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alloy 301 super alloy material property data sheet - product availability and request a quote

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Super Alloy Alloy 301


Availability

Super Alloy Alloy 301 is stocked by 1 North American distributors and produced by 2 large mills. Distributors will offer small quantity buys while mills will generally only sell large quantities, with delivery times anywhere from 10 to 50 weeks depending on size and form required

This material is stocked primarily in Wire Products by 1 distributors.

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Specifications

The following specifications cover Super Alloy Alloy 301

No Specifications.


Property Results

Related Metals:


Chemistry Data : [top]

Aluminum

4 - 4.75

Carbon

0.3 max

Copper

0.25 max

Iron

0.6 max

Manganese

0.5 max

Nickel

Balance

Silicon

1 max

Sulphur

0.01 max

Titanium

0.25 - 1


Principal Design Features This is an age-hardenable alloy, similar to Nickel 200 but with greater strength and hardness.

Applications Applications include electrical conductivity parts, such as springs, parts that need good thermal conductivity and good fatigue strength.

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.

Forming Formability by conventional means is good. Cold working does strengthen (harden) the alloy.

Welding 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.

Heat Treatment 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.

Forging The alloy may be forged in the range of 2250 F to 1900 F.

Hot Working Hot work in the temperature range of 2150 F to 1600 F.

Cold Working 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.

Annealing Anneal art 1700 F for 5 minutes at temperature and rapid cool.

Aging See "Heat Treat".

Hardening Hardens by cold working or aging - see "Heat Treat".

Physical Data : [top]

Density (lb / cu. in.) 0.296
Specific Gravity 8.26
Specific Heat (Btu/lb/Deg F - [32-212 Deg F]) 0.104
Electrical Resistivity (microhm-cm (at 68 Deg F)) 255
Melting Point (Deg F) 2600
Poissons Ratio 0.3
Thermal Conductivity 280
Mean Coeff Thermal Expansion 7.2
Modulus of Elasticity Tension 30


Mechanical Data : [top]

Form

Strip

Condition

Test Specimen Annealed

Temper

70

Tensile Strength

105

Yield Strength

47

Elongation

40

Rockwell

B85



Videos :

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