Impact Behavior and Residual Strength of PEEK/CF-Laminated Composites with Various Stacking Sequences

被引:3
作者
Eremin, Alexander V. [1 ]
Burkov, Mikhail V. [1 ]
Bogdanov, Alexey A. [1 ]
Kononova, Anastasia A. [1 ]
Lyubutin, Pavel S. [1 ]
机构
[1] Russian Acad Sci, Inst Strength Phys & Mat Sci, Siberian Branch, Lab Mech Polymer Composite Mat, Tomsk 634055, Russia
基金
俄罗斯科学基金会;
关键词
polymer composite; polyetheretherketone; carbon fiber; stacking sequence; mechanical properties; impact behavior; finite element modelling; DAMAGE; EPOXY; PERFORMANCE; RESISTANCE; CF/PEEK;
D O I
10.3390/polym16050717
中图分类号
O63 [高分子化学(高聚物)];
学科分类号
070305 ; 080501 ; 081704 ;
摘要
Carbon fiber-reinforced composites are popular due to their high strength and light weight; thus, the structures demonstrate high performance and specific strength. However, these composites are susceptible to impact damage. The objective of this research was to study the behavior of carbon fiber-reinforced laminates based on a polyetheretherketone (PEEK) matrix with six stacking sequences under static and impact loading. Four-point bending, short-beam bending, drop weight impact, and compression after impact tests were carried out. The results were complemented with digital shearography to estimate the damaged areas. Finite element modeling served to assess the failure mechanisms, such as fiber and matrix failure, in different layers due to tension of compression. Three behavior pattern of layups under drop-weight impact were found: (i)-energy redistribution due to mostly linear behavior (like a trampoline) and thus lower kinetic energy absorption for damage initiation, (ii)-moderate absorption of energy with initiation and propagation of concentrated damage with depressed redistribution of energy in the material, (iii)-moderate energy absorption with good redistribution due to initiation of small, dispersed damage. The results can be used to predict the mechanical behavior of composites with different stacking sequences in materials for proper structural design.
引用
收藏
页数:16
相关论文
共 28 条
[1]   Flexural Creep Behaviour of Pultruded GFRP Composites Cross-Arm: A Comparative Study on the Effects of Stacking Sequence [J].
Alhayek, Abdulrahman ;
Syamsir, Agusril ;
Supian, Abu Bakar Mohd ;
Usman, Fathoni ;
Asyraf, Muhammad Rizal Muhammad ;
Atiqah, Mohd Afdzaluddin .
POLYMERS, 2022, 14 (07)
[2]  
[Anonymous], 2016, ASTM Standard D2344/D2344M
[3]  
[Anonymous], 2012, ASTM Standard D7137/D7137M
[4]  
[Anonymous], 2015, ASTM Standard D7264/D7264M
[5]  
[Anonymous], 2015, D7136D7136M15 ASTM
[6]   Measurement of mixed-mode delamination fracture toughness of unidirectional glass/epoxy composites with mixed-mode bending apparatus [J].
Benzeggagh, ML ;
Kenane, M .
COMPOSITES SCIENCE AND TECHNOLOGY, 1996, 56 (04) :439-449
[7]   THE MECHANICAL PERFORMANCE AND IMPACT BEHAVIOR OF CARBON-FIBRE REINFORCED PEEK [J].
BISHOP, SM .
COMPOSITE STRUCTURES, 1985, 3 (3-4) :295-318
[8]   Numerical study of the structural behaviour of impacted composite laminates subjected to compression load [J].
Caputo, F. ;
De Luca, A. ;
Sepe, R. .
COMPOSITES PART B-ENGINEERING, 2015, 79 :456-465
[9]   Numerical study for the structural analysis of composite laminates subjected to low velocity impact [J].
Caputo, F. ;
De Luca, A. ;
Lamanna, G. ;
Borrelli, R. ;
Mercurio, U. .
COMPOSITES PART B-ENGINEERING, 2014, 67 :296-302
[10]   ON THE IMPACT PERFORMANCE OF CARBON-FIBER LAMINATES WITH EPOXY AND PEEK MATRICES [J].
DOREY, G ;
BISHOP, SM ;
CURTIS, PT .
COMPOSITES SCIENCE AND TECHNOLOGY, 1985, 23 (03) :221-237