journal article·1990-12

The performance of Superalloys

Tom B. Gibbons

Advanced Materials· Volume 2· Issue 12
Publisher page

Abstract

Hot‐end components in today's aero turbofan engines are made from materials known as superalloys, typically based on NiCr, NiCrFe or CoCr systems. In the fifty years or so that have elapsed since the first superalloys were introduced, the temperature capability of the materials has increased by approximately 500° and the power output of aero gas turbines has risen from ∼︁ 20 kN of thrust to the 250 kN achievable today. The materials and their development are described.
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Research context

OpenAlex topics: High Temperature Alloys and Creep · Advanced Aircraft Design and Technologies · High-Temperature Coating Behaviors

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