复合材料修理技术研究进展

摘要/Abstract

摘要： 本文首先阐述了复合材料修理的背景、关键技术、方案设计及修理容限等。随后,针对国内外复合材料修理技术,就解析法、有限元法及优化等计算研究进行了总结及评价,并对实验和测量方面进行讨论,给出复合材料修理问题的研究现状。最后,基于复合材料修理的最新技术,提出该问题亟待解决的几个关键领域,指出未来飞机维修的发展趋势。

关键词: 复合材料修理, 胶结, 解析法, 优化, 冲击, 自动维修系统

Abstract: To begin with, this paper introduced the background, key technique, project design and repair tolerance of the composite repair. Then, the research status of composite repair at home and abroad were summarized and evaluated in two aspects, i.e., the computational research of analytical method, FEM and optimization, and the experiment and measurement. At last, some key fields and development tendency were pointed out on the basis of the newest technique of the composite repair.

Key words: composite repair, bonded, analytical method, optimization, impact, automatic repair system

中图分类号:

TB332
V224

徐绯, 刘斌, 李文英, 谢伟. 复合材料修理技术研究进展[J]. 复合材料科学与工程, 2014, 0(8): 105-112.

XU Fei, LIU Bin, LI Wen-ying, XIE Wei. RESEARCH PROGRESS OF COMPOSITE REPAIR TECHNIQUE[J]. COMPOSITES SCIENCE AND ENGINEERING, 2014, 0(8): 105-112.

