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 % | C | Si | Ni | Co | Al | Fe | Mn | Cr | Mo | Ti | B |
| R41 Rene 41 |
0.06 – 0.12 | 0.20 max | Bal | 10-12 | 1.4-1.6 | 5.0 max | 0.10 max | 18-20 | 9.0-10.50 | 3-3.30 | 0.003-0.010 |
Typical 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 |
