Effect of Temperature on the Energy Release Rate Variation in Repaired Laminate Composites

被引:4
作者
Belhouari, M. [1 ]
Benkheira, A. [2 ]
Madani, K. [1 ]
Campilho, R. D. S. G. [3 ,4 ]
Gong, X. L. [5 ]
机构
[1] Univ Djillali Liabes Sidi Bel Abbes, Dept Mech Engn, Sidi Bel Abbes, Algeria
[2] Univ Djelfa, Dept Mech Engn, Djelfa, Algeria
[3] Polytech Porto, ISEP Sch Engn, Porto, Portugal
[4] INEGI Inst Sci & Innovat Mech & Ind Engn, Porto, Portugal
[5] Univ Technol Troyes, LASMIS, Troyes, France
关键词
Composite patch; Laminate composite; Repair; Fracture energy; Mechanical properties; Temperature; THERMAL RESIDUAL-STRESSES; ADHESIVELY BONDED JOINTS; MECHANICAL-PROPERTIES; SINGLE LAP; TENSILE PROPERTIES; FRP COMPOSITES; STRENGTH; BEHAVIOR; CFRP; DELAMINATION;
D O I
10.1007/s11668-023-01594-y
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
This work initially aims to study the influence of temperature on the mechanical properties of composite materials and adhesive. With this purpose, the mechanical properties of the adhesive and composite were measured experimentally under different temperature to provide the requested information for finite element modeling, and then inserted in a numerical model of bonded composite patch on cracked laminate composite plate to evaluate the fracture energy variations at repaired crack tip for different temperatures. The main results obtained confirm the beneficial effects of the composite patch on the mechanical behavior of a cracked composite. Moreover, the reduction in the mechanical properties induced by temperature negatively affects the repair strength. On the other hand, the fracture energy is strongly related to crack length and temperature.
引用
收藏
页码:420 / 435
页数:16
相关论文
共 46 条
[1]   Thermal residual stresses in bonded composite repairs on cracked metal structures [J].
Albat, AM ;
Romilly, DP ;
Raizenne, MD .
MATERIALS TECHNOLOGY, 2000, 15 (04) :299-308
[2]   Mode I fracture of epoxy bonded composite joints: 1. Quasi-static loading [J].
Ashcroft, IA ;
Hughes, DJ ;
Shaw, SJ .
INTERNATIONAL JOURNAL OF ADHESION AND ADHESIVES, 2001, 21 (02) :87-99
[3]  
Baker A.A., 1988, Bonded repair of aircraft structures
[4]  
BAKER A.A., 1984, THEOR APPL FRACT MEC, V2, P1, DOI DOI 10.1016/0167-8442(84)90035-1
[5]  
Baker A.A.A., 1987, J COMPOS, V9, pI
[6]   Effect of temperature on the shear strength of aluminium single lap bonded joints for high temperature applications [J].
Banea, M. D. ;
da Silva, L. F. M. ;
Campilho, R. D. S. G. .
JOURNAL OF ADHESION SCIENCE AND TECHNOLOGY, 2014, 28 (14-15) :1367-1381
[7]   Effect of Temperature on Tensile Strength and Mode I Fracture Toughness of a High Temperature Epoxy Adhesive [J].
Banea, M. D. ;
da Silva, L. F. M. ;
Campilho, R. D. S. G. .
JOURNAL OF ADHESION SCIENCE AND TECHNOLOGY, 2012, 26 (07) :939-953
[8]   Effects of Temperature and Loading Rate on the Mechanical Properties of a High Temperature Epoxy Adhesive [J].
Banea, M. D. ;
de Sousa, F. S. M. ;
da Silva, L. F. M. ;
Campilho, R. D. S. G. ;
de Bastos Pereira, A. M. .
JOURNAL OF ADHESION SCIENCE AND TECHNOLOGY, 2011, 25 (18) :2461-2474
[9]   The effect of temperature on the mechanical properties of adhesives for the automotive industry [J].
Banea, M. D. ;
da Silva, L. F. M. .
PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART L-JOURNAL OF MATERIALS-DESIGN AND APPLICATIONS, 2010, 224 (L2) :51-62
[10]   Experimental and Numerical Study of the Effect of Debonding Defect in Composite Patch Repairs on Composite Plate [J].
Benkheira, A. ;
Belhouari, M. ;
Madani, K. ;
Gong, X. L. .
JOURNAL OF FAILURE ANALYSIS AND PREVENTION, 2022, 22 (04) :1669-1692