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An Optimum Application of Austenitic Nodular Iron for Gas Turbine Components PUBLIC ACCESS

[+] Author Affiliations
J. T. Hageboeck

Frank Foundries Corporation, Moline, IL

W. S. Roberts

W. S. Roberts Engineering Co., Indianapolis, IN

Paper No. 68-GT-47, pp. V001T01A047; 7 pages
doi:10.1115/68-GT-47
From:
  • ASME 1968 Gas Turbine Conference and Products Show
  • ASME 1968 Gas Turbine Conference and Products Show
  • Washington, DC, USA, March 17–21, 1968
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7987-0
  • Copyright © 1968 by ASME

abstract

A new modification of an economical casting material is presented for use in the intermediate temperature range, which is considered to be 800 to 1300 F. An illustration is given of two large castings actually produced for the 1500-hp ATAC regenerative gas turbines engine. Comparisons are made with other materials, giving information stress-rupture at various temperature levels and some cost information. Also included are design suggestions for better utilization of foundry techniques.

Copyright © 1968 by ASME
This article is only available in the PDF format.

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