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

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

Rene 41/UNS N07041/Alloy R41

Grade: Rene 41/UNS N07041/Alloy R41

Sheet/Plate: 0.3mm-150mm

Strip/Foil: 0.02mm-16mm

Pipe: 6mm*0.5mm-1200mm*100mm

Bar: Ф6mm – Ф600mm

Wire: Ф0.01mm – Ф6mm

Others: Forged Rings, Flanges, Elbows, Tees, Reducers etc.

Standard: ASTM/ASME/AMS

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.

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

Rene 41 Applications

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

Introduction

Specification

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

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

Application

Rene 41 Applications

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