参考文献

[1] Berenberg B. Unmanned Composite Aircraft Patr-olthe Skies[J].High Performance Composite,2002,(5):18-22.
[2] 范乔乔,廖明华.2008年各国教练机发展综述[J].世界空军装备,2009,(2):45-51.
[3] Guy Norris. Boeing Awaits FAA Ruling on 87's Composite Structure[J]. Flight International, 2007,171,5079:4.
[4] 杜龙,万建平.复合材料损伤及结构修理技术[J].教练机,2012,4.
[5] 陈绍杰.复合材料设计手册[M].北京:航空工业出版社,1990.
[6] 徐绯,刘亚各,闫慧敏. 蜂窝夹芯结构冲击损伤后的压缩行为研究[J]. 应用力学学报,2013,(5):229.
[7] 闫蕊,徐绯,马春浩. 基于应变损伤模型的复合材料层合板低速冲击数值模拟[J]. 机械科学与技术,2013, 32(2): 235-239.
[8] 夏龙,徐绯,李巧,姚雄华. 复合材料泡沫夹芯结构低速冲击损伤研究[J]. 航空工程进展,2011,2(4):425- 431
[9] Wang Bo, Xu Fei, Wei Yujie. Size effect of failure modes in composite laminates under compression[J]. ICAS,2012,25-28 .
[10] Xu Fei,Duan Min-ge. The sensibility of the foam-core parameters under impact loading[J]. Key Engineering Materials,2013, 525-526:289-292.
[11] 汤洪涛. 航空复合材料维修[J]. 航空制造技术, 2007.
[12] 耿甦,崔旭. 复合材料修理技术研究[J]. 沈阳航空工业学院学报, 2002.
[13] 刘国春,等. 复合材料胶接修补飞机金属结构技术的研究进展及关健技术[J].材料导报, 2007.
[15] Qinetiq. Patching it up-How composites are being used to repair ship and aircraft structures[J]. U. K. Reinforced Plastics, 2004.
[15] Lubkin JL. A theory of adhesive scarf joints[J]. J Appl Mech,1957,24:255.
[16] Hart-Smith LJ. Adhesive-bonded scarf and stepped-lap joints[R]. NASA CR-112237, 1973.
[17] Ahn S.H, Springer G S. Repair of composite laminatesⅡ: Models[J]. Journal of Composite Materials, 1998, 32(11):1076-1114.
[18] Ahn S.H, Springer G S. Repair of composite laminates[R]. DOT/FAA/AR-00/46, 2000.
[19] Chu W.S, Ahn S H. Internet-based composite repair[J]. Journal of Composite Materials, 2005,39(9):827-845.
[20] A.B. Harman, C.H. Wang. Improved design methods for scarf repairs to highly strained composite aircraft structure[J]. Composite Structures,2006,(75):132-144.
[21] A.Barut, J.Hanauska, E.Madenci, et al. Analysis method for bonded patch repair of a skin with acutout[J]. Composite Structures, 2002,55:277-294.
[22] H.Engels, W.Becker. Closed-form analysis for external patch repairs of laminates[J]. Composite Structures, 2002,56:259-268.
[23] Li Dinghe, Qing Guanghui, Liu Yanghong. A three-dimentional semi-analytical model for the composite laminated plates[J]. Comosite Structures,2001,93:1673-1682.
[24] Barut A, Hanauska J, Madenci E, Ambur DR. Analysis method for bonded patch repair of a skin with a cutout[J]. Composite Structures, 2002,55:277-294.
[25] Goland M, Reissner E. The stresses in cemented joints[J]. J Appl Mech, 1944,(11):A17-A27.
[26] Hart-Smith LJ. Design methodology for bonded-bolted composite joints, analysis derivations and illustrative solutions[R]. Technology report AFWAL-TR-81-3154, 1982.
[27] Oplinger D. Effects of adherend deflections in single lap joints[J]. Int Solids Struct,1994,31(18):2565-2587.
[28] Tsai MY, Morton J. An evaluation of analytical and numerical solutions to the single-lap joint[J]. Int Solids Struct, 1994,31(18):2537-2563.
[29] Siener. Stress field sensitivity of a composite patch repair as aresult of varying patch repair thickness[J]. Composite Materials, 1992,(10):444-464.
