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Ultrahigh-Temperature Materials for Jet Engines

Published online by Cambridge University Press:  31 January 2011

J.-C. Zhao  and
J. H. Westbrook

Abstract

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This introductory article provides the background for the September 2003 issue of MRS Bulletin on Ultrahigh-Temperature Materials for Jet Engines. It covers the need for these materials, the history of their development, and current challenges driving continued research and development. The individual articles that follow review achievements in four different material classes (three in situ composites—based on molybdenum silicide, niobium silicide, and silicon carbide, respectively—and high-melting-point platinum-group-metal alloys), as well as advances in coating systems developed both for oxidation protection and as thermal barriers. The articles serve as a benchmark to illustrate the progress made to date and the challenges ahead for ultrahigh-temperature jet-engine materials.

Keywords

coatingscompositesductilityjet enginesoxidationoxidesplatinum-group-metal alloys (PGM alloys)silicidesstrengthstructural materialsthermal-barrier coatingstoughnessultrahigh-temperature materials
Type
Research Article
Information
MRS Bulletin , Volume 28 , Issue 9: Ultrahigh-Temperature Materials for Jet Engines , September 2003 , pp. 622 - 630
Copyright
Copyright © Materials Research Society 2003

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