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Ceramic Composites for Gas Turbine Engines via a New Process FREE

[+] Author Affiliations
G. H. Schiroky, A. W. Urquhart

Lanxide Corporation, Newark, DE

B. W. Sorenson

Du Pont Lanxide Composites Inc., Newark, DE

Paper No. 89-GT-316, pp. V002T02A015; 6 pages
doi:10.1115/89-GT-316
From:
  • ASME 1989 International Gas Turbine and Aeroengine Congress and Exposition
  • Volume 2: Aircraft Engine; Marine; Microturbines and Small Turbomachinery
  • Toronto, Ontario, Canada, June 4–8, 1989
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7914-6
  • Copyright © 1989 by ASME

abstract

A new process for ceramic composites involves the growth of ceramic matrices through shaped preforms using directed oxidation reactions of molten metals. The preforms may consist of reinforcing fibers, whiskers, platelets, or particles, as needed to produce the desired properties in the finished component. This new technology is being developed by Lanxide Corporation and is being applied to gas turbine engine components by Du Pont Lanxide Composites Inc., a joint venture. The paper includes a description of the technology and a discussion of the status of its application to materials for gas turbine engine components.

Copyright © 1989 by ASME
This article is only available in the PDF format.

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