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Demonstration of Ceramic Hot-Section Static Components in a Radial Flow Turbine FREE

[+] Author Affiliations
J. P. Arnold, W. McGovern

U.S. Army Mobility Equipment Research & Development Command, Fort Belvoir, VA

J. C. Napier, A. P. Batakis

Solar Turbines Incorporated, San Diego, CA

Paper No. 82-GT-184, pp. V005T12A003; 6 pages
doi:10.1115/82-GT-184
From:
  • ASME 1982 International Gas Turbine Conference and Exhibit
  • Volume 5: Manufacturing Materials and Metallurgy; Ceramics; Structures and Dynamics; Controls, Diagnostics and Instrumentation; Education; Process Industries; Technology Resources; General
  • London, England, April 18–22, 1982
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7960-3
  • Copyright © 1982 by ASME

abstract

Ceramic hot-section turbine components allow higher temperature for up-rated power and improved fuel economy. The methodology used in arriving at a successful 200-hr engine demonstration of an all ceramic nozzle is presented along with current progress in demonstrating the remaining ceramic hot-section static components.

Copyright © 1982 by ASME
This article is only available in the PDF format.

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