Skip to content
1887
  1. Home
  2. A-Z Publications
  3. Platinum Metals Review
  4. Volume 25, Issue 3
  5. Article
Volume 25, Issue 3
  • ISSN: 0032-1400
file format pdf download PDF

Abstract

Turbine blades in gas turbine engines operate at elevated temperatures and in highly oxidising atmospheres that can be contaminated with fuel residues and sea water salts. These components, which are expensive to produce, are subjected to high stresses during operation but must be totally reliable during their design life. An economic way to maintain blade properties is to coat the base metal superalloy with a protective layer capable of resisting both high temperature oxidation and hot corrosion. Conventional aluminide coatings are widely used for this purpose but platinum aluminides offer improved corrosion resistance. A collaborative exercise involving Rolls-Royce and Johnson Matthey has now resulted in the development of a platinum aluminide diffusion coating that offers some advantages over the commercial systems.

© Johnson Matthey
Loading

Article metrics loading...

/content/journals/10.1595/003214081X25394105
1981-01-01
2024-12-21
Loading full text...

Full text loading...

/deliver/fulltext/pmr/25/3/pmr0025-0094.html?itemId=/content/journals/10.1595/003214081X25394105&mimeType=html&fmt=ahah

References

  1. D. R. Coupland, I. R. McGill, C. W. Corti, G. L. Selman, Spring Residential Conf. on the Environ. Degradation of High Temp. Mater., Isle of Man, 31 March–3 April, 1980, Series 3, 2, (13), p. 26, Inst. of Metall., London, 1980 [Google Scholar]
  2. S. W. K, Shaw, Third Int. Conference on Gas Turbine Materials in a Marine Environment, Univ. of Bath, 21–23 Sept. 1976, Session VI, Paper 1, p. 1 [Google Scholar]
  3. J. E. Restall, Metallurgia, 1979, 46, (11), 676 [Google Scholar]
  4. N. S. Bornstein, M. A. DeCrescente, Trans. Metall. Soc. AIME, 1969, 245, (9), 1947 [Google Scholar]
  5. R. Sivakumar, L. L. Seigle, Metall. Trans., 1976, 7A, (8), 1073 [Google Scholar]
  6. M. R. Jackson, J. R. Rairden, Metall. Trans., 1977, 8A, (11), 1697 [Google Scholar]
  7. G. Lehnert, H. Meinhardt, Electrodeposition Surf. Treat., 1972, 1, (1), 71 [Google Scholar]
  8. I. A. Kvernes, P. Kofstad, Metall. Trans., 1972, 3, (6), 1511 [Google Scholar]
  9. I. M. Allam, D. P. Whittle, J. Stringer, Progress Report, Dept. Metall. and Mater. Sci., University of Liverpool, February, 1976 [Google Scholar]
  10. O. M. Trela, T. K. Glasgow, L. J. Ebert, Metall. Trans., 1976, 7A, (10), 1593 [Google Scholar]
  11. D. L. Deadmore,
  12. E. J. Felten, Oxid. Met., 1976, 10, (1), 23 [Google Scholar]
  13. V. Partarini, N. S. Bornstein, M. A. DeCrescente, 1978
  14. G. W. Goward, J. Met., 1970, 22, (10), 31 [Google Scholar]
  15. British Patent 1,210,026; 1970 [Google Scholar]
  16. J. H. F. Notton, Platinum Metals Rev., 1977, 21, (4), 122 [Google Scholar]
  17. G. W. Meetham, D. Coutsouradis, P. Felix, H. Fischmeister, L. Habraken, V. Lindblom, M. O. Speidel, in “High Temperature Alloys for Gas Turbines”, Applied Science Publishers Ltd, London, 1978, p. 837 [Google Scholar]
/content/journals/10.1595/003214081X25394105
Loading
The Protection of Gas Turbine Blades
Platinum Metals Review 25, 94 (1981); https://doi.org/10.1595/003214081X25394105
/content/journals/10.1595/003214081X25394105
/content/journals/10.1595/003214081X25394105
Loading

Data & Media loading...

  • Article Type: Research Article

Most Cited Most Cited RSS feed

This is a required field
Please enter a valid email address
Approval was a Success
Invalid data
An Error Occurred
Approval was partially successful, following selected items could not be processed due to error
Please enter a valid_number test