A precipitation hardenable nickel-chromium alloy containing significant amounts of cobalt and molybdenum along with lesser amounts aluminum and titanium that exhibits extremely high room and elevated temperature mechanical properties. Excellent corrosion resistance and fabricability have led to wide usage in critical aircraft engine components such as nozzle partitions, turbine blades and wheels, combustion chamber liners and structural hardware.

UNS: N07041
W.Nr.: n/a

Technical Bulletin (PDF, 73KB)

Available Product Forms: Forging billet, bar, sheet and plate

Technical Papers
n/a

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