X11CrNiMoN12
2026-04-09 14:40:00 Origin: Remark:0 Click:
Superalloy is widely used to produce the high temperature components for gas turbine in the field of aviation, naval vessels and industry, such as turbine blade, guide blade, turbine disc, high pressure compressor disc, combustor, and also production of energy conversion devices, such as aerospace craft, rocket motor, nuclear reactor, petrochemical equipments, coaly transforming and so on.
MATERIAL DATA SHEET - X11CrNiMoN12
MATERIAL CATEGORY - High temperature high strength steel and superalloy
Silicon, Si (%): ≤ 0.50
Manganese, Mn (%): 0.40~0.90
Phosphorus, P (%): ≤ 0.025
Sulfur, S (%): ≤ 0.015
Chromium, Cr (%): 11.0~12.5
Nickel, Ni (%): 2.00~3.00
Molybdenum, Mo (%): 1.50~2.00
Vanadium, V (%): 0.25~0.40
Mechanical property above 200℃ σ0.2/MPa,at following temperature /℃|300: 770
Mechanical property above 200℃ σ0.2/MPa,at following temperature /℃|400: 700
Mechanical property above 200℃ σ0.2/MPa,at following temperature /℃|500: 590
Mechanical property above 200℃ σ0.2/MPa,at following temperature /℃|600: 350
Mechanical property above 200℃ σ0.2/MPa,at following temperature /℃|700: -
Mechanical property above 200℃ σ0.2/MPa,at following temperature /℃|800: -
Creep rupture strength /MPa,at following time/h and temperature /℃|1000h|700: -
Creep rupture strength /MPa,at following time/h and temperature /℃|1000h|800: -
Creep rupture strength /MPa,at following time/h and temperature /℃|1000h|900: -
Creep rupture strength /MPa,at following time/h and temperature /℃|10000h|700: -
Creep rupture strength /MPa,at following time/h and temperature /℃|10000h|800: -
Creep rupture strength /MPa,at following time/h and temperature /℃|10000h|900: -
Creep rupture strength /MPa,at following time/h and temperature /℃|100000h|800: -
Creep rupture strength /MPa,at following time/h and temperature /℃|100000h|900: -
These materials must stand up to high heat, extreme oxidation potential and recycling.
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