An oxidation-resistant low coefficient of thermal expansion (low CTE) superalloy developed for gas turbine applications. The alloy is strengthened by a precipitation-hardening heat treatment made possible by additions of niobium and aluminum. In addition, the aluminum content provides excellent resistance to oxidation at high temperature. The alloy’s density is 5% less than those of superalloys such as INCONEL alloy 718. The combination of low expansion, high strength and excellent resistance to oxidation makes the alloy especially useful for gas turbine and steam turbine components. The low expansion enables closer control of clearances and tolerances for greater power output and fuel efficiency.

UNS: R30783
W.Nr.: n/a

Technical Bulletin (PDF, 192KB)

Available Product Forms: Sheet, round bar, wire and extruded section

Technical Papers
Effect of Prolonged Isothermal Exposure on Elevated-Temperature Time-Dependent Fatigue Crack Propagation in INCONEL alloy 783 (PDF, 1.6MB)

Effect of NiAl-Beta Precipitates on Fatigue Crack Propagation of INCONEL alloy 783 Under Time-Dependent Conditions with Various Load Ratios (PDF, 660KB)

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