Improving interlaminar fracture toughness of carbon fibre/epoxy laminates by incorporation of nano-particles

被引:128
|
作者
Zeng, Ying [1 ]
Liu, Hong-Yuan [1 ]
Mai, Yiu-Wing [1 ]
Du, Xu-Sheng [1 ]
机构
[1] Univ Sydney, CAMT, Sch Aerosp Mech & Mech Engn 107, Sydney, NSW 2006, Australia
基金
澳大利亚研究理事会;
关键词
Mode I delamination; Carbon fibre composite; Silica nano-particles; Rubber nano-particles; FILLED EPOXY; SILICA; COMPOSITES; BEHAVIORS; TEMPERATURES; MECHANISMS;
D O I
10.1016/j.compositesb.2011.04.036
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
Double-cantilever-beam tests were applied to investigate the mode I interlaminar fracture toughness of carbon fibre/epoxy laminates, in which the epoxy matrices were incorporated with rubber and silica nano-particles, either singly or jointly. It is shown that the toughness is improved owing to the presence of these nano-particles although nano-rubber is more effective than nano-silica. Further, by keeping the total particle weight percentage constant in epoxies (e.g., at 8 and 12 wt.%) filled with equal amount of nano-silica and nano-rubber, the interlaminar toughness values of the hybrid laminates are always higher than those with nano-silica filled epoxies but lower than those with nano-rubber filled matrices. Scanning electron microscopy examination of the delaminated surfaces of composite laminates filled with nano-particles revealed that cavitation of nano-rubber particles/void growth and debonding of nano-silica from epoxy matrix are responsible for the improved interlaminar toughness observed. It is also shown that the bulk toughness of nano-particle filled epoxies cannot be fully transferred to the interlaminar toughness of composite laminates, being limited by the constraint effect imposed by the carbon fibres. Finally, the role of fibre-bridging on the delaminated crack and hence delamination toughness is discussed. (C) 2011 Elsevier Ltd. All rights reserved.
引用
收藏
页码:90 / 94
页数:5
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