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Integration of Multi-Disciplinary Factors Into Turbine Cooling Design

[+] Author Affiliations
Boris Glezer

Optimized Turbine Solutions, San Diego, CA

Paper No. 2001-GT-0179, pp. V003T01A055; 8 pages
  • ASME Turbo Expo 2001: Power for Land, Sea, and Air
  • Volume 3: Heat Transfer; Electric Power; Industrial and Cogeneration
  • New Orleans, Louisiana, USA, June 4–7, 2001
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7852-1
  • Copyright © 2001 by ASME


The presented paper describes a multi-disciplinary cooling selection practice applied to major gas turbine engine hot section components, including turbine nozzles, blades, discs, combustors and support structures maintaining blade tip clearances. The paper demonstrates the benefits of close interaction between participating disciplines, when this interaction starts in the early phase of the hot section development. The approach targets advances in engine performance and cost by optimizing the design process, often requiring compromises within individual disciplines.

Copyright © 2001 by ASME
Topics: Cooling , Design , Turbines



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