Mechanical properties of composite laminates reinforced with rectangular z-pins in monotonic and cyclic tension

被引:43
作者
Hoffmann, Julian [1 ]
Scharr, Gerhard [1 ]
机构
[1] Univ Rostock, Dept Mech Engn, Chair Lightweight Design, Albert Einstein Str 2, D-18059 Rostock, Germany
关键词
Laminate; Mechanical properties; Fatigue; z-pinning; FATIGUE PROPERTIES; FLEXURAL PROPERTIES; FAILURE MECHANISMS; MODE-I; DELAMINATION; ENVIRONMENT; THICKNESS; DAMAGE;
D O I
10.1016/j.compositesa.2018.03.004
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
This paper presents an experimental study investigating the static and fatigue tensile properties of unidirectional and quasi-isotropic carbon fiber/epoxy laminates reinforced with rectangular and circular z-pins. All z-pinned laminates showed reduced tensile stiffness and strength compared to unpinned specimens. The insertion of rectangular z-pins that were aligned lengthwise to the fiber direction of a laminate ply was observed to cause minor microstructural damage, such as in-plane fiber waviness. Therefore, the use of rectangular z-pins led to significantly higher tensile stiffness and strength in both unidirectional and quasi-isotropic laminates. Unpinned laminates showed only minor fatigue effects. The insertion of z-pins resulted in a decrease in the fatigue performance of the tested unidirectional and quasi-isotropic laminates. Since this deterioration was primarily caused by the initial knockdown of the static tensile strength of the z-pinned laminates, rectangular z-pins showed superior fatigue performance in both unidirectional and quasi-isotropic laminates.
引用
收藏
页码:163 / 170
页数:8
相关论文
共 27 条
[1]  
[Anonymous], 2001, P ICCM 13 13 INT C C
[2]  
[Anonymous], 2003, P ICCM14 JUL 2003 SA
[3]   Delamination of Z-pinned carbon fibre reinforced laminates [J].
Cartié, DDR ;
Troulis, M ;
Partridge, IK .
COMPOSITES SCIENCE AND TECHNOLOGY, 2006, 66 (06) :855-861
[4]   Fatigue delamination behaviour of unidirectional carbon fibre/epoxy laminates reinforced by Z-Fiber® pinning [J].
Cartie, Denis D. R. ;
Laffaille, Jean-Martin ;
Partridge, Ivana K. ;
Brunner, Andreas J. .
ENGINEERING FRACTURE MECHANICS, 2009, 76 (18) :2834-2845
[5]   Flexural properties of z-pinned laminates [J].
Chang, P. ;
Mouritz, A. P. ;
Cox, B. N. .
COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 2007, 38 (02) :244-251
[6]   Properties and failure mechanisms of z-pinned laminates in monotonic and cyclic tension [J].
Chang, P. ;
Mouritz, A. P. ;
Cox, B. N. .
COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 2006, 37 (10) :1501-1513
[7]   Properties and failure mechanisms of pinned composite lap joints in monotonic and cyclic tension [J].
Chang, P. ;
Mouritz, A. P. ;
Cox, B. N. .
COMPOSITES SCIENCE AND TECHNOLOGY, 2006, 66 (13) :2163-2176
[8]  
Chang P., 2006, THESIS
[9]  
FREITAS G, 1994, J ADV MATER, V25, P36
[10]   Compression fatigue properties of z-pinned quasi-isotropic carbon/epoxy laminate with barely visible impact damage [J].
Isa, M. D. ;
Feih, S. ;
Mouritz, A. P. .
COMPOSITE STRUCTURES, 2011, 93 (09) :2269-2276