Rene 41

Nickel Super Alloy UNS N07041

Material Data Sheet

Rene 41 is an age-hardening nickel-base superalloy with exceptional strength from room temperature through about 1600°F. The alloy is sensitive to strain age cracking during welding. Sound welds can be made by the resistance and electron beam methods. GTAW using DC straight polarity requires good joint fit-up and cooling by means of copper backup bars or water-cooled fixtures. Rene 41 should be in the fully solution treated condition prior to welding. After welding the assembly should be solution treated using rapid heating and cooling rates through the 1200-1600°F range, followed by aging.

Mechanical properties vary with the solution and aging treatments. Higher solution temperatures result in better room temperature ductility and elevated temperature creep-rupture strength. Lower solution temperatures give higher tensile strengths.

Two commonly used heat treatments are:
1. Solution treat: 2150°F 4 hours, air cool. Age: Reheat 1650 °F 4 hours, air cool.

2. Solution treat: 1975 °F 4 hours, air cool. Age: Reheat 1400°F 16 hours, air cool.

Chemical Composition
Element Content %
Nickel, Ni 52.0
Chromium, Cr 19.0
Cobalt, Co 11.0
Molybdenum, Mo 9.75
Titanium, Ti 3.15
Iron, Fe 3.0
Aluminum, Al 1.60
Carbon, C 0.060
Boron, B 0.007
Physical Properties
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Properties Metric Imperial
Density 8.25 g/cm³ 0.298 lb/in³
Melting Point 1345°C 2450°F
Modulus of Elasticity 218 GPa 31.6 x 103 ksi
Modulus of Rigidity 83.4 GPa 12.1 x 103 ksi
Coefficient of Expansion 13.5 µm/m-°C 7.5 µin/in.-°F
Electrical Resistivity 131 µΩ.cm 51.5 µΩ.in
Thermal Conductivity 9.0 W/m-K 62 Btu-in/ft2hr-°F
MechanicalProperties
Properties Metric Imperial
Hardness, Brinell 334/td> 334
Hardness, Knoop 363 363
Hardness, Rockwell C 36 36
Hardness, Vickers 349 349
Tensile Strength, Ultimate 1241 MPa 180,000 psi
Tensile Strength, Yield 793 MPa 115,000
Elongation at Break 20% 20%
Reduction of Area 25% 25%
Specifications
  • AMS 5545
  • AMS 5712
  • AMS 5713
  • AMS 5800
  • EN 2.4973
  • GE B50T59
  • GE B50TF109
  • GE B50TF76
  • UNS N07041
  • Werkstoff 2.4973
Applications
  • Jet engine hot components
  • Missile components
  • Bolting
  • Springs

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