涡轮垫片失效

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引用次数: 0

摘要

涡轮垫片由AMS 5661合金(incoly 901;成分:Fe-43Ni-13Cr-6Mo-2.5Ti)因径向轮辋前侧出现裂纹而退出使用。裂纹沿间隔条沿轴向延伸16mm的距离;在径向上,它延伸到腹板部分6.4毫米的深度。分析(目视检查,5000倍和10000倍的TEM断口,化学分析和9倍金相检查)支持了这样的结论:垫片前缘的开裂发生在疲劳中,始于前缘表面,并向边缘和腹板区域发展。由于没有明显的冶金原因导致开裂,问题被分配给工程。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Failure of a Turbine Spacer
A turbine spacer made of AMS 5661 alloy (Incoloy 901; composition: Fe-43Ni-13Cr-6Mo-2.5Ti) was removed from service because of a crack in the forward side of the radial rim. The crack extended axially for a distance of 16 mm across the spacer rim; radially, it extended to a depth of 6.4 mm into the web section. Analysis (visual inspection, 5000 and 10,000x TEM fractographs, chemical analysis, and 9x metallographic examination) supported the conclusions that cracking on the forward rim of the spacer occurred in fatigue that initiated on the forward rim face and that progressed into the rim and web areas. Because there was no apparent metallurgical cause for the cracking, the problem was assigned to engineering.
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