[30] Bair. Analysis and repair of damaged composite laminates[C]. Proceedings 36^th International SAMPE symposium, SAMPE, Covina, CA USA, 1991,36:2264-2278.
[31] C.Soutis, F.Z.Hu. Design and performance of bonded patch repairs of composite structures[C]. The IMECHE Conference on Airworthiness Aspects of New Technologies, 1996, Bristol.
[32] C.Soutis and F.Z.Hu. A 3D failure analysis of scarf patch repaired CFRP plates[R]. AIAA-98-1943,1998.
[33] Baker A.A; Chester R.J; Hugo G.R, Radtke T.C. Scarf repairs to graphite/epoxy components[C]. AGARD-CP-550,AGARD,NATO,1995.
[34] Mary A. Mahler. Bonded composite repair of composite structures[J]. University of Clifornia LosAngeles,1999.
[35] Randolph A. Odi and Clifford M. Friend. A comparative study of finite element models for the bonded repair of composite structures[J]. Journal of Reinforced Plastics and Composites,2002,(21):321-330.
[36] C.H. Wang, A. Gunnion. Design methodology for scarf repairs to composite structures[J]. DSTO-RR-0317, 2006.
[37] Randolph A. Odi, Clifford M. Friend. An Improved 2D model for bonded composite joints[J]. International Journal of Adhesives, 2004,(24):389-405.
[38] Andrew J. Gunnion, Isreal Herszberg. Parametric study of scarf joints in composite structures[J]. Composite Structures.2006,75:364-376.
[39] Chun H.Wang, Andrew J.Gunnion. On the design methodology of scarf repairs to composite laminates[J]. Composites Science and Technology, 2008,68:35-46.
[40] Md Shamsuddoha. Effectiveness of using fibre-reinforced polymer composites for underwater steel pipeline repairs[J]. Composite Structures,2013,100:40-54.
[41] F.Benyahia. Analysis of the adhesive damage for different patch shapes in bonded composite repair of aircraft structures[J]. Materials and Design,2014,54:18-24.
[42] S.B.Kumar, I.Sridhar, S.Sivashanker, S.O.Osiye-mi. Tensile failure of adhesive bonded CFRP composite scarf joints[J]. Materials Science and Engineering B, 2006, 132:113-120.
[43] Chou Shih pin. Finite element application for strength analysis of scarf-patch-repaired composite laminate[J]. Department of aerospace engineering, 1998.
[44] R.D.S.G. Campilho, M.F.S.F Demoura, J.J.M.S. Domingues. Stress and failure anlyses of scarf repaired CFRP laminates using a cohesive damage model[J]. Journal Adhesion Science Technology, 2007,21(9):855-870.
[45] A.M.G Pinto, R.D.S.G. Campilho, M.F.S.F. de Moura, I.R. Mendes. Numerical evaluation of three-dimentional scarf repairs in carbon-epoxy structures[J]. International Journal of Adhesion & Adhesives.2010,30:329-337.
[46] J.Y. Goh, S. Georgiadis, A.C. Orifici, C.H. Wang, Effects of bondline flaws on the damage tolerance of composite scarf joints[J]. Composites: Part A,2013, 55:110-119.
[47] T.D. Breitzman, E.V. Iarve, B.M. Cook, G.A. Schoeppner, R.P. Lipton. Optimization of a composite scarf repair patch under tensile loading[J].Composites: Part A,2009, 40:1921-1930
[48] Chun H. Wang, Andrew J. Gunnion. Optimum shapes of scarf repairs[J]. Composites: Part A, 2009, 40: 1407-1418.
