Behavior of pin-loaded laminated composites

被引:50
作者
Baba, B. Okutan [1 ]
机构
[1] Canakkale Onsekiz Mart Univ, Canakkale, Turkey
关键词
pin; laminated composite; E/glass-epoxy; failure modes; joint geometry;
D O I
10.1007/s11340-006-8735-z
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
In this study, an investigation was carried out to determine the effects of joint geometry and fiber orientation on the failure strength and failure mode in a pinned joint laminated composite plate. Behavior of pin-loaded laminated composites with different stacking sequence and different dimensions has been observed experimentally. E/glass-epoxy composites were manufactured to fabricate the specimens. Mechanical properties of the composites were characterized under tension, compression and in-plane shear in static loading conditions. Laminated composites were loaded through pins. Single-hole pin-loaded specimens were tested for their tensile response and width-to-hole diameter (W/D) and edge distance-to-hole diameter (E/D) ratios evaluated. A series of experiments was performed with six different material configurations ([0/+/- 45](s)-[90/+/- 45](s), [0/90/0](s)-[90/0/90](s) and [90/0](2s)-[+/- 45](2s)), in all, over 120 specimens. E/D ratios and W/D ratios of plates were changed from 1 to 5 and 2 to 5, respectively. Failure propagation and failure type were observed on the specimens. The influence of the joint geometry on the strength of the pin-loaded composites was assessed. When laminated composite plates were loaded to final failure, three basic failure modes consisting of net-tension, shear out and bearing failure were observed for the different geometric dimensions. All the connections tested showed that the fiber orientations have a definite influence on the position around hole circumference at which failure initiated. Net-tension failure occurred for specimens that had small width and large end distance. When the width was increased, the specimens which had small end distances failed in the shear-out modes. When the end distance was increased, bearing failure developed in addition to shear-out failure. The experimental results showed that the ultimate load capacities of E/glass-epoxy laminate plates with pin connection were increased by increasing W and E. However, increasing the E/D and W/D ratios beyond a critical value has an insignificant effect on the ultimate load capacity of the connection.
引用
收藏
页码:589 / 600
页数:12
相关论文
共 16 条
[1]   THE EXPERIMENTAL BEHAVIOR OF BOLTED JOINTS IN PULTRUDED GLASS POLYESTER MATERIAL .1. SINGLE-BOLT JOINTS [J].
ABDELNABY, SFM ;
HOLLAWAY, L .
COMPOSITES, 1993, 24 (07) :531-538
[2]  
BAKER A, 1997, COMPOSITES ENG HDB
[3]   Stress analysis and strength prediction of mechanically fastened joints in FRP: A review [J].
Camanho, PP ;
Matthews, FL .
COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 1997, 28 (06) :529-547
[4]   ON THE INFLUENCE OF WEAVE STRUCTURE ON PIN-LOADED STRENGTH OF ORTHOGONAL 3D COMPOSITES [J].
CHEN, JC ;
LU, CK ;
CHIU, CH ;
CHIN, H .
COMPOSITES, 1994, 25 (04) :251-262
[5]  
COHEN D, 1989, P AM SOC COMP, P72
[6]  
Collings T, 1977, COMPOS Compos, V8, P43
[7]   ON THE BEARING STRENGTHS OF CFRP LAMINATES [J].
COLLINGS, TA .
COMPOSITES, 1982, 13 (03) :241-252
[8]   A REVIEW OF THE STRENGTH OF JOINTS IN FIBER-REINFORCED PLASTICS .1. MECHANICALLY FASTENED JOINTS [J].
GODWIN, EW ;
MATTHEWS, FL .
COMPOSITES, 1980, 11 (03) :155-160
[9]   NONLINEAR BEHAVIOR OF LAMINATED COMPOSITES [J].
HAHN, HT .
JOURNAL OF COMPOSITE MATERIALS, 1973, 7 (APR) :257-271
[10]  
HARTSMITH LJ, 1980, FIBROUS COMPOSITES S