Chemical composition Element Weight percent Element Weight percent Ni Balance Cr 25.0 nominal Mo 10.0 nominal C 0.05 nominal Mg 0.015 nominal Ce 0.03 nominal

Mechanical properties Cold-rolled sheet, 0.7–2.0 mm thick; solution treated at 1150°C for 5–15 min and air cooled. Special Metals Table 5. Elongation measured over 50 mm. Test temperature °C 0.2% proof MPa Tensile MPa Elongation % 20 438 873 45 750 250 502 74 850 184 310 83 900 125 237 66 1050 44 98 50

Application areas Gas turbine combustion chambers Afterburner components Heat-treatment furnace equipment Fabricated high-temperature sheet structures

Chemical composition Element Weight percent Element Weight percent Ni Balance Cr 25.0 nominal Mo 10.0 nominal C 0.05 nominal Mg 0.015 nominal Ce 0.03 nominal

Mechanical properties Cold-rolled sheet, 0.7–2.0 mm thick; solution treated at 1150°C for 5–15 min and air cooled. Special Metals Table 5. Elongation measured over 50 mm. Test temperature °C 0.2% proof MPa Tensile MPa Elongation % 20 438 873 45 750 250 502 74 850 184 310 83 900 125 237 66 1050 44 98 50

Application areas Gas turbine combustion chambers Afterburner components Heat-treatment furnace equipment Fabricated high-temperature sheet structures

Alloy 86/Nimonic 86

Grade:Nimonic 86

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

NIMONIC 86 is a solid-solution nickel chromium molybdenum alloy with a small cerium addition. It was developed to combine formability, ductility and weldability with high-temperature creep strength and strong cyclic oxidation resistance. Its oxidation performance is particularly relevant near 1050°C. The alloy is primarily used for fabricated sheet components in gas turbines and heat-treatment equipment, where resistance to scaling and reliable fabrication are important.