HOT CRACKING OF NICKEL-BASED SUPERALLOY TURBINE BLADE

Authors

  • Łukasz Rakoczy AGH University of Science and Technology, Faculty of Metals Engineering and Industrial Computer Science, Krakow, Poland
  • Lechosław Tuz AGH University of Science and Technology, Faculty of Metals Engineering and Industrial Computer Science, Krakow, Poland
  • Krzysztof Pańcikiewicz AGH University of Science and Technology, Faculty of Metals Engineering and Industrial Computer Science, Krakow, Poland

DOI:

https://doi.org/10.7494/mafe.2015.41.4.181

Keywords:

superalloys, nickel alloys, liquation, hot cracking, turbine blades

Abstract

The aim of this study was to present the hot cracking behavior of a blade originating from a turbine blade segment. The crack was induced by a gas tungsten arc welding process, and the research material was a MAR-M247 nickel based superalloy. This alloy is considered to be difficult to weld because of its high tendency to crack. Light microscopy and scanning electron microscopy show the occurrence of cracking in the melted zone, heat-affected zone, and base alloy. A scanning electron microscopy investigation revealed that cracks are propagated by stresses and liquation of the low temperature constituent.

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References

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Published

2017-11-08

How to Cite

Rakoczy, Łukasz, Tuz, L., & Pańcikiewicz, K. (2017). HOT CRACKING OF NICKEL-BASED SUPERALLOY TURBINE BLADE. Metallurgy and Foundry Engineering, 41(4), 181. https://doi.org/10.7494/mafe.2015.41.4.181

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