Restoration of the mechanical performance of damaged Al panels using bonded composite repair patches

被引:8
作者
Constantin, Nicolae [1 ]
Sandu, Marin [1 ]
Sorohan, Stefan [1 ]
机构
[1] Univ Politehn Bucuresti, Bucharest, Romania
关键词
Composite repair patch; Numerical simulation; Strain gauge measurements; ELEMENT ANALYSIS; AIRWORTHINESS; AIRCRAFT;
D O I
10.1016/j.ijadhadh.2013.01.003
中图分类号
TQ [化学工业];
学科分类号
0817 ;
摘要
The paper presents a study upon the behaviour of repaired Al panels under lateral pressure loads, in which various geometries and materials are used for the bonded composite repair patches. The repaired part of the panel is considered in central and side positions. The numerical simulations were validated by experiments in a number of cases, and then used to evaluate the whole proposed range of repair patching configurations. In all key studies, the stress distribution in the adhesive layer and restoration of the mechanical performance at the level of the pristine panel were assessed, in order to make possible the establishment of margins of safety for a wider range of repair patching parameters or configurations. (C) 2013 Elsevier Ltd. All rights reserved.
引用
收藏
页码:69 / 76
页数:8
相关论文
共 20 条
  • [11] Large deflection effects of cracked aluminum plates repaired with bonded composite patches
    Klug, JC
    Sun, CT
    [J]. COMPOSITE STRUCTURES, 1998, 42 (03) : 291 - 296
  • [12] A standard analysis methodology for the stress analysis of repaired aircraft structures with the method of composite patch repair
    Marioli-Riga, Z
    Xenos, D
    Vrettos, C
    [J]. APPLIED COMPOSITE MATERIALS, 2004, 11 (04) : 191 - 203
  • [13] Progressive damage modelling of bonded composite repairs
    Papanikos, P
    Tserpes, KI
    Labeas, G
    Pantelakis, S
    [J]. THEORETICAL AND APPLIED FRACTURE MECHANICS, 2005, 43 (02) : 189 - 198
  • [14] Optimization of composite patch repair processes with the use of genetic algorithms
    Papathanassiou, Theodosios K.
    Filopoulos, Sotirios P.
    Tsamasphyros, George J.
    [J]. OPTIMIZATION AND ENGINEERING, 2011, 12 (1-2) : 73 - 82
  • [15] Rose LRF, 2002, ADVANCES IN THE BONDED COMPOSITE REPAIR OF METALLIC AIRCRAFT STRUCTURE, VOLS 1 AND 2, P137
  • [16] A CRACKED PLATE REPAIRED BY BONDED REINFORCEMENTS
    ROSE, LRF
    [J]. INTERNATIONAL JOURNAL OF FRACTURE, 1982, 18 (02) : 135 - 144
  • [17] St Sorohan N, P 16 INT C COMP MAT
  • [18] Analysis of out-of-plane bending in one-sided bonded repair
    Wang, CH
    Rose, LRF
    Callinan, R
    [J]. INTERNATIONAL JOURNAL OF SOLIDS AND STRUCTURES, 1998, 35 (14) : 1653 - 1675
  • [19] Wang CH, 1997, P 11 INT C COMP MAT, V5, P347
  • [20] Boundary element analysis of flat cracked panels with adhesively bonded patches
    Wen, PH
    Aliabadi, MH
    Young, A
    [J]. ENGINEERING FRACTURE MECHANICS, 2002, 69 (18) : 2129 - 2146