欢迎登录材料期刊网

材料期刊网

高级检索

介绍了复合材料补片胶接修补的优越性及关键技术。详细论述了复合材料补片胶接修补的设计分析以及修补的无损检测和试验验证。追踪报道了补片胶接修补的研究方法。

参考文献

[1] Baker A A .Repair of cracked or defective metallic aircraft-components with advanced fibre composites[J].Computers and Structures,1984,2:153-234.
[2] Baker A A .Fiber composite repair of cracked metallic aircraft component-practical and basic aspects[J].Composites,1987,18(04):293-307.
[3] Jones R;Callinan R J.Bonded repairs to surface flaws[A].New Delhi,India,1984:3517-3522.
[4] 陈绍杰.复合材料结构修理指南[M].北京:航空工业出版社,2001:109-111.
[5] Turaga V. R. S. Umamaheswar;Ripudaman Singh .Modelling of a patch repair to a thin cracked sheet[J].Engineering Fracture Mechanics,1999(2/3):267-289.
[6] Mahadesh Kumar A;Hakeem S A.Optimum design of symmetric composite patch repair to centre cracked metallic sheet[J].Computers and Structures,2000(49):285-292.
[7] Mahler M A.Bonded composite repair of composite structures[M].Los Angeles, USA,1999:165-167.
[8] 徐建新 .损伤金属结构的复合材料胶接修补技术研究[D].南京航空航天大学,1996.
[9] 金观昌.电子错位散斑干涉术用于无损检测的探讨[J].实验力学,1992(07):26-38.
[10] 陈金根 .复合材料制品的超声检测[J].无损探伤,1995,6:1-8.
[11] Bossi RH;Coopride K K.X-ray computed tomography of composite[A].,1996:224-239.
[12] Ferraro P;Stetson K A .On the holographic detection of core-to-skin disbonds in composite sandwich structures[J].Journal of Mater Eval,1994,61(12):1376-1381.
[13] Qin Y W;Bao N K .Infrared thermography to its application in the NDT of sandwich structures[J].Optics and Laser in Engineering,1996(21):205-211.
[14] 陈金龙,秦玉文,计欣华.双材料界面粘接质量定量检测的相移错位散斑技术[J].复合材料学报,2001(01):128-130.
[15] Chiu W K;Galea SC;Koss L L;Rajic N.Damage detection in bonded repairs using PZT material[J].Smart Materials and Structures,1999(31):121-158.
[16] Koh Y L;Chiu W K .Smart-structure for composite repair[J].Computers and Structures,1999,47:745-752.
[17] Erdogan F;Arin K A .Sandwich plate with a part-through and a debonding crack[J].Engineering Fracture Mechanics,1972,4(02):449-458.
[18] ROSE L R F .An application of the inclusion analogy for bonded reinforcement[J].International Journal of Solids and Structures,1981,17:827-838.
[19] Davis M J;Bond D A.The importance of failure mode identification in adhesive bonded aircraft structures and repairs[A].,2000:132.
[20] Jones R .Crack-patching: analysis and design[J].Journal of Strural Mechanics,1982,10(02):177-190.
[21] Sun C T;Klug J;Arendt C.Analysis of cracked aluminum plates repaired with bonded composites patches[J].AIAA Journal:369-374.
[22] 白金泽,孙秦,董善艳.复合材料补片胶接补强修补技术参数分析[J].机械科学与技术,2001(05):748-750.
[23] Molent L;Callinan R J;Jones R .Design of an all boron/epoxy doubler reinforcement for the F-111 wing pivot fitting[J].Computers and Structures,1989,11:57-83.
[24] Davis M J;Bond D A.Adhesive bonded patch repair of damaged composite laminate[M].Imperial College, London,1996:21-26.
[25] 乔新.波音飞机复合材料结构修理教程[M].北京:中国民航出版社,1996:38-75.
[26] Ratwani M M;Kan H P;Fitagerald J H .Experimental investigations of fiber composite reinforcement of cracked metallic structures[R].ASTM STP787,Philadelphia,USA:ASTM,1982.
[27] Sandow F A;Cannon R K .Composite repair of cracked aluminum alloy aircraft structure[R].AD-A 190 514
[28] Denny 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(05):507-525.
[29] Alawi H;Saleh I E .Fatigue crack growth retardation by bonding patches[J].Engineering Fracture Mechanics,1992,42(05):861-868.
上一张 下一张
上一张 下一张
计量
  • 下载量()
  • 访问量()
文章评分
  • 您的评分:
  • 1
    0%
  • 2
    0%
  • 3
    0%
  • 4
    0%
  • 5
    0%