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Assessment of damage tolerance approaches for composite aircraft with focus on barely visible impact damage

机译:评估复合材料飞机的损伤容忍方法,重点是几乎看不见的冲击损伤

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摘要

Industry practice in composite aircraft damage tolerance, as reported in the open literature, is reviewed and examined in view of the current knowledge in the field of damage and failure of composite materials. Particular attention is paid to the challenging regime of damage tolerance when barely visible impact damage (BVID) is of concern. The validity of the compression after impact (CAI) testing as a means of assuring safety against failure from BVID is critically assessed. The role of in-field nondestructive evaluation (NDE) for quantifying the damage severity is considered as an integral part of the damage tolerance assessment. Finally, recommendations are made toward exploring other avenues for improving the current damage tolerance approaches as they apply to the case of BVID in composite structures.
机译:公开文献中报道的复合材料飞机损坏容限的行业实践是根据复合材料损坏和故障领域的最新知识进行审查和检查的。当关注几乎看不见的冲击损伤(BVID)时,应特别注意具有挑战性的损伤承受能力。严格评估冲击后压缩(CAI)测试作为确保BVID失效安全性的一种手段。现场非破坏性评估(NDE)在量化破坏严重性方面的作用被认为是破坏耐受性评估的组成部分。最后,提出了一些建议,以探索其他途径来改进当前的损伤耐受方法,因为它们适用于复合结构中的BVID。

著录项

  • 来源
    《Composite Structures》 |2019年第7期|1-7|共7页
  • 作者

    Talreja Ramesh; Nam Phan;

  • 作者单位

    Texas A&M Univ, Dept Mat Sci & Engn, Dept Aerosp Engn, College Stn, TX 77843 USA;

    Naval Air Syst Command NAVAIR, Struct Div, Patuxent River, MD 20670 USA;

  • 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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