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Cobalt Alloy R41 / Rene 41

Technical Data Sheet

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.

Chemical Composition Limits
Weight %CSiNiCoAlFeMnCrMoTiB
R41
Rene 41
0.06 - 0.120.20 maxBal10-121.4-1.65.0 max0.10 max18-209.0-10.503-3.300.003-0.010

Typical Mechanical Properties

MaterialTensile Strength ksiYield Strength ksiElongation in 4DReduction of AreaHardness
Rene 41 (R41)
Solution Treated Bar




363 HB max
Rene 41 (R41)
Solution Treated Aged Bar
170130810311 HB min
Rene 41 (R41)
Solution Treated Sheet
170 max100 max30 max
30HRC max
Rene 41 (R41)
Solution Treated Aged Sheet
170 min130 min10 min
35 HRC min

Availability

Alloy R41 (Rene 41) is available in Sheet, Strip, Plate, Wire, Rod, Bar (round bar, flat bar), Forging Stock and Welding Wire. For all stock availability contact Sales.

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

Tradenames - Rene 41, Pyromet Alloy 41

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