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Advanced composite repair for solid monolithic carbon structures.

机译:用于固体整体式碳结构的高级复合材料修复。

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摘要

Repairability is an essential element in the effective use of composite components. Composite structures offer significant benefits over metallic components in terms of lighter weight, fatigue and corrosion resistance. Composite designs are usually tailored to maximize performance by defining application dependent materials, ply orientation, stiffening concepts, and attachment mechanisms. High performance designs are often less supportable due to increased strain levels, fewer redundant load paths, and a mix of highly tailored materials and geometries.;This thesis provides guidelines and repair procedures for design of prepreg repair patch. It also emphasizes on step sanding (per ply) of the repair edges to achieve an optimum load transfer. Advantages of pre-cured patch over a co-cured patch for large size damage are also shown. These techniques are not new, however it is not customary to see a repair to advanced composite structure that has utilized the combination of these methods.
机译:可修复性是有效使用复合材料组件的基本要素。复合材料结构在重量轻,抗疲劳和抗腐蚀方面比金属组件具有明显优势。通常,通过定义依赖于应用的材料,层定向,加强概念和附着机制,来定制复合设计以最大化性能。高性能设计通常由于应变水平提高,冗余负载路径减少以及高度定制的材料和几何形状的混合而难以获得支持。;本文提供了预浸料修补片的设计指南和修补程序。它还强调了对修整边缘进行逐步打磨(每层)以实现最佳的负载传递。还显示了预固化贴片相对于共固化贴片的大尺寸损坏的优势。这些技术不是新技术,但是习惯于利用这些方法的组合来修复高级复合材料结构并不常见。

著录项

  • 作者

    Rashi-Dian, David.;

  • 作者单位

    California State University, Long Beach.;

  • 授予单位 California State University, Long Beach.;
  • 学科 Engineering Aerospace.
  • 学位 M.S.
  • 年度 1997
  • 页码 51 p.
  • 总页数 51
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 航空、航天技术的研究与探索;
  • 关键词

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