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US 2015/0315919 A1Published application
LIGHTWEIGHT STRUCTURAL NiAl ALLOY WITH A HIGH HIGH-TEMPERATURE STRENGTH
AssigneeMTU Aero Engines AG
InventorWilfried SMARSLY
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Abstract
Disclosed is a material on the basis of intermetallic nickel aluminides for applications which require a high high-temperature strength. The material comprises more than 50 at. % nickel and ternary Laves phases. Also disclosed is a component of a turbomachine produced from the material.
Claims20
A material on the basis of intermetallic nickel aluminides for applications which require a high high-temperature strength, wherein the material comprises more than 50 at. % nickel and ternary Laves phases.
Dependencies are inferred from the claim text.