Charpy test investigation of the influence of fabric weave and fibre nature on impact properties of PEEK-reinforced composites

被引:11
作者
De Almeida, Olivier [1 ]
Ferrero, Jean-Francois [2 ]
Escale, Laurent [1 ]
Bernhart, Gerard [1 ]
机构
[1] Univ Toulouse, CNRS, Mines Albi, INSA,UPS,ISAE,ICA, Albi, France
[2] Univ Toulouse, CNRS, Mines Albi, INSA,UPS,ISAE,ICA, 118,Rte Narbonne, F-31062 Toulouse, France
关键词
Thermoplastic composites; impact; Charpy test; fibre nature; yarn crimp effect; THERMOSETTING-COMPOSITES; BEHAVIOR; DAMAGE; PERFORMANCE; FAILURE; TOUGHNESS; EPOXY;
D O I
10.1177/0892705718778744
中图分类号
TB33 [复合材料];
学科分类号
摘要
The aim of the work is to use Charpy impact test for quick evaluations of different Polyether-ether-ketone (PEEK)-reinforced composites to be used for impact protection. In the first part, the influence of weave pattern was first analysed by comparing the impact behaviour of three PEEK composites reinforced with plies of unidirectional (UD) tapes, 5H satin fabrics and 2 x 2 twill fabrics made of high-strength carbon fibres. In the second part, the influence of fibre nature was investigated for the same weave pattern. The impact behaviour of five 2 x 2 twill fabrics made from inorganic fibre (carbon, glass and basalt) and organic fibre (aramid and poly(p-phenylene-2,6-benzobisoxazole) (PBO)) has been compared. Two main types of failure modes were identified: a brittle behaviour mode with high failure strength and a highly deformable behaviour mode in which energy absorption is more important. The balance between brittle behaviour and highly deformable behaviour results from competition between the yarn crimp, weave pattern and fibre properties of the composite. Slight yarn crimp and small ply thickness increase the stiffness of the composite and induce brittle behaviour characterized by fibre failure in tension and a steep peak on the loading curves. This behaviour is observed in UD and 5H satin carbon-reinforced composites or 2 x 2 twill glass and basalt fabric-reinforced composites. In contrast, aramid and PBO 2 x 2 twill fabric composites exhibit high shear strength. The highly deformable behaviour of the specimens during the Charpy impact led, in the case of organic fibres, to a non-breakage of the fibres and consequently to a high level of energy absorption. This behaviour is necessarily interesting in armour applications.
引用
收藏
页码:729 / 745
页数:17
相关论文
共 30 条
  • [1] Influence of internally dropped-off plies on the impact damage of asymmetrically tapered laminated CFRP
    Abdulhamid, Hakim
    Bouvet, Christophe
    Michel, Laurent
    Aboissiere, Jacky
    Minot, Clement
    [J]. COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 2015, 68 : 110 - 120
  • [2] Effect of woven fabric architecture on interlaminar mechanical response of composite materials: an experimental study
    Abot, Jandro L.
    Gabbai, Rene D.
    Harsley, Kevin
    [J]. JOURNAL OF REINFORCED PLASTICS AND COMPOSITES, 2011, 30 (24) : 2003 - 2014
  • [3] Abrate Serge., 1998, IMPACT COMPOSITE STR, DOI 10.1017/CBO9780511574504
  • [4] Adams D.F., 1975, FIBRE SCI TECHNOL, V8, P275, DOI [10.1016/0015-0568(75)90020-2, DOI 10.1016/0015-0568(75)90020-2]
  • [5] LOW-LEVEL CHARPY IMPACT RESPONSE OF GRAPHITE-EPOXY HYBRID COMPOSITES
    ADAMS, DF
    PERRY, JL
    [J]. JOURNAL OF ENGINEERING MATERIALS AND TECHNOLOGY-TRANSACTIONS OF THE ASME, 1977, 99 (03): : 257 - 263
  • [6] Adanur S, 2002, HDB WEAVING
  • [7] Investigation of the behaviour of a chopped strand mat/woven roving/foam-Klegecell composite lamination structure during Charpy testing
    Arifin, A. M. T.
    Abdullah, S.
    Rafiquzzaman, Md.
    Zulkifli, R.
    Wahab, D. A.
    Arifin, A. K.
    [J]. MATERIALS & DESIGN, 2014, 59 : 475 - 485
  • [8] Bessard E, 2012, THESIS
  • [9] THE MECHANICAL PERFORMANCE AND IMPACT BEHAVIOR OF CARBON-FIBRE REINFORCED PEEK
    BISHOP, SM
    [J]. COMPOSITE STRUCTURES, 1985, 3 (3-4) : 295 - 318
  • [10] Effect of hot water immersion on the performance of carbon reinforced unidirectional poly(ether ether ketone) (PEEK) composites:: Stress rupture under end-loaded bending
    Bismarck, Alexander
    Hofmeler, Markus
    Doerner, Guenter
    [J]. COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 2007, 38 (02) : 407 - 426