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The influence of electron beam welding parameters on heat affected zone and weld metal cracking of nickel-based superalloys.

机译:电子束焊接参数对镍基高温合金热影响区和焊接金属开裂的影响。

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摘要

Nickel-based Superalloys IN 738, Rene 80, and a proprietary single crystal material were studied in this project. These three alloys are commonly used in the hot section of gas turbine engines due to their excellent properties at elevated temperatures. In this study the influence of electron beam welding parameters on the cracking susceptibility of the alloys was investigated. The welding of the samples was performed at Bristol Aerospace located in Winnipeg, Manitoba. Focus coil current and welding speed were varied on samples of varying thicknesses of each alloy to simulate different types of blade repair. The total weld metal and heat affected zone (HAZ) crack lengths along with the weld and HAZ areas were measured using an optical microscope equipped with an image analysis system. The crack length per unit area, termed cracking index, was calculated and used to evaluate the cracking tendency of the alloy with respect to varying welding parameters. Orientation image microscopy was also used to determine if changes in crystal orientation were responsible for the cracking present in the single crystal and directionally solidified alloys. The experimental results showed that (1) The hardness of all three alloys can be reduced significantly by performing a special heat treatment called UMT. (2) IN 738 had a base microstructure of primary and secondary gamma' with intermetallics present. The microstructure of the post heat treated alloy consisted of coarsened primary and secondary gamma' plus the presence of M23C6 carbides. (3) The as-received microstructure of Rene 80 consisted of secondary gamma' along with a variety of carbides, borides and intermetallics. After heat treating the secondary gamma' was coarsened and M6C carbides were present. (4) The single crystal microstructure had very few phases present with only secondary gamma' and MC carbides visible. This is expected as fewer minor alloying elements are present as there is no need for grain boundary strengthening. Heat treating coarsened the gamma' phase. (5) Analysis of the cracking index of each alloy indicates that the welding parameters play a key role in determining the cracking susceptibility of the weld. The effects of focus coil current and welding speed on the cracking susceptibility are discussed. (6) The post weld microstructure of the directionally solidified and single crystal alloys have been analysed and the results tend to agree with the reports of other investigators.
机译:本项目研究了镍基超级合金IN 738,Rene 80和专有的单晶材料。这三种合金由于它们在高温下的优异性能而常用于燃气涡轮发动机的热区。在这项研究中,研究了电子束焊接参数对合金开裂敏感性的影响。样品的焊接在位于曼尼托巴省温尼伯的布里斯托尔航空航天公司进行。在每种合金厚度不同的样品上改变聚焦线圈电流和焊接速度,以模拟不同类型的叶片修复。使用配备有图像分析系统的光学显微镜测量焊缝和热影响区(HAZ)的总裂纹长度以及焊缝和HAZ区域。计算出每单位面积的裂纹长度,称为裂纹指数,并用于评估合金在不同焊接参数下的裂纹倾向。取向图像显微镜还用于确定晶体取向的变化是否导致单晶和定向凝固合金中出现裂纹。实验结果表明:(1)通过执行称为UMT的特殊热处理,可以显着降低所有三种合金的硬度。 (2)IN 738具有主要和次要γ'的基本微观结构,并存在金属间化合物。后热处理合金的微观结构由粗化的一级和二级γ'以及M23C6碳化物的存在组成。 (3)Rene 80的微观组织包括次级γ'以及各种碳化物,硼化物和金属间化合物。在热处理之后,将次级γ′粗化并且存在M 6 C碳化物。 (4)单晶微结构几乎没有相,只有次级γ'和MC碳化物可见。可以预期,因为不需要晶界强化,因此存在的微量合金元素较少。热处理使γ′相变粗。 (5)对每种合金的开裂指数的分析表明,焊接参数在确定焊缝的开裂敏感性中起关键作用。讨论了聚焦线圈电流和焊接速度对裂纹敏感性的影响。 (6)对定向凝固和单晶合金的焊后显微组织进行了分析,结果趋于与其他研究者的报告相吻合。

著录项

  • 作者

    Churchman, Craig.;

  • 作者单位

    University of Manitoba (Canada).;

  • 授予单位 University of Manitoba (Canada).;
  • 学科 Engineering Mechanical.;Engineering Materials Science.;Engineering Metallurgy.
  • 学位 M.Sc.
  • 年度 2009
  • 页码 105 p.
  • 总页数 105
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 机械、仪表工业;冶金工业;工程材料学;
  • 关键词

  • 入库时间 2022-08-17 11:37:40

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