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A novel, one-step, low-VOC, primer for the corrosion protection of aerospace alloys and metals.

机译:一种新颖的,一步法,低VOC的底漆,用于航空航天合金和金属的腐蚀防护。

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摘要

Chromate-based technology used currently in the aerospace industry provides excellent corrosion protection for the aerospace metals and alloys such as AA 2024-T3. However, chromates are toxic and carcinogenic and the Environmental Protection Agency of the United States has identified chromates for replacement. This has resulted in a global research effort to find an effective alternative.; In this dissertation the above problem has been addressed through the development of a novel primer system consisting of silanes and resins (called Superprimer from hereon), which obviates the need for any pretreatment and offers a low-VOC, water-based polymeric coating which can be loaded to high levels for the corrosion protection of the substrate and result in a chromate-equivalent performance.; The initial results of various systems tested are reported. The silanes used for formulation of these preliminary formulations were bis-[triethoxysilylpropyl] tetrasuflide and bis-[triethoxysilylpropyl] ethane, used individually and in combinations of with various ratios. The resins used were an acrylate copolymer and a bis-phenol A-type epoxy. The results of various performance evaluation tests are reported in this chapter.; As a second part of this research, efforts were carried out to optimize the five systems discussed in Chapter 3. A Taguchi method approach was used for this and L9 orthogonal arrays were used to determine the ideal formulation for each of the five systems that were to be optimized. The results of this optimization study are reported in Chapter 4. It was found that all the 5 optimized systems gave improved performance and the bis-[triethoxysilylpropyl] tetrasulfide-based Superprimer performed the best.; The characterization of the bis-[triethoxysilylpropyl] tetrasulfide-based Superprimer coatings for development of models to explain the corrosion protection mechanism, cure chemistry and interfacial adhesion forms the third part of this dissertation. This has been discussed in Chapters 5, 6, 7 and 8. The characterization was conducted using SEM/EDX, FTIR-ATR, NMR and TOFSIMS to understand the structure, cure and solution chemistry and metal-primer interface of the coating system. Chapter 9 discusses the general conclusions, a summary of the proposed model for the mechanism of corrosion protection and the current status of research.
机译:当前在航空航天工业中使用的基于铬酸盐的技术为航空航天金属和合金(例如AA 2024-T3)提供了出色的腐蚀防护。但是,铬酸盐是有毒的,并且具有致癌性,美国环境保护署已经确定了铬酸盐可以替代。这导致了全球研究努力,以寻找有效的替代方案。在本文中,上述问题已通过开发由硅烷和树脂组成的新型底漆体系(在下文中称为Superprimer)解决了,该体系消除了对任何预处理的需求,并提供了低VOC,水基聚合物涂料,该涂料可以负载量高,以保护基材免受腐蚀,并产生相当于铬酸盐的性能。报告了各种测试系统的初步结果。用于配制这些初步制剂的硅烷是双-[三乙氧基甲硅烷基丙基]四硫化物和双-[三乙氧基甲硅烷基丙基]乙烷,分别使用或以各种比例组合使用。所使用的树脂是丙烯酸酯共聚物和双酚A型环氧树脂。本章报告了各种性能评估测试的结果。作为本研究的第二部分,我们努力优化了第3章中讨论的五个系统。为此使用了Taguchi方法,并使用L9正交阵列确定了五个系统中每个系统的理想配方。优化。该优化研究的结果在第4章中进行了报告。结果发现,所有5个优化的系统均具有改进的性能,并且基于双-[三乙氧基甲硅烷基丙基]四硫化物的Superprimer性能最佳。本论文的第三部分是对双[三乙氧基甲硅烷基丙基]四硫化物基超级底漆进行表征,以建立模型来解释其腐蚀防护机理,固化化学和界面附着力。第5、6、7和8章对此进行了讨论。使用SEM / EDX,FTIR-ATR,NMR和TOFSIMS进行了表征,以了解涂层系统的结构,固化和溶液化学以及金属底漆界面。第9章讨论了一般结论,总结了所提出的腐蚀防护机理模型和研究现状。

著录项

  • 作者

    Seth, Anuj.;

  • 作者单位

    University of Cincinnati.;

  • 授予单位 University of Cincinnati.;
  • 学科 Engineering Materials Science.
  • 学位 Ph.D.
  • 年度 2007
  • 页码 544 p.
  • 总页数 544
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 工程材料学;
  • 关键词

  • 入库时间 2022-08-17 11:39:05

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