Skip to main content
Log in

Experimental studies of erosion and corrosion interaction in an axial compressor first stage rotating blade material

  • Published:
Applied Physics A Aims and scope Submit manuscript

Abstract

A first stage compressor blade of a gas turbine failed after a long period of operating onshore. Initial investigations showed that there were some pits and micro-cracks on the pressure side of the blade created by erosion and corrosion mechanisms. In this research, experimental examinations were conducted on erosion, corrosion, and interaction between erosion and corrosion of the samples extracted from the compressor blade under simulated blade operation conditions such as high-velocity erosion and corrosive medium. The results reveal that erosion and corrosion pits can severely appear on the blade in real operation conditions, leading to a large reduction in crack initiation time, which has the longest time period in the fatigue life.

This is a preview of subscription content, log in via an institution to check access.

Access this article

Price excludes VAT (USA)
Tax calculation will be finalised during checkout.

Instant access to the full article PDF.

Fig. 1
Fig. 2
Fig. 3
Fig. 4
Fig. 5
Fig. 6
Fig. 7
Fig. 8
Fig. 9
Fig. 10
Fig. 11
Fig. 12
Fig. 13
Fig. 14
Fig. 15

Similar content being viewed by others

References

  1. E. Poursaeidi, A. Babaei, M.R.M. Arhani, M. Arablu, Eng. Fail. Anal. 25, 304 (2012)

    Article  Google Scholar 

  2. R.R. de Swardt, A.M. Venter, M.W. van der Watt, Appl. Phys. A 74, s1412 (2002)

    Article  Google Scholar 

  3. E. Poursaeidi, A. Babaei, F. Behrouzshad, M.R.M. Arhani, Eng. Fail. Anal. 28, 25 (2013)

    Article  Google Scholar 

  4. E. Silveira, G. Atxaga, A.M. Irisarri, Eng. Fail. Anal. 15, 666 (2008)

    Article  Google Scholar 

  5. Y. Fu, J. Xiong, R.A. Shenoi, Proc. Inst. Mech. Eng. Part C J. Mech. Eng. Sci. 231, 207 (2017)

    Article  Google Scholar 

  6. E.K. Armstrong, R.S. Crowcroft, T.M. Hunt, In Proceedings of the Institution of Mechanical Engineers Conference Proceedings. (SAGE Publications: London, 1965), pp. 61–70

  7. O. Schalm, A. Crabb�, P. Storme, R. Wiesinger, A. Gambirasi, E. Grieten, P. Tack, S. Bauters, C. Kleber, M. Favaro, D. Schryvers, L. Vincze, H. Terryn, A. Patelli, Appl. Phys. A 122, 903 (2016)

    Article  ADS  Google Scholar 

  8. X. Zhang, W. Li, F. Liou, Int. J. Adv. Manuf. Technol. 95, 2393 (2018)

    Article  Google Scholar 

  9. E. Poursaeidi, H. Bakhtiari, Eng. Fail. Anal. 45, 314 (2014)

    Article  Google Scholar 

  10. O. Pedram, E. Poursaeidi, J. Fail. Anal. Prev. 18, 423 (2018)

    Article  Google Scholar 

  11. P. Piccardo, M. Mödlinger, G. Ghiara, S. Campodonico, V. Bongiorno, Appl. Phys. A 113, 1039 (2013)

    Article  ADS  Google Scholar 

  12. E. Poursaeidi, M. Arablu, Humidity effects on corrosion-assisted fatigue fracture of heavy-duty gas turbine compressor blades. J. Propuls. Power 29(5), 1009–1016 (2013)

    Article  Google Scholar 

  13. R. Kurz, K. Brun, In 36th Turbomach. Symposium, Houston, TX, pp. 10–13 (2007)

  14. A. Suman, M. Morini, R. Kurz, N. Aldi, K. Brun, M. Pinelli, P.R. Spina, J. Eng. Gas Turbines Power 139, 12604 (2017)

    Article  Google Scholar 

  15. W. Tabakoff, Wear 119, 51 (1987)

    Article  Google Scholar 

  16. D. Linden, In Proceedings of 40th Turbomach. Symposium, (Texas A&M University. Turbomachinery Laboratories, 2011)

  17. A. Evstifeev, N. Kazarinov, Y. Petrov, L. Witek, A. Bednarz, Eng. Fail. Anal. 87, 15 (2018)

    Article  Google Scholar 

  18. K. Becker, A. Rukwied, D. Allen, B. Knosp, H. Saisse, P. Brøndsted, M. Bridge, M. Lyons, Mater. Des. 14, 175 (1993)

    Article  Google Scholar 

  19. A.A. Hamed, W. Tabakoff, R.B. Rivir, K. Das, P. Arora, J. Turbomach. 127, 445 (2005)

    Article  Google Scholar 

  20. E. Poursaeidi, A.M. Niaei, M. Arablu, A. Salarvand, Int. J. Surf. Sci. Eng. 11, 85 (2017)

    Article  Google Scholar 

  21. R.W. Haskell, ASME 1989 International Gas Turbine and Aeroengine Congress and Exposition (American Society of Mechanical Engineers 1989), p. V005T11A002

  22. R. Malka, S. Nešić, D.A. Gulino, Wear 262, 791 (2007)

    Article  Google Scholar 

  23. S. Zhou, M.M. Stack, R.C. Newman, Corrosion 52, 934 (1996)

    Article  Google Scholar 

  24. E. McCafferty, Introduction to Corrosion Science (Springer, New York, 2010)

    Book  Google Scholar 

  25. S.S. Rajahram, T.J. Harvey, R.J.K. Wood, Wear 267, 1883 (2009)

    Article  Google Scholar 

  26. N. Khayatan, H.M. Ghasemi, M. Abedini, Wear 380, 154 (2017)

    Article  Google Scholar 

  27. E. Poursaeidi, M. Arablu, M.R. Mohammadi Arhani, Root cause analysis of unit 2 refinery powerplant gas turbine compressors 1st row rotating blade fractures (Technical Report, South Pars Gas Company, Iran, 2010), p. 30557

    Google Scholar 

  28. ASTM, G76-95, Standard Test Method for Conducting Erosion Tests by Solid Particles Impingement Using Gas Jets (ASTM International, West Conshohocken, 2000)

    Google Scholar 

  29. ASTM, G05-94, Standard Reference Test Method for Making Potentiostatic and Potentiodynamic Anodic Polarization Measurements (ASTM International, West Conshohocken, 1999)

    Google Scholar 

  30. S.J. Doktycz, K.S. Suslick, Science (80). 247, 1067 (1990)

    Article  ADS  Google Scholar 

Download references

Acknowledgements

The authors would like to thank Dr. Zamani, the manager of the environmental sciences laboratory of the University of Zanjan and Mr. Rezaei, the head of the measurement department of Zanjan Gas Company for their equipment support.

Author information

Authors and Affiliations

Authors

Corresponding author

Correspondence to Esmaeil Poursaeidi.

Rights and permissions

Reprints and permissions

About this article

Check for updates. Verify currency and authenticity via CrossMark

Cite this article

Poursaeidi, E., Mohammadi Niaei, A., Lashgari, M. et al. Experimental studies of erosion and corrosion interaction in an axial compressor first stage rotating blade material. Appl. Phys. A 124, 629 (2018). https://doi.org/10.1007/s00339-018-2007-5

Download citation

  • Received:

  • Accepted:

  • Published:

  • DOI: https://doi.org/10.1007/s00339-018-2007-5

Navigation