Numerical analysis of the beneficial effect of the double symmetric patch repair compared to single one in aircraft structures

被引:18
作者
Bouiadjra, B. Bachir [1 ]
Fekinni, H. [1 ]
Serier, B. [1 ]
Benguediab, M. [1 ]
机构
[1] Univ Djillali Liabes Sidi Bel Abbes, Dept Mech Engn, Sidi Bel Abbes 22000, Algeria
关键词
single patch; double patch; composite patch; SIF; adhesive; thickness; shear modulus; reduction ratio;
D O I
10.1016/j.commatsci.2006.05.020
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
This paper concerns a numerical study by the finite element method of the cracked structure repaired by single and double bonded composite patches. The stress intensity factor is used as fracture criteria. The obtained results showed the advantage of the double patch compared to single on the reduction of the stress intensity factor at the crack tip. The effects of the properties of the plate and the patch and the adhesive on the beneficial effect of the double patch are highlighted. The adhesive properties must be optimised in order to increase the advantage of the double patch and to avoid the adhesive failure. The patch properties have a significant effect on the beneficial effects of the double symmetric patch. (c) 2006 Elsevier B.V. All rights reserved.
引用
收藏
页码:824 / 829
页数:6
相关论文
共 12 条
[1]   Numerical analysis of the performances of the bonded composite patch for reducing stress concentration and repairing cracks at notch [J].
Achour, T ;
Bouiadjra, BB ;
Serier, B .
COMPUTATIONAL MATERIALS SCIENCE, 2003, 28 (01) :41-48
[2]   Bonded composite repair of fatigue-cracked primary aircraft structure [J].
Baker, A .
COMPOSITE STRUCTURES, 1999, 47 (1-4) :431-443
[3]   Computation of the stress intensity factors for repaired cracks with bonded composite patch in mode I and mixed mode [J].
Bouiadjra, BB ;
Belhouari, M ;
Serier, B .
COMPOSITE STRUCTURES, 2002, 56 (04) :401-406
[4]  
CALLINAN RJ, 1997, DSTOTN0067
[5]   ESTIMATION OF STRESS INTENSITY FACTORS IN PARTIALLY PATCHED CRACKED COMPOSITE LAMINATES BY MULTILAYER HYBRID-STRESS FINITE-ELEMENT METHOD [J].
CHEN, WH ;
YANG, SH .
FINITE ELEMENTS IN ANALYSIS AND DESIGN, 1995, 21 (1-2) :21-44
[6]   Composite repairs to cracks in thick metallic components [J].
Jones, R ;
Chiu, WK .
COMPOSITE STRUCTURES, 1999, 44 (01) :17-29
[7]   Characterization of fatigue behavior of bonded composite repairs [J].
Klug, J ;
Maley, S ;
Sun, CT .
JOURNAL OF AIRCRAFT, 1999, 36 (06) :1016-1022
[8]   Computation of the stress intensity factor for patched crack with bonded composite repair in pure mode II [J].
Megueni, A ;
Bouiadjra, BB ;
Boutabout, B .
COMPOSITE STRUCTURES, 2003, 59 (03) :415-418
[9]   Modeling of cracked thick metallic structure with bonded composite patch repair using three-layer technique [J].
Schubbe, JJ ;
Mall, S .
COMPOSITE STRUCTURES, 1999, 45 (03) :185-193
[10]  
SWENSON D, 1998, FRANC2D L VERSION 1