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Erschienen in:
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2017 | OriginalPaper | Buchkapitel

10. Structural Intermetallics

verfasst von : R. Mitra, R. J. H. Wanhill

Erschienen in: Aerospace Materials and Material Technologies

Verlag: Springer Singapore

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Abstract

Development of materials for structural applications at elevated temperatures in aeroengines has encouraged research on intermetallic alloys. A select group of aluminides and silicides has shown significant promise for high temperature structural applications owing to their high melting temperatures, as well as their ability to retain strength and oxidation resistance at elevated temperatures. In recent years the focus is on multiphase multicomponent intermetallic alloys with significant volume fractions of ductile constituents to achieve an optimum combination of toughness and elevated temperature strength. The engineering properties and actual or potential aerospace applications of the currently most important structural intermetallics, the nickel, iron, and titanium aluminides, are concisely discussed.

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Vorheriges Kapitel Nickel-Based Superalloys
Nächstes Kapitel Bronzes for Aerospace Applications
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Metadaten
Titel
Structural Intermetallics
verfasst von
R. Mitra
R. J. H. Wanhill
Copyright-Jahr
2017
Verlag
Springer Singapore
Buch
Aerospace Materials and Material Technologies

Print ISBN: 978-981-10-2133-6

Electronic ISBN: 978-981-10-2134-3

Copyright-Jahr: 2017

DOI
https://doi.org/10.1007/978-981-10-2134-3_10

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