首页> 外文会议>Contribution of metallography to production problem solutions II >Combining 3D Scanning with Standard Microscopy Methods for Assessment of Pitting Corrosion in Turbine Blades
【24h】

Combining 3D Scanning with Standard Microscopy Methods for Assessment of Pitting Corrosion in Turbine Blades

机译:将3D扫描与标准显微镜方法相结合以评估涡轮叶片的点蚀

获取原文
获取原文并翻译 | 示例

摘要

Pitting corrosion is a known process in metals. Pitting, observed in turbine blades, is caused by corrosion mechanisms in operation environment that may contain aggressive chemical compounds. Environment, material composition and operating conditions determine the corrosion process causing a cavity formation and their critical growth. Crack initiation can be a following mechanism. Thus the critical cavity size is the important parameter and its precise estimation can avoid a turbine blade failure. Cavity shape as well as corrosion products inside cavities should be taken into account. 3D scanning technique performed during turbine shutdowns is shown to be a suitable method for measurement of critical cavity size. In this study, the accuracy of 3D technique was confirmed by standard sample preparation methods followed by microscopy focused on corrosion products observation. Cross-sectioning of blades was performed close to the cavities, sections were grinded to show the maximum cavity dimensions and finally polished. Cavity size was measured in few steps by Light Optical Microscopy during grinding to find the maximum dimensions and compare to 3D measurements. Local corrosion in cavities was evaluated by Scanning Electron Microscopy using Backscattered Electrons and Energy Dispersive X-ray Spectroscopy. Non-uniform Fe, Cr, Si rich oxides with dimensions from tens up to hundreds of micrometres were analysed in cavities. No significant effect on oxide removing was observed after using sandblasting technology except possible effect in larger pits. Cracks and pores were detected close to the vicinity of trailing edge of blade.
机译:点蚀是金属中已知的过程。在涡轮机叶片中观察到的点蚀是由运行环境中的腐蚀机制引起的,该腐蚀机制可能包含腐蚀性化合物。环境,材料成分和操作条件决定了导致空腔形成及其临界生长的腐蚀过程。裂纹萌生可以是以下机制。因此,临界腔尺寸是重要的参数,其精确估算可以避免涡轮机叶片故障。应考虑腔体形状以及腔体内的腐蚀产物。涡轮机停机期间执行的3D扫描技术显示为一种用于测量关键腔尺寸的合适方法。在这项研究中,3D技术的准确性通过标准的样品制备方法以及随后针对腐蚀产物观察的显微镜进行了确认。叶片的剖切是在靠近型腔的地方进行的,将切片磨碎以显示最大型腔尺寸,最后进行抛光。在研磨过程中,通过光学显微镜分几步测量型腔尺寸,以找到最大尺寸并将其与3D测量值进行比较。通过使用反向散射电子和能量色散X射线光谱的扫描电子显微镜评估腔体中的局部腐蚀。在型腔中分析了尺寸从数十微米到数百微米不均匀的富含Fe,Cr,Si的氧化物。使用喷砂技术后,除大型矿坑中可能产生的影响外,未观察到对氧化物去除的显着影响。在叶片后缘附近检测到裂缝和气孔。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号