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Advanced Cooled First Stage Vane Design FREE

[+] Author Affiliations
G. N. Levari

Westinghouse Electric Corporation, Concordville, PA

R. E. Jeffries

General Motors Corporation, Indianapolis, IN

A. Cohn

Electric Power Research Institute, Palo Alto, CA

Paper No. 84-GT-219, pp. V004T10A026; 11 pages
doi:10.1115/84-GT-219
From:
  • ASME 1984 International Gas Turbine Conference and Exhibit
  • Volume 4: Heat Transfer; Electric Power
  • Amsterdam, The Netherlands, June 4–7, 1984
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7949-8
  • Copyright © 1984 by ASME

abstract

This paper discusses the design of an advanced cooled 1st stage vane, including airfoil and endwalls, for a full-scale utility combustion turbine. Shell/spar cooling technology is used, in which cooling air flows through channels between a thin metal external sheet (shell) and a hollow-cast internal support member (spar), which are joined by diffusion bonding. Heat transfer and stress analyses of this design are featured; however, design criteria, fabrication considerations, material selection, flow analysis, and future program direction are also discussed.

Copyright © 1984 by ASME
Topics: Design
This article is only available in the PDF format.

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