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Turbomachinery Alloys Affected by Solid Particles FREE

[+] Author Affiliations
W. Tabakoff

University of Cincinnati, Cincinnati, OH

Paper No. 88-GT-295, pp. V003T05A014; 8 pages
doi:10.1115/88-GT-295
From:
  • ASME 1988 International Gas Turbine and Aeroengine Congress and Exposition
  • Volume 3: Coal, Biomass and Alternative Fuels; Combustion and Fuels; Oil and Gas Applications; Cycle Innovations
  • Amsterdam, The Netherlands, June 6–9, 1988
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7920-7
  • Copyright © 1988 by ASME

abstract

In operating gas turbine engines in dusty environments, severe erosion of compressor and turbine components results. This erosion adversely effects engine performance. Predicting erosion in the rotating machine of gas turbine is a complex problem. This paper presents test data from the high temperature material erosion facility at the University of Cincinnati. Data was obtained between a target temperature of ambient and 649°C (1200°F) for AM355, Rene 41 and L605 cobalt. In addition, particle velocity and impingement angle were varied.

Copyright © 1988 by ASME
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