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Rene 41


Rene 41 material is ASTM SAE AMS 5399D (2006) Nickel Alloy, Corrosion and Heat-Resistant, Investment Castings 52Ni - 19Cr - 11Co - 9.8Mo - 3.2Ti - 1.6Al - 0.006B Vacuum-Melted, Vacuum-Cast, Solution Heat Treated ASTM SAE AMS 5545F (2010) Nickel Alloy, Corrosion and Heat-Resistant, Sheet, Strip, and Plate 54Ni - 19Cr - 11Co - 9.8Mo - 3.2Ti - 1.5Al - 0.006B Vacuum Induction and Consumable Electrode Melted, Solution Heat Treatable Precipitation Heat Treated ASTM SAE AMS 5712J (2006) Nickel Alloy, Corrosion and Heat-Resistant, Bars, Forgings, and Rings 53Ni - 19Cr - 11Co - 9.8Mo - 3.2Ti - 1.6Al - 0.006B Vacuum Melted, Solution Heat Treated Precipitation Hardenable ASTM SAE AMS 5713J (2007) Nickel Alloy, Corrosion and Heat-Resistant, Bars, Forgings, and Rings 53Ni - 19Cr - 11Co - 9.8Mo - 3.2Ti - 1.6Al - 0.006B Vacuum Melted, Solution and Precipitation Heat Treated ASTM SAE AMS 5800F (2006) Nickel Alloy, Corrosion and Heat-Resistant, Welding Wire 54Ni - 19Cr - 11Co - 10Mo - 3.2Ti - 1.5Al - 0.006B Vacuum Induction Melted ASTM SAE J 467 (1968) Special Purpose Alloys ("Superalloys") These products have been used typically for parts requiring high strength up to 1600 °F (871 °C) and oxidation resistance up to 1800 °F (982 °C), but usage is not limited to such applications.

Chemical composition of Rene 41, Rene 41 mechanical properties, Rene 41 datasheet, Rene 41 equivalent grade, Heat treatment and temperature process of Rene 41.


Rene 41 property sheet

Rene 41 Spec.

ASTM SAE AMS 5399D (2006)
Nickel Alloy, Corrosion and Heat-Resistant, Investment Castings 52Ni - 19Cr - 11Co - 9.8Mo - 3.2Ti - 1.6Al - 0.006B Vacuum-Melted, Vacuum-Cast, Solution Heat Treated
ASTM SAE AMS 5545F (2010)
Nickel Alloy, Corrosion and Heat-Resistant, Sheet, Strip, and Plate 54Ni - 19Cr - 11Co - 9.8Mo - 3.2Ti - 1.5Al - 0.006B Vacuum Induction and Consumable Electrode Melted, Solution Heat Treatable Precipitation Heat Treated
ASTM SAE AMS 5712J (2006)
Nickel Alloy, Corrosion and Heat-Resistant, Bars, Forgings, and Rings 53Ni - 19Cr - 11Co - 9.8Mo - 3.2Ti - 1.6Al - 0.006B Vacuum Melted, Solution Heat Treated Precipitation Hardenable
ASTM SAE AMS 5713J (2007)
Nickel Alloy, Corrosion and Heat-Resistant, Bars, Forgings, and Rings 53Ni - 19Cr - 11Co - 9.8Mo - 3.2Ti - 1.6Al - 0.006B Vacuum Melted, Solution and Precipitation Heat Treated
ASTM SAE AMS 5800F (2006)
Nickel Alloy, Corrosion and Heat-Resistant, Welding Wire 54Ni - 19Cr - 11Co - 10Mo - 3.2Ti - 1.5Al - 0.006B Vacuum Induction Melted
ASTM SAE J 467 (1968)
Special Purpose Alloys ("Superalloys")

Chemical Composition of Rene 41

Al: 1.40 1.60
B: 0.0030 0.0100
C: Max 0.12
Co: 10.00 12.00
Cr: 18.00 20.00
Cu: Max 0.50
Fe: Max 5.0
Mn: Max 0.10
Mo: 9.0 10.50
Ni: Max Remainder
S: Max 0.0150
Si: Max 0.5000
Ti: 3.0 3.3

Mechanical Properties of Rene 41

Rp0.2 (MPa) 767 (≥)
Rm (MPa) 462 (≥)
AKV (J) 12
A (%) 41
Z (%) 23
Hardness HBW 142

Rene 41 shape and dimensions

Rene 41 Round bar: 1mm-800mm
Rene 41 Square bar: 10mm * 10mm-600mm *600mm
Rene 41 Flat bar: Thickness:8mm-800mm Width:10mm to 1500mm
Rene 41 Sheet or Plate: Thickness:3mm-80mm Width:1.5mm to 1500mm
Rene 41 Strip or Coil: Thickness:0.1mm-3mm Width:1.5mm-1500mm
Rene 41 Forgings: Shafts with flanks/pipes/tubes/slugs/donuts/cubes/other shapes