复合材料修复含破孔损伤2A12铝合金板的拉伸性能研究
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1南京航空航天大学材料科学与技术学院,南京 210000;2中国直升机设计研究所,景德镇 333001

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TB332

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企事业委托横向课题(1006-KFB23390)


Study on Tensile Properties of 2A12 Aluminum Alloy Plate With Composites for Repairing Damage Containing Circular Holes
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1School of Materials Science and Technology,Nanjing University of Aeronautics and Astronautics,Nanjing 210000;2China Helicopter Design and Research Institute,Jingdezheng 333001

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    摘要:

    采用复合材料贴补修复圆形穿透损伤的2A12铝合金板材,对比了完好、圆形穿透损伤、单面修复、双面修复4种修复形式试验件的拉伸强度,并基于复合材料贴补的单面修复工艺,研究了3种不同孔径的圆形穿透损伤胶接修复试验件的拉伸强度;同时,考虑到受损铝合金本征弹性强度和胶接强度对修复件强度恢复率的影响,提出了损伤比例和应有胶接面积S之间的关系公式。研究结果表明,复合材料单面贴补和双面贴补的修复效果均满足修理后结构强度的验收标准,其强度恢复率分别达到99.68%和109.43%;3种损伤孔径胶接修复件的拉伸强度随孔径变化较小;断裂均发生在金属母材通孔所在的横截面,复合材料补片形状完整,破坏模式主要为母板拉伸破坏和胶层剪切破坏。

    Abstract:

    This study used composite patches to repair circular penetration damage on 2A12 metal sheets,and compared the tensile strength of four repair forms of test specimens:intact,circular penetration damage,single-sided repair and double-sided repair.Based on the single-sided repair process of composite patches,the tensile strength of three different aperture circular penetration damage adhesive repair test specimens was studied.Meanwhile,considering the influence of the intrinsic elastic strength and bonding strength of damaged aluminum alloys on the strength recovery rate of repaired parts,a correlation formula between the damage ratio and the required bonding area was proposed.The research results indicate that the repair effects of single-sided and double-sided patches on composite materials meet the acceptance criteria for the strength of repaired structures,with strength recovery rates reaching 99.68% and 109.43%,respectively.The tensile strength of three types of damaged pore size adhesive repair parts varies less with pore size.The fractures all occur at the cross-section where the metal base metal through-hole is located,and the composite patch shape is intact.The main failure modes are tensile failure of the mother plate and shear failure of the adhesive layer.

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肖丽,关肖虎,朱洪伟,高奇玉,占小红.复合材料修复含破孔损伤2A12铝合金板的拉伸性能研究[J].宇航材料工艺,2026,56(2):48-55.

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  • 收稿日期:2024-05-11
  • 最后修改日期:2026-03-26
  • 录用日期:2024-08-14
  • 在线发布日期: 2026-05-07
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