Improvements in mechanical properties of a carbon fiber epoxy composite using nanotube science and technology

被引:205
作者
Davis, Daniel C. [1 ]
Wilkerson, Justin W. [1 ]
Zhu, Jiang [2 ]
Ayewah, Daniel O. O. [1 ]
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
基金
美国国家科学基金会;
关键词
Cyclic fatigue loading; Composites; Epoxy; Carbon nanotubes; Carbon fiber; Functionalization; FATIGUE; FUNCTIONALIZATION; FLUORINATION; COMPRESSION; STRENGTH; MODEL;
D O I
10.1016/j.compstruct.2010.03.019
中图分类号
O3 [力学];
学科分类号
070301 [无机化学];
摘要
Carbon fiber reinforced epoxy composite laminates, with strategically incorporated fluorine functionalized carbon nanotubes (f-CNTs) at 0.2, 0.3 and 0.5 weight percent (wt.%), are studied for improvements in tensile strength and stiffness and durability under both tension-tension (R = +0.1) and tension-compression (R = -0.1) cyclic loadings, and then compared to the neat (0.0 wt.% CNTs) composite laminate material. To develop the nanocomposite laminates, a spraying technology was used to deposit nanotubes on both sides of each four-harness satin weave carbon fiber fabric piece for the 12 ply laminate lay up. For these experimental studies the carbon fiber reinforced epoxy laminates were fabricated using a heated vacuum assisted resin transfer molding (H-VARTM (R)) method followed by a 2 soak curing cycle. The f-CNTs toughened the epoxy resin-fiber interfaces to mitigate the evolution of fiber/fabric-matrix interfacial cracking and delamination under both static and cyclic loadings. As a consequence, significant improvements in the mechanical properties of tensile strength, stiffness and resistance to failure due to cyclic loadings resulted for this carbon fiber reinforced epoxy composite laminate. (C) 2010 Elsevier Ltd. All rights reserved.
引用
收藏
页码:2653 / 2662
页数:10
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