Superalloy optimized for high-temperature performance in high-pressure turbine disks

This invention relates to nickel-base superalloys and, more particularly, to such a superalloy optimized for use in high-temperature components of jet engines such as turbine disks. A superalloy has a composition of, in weight percent, from about 16.0 percent to about 22.4 percent cobalt, from about...

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Hauptverfasser:	Mourer, David P, Huron, Eric S, Bain, Kenneth R, Montero, Enrique E, Reynolds, Paul L, Schirra, John J
Format:	Patent
Sprache:	eng
Online-Zugang:	Volltext bestellen
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