Compressive failure of hybrid multidirectional fibre-reinforced composites

被引:19
|
作者
Tsampas, S. A. [1 ]
Greenhalgh, E. S. [2 ]
Ankersen, J. [3 ]
Curtis, P. T. [2 ,4 ]
机构
[1] Swerea SICOMP, Mat Technol, S-43153 Gothenburg, Sweden
[2] Univ London Imperial Coll Sci Technol & Med, Dept Aeronaut, London SW7 2AZ, England
[3] Natl Composites Ctr, GKN Aerosp CTC, Bristol BS16 7ES, Avon, England
[4] DSTL, Dept Phys Sci, Porton Down SP4 0IQ, Wilts, England
基金
英国工程与自然科学研究理事会;
关键词
Carbon fibres; Fracture; Fractography; Electron microscopy; FRACTURE-TOUGHNESS; STRENGTH;
D O I
10.1016/j.compositesa.2015.01.002
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
In this paper, the hybridisation of multidirectional carbon fibre-reinforced composites as a means of improving the compressive performance is studied. The aim is to thoroughly investigate how hybridisation influences the laminate behaviour under different compression conditions and thus provide an explanation of the "hybrid effect". The chosen approach was to compare the compressive performance of two monolithic carbon fibre/epoxy systems, CYTEC HTS/MTM44-1 and IMS/MTM44-1, with that of their respective hybrids. This was done by keeping the same layup throughout ((0/90/45/-45)(2S)) while replacing the angle plies in one case or the orthogonal plies in the other case with the second material, thus producing two hybrid systems. To investigate the compressive performance of these configurations, compact and plain compression test methods were employed which also allowed studying the sensitivity of compressive failure to specimen geometry and loading conditions. The experimental results and the subsequent fractographic analysis revealed that the hybridisation of selective ply interfaces influenced the location and severity of the failure mechanisms. Finally, in light of this knowledge, an update of the generic sequence of events, previously suggested by the authors, which lead to global fracture in multidirectional fibre-reinforced composites under compression is presented. (C) 2015 Elsevier Ltd. All rights reserved.
引用
收藏
页码:40 / 58
页数:19
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