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Experimental investigation of GF/epoxy laminates with different SMAs positions subjected to low-velocity impact

机译:低速冲击下具有不同SMAs位置的GF /环氧层压板的实验研究

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摘要

In this paper, the impact response of unidirectional cross-ply GF/epoxy laminates with different shape memory alloys (SMAs) positions was investigated. According to vacuum assisted resin injection (VARI) process, we manufactured the laminates without SMAs, the laminates with one layer of SMAs were inserted in 1/8 thickness, in 1/2 thickness, in 14/16 thickness, and in 15/16 thickness of specimen, respectively, the laminates with two layers of SMAs were inserted in the 15/16 and 14/16 thickness, in 15/16 and 1/2 thickness, in 15/16 and 1/8 thickness, in 14/16 and 1/2 thickness, in 14/16 and 1/8 thickness, and in 1/2 and 1/8 thickness of specimen, respectively. The low-velocity impact experiment was performed by Dynatup 9250HV Drop Weight Impact Testing Machine under the impact energy of 28 J to analyze the impact response, and the impact parameters such as contact force (F), displacement (D) and energy (E) of the laminates were obtained. To further observe and analyze the impact damage morphology, we also adopted visual inspection and scanning electron microscope (SEM) technology. The experimental results showed that impact performance of laminates improved by embedding SMAs. By contrast, the impact performance of the laminates with two layers of SMAs was optimum. (C) 2017 Elsevier Ltd. All rights reserved.
机译:本文研究了具有不同形状记忆合金(SMAs)位置的单向交叉GF /环氧树脂层压板的冲击响应。根据真空辅助树脂注射(VARI)工艺,我们制造了不带SMA的层压板,将具有SMA一层的层压板以1/8厚度,1/2厚度,14/16厚度和15/16的厚度插入分别将厚度为2的SMA层压板插入15/16和14/16厚度,15/16和1/2厚度,15/16和1/8厚度,14/16和1/2厚度,分别为14/16和1/8厚度,以及1/2和1/8厚度的样品。 Dynatup 9250HV落锤冲击试验机在28 J的冲击能量下进行了低速冲击实验,以分析冲击响应以及冲击参数,例如接触力(F),位移(D)和能量(E)获得了层压板中的一部分。为了进一步观察和分析冲击损伤的形态,我们还采用了视觉检查和扫描电子显微镜(SEM)技术。实验结果表明,通过嵌入SMA可以提高层压材料的冲击性能。相反,具有两层SMA的层压板的冲击性能最佳。 (C)2017 Elsevier Ltd.保留所有权利。

著录项

  • 来源
    《Composite Structures》 |2017年第7期|170-184|共15页
  • 作者单位

    Harbin Engn Univ, Coll Aerosp & Civil Engn, Harbin 150001, Peoples R China;

    Harbin Engn Univ, Coll Aerosp & Civil Engn, Harbin 150001, Peoples R China;

    East China Univ Sci & Technol, Sch Mech & Power Engn, Shanghai 200237, Peoples R China;

    Harbin Engn Univ, Coll Aerosp & Civil Engn, Harbin 150001, 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

    Unidirectional cross-ply GE/epoxy laminates; SMAs positions; Low-velocity impact; Energy;

    机译:单向交联GE /环氧树脂层压板;SMAs位置;低速冲击;能量;

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