为选取一款适用于飞机主承力结构复合材料胶接修理的胶粘剂,以飞机起落架梁结构为胶接修理对象,首先根据起落架梁胶接修理场景,初步筛选了4种环氧树脂类胶粘剂。然后对这4种胶粘剂进行了基本性能考核,其次通过开展元件级修理件疲劳性能测试,从中筛选出了3M公司的D型胶粘剂,最后为了充分验证D型胶粘剂对胶接修理起落架梁疲劳寿命的提升效果,根据起落架梁服役载荷特点开展了起落架梁典型实验件疲劳性能测试。结果表明:经过D型胶粘剂胶接修理后的实验件通过了实际服役环境下的考核,修理件的止扩周次和破坏周次分别是未修理件的16倍和4.9倍,疲劳寿命增益效果显著。
To select an adhesive suitable for composite bonded repairs of aircraft primary load-bearing structures,this paper chose an aircraft landing gear beam as the repair target.Initially,four types of epoxy adhesives were preliminarily selected based on the repair scenarios for landing gear beams.Subsequently,these four adhesives underwent basic performance evaluations.Following that,fatigue performance tests at the component level were conducted to further screen the adhesives,from which D-type adhesive,manufactured by 3M,was chosen.Finally,to fully validate the effectiveness of D-type adhesive in enhancing the fatigue life of repaired landing gear beams,a typical test specimen of the landing gear beam was subjected to fatigue performance testing based on the load characteristics of the landing gear beam in service.The experimental results showed that after being repaired with D-type adhesive,the test specimens passed the evaluation under real operational loading conditions.The crack arrest and failure cycles for the repaired specimens were 16 times and 4.9 times those of the unrepaired specimens,respectively,indicating a significant improvement in fatigue life.
[1] 王锋,秦剑波,梁振武,等.飞机铝合金壁板结构广布疲劳多裂纹扩展与剩余强度研究[J].现代制造工程,2022(10):87-95.
[2] 周懿明,崔荣洪,宋雨键,等.基于格栅式薄膜传感器的金属结构裂纹监测[J].西北工业大学学报,2021,39(6):1204-1211.
[3] Daryabor P,Safizadeh M S.Comparison of three thermographic post processing methods for the assessment of repaired aluminum plate with composite patch[J].Infrared Physics & Technology,2016,79:58-67.
[4] 汪云波.某型飞机结构破孔损伤异地修理通用方法[J].航空维修与工程,2024(6):78-80.
[5] Wen S W,Xiao J Y,Wang Y R.Accelerated ageing behaviors of aluminum plate with composite patches under salt fog effect[J].Composites:Part B,2013,44:266-275.
[6] 贺旺,孙运刚,杜永华,等.复合材料双面修理边缘裂纹铝合金厚板的静态和疲劳特性[J].南京理工大学学报,2019,43(4):511-517.
[7] 杨海冬,王帅,王德志,等.环氧胶膜对聚四氟乙烯薄片和铝合金胶接研究[J].中国胶粘剂,2022,31(10):17-22.
[8] Nasreen A,Bangash M K,Shaker K,et al.Effect of surface treatment on the performance of composite-composite and composite-metal adhesive joints[J].Polymer Composites,2022,43(9):6320-6331.
[9] Merah A,Houari A,Madani K,et al.Experimental investigation into the tensile strength post-repair on damaged aluminium 2024-T3 plates using hybrid bonding/riveting[J].Acta Mechanica et Automatica,2024,18(3):514-525.
[10] 梁浩忠,娄星原,冯朝波,等.不同种类环氧树脂对金属基材粘接的研究[J].中国胶粘剂,2024,33(12):51-56.
[11] Baker A A.Repair of cracked or defective metallic aircraft components with advanced fiber composites[J].Composites Structure,1984,2(2):153-160.
[12] Errahmane M A,Benyettou M,Madani K,et al.Numerical and experimental analysis of the performance of the metal patch compared to the composite patch under aging conditions in water immersion[J].International Journal of Adhesion and Adhesives,2025,138:103943.
[13] Shahrezaee B,Latifi M,Mostofi T M.Influence of hygrothermal aging on the lifetime and mechanical properties of GFRP/Al adhesive joints[J].International Journal of Adhesion & Adhesives,2025,136:103880.
[14] Kumar 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.
[15] 徐喻琼,钟紫珊,郑黔松.基于几何优化的复合材料胶接接头强度改进的研究进展[J].材料导报,2024,38(24):256-264.
[16] 王中强,张开富,李原,等.CFRP/Al复合构件胶接界面力学建模与强度分析[J].西北工业大学学报,2010,28(6):858-865.
[17] 赵召,何惊华,张浩然,等.金属/复合材料胶接界面强韧化技术研究进展[J].航空制造技术,2024,67(8):64-75.
[18] Rasane A,Kumar P,Khond M.Determination of an optimum patch configuration in the repair of a center crack in thin aluminum sheet using polymer composite patch[J].Polymer Composites,2025,46(3):23333-23344.
[19] 冯春苗,张欲欣,付博彬.军用倒装焊器件底部填充胶选型及验证方法讨论[J].电子与封装,2020,20(5):050201.
[20] 王紫潇,龙宇,陈全义,等.复材粘接修理金属结构的载荷分布及刚度对修复效果的影响研究[J].工程技术研究,2022,7(2):1-5.
基金资助
安徽省科技重大专项项目(202203a05020039)