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Super Alloy Invar 36 (Standard Invar)


Availability

Super Alloy Invar 36 (Standard Invar) is stocked by 32 North American distributors and produced by 26 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 Flat Rolled Products by 20 distributors but is also available to a lesser extent in Bar Products, Tubular Products, Wire Products, Forging Products, Casting Products, and Fasteners.

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Specifications

The following specifications cover Super Alloy Invar 36 (Standard Invar)

  • ASTM B388
  • DIN 1.3912
  • MIL I-16598
  • MIL I-23011 Class 7
  • UNS K93600

Property Results

Related Metals:


Chemistry Data : [top]

Carbon

Iron

Balance

Manganese

Nickel

Silicon


Principal Design Features This is one of the controlled expansion alloys. It has an expansion rate roughly 10 % that of standard carbon steels. Also known as Invar 36 or Alloy 36, the only alloy with lower CTE is Super Invar, or Alloy 32-6, but this alloy is extremely rare and is generally only produced by the mill in heat lot quantities. Note: Recent testing has determined that increased hardness will decrease CTE in all temperature ranges in Invar alloys.

Applications Commonly employed in electronic equipment such as radios, laser systems and thermostats.

Machinability This alloy can be machined employing most common methods. It is known to produce "gummy" chips and is best machined at slow speeds with positive and constant feeds.

Forming The alloy is readily formed using most common practices and should not present any unusual problems. For maximum properties, material should be fully annealed after any forming operations.

Welding All common joining techniques can be successfully employed here. When a filler metal is required, it is suggested to use a similar composition alloy, available from the manufacturer.

Forging Heat to 2150 F(1180 C) rapidly and cool rapidly following working. Do not soak at temperature.

Cold Working This alloy can be cold upset and swaged successfully.

Annealing Hold at 1450 F(790 C) 30 minutes for every inch of thickness, followed by air cooling. To obtain maximum dimensional stability, soak at 1500 F(815 C) and water quench. Reheat to 600 F(315 C) for 1 hour and air cool.

Hardening This alloy will not respond to hardening by thermal treatment.

Physical Data : [top]

Density (lb / cu. in.) 0.293
Specific Gravity 8.11
Specific Heat (Btu/lb/Deg F - [32-212 Deg F]) 0.12
Electrical Resistivity (microhm-cm (at 68 Deg F)) 495
Melting Point (Deg F) 2600
Modulus of Elasticity Tension 21


Mechanical Data : [top]

Form

Strip

Condition

Cold Rolled

Temper

70

Tensile Strength

105

Yield Strength

98

Elongation

6

Rockwell

B97


Form

Strip

Condition

Test Specimen Annealed

Temper

70

Tensile Strength

64

Yield Strength

39

Elongation

34

Reduction of Area

65

Rockwell

B69



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