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Model No: Rene 41

UNS N07041 / Alloy R41 / 2.4973

ZYTC Alloy is a leading supplier of Alloy R41 (UNS N07041 / 2.4973), a high-strength, age-hardenable nickel superalloy for jet engine & rocket components. Available in bar, sheet, plate, and wire. Get a competitive quote.
Delivery :
FOB
minimum order :
50 kilograms
Supply Ability :
5000kilograms / Month
Stock Time :
7-10Day
Country of Origin :
CHINA
Quantity :
Contact Now

Alloy R41 (UNS N07041 / 2.4973) is an age-hardenable nickel-chromium superalloy strengthened by cobalt, molybdenum, titanium, and aluminum additions. Designed for severely stressed applications up to 980°C (1800°F), it delivers exceptional tensile and creep strength in jet engine hot sections, rocket hardware, and high-temperature fasteners. The alloy requires careful thermal processing due to susceptibility to strain-age cracking during welding .


1. Product Specifications & Physical Data

ZYTC Alloy supplies UNS N07041 in mill forms for aerospace and power generation applications requiring verified high-temperature properties and complete material traceability.

  • Available Forms: Bar, rod, forging stock, sheet, strip, plate, wire, and welding wire.

  • Specifications: AMS 5545, AMS 5712, AMS 5713, AMS 5800, GE C50T71 .

Chemical Composition (Weight %)Rene® 41 Specification
Nickel (Ni)Balance
Chromium (Cr)18.0 - 20.0
Cobalt (Co)10.0 - 12.0
Molybdenum (Mo)9.0 - 10.5
Titanium (Ti)3.0 - 3.3
Aluminum (Al)1.4 - 1.6
Carbon (C)0.06 - 0.12
Boron (B)0.003 - 0.010
Iron (Fe)5.0 max.
 
Physical PropertiesMetricImperial
Density8.24 - 8.25 g/cm³0.298 lb/in³
Melting Point1345°C2450°F
Modulus of Elasticity (RT)218 GPa31.6 × 10⁶ psi
Thermal Conductivity (RT)9.0 W/m·K62 BTU·in/hr·ft²·°F
Coefficient of Expansion (20-538°C)13.5 µm/m·°C7.5 µin/in·°F
 
Mechanical PropertiesConditionMetricImperial
Tensile Strength (min.)Aged bar1172 MPa170 ksi
Yield Strength (min.)Aged bar896 MPa130 ksi
Elongation (min.)Aged bar8%8%
Tensile Strength (RT)Annealed sheet1172 MPa max170 ksi max
Tensile Strength (RT)Annealed + Aged1350-1550 MPa196-225 ksi
Hardness (Aged bar)Min.311 HB311 HB

2. Fabrication & Material Comparison

Rene 41 requires precise thermal processing to develop gamma-prime precipitate structure while avoiding strain-age cracking.

  • Heat Treatment Options :

    • Option 1 (Higher Ductility/Creep): Solution 1177°C (2150°F) × 4 hours, air cool; age 899°C (1650°F) × 4 hours, air cool.

    • Option 2 (Higher Tensile): Solution 1079°C (1975°F) × 4 hours, air cool; age 760°C (1400°F) × 16 hours, air cool .

    • Spring Temper: 1065°C (1950°F) × 4 hours solution + age as above .

  • Hot Working: Forge in range 1065-1175°C (1950-2150°F); avoid low-temperature working.

  • Cold Working: Limited formability in annealed condition; intermediate anneals required for severe deformation.

  • Machining: Requires heavy-duty equipment, rigid setups, and sharp tools. Carbide tooling recommended with positive rake angles. Water-based coolants for high-speed operations.

  • Welding: Susceptible to strain-age cracking. Weld only in fully solution-treated condition using GTAW (DC straight polarity) with copper backup bars or water-cooled fixtures for rapid cooling. Resistance and electron beam welding preferred. Post-weld solution treatment with rapid heating/cooling through 650-870°C range required before aging .


Applications 

  • Aerospace & Jet Engines: Turbine blades, turbine discs, wheels, combustion chamber liners, afterburner components, nozzle guide vanes, divergent seals, flap components, exhaust nozzles

  • Rocket Engines: Thrust chambers, turbo pump seals, hot-section hardware

  • Fasteners & Springs: High-temperature bolts, nuts, fasteners retaining tension up to 980°C

  • Structural Components: Torque rings, shafts, casings, space shuttle components

Contact ZYTC Alloy for certified Alloy R41 (UNS N07041 / 2.4973) materials with complete traceability, AMS specifications, technical datasheets, and competitive pricing on standard sizes or custom-forged components.

Email: daisy@zytcsteel.com

WhatsApp/WeChat: +86 17335753350