Compression fatigue properties of z-pinned quasi-isotropic carbon/epoxy laminate with barely visible impact damage

被引:77
作者
Isa, M. D. [1 ,2 ]
Feih, S. [1 ]
Mouritz, A. P. [1 ]
机构
[1] Univ Kuala Lumpur, Malaysian Inst Aviat Technol, Dengkil 43800, Selangor, Malaysia
[2] RMIT Univ, Sch Aerospace Mech & Mfg Engn, Melbourne, Vic 3001, Australia
关键词
Polymer matrix composites; Z-pins; Impact; Fatigue; Mechanical properties; I DELAMINATION TOUGHNESS; COMPOSITE; THICKNESS; MECHANISMS; FRACTURE;
D O I
10.1016/j.compstruct.2011.03.015
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
This paper presents an experimental study into the use of z-pins to improve the compression fatigue properties of quasi-isotropic carbon fibre-epoxy composite containing barely visible impact damage (BVID). The study investigates the effect of increasing volume content of z-pins (up to 4%) on the barely visible impact damage resistance, post-impact compression fatigue properties, and fatigue damage mechanisms of a quasi-isotropic carbon-epoxy material. The study reveals new insights into the impact damage resistance of z-pinned composites. Z-pins induce different responses in the compression fatigue properties of the quasi-isotropic composite following low or high-energy impact loading. Z-pins proved ineffective at increasing the fatigue properties when the quasi-isotropic composite contained low-energy BVID. However, z-pins were effective at improving the fatigue performance of the composite with high-energy BVID, with the post-impact fatigue life and fatigue endurance limit increasing with the pin content. The improvement in fatigue performance is due solely to the increased resistance against high-energy impact damage imposed by the z-pins. It is also found that z-pins do not affect the fatigue mechanism or fatigue damage growth rate of the composite containing BVID. (C) 2011 Elsevier Ltd. All rights reserved.
引用
收藏
页码:2269 / 2276
页数:8
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