Evaluation of toughening concepts at structual features in CFRP - Part 1: Stiffener pull-off

被引:36
作者
Greenhalgh, Emile [1 ]
Lewis, Aaron
Bowen, Richard
Grassi, Marcello
机构
[1] Univ London Imperial Coll Sci Technol & Med, Composites Ctr, London SW7 2AZ, England
[2] QinetiQ, Farnborough GU14 0LX, Hants, England
[3] Airbus UK, Filton B599 7AR, England
关键词
polymer matrix composites (PMCs); damage tolerance; mechanical testing; prepreg;
D O I
10.1016/j.compositesa.2005.11.009
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
The objective of this work was to evaluate two damage tolerance concepts; improved toughness matrix and Z-pinning, under structural conditions using stiffener pull-off tests, which is a typical element test used to characterise structural performance of full-scale components. Both concepts had a negligible effect on initiation of failure, but Z-pinning did stiffen the element, leading to lower strains at damage initiation. However, the Z-pins promoted additional energy absorbing mechanisms which resulted in stable growth and a considerable increase in load carrying capacity. The effect of increasing matrix toughness was less significant, leading to an increase in scatter but some stable damage growth. Combining concepts did not lead to a net improvement due to the parent architecture being modified by the Z-pins, which led to defects such as resin-rich zones, fibre waviness and voids. This suggests that Z-pins may not be compatible with multiphase toughened systems. The results have important implications for damage tolerant design of composites; concepts such as Z-pinning offer the opportunity to design a structure that can withstand significant damage whilst still being fit for purpose. (c) 2006 Elsevier Ltd. All rights reserved.
引用
收藏
页码:1521 / 1535
页数:15
相关论文
共 32 条
[1]  
ALLEGRI G, 2004, 11 EUR C COMP MAT RH
[2]  
CARTIE D, 2001, 6 C DEF FRACT COMP M
[3]  
CARTIE D, 2003, 44 AIAA ASME ASCE AH
[4]   Mechanisms of crack bridging by composite and metallic rods [J].
Cartié, DDR ;
Cox, BN ;
Fleck, NA .
COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 2004, 35 (11) :1325-1336
[5]  
CLARKE A, 2003, 44 AIAA ASME ASCE AH
[6]   A traction law for inclined fiber tows bridging mixed-mode cracks [J].
Cox, BN ;
Sridhar, N .
MECHANICS OF ADVANCED MATERIALS AND STRUCTURES, 2002, 9 (04) :299-331
[7]   Constitutive model for a fiber tow bridging a delamination crack [J].
Cox, BN .
MECHANICS OF COMPOSITE MATERIALS AND STRUCTURES, 1999, 6 (02) :117-138
[8]  
CRAIG A, 1999, 5 INT C DEF FRACT CO
[9]   Finite element analyses of mode I interlaminar delamination in z-fibre reinforced composite laminates [J].
Grassi, M ;
Zhang, X .
COMPOSITES SCIENCE AND TECHNOLOGY, 2003, 63 (12) :1815-1832
[10]   Prediction of stiffness and stresses in z-fibre reinforced composite laminates [J].
Grassi, M ;
Zhang, X ;
Meo, M .
COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 2002, 33 (12) :1653-1664