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A superalloy, or high-performance alloy, is an alloy with the ability to operate at a high fraction of its melting point. [1] Key characteristics of a superalloy include mechanical strength , thermal creep deformation resistance, surface stability, and corrosion and oxidation resistance.
Aerospace structures. The Boeing 787 is 15% titanium by weight, [19] and the Airbus A350 is 14%. [20] Biomedical implants and prostheses [21] High-performance race cars; High-end bicycles; Additive manufacturing [22] Apple iPhone 15 Pro (Max) case, iPhone 16 Pro and Pro Max cases and Apple Watch Series 10 titanium and Ultra 2 cases
Since it is the most commonly used alloy – over 70% of all alloy grades melted are a sub-grade of Ti6Al4V, its uses span many aerospace airframe and engine component uses and also major non-aerospace applications in the marine, offshore and power generation industries in particular." [21]
Inconel is a nickel-chromium-based superalloy often utilized in extreme environments where components are subjected to high temperature, pressure or mechanical loads. Inconel alloys are oxidation- and corrosion-resistant. When heated, Inconel forms a thick, stable, passivating oxide layer protecting the surface from further attack.
Carpenter Signs Multi-Level Agreement with UTC; Will Build New Facility for Superalloy Powders 10-Year Supply Agreement Also Reached with Aerospace Business Units WYOMISSING, Pa.--(BUSINESS WIRE ...
Pole figures displaying crystallographic texture of gamma-TiAl in a rolled sheet of alpha2-gamma alloy, as measured by high energy X-rays. [2]Gamma TiAl has excellent mechanical properties and oxidation and corrosion resistance at elevated temperatures (over 600 °C), which makes it a possible replacement for traditional Ni based superalloy components in aircraft turbine engines.
Inconel 625 was designed as a solid solution strengthened material with no significant microstructure. This holds true at low and high temperatures, but there is a region (923 to 1148 K) where precipitates form that are detrimental to the creep properties, and thus the strength, of the alloy.
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