Rene 41 nickel wire rod, Rene 41 round bar, Rene 41 plate, Rene 41 sheet, Rene 41 strip

Cobalt Alloy R41 / Rene 41 Alloy R41 (Rene 41) is an age hardening nickel base super alloy with has exceptional strength from room temperature through to between 650°C - 980°C (1200 - 1800ºF). R 41 is designed for use in severely stressed high temperature applications. R41 (Rene 41) is typically used in hot components for jet engines, rocket engines, turbine blades, turbine wheels, torque rings, bolting, springs and much more.

Products Details

C Si Ni Co Al Fe Mn Cr Mo Ti B
0.06 - 0.12 0.20 max Bal 10-12 1.4-1.6 5.0 max 0.1 max 18-20 9.0-10.5 3-3.3 0.003-0.01
▪ UNS N07041 ▪ Werkstoff Nr. 2.4973 ▪ AISI 683 ▪ SAE AMS 5712 Bar ▪ SAE AMS 5545 Sheet, Strip and Plate ▪ GE B50T59 Sheet, Plate, Strip, Bars and Forgings ▪ GE B50TF76C Sheet, Plate, Strip ▪ GE B50TF109C Sheet, Strip, Plate, Solution Treated ▪ SAE AMS 5713 Bar (VAC MELT) ▪ SAE AMS 5800 Welding Wire ▪ MSRR 9500/241 Welding Wire
Material Tensile Strength ksi Yield Strength ksi Elongation in 4D Reduction of Area Hardness
Rene 41 (R41) Solution Treated Bar         363 HB max
Rene 41 (R41) Solution Treated Aged Bar 170 130 8 10 311 HB min
Rene 41 (R41) Solution Treated Sheet 170 max 100 max 30 max   30HRC max
Rene 41 (R41) Solution Treated Aged Sheet 170 min 130 min 10 min   35 HRC min
▪ Aircraft engine components ▪ Aircraft turbine blades ▪ Aircraft wheel ▪ Aircraft combustion chamber liners ▪ Aircraft structural hardware ▪ Afterburner parts

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