[49] S.V. Neilson,A.C. Orifici, CH. Wang. Investigation into optimised composite scarf repairs with practical constrains[C]. In:28th International comgress of the areonautical sciences, ICAS, 2012.
[50] 汪海,等. 复合材料蜂窝夹芯结构修理后强度研究[J]. 航空学报, 2001,22(3):270-273.
[51] 孟凡颢,陈绍杰,童小燕. 层压板修理设计中的参数选择问题[J]. 复合材料学报, 2001,18(4):123-127.
[52] 孟凡颢,陈绍杰,童小燕. 复合材料损伤结构胶接补强修补分析及设计[J]. 飞机设计, 2002,1.
[53] 姚磊江,童小燕,董善艳. 损伤复合材料层板胶接修理强度分析[J]. 机械科学与技术, 2005,24(5):676-678.
[54] 喻梅,许希武. 复合材料挖补修理结构的压缩强度分析[J]. 中国矿业大学学报,2008,37(5):709-714.
[55] 王跃全,童明波,朱书华. 基于CDM 的复合材料层合板三维非线性渐进损伤分析[J]. 南京航空航天大学学报, 2009,41(6):709-714.
[56] 林国伟, 陈普会. 胶接修补复合材料层合板失效分析的PDA-CZM方法[J]. 航空学报,2009,30(10):1877-1882.
[57] 王跃全,童明波. 飞机复合材料结构修理设计渐进损伤分析[D]. 南京航空航天大学博士学位论文,2010.
[58] 张玎,杨晓华. 复合材料补片参数对修理后金属结构疲劳性能的影响[J].南京航空航天大学学报,2010,42(3).
[59] 赵立涛,王志瑾. 复合材料胶接修补金属裂纹板及其应力强度因子的研究[D]. 南京航空航天大学硕士学位论文,2010.
[60] 李小刚,赵美英,等. 复合材料胶结修补参数优化研究[J].玻璃钢/复合材料,2010,(1):28-31.
[61] 梁艳勤,汪海. 民机复合材料结构修理容限与修理后适航符合性验证研究[D]. 上海交通大学硕士学位论文,2011.
[62] 高宇剑,程小全. 先进复合材料挖补修理技术的研究进展[J]. 航空制造技术, 2011, 20:97-99.
[63] 徐建新. 复合材料层合板阶梯式挖补修理参数分析[J]. 机械科学与技术, 2011,30(8):1304-1307.
[64] 程起有,朱银垂,等. ANN技术在复合材料胶接修理分析中的应用[J]. 直升机技术, 2011,2.
[65] 李顶河,赵鲁春,等. 复合材料正交加筋层合圆柱壳结构阶梯式挖补修理的参数化研究[J]. 工程力学, 2012,29(9):308-317.
[66] 江毅,卿光辉. 复合材料层合板阶梯式挖补修理的屈曲分析[J]. 航空维修与工程, 2012,1.
[67] 贾宝惠,窦晨,等. 复合材料蜂窝夹芯板斜接式挖补修理的稳定性分析研究[J]. 机械科学与技术,2012,31(4):587-591.
[68] 汪源龙,程小全,等. 挖补修理复合材料层合板拉伸性能研究[J]. 工程力学, 2012,29(7):328-352.
[69] 徐建新,杨维嫣,等. 基于遗传算法的复合材料层合板修理方案优化[J]. 中国民航大学学报,2013,31(1):76-81.
[70] 郭彦江,等. 复合材料层合板贴补修理稳定性研究[J]. 玻璃钢/复合材料, 2013,(2).
[71] 韩坤华,余音. 复合材料胶接修理的湿-热-力耦合瞬时响应分析方法[D]. 上海交通大学大学硕士学位论文,2013.
[72] 李剑峰,燕瑛,廖宝华,等. 复合材料蜂窝夹芯结构单面贴补弯曲性能的分析模型与试验研究[J]. 航空学报, 2013,34(8):1884-1891.
[73] 关志东,刘遂,等. 含半穿透损伤层合板挖补修理后的拉伸性能[J]. 复合材料学报,2013,30(2):144-151.
[74] 郭霞,关志东,等. 蜂窝夹层修理结构的弯曲性能试验分析[J]. 复合材料学报, 2013,30(5):187-194.
[75] Alawi H, Saleh I.E. Fatigue crack growth retardation by bonding patches[J].Eng Fract Mechan, 1992,42(5):861.
[76] Denney J.J. Fatigue response of cracked aluminum panel with partially bonded composite patch[R]. ADA306361,1995.
[77] Denney J.J, Mall S. Effect of disbond on fatigue behavior of cracked aluminum panel with bonded composite patch[R]. AIAA-96-1332,1996.
[78] Jones R, Chiu W.K, Marshall I.H. Weight functions for composite repairs to stiffened panels[J]. Engineering Failure Analysis, 2004,(11):49.
[79] Jones R, Chiu W.K. Composite repairs to cracks in thick metallic components[J]. Composite Structure,1999,(44):17.
[80] Ting T, Jones R, Chiu W.K. Composite repairs to rib stiffened panels[J]. Composite Structure,1999,(47):737.
[81] Cho J, Sun C.T. Multi-step bonding cycles for lowering thermal residual stresses in composite patch repair[R]. AIAA-2002-1725,2002.
[82] Andrew R, Ian W.E, Leo M. Environmental durability trial of bonded composite repairs to metallic aircraft structure[R]. ADA449404,2005.
[83] Ahn S.H., Springer G.S. Repair of Composite Laminates[J]. Office of Aviation research,DOT/FAA/AR-00/46,2000.
