A strategy for improving mechanical properties of a fiber reinforced epoxy composite using functionalized carbon nanotubes

被引:207
作者
Davis, Daniel C. [1 ]
Wilkerson, Justin W. [1 ]
Zhu, Jiang [2 ]
Hadjiev, Viktor G. [3 ]
机构
[1] Texas A&M Univ, Dept Aerosp Engn, Texas Inst Intelligent Bionano Mat & Struct Aeros, College Stn, TX 77843 USA
[2] NanoRidge Mat Inc, Houston, TX 77023 USA
[3] Univ Houston, Texas Ctr Superconduct, Houston, TX 77204 USA
基金
美国国家科学基金会;
关键词
Carbon nanotubes; Carbon fiber; Epoxy; Fatigue; Polymer-matrix composites(PMCs); Mechanical properties; Resin transfer moulding(RTM); Raman spectroscopy; YOUNGS MODULUS; MODEL;
D O I
10.1016/j.compscitech.2011.03.014
中图分类号
TB33 [复合材料];
学科分类号
080505 [复合材料];
摘要
Carbon fiber reinforced epoxy composite laminates are studied for improvements in quasi static strength and stiffness and tension-tension fatigue cycling at stress-ratio (R-ratio) = +0.1 through strategically incorporating amine functionalized single wall carbon nanotubes (a-SWCNTs) at the fiber/fabric-matrix interfaces over the laminate cross-section. In a comparison to composite laminate material without carbon nanotube reinforcements there are modest improvements in the mechanical properties of strength and stiffness; but, a potentially significant increase is demonstrated for the long-term fatigue life of these functionalized nanotube reinforced composite materials. These results are compared with previous research on the cyclic life of this carbon fiber epoxy composite laminate system reinforced similarly with side wall fluorine functionalized industrial grade carbon nanotubes. Optical and scanning electron microscopy and Raman spectrometry are used to confirm the effectiveness of this strategy for the improvements in strength, stiffness and fatigue life of composite laminate materials using functionalized carbon nanotubes. (C) 2011 Elsevier Ltd. All rights reserved.
引用
收藏
页码:1089 / 1097
页数:9
相关论文
共 39 条
[1]
A mechanistic model for fatigue damage evolution in composite laminates [J].
Akshantala, NV ;
Talreja, R .
MECHANICS OF MATERIALS, 1998, 29 (02) :123-140
[2]
*ASTM, D476204 ASTM
[3]
*ASTM, 2007, D3479D3479396 ASTM
[4]
BOLICK RL, 2007, SAMPE EUROPE 28 INT
[5]
Improvements in mechanical properties of a carbon fiber epoxy composite using nanotube science and technology [J].
Davis, Daniel C. ;
Wilkerson, Justin W. ;
Zhu, Jiang ;
Ayewah, Daniel O. O. .
COMPOSITE STRUCTURES, 2010, 92 (11) :2653-2662
[6]
Covalent functionalization of single-walled carbon nanotubes for materials applications [J].
Dyke, CA ;
Tour, JM .
JOURNAL OF PHYSICAL CHEMISTRY A, 2004, 108 (51) :11151-11159
[7]
Glover B.M., 2004, AVIATION ENG, V592, P16
[8]
Carbon nanotube-reinforced epoxy-compo sites:: enhanced stiffness and fracture toughness at low nanotube content [J].
Gojny, FH ;
Wichmann, MHG ;
Köpke, U ;
Fiedler, B ;
Schulte, K .
COMPOSITES SCIENCE AND TECHNOLOGY, 2004, 64 (15) :2363-2371
[9]
Raman microscopy of residual strains in carbon nanotube/epoxy composites [J].
Hadjiev, V. G. ;
Warren, G. L. ;
Sun, Luyi ;
Davis, D. C. ;
Lagoudas, D. C. ;
Sue, H. -J. .
CARBON, 2010, 48 (06) :1750-1756
[10]
Hadjiev VG, 2007, P SAMPE FALL TECHN C