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 982°C

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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 982°C

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

Property Data

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