[84] Kohei Ichikawa, Yuichiro Shin, Toshiyuki Sawa. A three-dimentional finite-element stress analysis and strength evaluation of stepped-lap adhesive joints subjected to static tensile loadings[J]. International Journal of Adhesion & Adhesive, 2008,28:464-470.
[85] Toshiyuki Sawa, Kohei Ichikawa, Yuichiro Shin, Takashi Kabayashi. A three-dimensional finite element stress analysis and strength prediction of stepped-lap adhesive joints of dissimilar adherends subjected[J]. International Journal of Adhesion & Adhesive, 2010, 30: 298-305.
[86] M.K. Kim, D.J. Elder, C.H. Wang. Interaction of laminate damage and adhesive disbonding in composite scarf jonits subjected to combined in-plane loading and impact[J]. Composite Structure, 2012, 94: 945-953.
[87] Michael W. Keller, Bradley D. Jellison, Travis Ellison. Moisture effects on the thermal and creep performance of carbonfiber/epoxy composites for structural pipeline repair[J].Composites: Part B, 2013, 45:1173-1180.
[88] Hyunbum Park, Changduk Kong. Experi-mental study on barely visible impact damage and visible impact damage for repair of small aircraft composite structure[J]. Aerospace Science and Technology, 2013, 29:363-372.
[89] S.W.Wen, J.Y.Xiao, Y.R.Wang. Accelerated ageing behaviors of aluminum plate with composite patches under salt fog effect[J]. Composites: Part B, 2013, 44:266-273.
[90] B.M. Fredrickson, G.A. Schoeppner, D.H. Mollenhauer, A.N. Palazotto. Application of three-dimentional spline variational analysis for composite repair[J]. Composite Structures, 2008, 83: 119-130.
[91] M.A.Caminero , M.Lopez-Pedrosa, C.Pinna, C.Soutis.Damage monitoring and analysis of co-mposite laminates with an open hole and adhesively bonded repairs using digital image correlation[J]. Composites:Part B, 2013, 53:76-91.
[92] 路阳,赵宇,代永朝. 复合材料损伤微波修理试验研究[J]. 航空维修与工程, 2009,3:50-51.
[93] 吴平,万建平,甘武奎. 某型号教练机用树脂基复合材料层压板结构件修补工艺的研究[J]. 教练机, 2011,3:17-22.
[94] 杜龙,万建平. 复合材料损伤及结构修理技术[J]. 教练机,2012,40.
[95] 徐汶成,赵培仲. 光固化复合材料快速修复金属损伤结构[J]. 中国材料科技与设备, 2012,3.
[96] 郭霞,关志东,等. 层压板双面挖补修理的拉伸性能研究及参数分析[J]. 复合材料学报,2012,29(1):176-182.
[97] Cheng Xiaoquan, Yasir Baig. Study of failure mechanisms in scarf repaired CFRP laminates[J]. International Journal of Adhesion & Adhesives, 2013, 41: 177-185.
[98] 刘遂,关志东,等. 复合材料蜂窝夹芯板挖补修理后的侧压性能[J]. 科技导报, 2013,31(7):28-32.
[99] 纪朝辉,刘阔,等. 挖补修理对复合材料层合板拉伸性能的影响[J]. 中国民航大学学报,2013,31(3):50-53.
[100] B. Whittingham, A.A. Baker, A. Harman, D. Bitton. Micrographic studies on adhesively bonded scarf repairs to thick composite aircraft structure[J]. Composites: Part A, 2009,40:1419-1432.
[101] 化信. 德国汉莎开发飞机复合材料维修新技术[R]. 2012. 158-158.
[102] 陈建祥,王琼琦,罗小乐. 复合材料管与接头胶接构件的强度与疲劳性能研究[J]. 玻璃钢/复合材料, 2012,(1):19-23.
[103] 王耀东,何景武,夏盛来. 复合材料叶片结构设计中的几个关键问题探讨[J]. 玻璃钢/复合材料, 2012,(1):34-38.
[104] 赖娘珍,周洁鹏,王耀先, 董超亮,程树军. 芳纶纤维/AFR树脂复合材料界面粘结性能的研究[J]. 玻璃钢/复合材料, 2011,(4):3-8.
[105] K.B. Katnam, L.F.M.DaSilva, T.M.Young. Bonded repair of composite aircraft structures: A review of scientific challenges and opportunities[J]. Progress in Aerospace Sciences, 2013,61:26-42.

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