Chemical composition Element Weight percent Element Weight percent Ni Balance Cr 20 Co 10 Mo 8.5 Ti 2.1 Al 1.5 Fe 1.5 max Mn 0.3 max Si 0.15 max C 0.06 B 0.005 — —

Mechanical properties Sheet solution annealed at 1149°C, then aged at 1010°C for 2 h / air cool plus 788°C for 8 h / air cool. Typical tensile data. Test temperature °C 0.2% yield MPa Tensile MPa Elongation % RT 699 1132 30 649 631 1005 27 760 612 833 22 871 501 555 31 Source: Haynes International 282 alloy data. Typical values; not purchase acceptance limits.

Application areas Aircraft and industrial gas turbine combustors Turbine, exhaust and nozzle components Engine cases and rolled rings using an appropriate heat treatment Candidate material for advanced ultra-supercritical boilers and steam turbines Candidate material for supercritical CO2 and concentrating solar power systems

Chemical composition Element Weight percent Element Weight percent Ni Balance Cr 20 Co 10 Mo 8.5 Ti 2.1 Al 1.5 Fe 1.5 max Mn 0.3 max Si 0.15 max C 0.06 B 0.005 — —

Mechanical properties Sheet solution annealed at 1149°C, then aged at 1010°C for 2 h / air cool plus 788°C for 8 h / air cool. Typical tensile data. Test temperature °C 0.2% yield MPa Tensile MPa Elongation % RT 699 1132 30 649 631 1005 27 760 612 833 22 871 501 555 31 Source: Haynes International 282 alloy data. Typical values; not purchase acceptance limits.

Application areas Aircraft and industrial gas turbine combustors Turbine, exhaust and nozzle components Engine cases and rolled rings using an appropriate heat treatment Candidate material for advanced ultra-supercritical boilers and steam turbines Candidate material for supercritical CO2 and concentrating solar power systems

Alloy 282/UNS N07208

Grade: Haynes 282/UNS N07208

Sheet/Plate: 0.3mm-150mm

Strip/Foil: 0.02mm-16mm

Pipe: 6mm*0.5mm-1200mm*100mm

Bar: Ф6mm – Ф600mm

Wire: Ф0.01mm – Ф6mm

Others: Forged Rings, Flanges, Elbows, Tees, Reducers etc.

Standard: ASTM/ASME/AMS

HAYNES 282 is a wrought nickel-base superalloy strengthened by gamma-prime precipitation. It combines creep strength, thermal stability and weldability for demanding turbine structures. Its relatively controlled precipitation behavior supports fabrication in the solution-annealed condition, followed by aging to develop strength. Applications include aircraft and industrial gas turbines, while specially qualified heat treatments extend its relevance to advanced power generation and pressure equipment.