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Ceramic Matrix Composite Vane Subelement Testing in a Gas Turbine Environment

[+] Author Affiliations
Michael Verrilli, Anthony Calomino

NASA Glenn Research Center, Cleveland, OH

R. Craig Robinson

QSS Group at NASA Glenn Research Center, Cleveland, OH

David J. Thomas

OAI, Brookpark, OH

Paper No. GT2004-53970, pp. 393-399; 7 pages
  • ASME Turbo Expo 2004: Power for Land, Sea, and Air
  • Volume 2: Turbo Expo 2004
  • Vienna, Austria, June 14–17, 2004
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 0-7918-4167-7 | eISBN: 0-7918-3739-4
  • Copyright © 2004 by ASME


Vane subelements were fabricated from a silicon carbide fiber reinforced silicon carbide matrix (SiC/SiC) composite and were coated with an environmental barrier coating (EBC). A test configuration for the vanes in a gas turbine environment was designed and fabricated. Prior to testing, finite element analyses were performed to predict the temperatures and stress conditions present in vane during rig testing. This paper discusses the test configuration, the finite element analysis predictions, and results of the vane testing.

Copyright © 2004 by ASME



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