在修补含裂纹损伤的飞机金属结构和老龄化飞机延寿方面,复合材料胶接修补飞机金属结构是一门实用有效的技术.主要介绍了该技术的操作流程和关键技术,以及国内外该领域内近10年来在理论和实验方面的研究动态.
参考文献
| [1] | Baker A A;Rose L R F;Jones R.Advances in the bonded composite repair of metallic aircraft structure[J].Elsevier Applied Science,2002 |
| [2] | Baker A A .Bonded composite repair of fatigue-cracked primary aircraft structures[J].Computers & Structures,1999,47:431. |
| [3] | 王必宁 .复合材料胶接修补金属裂纹板的计算与实验研究[D].西北工业大学,2004. |
| [4] | Sun C T;Klug J;Arendt C .Analysis of cracked aluminum plates repaired with bonded composite patches[A9526863][R].,1995. |
| [5] | Schubbe J J;Mall s .Fatigue behavior in thick aluminum panels with a composite repair[AIAA-98-1997][R].,1998. |
| [6] | Naboulsi S;Mall S .Analysis of cracked metallic structure with imperfectly bond composite patch[AIAA-971363][R].,1997. |
| [7] | Pai P F;Schulz M J .Modeling and dynamic characteristics of composite repaired aluminum plates[AIAA-96-1349CP][R].,1996. |
| [8] | Megueni A;Tounsi A.The effect of a bonded hygrothermal aged composite patch on the stress intensity factor for repairing cracked metallic structures[J].Computers & Structures,2003(62):171. |
| [9] | Megueni A;Bouiadjra B B;Belhouari M .Disbond effect on the stress intensity factor for repairing cracks with bonded composite patch[J].COMPUTATIONAL MATERIALS SCIENCE,2004,29:407. |
| [10] | Bachir Bouiadjra B;Belhouari M .Computation of the stress intensity factors for repaired cracks with bond composite patch in mode I and mix modes[J].Computers & Structures,2002,56:401. |
| [11] | Tong L Y;Sun X N .Optimization of bonded patch to cylindrically curved shell structure[ADA398887][R].,2001. |
| [12] | Harman A B;Walker K F .Review of improved methods for analyzing load attraction and thermal effects in bonded composite repair design[ADA424267][R].,2003. |
| [13] | Alawi H;Saleh I E .Fatigue crack growth retardation by bonding patches[J].Engineering Fracture Mechanics,1992,42(05):861. |
| [14] | Denney J J .Fatigue Response of Cracked Aluminum Panel with Partially Bonded Composite Patch[ADA306361][R].,1995. |
| [15] | Denney J J;Matl S .Effect of disbond on fatigue behavior of cracked aluminum panel with bonded composite patch[AIA A-96-1332][R].,1996. |
| [16] | Jones R;Chiu W K;Marshall I H.Weight functions for composite repairs to stiffened panels[J].Engineering Failure Analysis,2004(11):49. |
| [17] | Jones R;Chiu W K.Composite repairs to cracks in thick metallic components[J].Computers & Structures,1999(44):17. |
| [18] | Jones R;Peng D.A simple method for computing the stress intensity factors for cracks at notches[J].Engineering Failure Analysis,2000(09):683. |
| [19] | Ting T;Jones R;Chiu W K.Composite repairs to rib stiffaned panels[J].Computers & Structures,1999(47):737. |
| [20] | Sun C T;Carather S .Modeling and lowering residual stresses in bonded composite patch repair of metallic aircraft structures[AD394588][R].,2001. |
| [21] | Cho J;Sun C T .Multi-step bonding cycles for lowering thermal residual stresses in composite patch repairs[AIAA-2002-1725][R].,2002. |
| [22] | Andraw R;Ian W E;Leo M .Environmental durability trial of bonded composite repairs to metallic aircraft structure[ADA449404][R].,2005. |
| [23] | Wakha K;Samud P .Damage detection in composite patches using a stiffness/energy sensor[AIAA-2004-1986][R].,2004. |
| [24] | Ihn J B;Chang F K .Smart patches for monitoring crack growth in aircraft structure[AIAA-2002-1544][R].,2002. |
| [25] | 童谷生,孙良新,刘英卫.飞机结构损伤的复合材料胶接修补技术研究进展[J].宇航材料工艺,2002(05):20-24,29. |
| [26] | 复合材料补片胶接修理技术的研究进展[J].航空学报,1999(04):381. |
| [27] | 徐建新 .复合材料胶接修理损伤金属结构的研究现状[J].力学进展,2000,30(03):415. |
| [28] | 徐建新.复合材料补片的修理决策[J].航空制造工程,1998(04):33. |
| [29] | 徐建新;张天达 .复合材料补片止裂性能的方法研究[J].工程力学,1999,16(02):93. |
| [30] | 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. |
| [31] | 白金泽 .复合材料胶接修补参数优化分析[D].西北工业大学,2000. |
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