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Evaluation of Aerogel as a Material Additive for the Creation of Synthetic Defects in Carbon Fiber Reinforced Plastics

机译:评估气凝胶作为在碳纤维增强塑料中产生合成缺陷的材料添加剂

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摘要

Damage within CFRP composites (commonly used in the aerospace industry) is often difficult to locate and identify, often occurring beneath the surface of the material. Many methods are used in an attempt to isolate these unseen defects, from thermography to a wide array of ultrasonic techniques. Real damage can be used to train personnel and calibrate inspection equipment, however synthetic damage is favorable for the same uses as it can be manufactured at will to any specification desired. Current methods are capable of creating foreign body defects, impact damage, and delaminations, however these methods can require expensive equipment and/or a great amount of time to manufacture. Aerogel was investigated to determine if the material could be used to simulate several types of damage common to CFRP. Samples were created by mixing Aerogel and Epoxy Resin and placing it within composite laminate layups. These samples were used to determine the material characteristics of Aerogel in relation to NDI and the response of the material under UT and Thermographic inspection. The Aerogel/epoxy mixture was optimized to achieve best ultrasonic response which could be a replacement of delamination. It was found that Aerogel was not only ultrasonically visible within the composite panel samples but had a pronounced signature compared to pure epoxy. By altering the amount of Aerogel used, the shape and size of the artificial defects could be controlled. Comprehensive scans of the samples revealed that Foreign Body Inserts (FBI) and delaminations could be matched almost exactly in UT signature and physical appearance, therefor the Aerogel method could be used in place of the current methods. Though in terms of time and cost the original method was better for creating FBIs, substantial savings could be attained with the Aerogel methods when creating synthetic delaminations.
机译:CFRP复合材料(通常在航空航天工业中使用)内的损坏通常难以定位和识别,通常发生在材料表面之下。从热成像技术到各种各样的超声技术,许多方法都试图隔离这些看不见的缺陷。实际损坏可用于培训人员和校准检查设备,但是综合损坏对于相同用途是有利的,因为可以按任意期望的规格随意制造。当前的方法能够产生异物缺陷,冲击损伤和分层,但是这些方法可能需要昂贵的设备和/或大量的制造时间。对气凝胶进行了研究,以确定该材料是否可用于模拟CFRP常见的几种损坏类型。通过将气凝胶和环氧树脂混合并将其放置在复合层压板中来创建样品。这些样品用于确定气凝胶相对于NDI的材料特性以及在UT和热成像检查下材料的响应。对气凝胶/环氧树脂混合物进行了优化,以实现最佳的超声响应,这可以代替分层。已发现气凝胶不仅在复合板样品中超声可见,而且与纯环氧树脂相比具有明显的特征。通过改变气凝胶的使用量,可以控制人造缺陷的形状和大小。样品的全面扫描显示,异物插入物(FBI)和分层几乎可以在UT标记和物理外观上完全匹配,因此可以使用气凝胶法代替​​现有方法。尽管就时间和成本而言,原始方法更适合于创建FBI,但在创建合成分层时,使用气凝胶方法可以节省大量资金。

著录项

  • 作者

    Benedict, Zach Glenn.;

  • 作者单位

    Iowa State University.;

  • 授予单位 Iowa State University.;
  • 学科 Aerospace engineering.
  • 学位 M.S.
  • 年度 2017
  • 页码 59 p.
  • 总页数 59
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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