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首页> 外文期刊>International journal of impact engineering >Response of aluminium honeycomb sandwich panels subjected to foam projectile impact - An experimental study
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Response of aluminium honeycomb sandwich panels subjected to foam projectile impact - An experimental study

机译:铝蜂窝夹芯板在泡沫弹丸冲击下的响应-实验研究

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摘要

Aluminium honeycomb sandwich panels have potential applications as a protective mechanism that can be used to prevent failure of an important structure subjected to impact loading. Therefore it is important to fully understand the resistance of the sandwich panels subjected to impact loading conditions. The main objective of this work was to study the resistance of sandwich panels with different aluminium honeycomb cores, air sandwich panels (no core between the two face sheets) and monolithic plates of equivalent mass subjected to impact from foam projectiles. The deformation and the elastic spring-back of the honeycomb sandwich panels and the monolithic plates have been compared and discussed. The resistance of the panels and plates has been quantified by their back-face deflection with respect to the projectile impulse. Five different types of aluminium honeycombs have been used as the core material. The front-face sheet and the back-face sheet of the honeycomb sandwich panels are made of aluminium plate with 1 mm thickness. Cylindrical ALPORAS aluminium foams with a relative density between 9% and 11% are employed as the metal foam projectiles. They are fired at several hundred metres per second towards the centre of the panels and plates using a gas gun. The deflection histories of the back-face have been measured using a laser displacement sensor. From the deflection histories, the maximum deflection and the final deflection of the back-face can be distinguished. Deformation modes and failure modes of the individual component have been observed and classified into several categories. Moreover, the deflections of the honeycomb sandwich panels have been compared with deflections from air sandwich panels. It is found that the honeycomb sandwich panels outperform both the air sandwich panels and the monolithic plates within an impulse range of 2.25 kNsm~(-2) ~ 4.70 kNsm~(-2). Outside this operational range, the advantages associated with employing the honeycomb sandwich panels as a protective structure upon impact of foam projectiles diminishes.
机译:铝蜂窝夹芯板作为保护机制具有潜在的应用前景,可以用来防止重要结构在受到冲击载荷的作用下失效。因此,重要的是要充分了解夹心板在冲击载荷条件下的抵抗力。这项工作的主要目的是研究具有不同铝蜂窝芯的夹芯板,空气夹芯板(两个面板之间没有芯)和等效质量的整体板在泡沫弹丸的作用下的抗力。对蜂窝夹芯板和整体板的变形和弹性回弹进行了比较和讨论。面板和平板的阻力已通过其相对于弹丸脉冲的背面挠度进行了量化。五种不同类型的铝蜂窝已用作核心材料。蜂窝状夹芯板的正面片和背面片由厚度为1mm的铝板制成。相对密度在9%和11%之间的圆柱形ALPORAS铝泡沫被用作金属泡沫弹丸。使用气枪将它们以每秒几百米的速度朝着板和板的中心发射。已经使用激光位移传感器测量了背面的偏转历史。根据挠曲历史,可以区分背面的最大挠度和最终挠度。已经观察到单个组件的变形模式和破坏模式,并将其分为几类。此外,已将蜂窝夹芯板的挠度与空气夹芯板的挠度进行了比较。结果表明,在2.25 kNsm〜(-2)〜4.70 kNsm〜(-2)的脉冲范围内,蜂窝夹芯板的性能优于空气夹芯板和整体板。在此操作范围之外,在泡沫弹丸撞击时采用蜂窝状夹层板作为保护结构的相关优势将减弱。

著录项

  • 来源
    《International journal of impact engineering》 |2015年第1期|100-109|共10页
  • 作者单位

    Defence Materials Technology Centre, Faculty of Science, Engineering and Technology, Swinburne University of Technology Hawthorn, VIC, 3122, Australia, Faculty of Mechanical Engineering, Universiti Teknologi MARA, Shah Alam, 40450, Malaysia;

    Defence Materials Technology Centre, Faculty of Science, Engineering and Technology, Swinburne University of Technology Hawthorn, VIC, 3122, Australia;

    School of Mechanical and Aerospace Engineering, Nanyang Technological University, 639798, Singapore;

    Defence Materials Technology Centre, School of Mechanical and Mining Engineering, The University of Queensland, St Lucia, QLD, 4072, Australia;

  • 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

    Metal foam projectile; Aluminium honeycomb core; Sandwich panels; Monolithic plates; Impact;

    机译:金属泡沫弹;铝蜂窝芯;夹心板;整体板;影响力;

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