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6-2-4-2-.1 titanium material property data sheet - product availability and request a quote

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Titanium 6-2-4-2-.1


Availability

Titanium 6-2-4-2-.1 is stocked by 2 North American distributors and produced by 6 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 Bar Products by 1 distributors but is also available to a lesser extent in Flat Rolled Products, and Wire Products.

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Specifications

The following specifications cover Titanium 6-2-4-2-.1

  • AMS 4975
  • AMS 4976

Property Results

Chemistry Data : [top]

Aluminum

5.5 - 6.5

Carbon

0.08 max

Hydrogen

0.0125 max

Iron

0.25 max

Molybdenum

1.75 - 2.25

Nitrogen

0.05 max

Oxygen

0.12 max

Silicon

0.1 max

Tin

1.75 - 2.25

Titanium

Balance

Zirconium

3.5 - 4.5


Principal Design Features This near beta alloy is generally intended for high temperature use in environments up to 538 C(1000 F).It is only available at the producer level in bar, billet, sheet and plate. Beta Transus (F +/- 25) 1820.

Applications Typical applications include "hot section" gas turbine components such as discs, impellers, turbines, etc. It is also employed in a variety of sheet metal components such as afterburner cans and hot airframe components.

Machinability As a family, titanium and its alloys have developed a mystique as a nightmare to machine. This is simply not the case. Experienced operators have compared its characteristics to those found in 316 stainless steel. Recommended practice includes high coolant flow(to offset the material's low thermal conductivity), slow speeds and relatively high feed rates. Tooling should be tungsten carbide designations C1-C4 or cobalt type high speed tools.

Forming This alloy can be hot or cold formed and will exhibit characteristics equivalent to those found in a 1/8 to 1/4 hard austenitic stainless steel.

Welding Rated as "fair in terms of weldability.

Heat Treatment Solution treat at beta minus 14 C(25 F).

Forging Rough forge at 1038-1066 C(1930-1980 F), finish at 954-982 C(1770-1825 F).

Hot Working Hot forming will reduce both the springback and required forming forces, and will increase the overall ductility of the material.

Cold Working The cold working characteristics of this alloy are similar to those found in austenitic stainless steels. In multiple forming operations, intermediate stress relieving is recommended to offset the alloy's tendency to work harden. Post-work annealing is recommended to reattain maximum performance characteristics.

Annealing Duplex anneal at 900 C(1670 F) for 1/2 hour, air cool to 788 C(1465 F) for 1/4 hour, air cool. Beta anneal at 1024 C(1900 F) for 1/2-1 hour, air cool to 593 C(1100 F), hold for 8 hours and air cool.

Aging Hold at 538-593 C(1000-1100 F) for 8 hours, air cool.

Other Physical Props Beta Transus (F +/- 25) 1820

Physical Data : [top]

Density (lb / cu. in.) 0.164
Specific Gravity 4.54
Electrical Resistivity (microhm-cm (at 68 Deg F)) 191
Melting Point (Deg F) 3100
Modulus of Elasticity Tension 16.5
Reduction of Area 25


Mechanical Data : [top]

Form

Sheet

Condition

Test Specimen Annealed

Temper

70

Tensile Strength

130

Yield Strength

120

Elongation

10

Reduction of Area

25


Form

Sheet

Condition

Test Specimen Annealed

Temper

600

Tensile Strength

95

Yield Strength

75

Elongation

15

Reduction of Area

40


Form

Sheet

Condition

Test Specimen Annealed

Temper

800

Tensile Strength

85

Yield Strength

70

Elongation

20

Reduction of Area

55


Form

Sheet

Condition

Test Specimen Annealed

Temper

1000

Tensile Strength

75

Yield Strength

60

Elongation

25

Reduction of Area

65



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