Effect of curing overheating on interlaminar shear strength and its modelling in thick FRP laminates

被引:54
作者
Esposito, Luca [1 ]
Sorrentino, Luca [2 ]
Penta, Francesco [1 ]
Bellini, Costanzo [2 ]
机构
[1] Univ Naples Federico II, Dept Ind Engn, Ple Tecchio 80, I-80125 Naples, Italy
[2] Univ Cassino & Southern Lazio, Dept Civil & Mech Engn, I-03043 Cassino, Italy
关键词
Prepreg; Thermosetting resin; Cure behaviour; Mechanical testing; CARBON FIBER/EPOXY COMPOSITES; CURE PROCESS; MECHANICAL PERFORMANCE; FIBRE/EPOXY COMPOSITES; KINETIC-MODEL; TEMPERATURE; OPTIMIZATION; METHODOLOGY; STRESSES; PARTS;
D O I
10.1007/s00170-016-8613-5
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
During the curing process, the exothermic cross-linking reaction inside epoxy resin-based composites causes overheating and, eventually, a thermal degradation of the matrix. Thick sectioned epoxy composites require an optimized curing cycle in order to minimize the temperature raise inside the composite. However, the recommended cycle for thin laminates is often wrongly used also for thick sectioned composites, resulting in an overheating. In this work, the mechanical behaviour of laminates having different thicknesses was investigated. Specimens were cured according to a curing cycle optimal for thin laminates which causes overheating in thicker laminates. The curing temperature histories at several positions inside the laminates were monitored and recorded and, following a new methodological approach, a series of comparative interlaminar shear tests was performed. Experimental results show a decrease of the interlaminar shear strength in thicker laminates. A simple model to account for the detrimental effect of the exothermic peak on the interlaminar shear strength is proposed.
引用
收藏
页码:2213 / 2220
页数:8
相关论文
共 33 条
[1]  
[Anonymous], 2013, E2070 ASTM
[2]  
[Anonymous], 2000, D2344D ASTM
[3]   A methodology to reduce thermal gradients due to the exothermic reactions in composites processing [J].
Antonucci, V ;
Giordano, M ;
Hsiao, KT ;
Advani, SG .
INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER, 2002, 45 (08) :1675-1684
[4]   Microlevel manufacturing process simulation of carbon fiber/epoxy composites to analyze the effect of chemical and thermal induced residual stresses [J].
Brauner, Christian ;
Block, Tim B. ;
Purol, Holger ;
Herrmann, Axel S. .
JOURNAL OF COMPOSITE MATERIALS, 2012, 46 (17) :2123-2143
[5]   Role of processing on interlaminar shear strength enhancement of epoxy/glass fiber/multi-walled carbon nanotube hybrid composites [J].
Chandrasekaran, V. C. S. ;
Advani, S. G. ;
Santare, M. H. .
CARBON, 2010, 48 (13) :3692-3699
[6]   A TECHNIQUE FOR DETERMINING MECHANICAL-PROPERTIES OF THICK COMPOSITE LAMINATES [J].
CIRISCIOLI, PR ;
SPRINGER, GS ;
WANG, Q .
JOURNAL OF COMPOSITE MATERIALS, 1991, 25 (10) :1330-1339
[7]   EFFECT OF SPECIMEN SIZE ON INTERLAMINAR SHEAR-STRENGTH OF UNIDIRECTIONAL CARBON FIBER-EPOXY [J].
CUI, WC ;
WISNOM, MR ;
JONES, M .
COMPOSITES ENGINEERING, 1994, 4 (03) :299-307
[8]  
Dmitriev O, 2011, ADV COMPOSITE MAT EC, P642
[9]  
Dragan A., 2015, Soft computing in the design and manufacturing of composite materials
[10]   Temperature field of thick thermoset composite laminates during cure process [J].
Guo, ZS ;
Du, SY ;
Zhang, BM .
COMPOSITES SCIENCE AND TECHNOLOGY, 2005, 65 (3-4) :517-523