Haynes 282 nickel alloy rod, Haynes 282 wire, Haynes 282 plate supplier, Haynes 282 pipe price

HAYNES 282 alloy (UNS N07208) is a, wrought, gamma-prime strengthened superalloy developed for high temperature structural applications, especially those in aero and industrial gas turbine engines. It possesses a unique combination of creep strength, thermal stability, weldability, and fabricability not found in currently available commercial alloys. The excellent creep strength in the temperature range of 1200 to 1700°F (649 to 927°C) surpasses that of Waspaloy alloy, and approaches R-41 alloy without sacrificing weldability.

Products Details

Ni 57.0 min Cr 19.5
Co 10.0 Mo 8.5
Ti 2.1 Al 1.5
Fe 1.5 max Mn 0.3 max
Ca 0.06 B 0.005
Temperature Yield Strength 0.2% Offset Ultimate Tensile Strength Elongation
°F °C ksi MPa ksi MPa %
RT RT 101.4 699 164.2 1132 30
1000 538 91.6 632 139.3 960 36
1200 649 91.5 631 145.7 1005 27
1300 704 90.5 624 136.5 941 24
1400 760 88.7 612 120.8 833 22
1500 816 82.3 567 100.3 692 24
1600 871 72.6 501 80.5 555 31
1700 927 43.9 303 50.2 346 37
1800 982 18.7 129 24.5 169 61
Haynes 282 available sizes and specifications
Grade Haynes 282
Nickel plate Thickness: 0.3mm - 150.0mm Width: 1000mm - 3000mm
Nickel strip/ nickel foil Thickness: 0.02mm - 16.0mm Width: 5mm - 3000mm
Nickel coil Thickness: 0.3mm - 16.0mm Width: 1000mm - 3000mm
Nickel pipe Outside diameter: 6mm - 1219mm Thickness: 0.5mm - 100mm
Nickel Capillary Pipe Outside diameter: 0.5mm - 6.0mm Thickness: 0.05mm - 2.0mm
Nickel bar Diameter: Ф4mm - Ф600mm
Nickel wire rod Diameter:Ф0.01mm - Ф6mm
▪ sheet fabrications ▪ Rings ▪ Cases found in compressor ▪ Combustion and turbine sections ▪ Engines for aircraft ▪ the transition sections and other hot-gas-path components in land-based gas turbines.

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