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Effect of adhesive quantity on failure behavior and mechanical properties of fiber metal laminates based on the aluminum-lithium alloy

机译:胶粘剂用量对铝锂合金纤维金属层压板破坏行为和力学性能的影响

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摘要

The effect of adhesive quantity on the failure behavior and mechanical properties of fiber metal laminates based on the aluminum-lithium alloys (NFMLs) was investigated to optimize the manufacture process and further recognize the interface interaction. The NFMLs with different adhesive quantities (0 g/m(2), 20 g/m(2), 40 g/m(2), 60 g/m(2)) were prepared primarily. Then, the influence of adhesive quantity on the interlaminar, tensile, flexural and fatigue properties of NFMLs was studied respectively. Also, the failure behaviors of NFMLs under different loading conditions were revealed. The results indicated that the adhesive layers significantly enhanced the interlaminar properties of the NFMLs within the investigated quantities. Moreover, the reasonable adhesive quantity also greatly improved the mechanical properties of the laminates, while an excessive amount deteriorated the performance. For the different properties, the peak values appeared under different adhesive quantities. Besides, the changing mechanical properties followed with the variation of failure mode. From the engineering perspective, the adhesive quantity of 40 g/m(2) is optimal to achieve the excellent performance of NFMLs. (C) 2016 Elsevier Ltd. All rights reserved.
机译:研究了粘合剂数量对基于铝锂合金(NFML)的纤维金属层压板的破坏行为和力学性能的影响,以优化制造工艺并进一步识别界面相互作用。最初准备了具有不同粘合剂量(0 g / m(2),20 g / m(2),40 g / m(2),60 g / m(2))的NFML。然后,分别研究了粘合剂数量对NFMLs的层间,拉伸,弯曲和疲劳性能的影响。此外,揭示了NFML在不同载荷条件下的失效行为。结果表明,粘合剂层在所研究的量内显着增强了NFML的层间性能。而且,合理的粘合量还极大地改善了层压板的机械性能,而过量的粘合性能则降低了性能。对于不同的性质,峰值出现在不同的粘合剂量下。此外,随着破坏模式的变化,机械性能的变化也随之变化。从工程角度来看,40 g / m(2)的粘合量是实现NFML优异性能的最佳选择。 (C)2016 Elsevier Ltd.保留所有权利。

著录项

  • 来源
    《Composite Structures 》 |2016年第9期| 687-692| 共6页
  • 作者单位

    Nanjing Univ Aeronaut & Astronaut, Coll Mat Sci & Technol, Nanjing 211100, Jiangsu, Peoples R China|Jiangsu Key Lab Adv Struct Mat & Applicat Technol, Nanjing 211100, Jiangsu, Peoples R China;

    Nanjing Univ Aeronaut & Astronaut, Coll Mat Sci & Technol, Nanjing 211100, Jiangsu, Peoples R China;

    Nanjing Univ Aeronaut & Astronaut, Coll Mat Sci & Technol, Nanjing 211100, Jiangsu, Peoples R China;

    Shanghai Aircraft Mfg Co Ltd, Shanghai 200436, Peoples R China;

    Shanghai Aircraft Mfg Co Ltd, Shanghai 200436, Peoples R China;

    Nanjing Univ Aeronaut & Astronaut, Coll Mat Sci & Technol, Nanjing 211100, Jiangsu, Peoples R China|Jiangsu Key Lab Adv Struct Mat & Applicat Technol, Nanjing 211100, Jiangsu, Peoples R China;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    Fiber metal laminates; Aluminum-lithium alloy; Adhesive quantity; Failure behavior; Mechanical properties;

    机译:纤维金属层压板;铝锂合金;粘合量;破坏行为;机械性能;

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