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Super Alloy Duranickel (tm)

Aging Procedure
See "Heat Treat".
Annealing Procedure
Anneal art 1700 F for 5 minutes at temperature and rapid cool.
Applications
Applications include electrical conductivity parts, such as springs, parts that need good thermal conductivity and good fatigue strength.
Cold Workability
Cold working is readily accomplished by conventional means. The alloy does work harden and, depending upon the amount of cold work, it may be necessary to give the part an intermediate anneal to complete working.
Forgeability
The alloy may be forged in the range of 2250 F to 1900 F.
Formability
Formability by conventional means is good. Cold working does strengthen (harden) the alloy.
Hardening Procedure
Hardens by cold working or aging - see "Heat Treat".
Heat Treatability
Anneal at 1700 F for approximately 5 minutes at temperature and rapid cool or water quench. Age-hardening is accomplished at 1090 F for 16 hours and furnace cool to 900 F at a slow, furnace cooled, rate of less than 15 degrees per hour. Cooling rate after 900 F is not critical -- furnace cooling or rapid cooling may be used.
Hot Workability
Hot work in the temperature range of 2150 F to 1600 F.
Machinability
The alloy may be readily machined by conventional methods. It is not as "gummy" as Nickel 200, but because of the aluminum content it tends to be abrasive to cutting tools. Machining this alloy in the cold worked or age-hardened condition is easier than in the soft annealed condition. High-speed-steel cutting tools with a high positive rake angle should be used.
Principle Design Features
This is an age-hardenable alloy, similar to Nickel 200 but with greater strength and hardness.
Weldability
If welding of this alloy is required it may be done with the ordinary welding techniques. It should be welded while in the annealed condition and then stress-relieved at 1550 F for 1/2 hour. Heating to the 1550 F temperature must be done rapidly to avoid cracking.

Known Forms

Bar-Hollow
Casting-Centrifugal
Flat Bar
Forgings-Discs
Open Die Forgings
Round Bar
Seamless Rolled Rings
Square Bar
Strip
Tube-Round (Welded)
Wire-Flat
Wire-Round
Wire-Shaped
Wire-Square
Coil
Contour Rings
Mandrel Rings
Shafts
Shapes-Extruded

Additional Data

Chemical Elements

Aluminum4 - 4.75
Carbon0.3 max
Copper0.25 max
Iron0.6 max
Manganese0.5 max
NickelBalance
Silicon1 max
Sulphur0.01 max
Titanium0.25 - 1

Physical Properties

Density: 0.296lb/in³
Electrical Resistivity: 255µΩ·cm
Melting Point: 2600°F
Specific Gravity: 8.26
Specific Heat: 0.104BTU/lb·°F
Thermal Conductivity: 23.3333BTU/hr·ft·°F
Thermal Expansion: 7.2µin/in·°F

Mechanical Properties

Modulus of Elasticity – Tension: 30MSI
Poissons Ratio: 0.3

Thermal Conductivity

ConditionTemperatureConductivity
Solution Annealed & Aged70 °F16.5 W/m·K
Solution Annealed & Aged400 °F19.7 W/m·K
Solution Annealed & Aged1000 °F26.6 W/m·K
Solution Annealed & Aged1400 °F30.4 W/m·K
Solution Annealed & Aged2000 °F36 W/m·K

Thermal Expansion

ConditionMinMaxExpansion Coefficient
Solution Annealed & Aged70 °F212 °F7.2 µin/in/°F
Solution Annealed & Aged70 °F392 °F7.5 µin/in/°F
Solution Annealed & Aged70 °F932 °F8.1 µin/in/°F
Solution Annealed & Aged70 °F1600 °F9.1 µin/in/°F

Mechanical Test Data

FormStrip
ConditionTest Specimen Annealed
Measurement Temperature70°F
Elongation40%
Rockwell HardnessB85HRX
Tensile Strength105KSI
Yield Strength47KSI
Periodic Table
Pipe Sizes
Hardness Conversion
Sheet Gauges
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