Haynes® R-41 alloy, 1.27 mm thick sheet, solution heat treated at 1079°C, water quenched, 30 minutes at 1066°C, air cooled, aged 16 hours at 760°C (1400°F), tested at 649°C (1200°F)
Subcategory: Superalloy; Nickel Base
Key Words: UNS N07041, AMS 5545, AMS 5712
Material Notes: Nickel content as balance. Vacuum melted, exceptionally high strength at temperature between 649-982°C. Precipitation-hardening type, strength developed by various solutioning and aging heat treatments. Applications include afterburner parts and nozzle diaphragm partitions in current gas turbine engines. Formed with success on drop-hammers, expanding mandrels and stretch formers. Data provided by the manufacturer, Haynes International, Inc.
Available Properties |
- Density
- Tensile Strength, Ultimate
- Tensile Strength, Yield
- Modulus of Elasticity
- Modulus of Elasticity at Elevated Temperature
- Poissons Ratio
- Poissons Ratio at Elevated Temperature
- Shear Modulus
- Shear Modulus at Elevated Temperature
- Magnetic Permeability
- CTE, linear 500°C
- CTE, linear 1000°C
- Specific Heat Capacity
- Thermal Conductivity at Elevated Temperature
- Melting Point
- Solidus
- Liquidus
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Property Data |
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