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METALLURGICAL EVALUATION AND CONDITION ASSESSMENT OF FSX NOZZLE SEGMENTS IN GAS TURBINES BY METALLOGRAPHIC METHODS

机译:金相法测定燃气轮机中FSX喷嘴段的冶金评价和状态评估

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Gas turbine components such as nozzle segments, buckets, transition pieces and combustion liners experience damages such as creep, fatigue, high temperature oxidation and corrosion. The reliability, availability and efficiency of high temperature gas turbine parts is based on condition assessment and remaining life analysis. These gas turbine components are normally repaired, refurbished after stipulated operating hours. The decision on the extent of repairs is based on various inspection stages. Among various methodologies of condition assessment, metallography followed by microscopic evaluation has gained wide acceptance since it is cost effective, quick and reliable. Extensive in-house efforts have been put forth in this field in the development of improved techniques of metallography for accurate determination of material degradation and condition assessment. Experimental studies on Frame 6, 1~(st) Stage Nozzle Segment (FSX 414 - cobalt based alloy) were conducted to assess the condition of the nozzle segment by using laboratory electropolishing technique for metallographic preparation. Sections taken from the nozzle segment were electropolished and examined in Light Optical Microscope (LOM) and Scanning Electron Microscope (SEM). It is concluded that the improved electropolishing technique is effective in assessing creep-fatigue, thermal fatigue and hot corrosion damage. Based on this the condition of the nozzlesegment is assessed. Typical results of Frame 6, 1st Stage Nozzle Segment are presented and discussed.
机译:燃气涡轮机部件(例如喷嘴段,轮叶,过渡件和燃烧衬套)会遭受蠕变,疲劳,高温氧化和腐蚀等损坏。高温燃气轮机零件的可靠性,可用性和效率基于状态评估和剩余寿命分析。这些燃气轮机部件通常在规定的运行时间后进行维修和翻新。维修范围的决定基于不同的检查阶段。在各种状态评估方法中,金相法和显微评估法因其具有成本效益,快速且可靠的特点而得到了广泛的认可。在该领域中,在内部开发方面已经进行了广泛的努力,以开发用于精确确定材料降解和状态评估的改进的金相技术。通过使用实验室电抛光技术进行金相制备,对第6帧第1阶段喷嘴段(FSX 414-钴基合金)进行了实验研究,以评估喷嘴段的状况。对从喷嘴段截取的切片进行电抛光,并在光学显微镜(LOM)和扫描电子显微镜(SEM)中进行检查。结论是,改进的电抛光技术可有效地评估蠕变疲劳,热疲劳和热腐蚀损伤。基于此,喷嘴的状态 段进行评估。呈现并讨论了第6帧第1阶段喷嘴段的典型结果。

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