期刊文献+

损伤金属结构件复合材料粘贴修补 被引量:20

COMPOSITE BONDED REPAIR OF DEFECTIVE STRUCTURES
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摘要 近年来 ,用复合材料贴片修补有缺陷 ,含裂纹或被腐蚀的金属结构件已成为十分引人注目的研究和发展课题。复合材料修补比传统的机械焊接 ,螺接或铆接具有多种的优越性 ,其中包括改善疲劳性能 ,恢复刚度和强度 ,均匀修补局部的应力分布 ,密封联接 ,减轻重量和增强抗腐蚀能力等方面。本文综述了损伤金属结构件复合材料贴片修补研究和发展方面的最新进展 ,主要包括材料及其技术发展 ,分析模型的有关研究 。 The use of composite patches in the repair of defective/cracked or corroded metallic structures has seen rapid expansion recently. Composite repairs offer various advantages over mechanical fastening or riveting, including improved fatigue behavior, restored stiffness and strength, even distribution of stress over the entire bonded area, sealing protection of joined assemblies, reduced weight and improved corrosion resistance. The purpose of this article is to summarize recent efforts into the research and development of composite repairs bonded to defective structures. This review focuses on analytical models, materials and technologies and experimental data or experiences related to adhesive bonded composite repair in cracked metallic structures.
机构地区 四川大学
出处 《玻璃钢/复合材料》 CAS CSCD 2003年第6期41-44,共4页 Fiber Reinforced Plastics/Composites
基金 教育部优秀青年教师资助计划 ( 2 0 0 2 - 350 )
关键词 复合材料贴片 修补 金属结构件 胶粘接 疲劳耐久性 飞机 composite repair composite patch adhesive bonding fatigue durability
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参考文献19

  • 1王清远,陶华.复合材料修补件的强度和疲劳性能[J].材料工程,2003,31(1):21-23. 被引量:25
  • 2陈浩然,尹向勇,刘相斌.具有分层损伤复合材料加筋与无加筋层合板热-机械力屈曲性态[J].复合材料学报,2000,17(2):70-73. 被引量:3
  • 3Wang Q Y, Pidaparti R M. Static characteristics and fatigue behavior of composite- repaired aluminum plates [ J ], Composite Structures, 2002, 56(2) : 151-155.
  • 4Klug J C, Maley S, Sun C T. Characterization of fatigue behavior of bonded composite repairs [J], Journal of aircraft, 1999, 36(6): 1016-1022.
  • 5Schubbe J J, Mall S, Modeling of cracked thick metallic structure with bonded composite patch repair using three- layer technique [J]. Composite Structures, 1999, 45(3): 185-193.
  • 6Kumar A M, Hakeem S A. Optimum design of symmetric composite patch repair to centre cracked metallic sheet [J], Composite Structures, 2000, 49(3): 285-292.
  • 7Denney J J, Mall S, Characterization of disbond effects on fatigue crack growth behavior in aluminum plate with bonded composite patch [J]. Engineering Fracture Mechanics, 1997, 57:507-525.
  • 8Tran - Cong T, Heller M. Reduction in adhesive shear strains at the ends of bonded reinforcements [ R]. Technical Report, DSTO- RR -0115.
  • 9Chow W T, Atluri T. Composite patch repairs of metal structures: adhesive nonlinearlity, thermal cycling, and debonding [J]. AIAA Journal, 1997, 35(9): 1528-1535.
  • 10Schubbe J J, Mall S. Investigation of a cracked thick aluminum panel repaired with a bonded composite patch [ J ]. Eng Fracture Mechanics, 1999, 63(3): 305-323.

二级参考文献16

  • 1[2]WANG Q Y, PIDAPARTI R M. Static characteristics and fatigue behavior of composite-repaired aluminum plates. Submitted to Composite Structures [J], in review, 2001.
  • 2[3]KUMAR A M, HAKEERN S A. Optimum design of symmetric composite patch repair to center cracked metallic sheet [J] .Composite Structures, 2000, 49 (3): 285-292.
  • 3[4]UMAMAHESWAR T V RS, SINGH R. Modeling of a patch repair to a thin cracked sheet [J] . Engineering Fracture Mechanics, 1999, 62: 267-289.
  • 4[5]WANG W C, HSU J S. Investigation of the size effect of composite patching repaired on edge-cracked plates [J] . Composite Structures, 2000, 49 (4): 415-423.
  • 5[6]VECCHIO F J, BUCCI F. Analysis of repaired reinforced concrete structures [J] . J of Structural Engineering, 1999, 125(6): 644 [652.
  • 6[7]KLUG J C, MALEY S, SUN C T. Characterization of fatigue behavior of bonded composite repairs [J] . Journal of aircraft,1999, 36 (6): 1016-1022.
  • 7[8]RENAUD G, HANSEN J S. Thermal model for cracked structures repaired with composite patches [J] . AIAA Journal,1998, 36 (12): 2229-2235.
  • 8[9]NABOULSI S, MALL S. Nonlinear analysis of bonded composite patch repair of cracked aluminium panels [J] . Composite Structures, 1998, 41 (3-4): 303-313.
  • 9[10]ROSE L R F. A cracked plate repaired by bonded reinforcements [J] . Int J Fracture, 1982, 18 (2): 135-144.
  • 10[11]ROSE L R F. An application of the inclusion analogy for bonded reinforcements[J]. Int J Solids Structures, 1981, 17: 827-838.

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二级引证文献103

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