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

Short Description:

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.

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Product Detail

Product Tags

Specifications

▪ 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

Rene 41 Applications

▪ Aircraft engine components
▪ Aircraft turbine blades
▪ Aircraft wheel
▪ Aircraft combustion chamber liners
▪ Aircraft structural hardware
▪ Afterburner parts

Chemical Composition

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

Mechanical Properties

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