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

机译:复合飞机的损伤耐受方法评估,重点在几乎可见的影响损伤

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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:鉴于复合材料损坏和失效的目前的知识,在开放文献中报告的复合飞机损坏耐受性的行业实践是审查和检查的。特别是当几乎可见的影响损伤(BVID)有所关注时,对损害耐受性的具有挑战性的政权。受到影响的影响(CAI)测试后的压缩的有效性,作为确保来自BVID的失败的安全性的手段是批判性评估的。用于量化伤害严重程度的现场非破坏性评估(NDE)的作用被认为是损害耐受性评估的一个组成部分。最后,建议探索其他途径,以改善当前损坏的耐受方法,因为它们适用于复合结构中的BVID的情况。

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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