Rene 41

Rene 41 is a precipitation hardening, nickel-based high temperature alloy possessing high strength in the 1200/1800°F (649/982°C) temperature range. This alloy is designed for use in severely stressed high temperature applications. Rene 41 has found applications in jet engine and high speed airframe components such as: afterburner parts, turbine casings, wheels, buckets, bolts, and fasteners.

TYPICAL SPECIFICATION PACKAGES

UNS-N-07041/N-08041

WERKSTOFF 2.4973

PLATE:AMS 5545

SHEET:AMS 5545

BAR:AMS5712 TY2/TY1 CAP 5713