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利用真空袋压工艺,采用单向炭纤维复合材料补片对中心裂纹铝合金板进行了单面胶接修补.测试了复合材料修补板的静态拉伸强度及修补板在拉拉疲劳过程中的裂纹扩展、界面脱粘和剩余拉伸强度等疲劳性能.结果表明,复合材料补片胶接修补能有效地提高裂纹板的破坏强度和刚度,降低裂纹板的疲劳裂纹扩展速率,提高其疲劳寿命.裂纹板经单向炭纤维/环氧复合材料补片修补后,其破坏强度从311.48 MPa提高到364.74 MPa,疲劳寿命从32217次提高到77546次.疲劳导致修补结构的粘接界面脱粘,脱粘区域近似椭圆形;脱粘面积随疲劳周次的增加而增加,且增加的幅度与疲劳周次相关.

参考文献

[1] Baker A A.Bonded repair of aircraft structure[M].Dordrecht,Netherlands:Martinus Nijhoff Publishers,1988:1-17.
[2] 陈绍杰.复合材料结构修理指南[M].北京:航空工业出版社,2001:34-44.Chen Shaojie.Manual of repair of composite structures[M].Beijing:Aviation Industry Publishing Company,2001:34-44.
[3] Michael L O.Carbon composite repairs of helicopter metallic primary structure[J].Composite Structures,1993,25(4):557-565.
[4] Baker A A.Bonded composite repair of fatigue-cracked primary aircraft structure[J].Composite Structures,1999,47(1/4):431-443.
[5] 王清远,袁祥明,李戍中.损伤金属结构件复合材料粘贴修补[J].玻璃钢/复合材料,2003(6):41-44.Wang Qingyuan,Yuan Xiangming,Li Shuzhong.Composite bonded repair of defective structures[J].FRP/Composites,2003(6):41-44.
[6] 张延民,常青,张付友.先进复合材料在飞机主承力件修理中的应用[J].航空制造技术,2004(7):89-90.Zhang Yanmin,Chang Qing,Zhang Fuyou.Application of advanced composite in the repairing of the main load-bearing structure of the aircraft[J].Aeronautical Manufacturing Technology,2004(7):89-90.
[7] 陈绍杰.用复合材料技术修理金属飞机结构的修理记实[J].航空工程与维修,2000(1):21-22.Chen Shaojie.Repair practice of using composite technology for aircraft metal structures[J].Aviation Engineering and Maintenance,2000(1):21-22.
[8] 徐建新.复合材料补片胶接修理技术的研究进展[J].航空学报,1999,20(4):381-383.Xu Jianxin.Advances in the development of bonded repairs with composite patches[J].Acta Aeronautica et Astronautica Sinica,1999,20(4):381-383.
[9] 徐建新,刘艳红,周煊,等.损伤金属结构的复合材料胶接修补试验研究[J].南京航空航天大学学报,2001,33(1):96-99.Xu Jianxin,Liu Yanhong,Zhou Xuan,et al.Experimental investigation of cracked metallic structures bonded with composite patches[J].Journal of Nanjing University of Aeronautics & Astronautics,2001,33(1):96-99.
[10] Wang Q Y,Pidaparti R M.Static characteristics and fatigue behavior of composite repaired aluminum plates[J].Composite Structures,2002,56(2):151-155.
[11] Seo D C,Lee J J.Fatigue crack growth behavior of cracked aluminum plate repaired with composite patch[J].Composite Structure,2002,57(1/4):323-330.
[12] Schubbe J J,Mall S.Investigation of a cracked thick aluminum panel repaired with a bonded composite patch[J].Engineering Fracture Mechanics,1999,63(3):305-323.
[13] Schubbe 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(5):507-525.
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