Rene 41™ - UNS N07041
Common Trade Names: Rene 41®, Alvac Rene® 41, Haynes® R-41, Udimet® R41
Rene 41® is a nickel-chromium alloy that contains cobalt, molybdenum and some aluminum and titanium. Rene 41® has a high corrosion resistance, easily fabricated which makes Rene 41® usable to aircraft engine components such as turbine blades, wheels, combustion chamber liners and structural hardware. Rene 41®’s specifications are AMS 5545, AMS 5712, and AMS 5713.
Available forms are seamless pipe, welded pipe, seamless tube, welded tube, bar, wire, sheet, plate, forgings, pipe fittings and flanges.
Sheet/Plate content |
AMS 5545 |
Round Bar/Wire content |
AMS 5712 |
C (Carbon content) |
.05 - .12 |
| MN | 0.10 max |
| P | |
| S | .015 max |
Si |
0.50 |
Cr |
18.0 - 20.0 |
Ni |
bal |
Mo |
9.0 - 10.5 |
Cu | |
Co |
10.0 - 12.0 |
| Cb | |
Ti (Titanium contenet) |
3.0 - 3.30 |
Al (Aluminum content) |
1.40 - 1.60 |
Fe (Iron content) |
5.0 max |
| B | .003 - .010 |
Zr (Zirconium content) | |
