-剩余强度关联模型[J].复合材料学报,2008(05):151-156.
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