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Hot Air Erosion Studies of Yttria-Stabilized Zirconia Thermal Barrier Coated Niobium Alloy

机译:氧化钇稳定的氧化锆热障涂层铌合金的热风蚀研究

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摘要

Hot air erosion studies were carried out on niobium (Nb) alloy, C-103 coated with yttria stabilized zirconia (YSZ) with a prior bond coat of NiCrAlY alloy by plasma-spraying method. Erosion behavior of coated alloys is compared with that of bare alloy. The test specimens were subjected to hot-air at a temperature of ~600 ℃ with a supersonic flow of Mach 2 using a Scramjet testing facility. Combustion of a mixture of compressed air and hydrogen was used as a heat source in the erosion studies. It was observed that the YSZ coated alloys with a bond coat showed lower back wall temperature as compared to the uncoated alloy, which is attributed to the lower thermal conductivity of the coating material in comparison to the Nb alloy. The erosion testing is accompanied with a negligible weight loss in bare alloy specimen; while a significant weight loss is observed in coated alloys. The numerical transient thermal analysis, carried out using ANSYS software, was employed to measure the temperature variations on the specimen surfaces with respect to time. The back wall temperature obtained from experiments on various specimens are found to be in excellent agreement with the computationally predicted temperature profiles. Computational simulations further suggests that the temperature gradients of ~20 ℃, 150 ℃ and 265 ℃ across the front and the back wall surface are found for bare alloy and 300 μm and 600 μm YSZ coated alloys, respectively with a progressive decrease in temperature from the front to back wall surface. The simulations furthermore reveal that the Von Mises stresses around most regions of the Nb alloy, bond coat and YSZ coated alloys were below their respective yield stresses. However, high stresses are observed at the interfaces of top and bond coats, which caused de-bonding of the YSZ top coat from the bond coat. The back wall temperatures of ~578 ℃, ~483 ℃ and ~448 ℃ were experimentally obtained for bare alloy and 300 μm and 600 μm YSZ coated alloys. X-ray diffraction studies suggest that YSZ has undergone a marginal phase-transformation from tetragonal to cubic phase due to hot-air erosion. More number of micro-cracks is observed in thicker YSZ coated alloys as a result of hot-air erosion as revealed by scanning electron microscopy.
机译:通过等离子喷涂方法对先涂有NiCrAlY合金的铌涂层的铌(Nb)合金C-103涂有氧化钇稳定的氧化锆(YSZ)进行了热风侵蚀研究。比较了涂层合金和裸合金的腐蚀行为。使用Scramjet测试设备,以2马赫的超音速气流将测试样品置于约600℃的温度下的热风中。在腐蚀研究中,压缩空气和氢气的混合物的燃烧被用作热源。观察到,与未涂覆的合金相比,具有粘结涂层的YSZ涂覆的合金显示出较低的后壁温度,这归因于与Nb合金相比,涂层材料的热导率较低。腐蚀测试伴随着裸合金试样的重量损失可忽略不计;而在涂层合金中观察到明显的重量损失。使用ANSYS软件进行的数值瞬态热分析用于测量样品表面相对于时间的温度变化。发现从各种样品上的实验获得的后壁温度与计算得出的温度曲线非常吻合。计算模拟进一步表明,裸合金和300μm和600μmYSZ涂层合金在前壁和后壁表面的温度梯度分别为〜20℃,150℃和265℃,且温度梯度逐渐降低。前后壁面。模拟还进一步表明,Nb合金,结合层和YSZ涂层合金的大多数区域周围的冯·米塞斯应力低于其各自的屈服应力。然而,在顶涂层和粘结涂层的界面处观察到高应力,这导致YSZ顶涂层从粘结涂层剥离。对于裸合金以及300μm和600μmYSZ涂层合金,通过实验获得的后壁温度分别为〜578℃,〜483℃和〜448℃。 X射线衍射研究表明,由于热风侵蚀,YSZ已经历了从四方相到立方相的边际相变。扫描电子显微镜显示,由于热风腐蚀,在较厚的YSZ涂层合金中观察到更多的微裂纹。

著录项

  • 来源
    《Materials Focus》 |2015年第6期|421-432|共12页
  • 作者单位

    Defence Research and Development Laboratory, Kanchanbagh, Hyderabad 500058, Telangana, India,Department of Materials Engineering, Defence Institute of Advanced Technology (Deemed University), Girinagar, Pune 411025, Maharashtra, India;

    Department of Materials Engineering, Defence Institute of Advanced Technology (Deemed University), Girinagar, Pune 411025, Maharashtra, India;

    Defence Research and Development Laboratory, Kanchanbagh, Hyderabad 500058, Telangana, India;

    Department of Materials Engineering, Defence Institute of Advanced Technology (Deemed University), Girinagar, Pune 411025, Maharashtra, India;

    Defence Metallurgical Research Laboratory, Kanchanbagh, Hyderabad 500058, Telangana, India;

  • 收录信息
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    Hot Air Erosion; Yttria Stabilized Zirconia; Niobium Alloy; Supersonic and Hypersonic Velocities;

    机译:热风蚀氧化钇稳定的氧化锆;铌合金超音速和高音速;

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