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首页> 外文期刊>Journal of Aircraft >Damage of Carbon/Epoxy Composite Plates Subjected to Mechanical Impact and Simulated Lightning
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Damage of Carbon/Epoxy Composite Plates Subjected to Mechanical Impact and Simulated Lightning

机译:碳/环氧复合材料板受到机械冲击和模拟雷击的损坏

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摘要

Damage is inflicted on carbon-flber/epoxy composite plates using both simulated lightning strike and mechanical impact in the effort to understand the relative effect of the two damage mechanisms. A methodology is proposed to characterize the damage resistance and tolerance of unconfigured composite plates subjected to lightning strike in a fashion that is consistent with the extensive work previously done on low-velocity impact Using current and voltage diagnostics, it is possible to extrapolate the amount of electromechanical energy absorbed by the plate during the strike and compare it to that absorbed during a mechanical impact. Damage resistance is characterized by means of ultrasonic C-scans and microscopy, whereas residual strength is measured by means of compression after impact testing. Results show that the energy dissipated in a specimen during the lightning strike is much greater than the strain energy introduced by mechanical impact, and hence a comparison based on energy is not recommended. However, based on the relative threat levels associated with the impact and the lightning strike events, the comparison yields insightful observations on both damage state and residual performance. In general, for the configurations tested, lightning strike damage seems to be less detrimental than the mechanical impact in terms of both damage area and residual strength.
机译:为了理解这两种损坏机制的相对作用,使用模拟的雷击和机械冲击对碳纤维/环氧树脂复合材料板造成了损坏。提出了一种方法来表征未配置的复合材料板的抗冲击性和耐受性,该复合材料板以与先前在低速冲击方面进行的大量工作一致的方式进行表征。使用电流和电压诊断程序,可以推断出板在撞击过程中吸收的机电能量,并将其与机械冲击过程中吸收的能量进行比较。耐损伤性是通过超声波C扫描和显微镜检查来表征的,而残余强度是通过冲击试验后的压缩来测量的。结果表明,雷击期间耗散在样本中的能量远大于机械冲击所引入的应变能,因此不建议基于能量进行比较。但是,基于与冲击和雷击事件相关的相对威胁级别,该比较可对破坏状态和剩余性能产生深刻的观察。通常,对于所测试的配置,就损坏面积和残余强度而言,雷击损坏似乎比机械冲击的危害要小。

著录项

  • 来源
    《Journal of Aircraft》 |2010年第3期|P.999-1012|共14页
  • 作者单位

    University of Washington, Seattle, Washington 98195-2400 Automobili Lamborghini Advanced Composite Structures Laboratory, Department of Aeronautics & Astronautics, Box 352400, Guggenheim Hall;

    rnUniversity of Washington, Seattle, Washington 98195-2400 Department of Aeronautics & Astronautics Japan Ministry of Defense, Tokyo;

  • 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

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