Fracture behaviour and toughening mechanism in Zanchor reinforced composites under mode I loading

被引:7
作者
Kusaka, Takayuki [1 ]
Watanabe, Keiko [2 ]
Hojo, Masaki [3 ]
Fukuoka, Toshiyasu [4 ]
Ishibashi, Masayasu [5 ]
机构
[1] Ritsumeikan Univ, Dept Mech Engn, Kusatsu 5258577, Japan
[2] Osaka Univ, Dept Mech Sci & Bioengn, Toyonaka, Osaka 5608531, Japan
[3] Kyoto Univ, Dept Mech Engn & Sci, Kyoto 6068501, Japan
[4] Mitsubishi Heavy Ind Co Ltd, Mitsubishi Aircraft Corp, Nagoya, Aichi 4558515, Japan
[5] Cent Res Lab, Shikibo, Higashiomi 5278577, Japan
关键词
Composites; Delamination; Fracture mechanics; Crack growth behaviour; Mode I fracture; DELAMINATION; TOUGHNESS; COMPRESSION; JAPAN; PINS;
D O I
10.1016/j.engfracmech.2011.10.015
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
The mode I interlaminar fracture behaviour and the reinforcing mechanism of Zanchor-reinforced composite laminates were investigated by using DCB (Double Cantilever Beams) and TIT (Through-Thickness Tension) specimens. The DCB test results demonstrated that the Zanchor process was highly effective at improving the mode I fracture toughness of composite laminates, where the fracture toughness increased almost linearly with the Zanchor density. The R-curves of Zanchor composites were approximately divided into the transition and stable regions, where the extent of the transition region was about 15 mm regardless of the Zanchor density. The TTT test results demonstrated that the effect of the Zanchor process could be approximately attributed to 'wedge effect' and 'bridging effect', where the bridging effect was dominant but the wedge effect was negligible against mode I fracture. The Zanchor process was effective at improving the bridging strength but not effective at improving the maximum strength, where the trend of R-curves could be predicted by considering the bridging effect. Microscopic observations of the DCB and TTT specimens indicated that the Zanchor process induced the fibre bridgings and increased the roughness of fracture surfaces, where the EFB (Entangled Fibre Bundles) played an important role in generating the fibre bridgings, resulting in the increase in mode I fracture toughness. (C) 2011 Elsevier Ltd. All rights reserved.
引用
收藏
页码:433 / 446
页数:14
相关论文
共 25 条
[11]  
Kusaka T, 2007, P 16 INT C COMP MAT
[12]  
Kusaka T, 2005, P JSME ASME INT C MA
[13]   Fracture behavior and toughening mechanism in Zanchor reinforced composites under mode II loading [J].
Kusaka, Takayuki ;
Watanabe, Keiko ;
Hojo, Masaki ;
Fukuoka, Toshiyasu ;
Ishibashi, Masayasu .
COMPOSITES SCIENCE AND TECHNOLOGY, 2009, 69 (14) :2323-2330
[14]   Experimental study on effect of loading rate on mode I delamination of z-pin reinforced laminates [J].
Liu, Hong-Yuan ;
Yan, Wenyi ;
Yu, Xiao-Yan ;
Mai, Yiu-Wing .
COMPOSITES SCIENCE AND TECHNOLOGY, 2007, 67 (7-8) :1294-1301
[15]   Finite element modelling of bridging micro-mechanics in through-thickness reinforced composite laminates [J].
Meo, M ;
Achard, F ;
Grassi, M .
COMPOSITE STRUCTURES, 2005, 71 (3-4) :383-387
[16]   Review of z-pinned composite laminates [J].
Mouritz, A. P. .
COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 2007, 38 (12) :2383-2397
[17]   A mechanistic approach to the properties of stitched laminates [J].
Mouritz, AP ;
Cox, BN .
COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 2000, 31 (01) :1-27
[18]   Influence of compression and shear on the strength of composite laminates with z-pinned reinforcement [J].
O'Brien, T. Kevin ;
Krueger, Ronald .
APPLIED COMPOSITE MATERIALS, 2006, 13 (03) :173-189
[19]   Development of TORAYCA prepreg P2302 carbon fiber reinforced plastic for aircraft primary structural materials [J].
Odagiri, N ;
Kishi, H ;
Yamashita, M .
ADVANCED COMPOSITE MATERIALS, 1996, 5 (03) :249-254
[20]   Mode I DCB testing of composite laminates reinforced with z-direction pins:: a simple model for the investigation of data reduction strategies [J].
Robinson, P ;
Das, S .
ENGINEERING FRACTURE MECHANICS, 2004, 71 (03) :345-364