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

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Metal Suppliers Online: Material Property Data

Titanium 6-2-4-6


Availability

Titanium 6-2-4-6 is stocked by 9 North American distributors and produced by 7 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 5 distributors but is also available to a lesser extent in Flat Rolled Products, Forging Products, Tubular Products, Wire Products, and Fasteners.

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Specifications

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

  • AMS 4981
  • DIN 3.7164
  • MIL T-9046
  • PWA 1222
  • PWA 1223
  • PWA 1224
  • PWA 1225
  • UNS R56260

Property Results

Related Metals:


Chemistry Data : [top]

Aluminum

5.5 - 6.5

Carbon

0.04 max

Hydrogen

0.0125 max

Iron

0.15 max

Molybdenum

5.5 - 6.5

Nitrogen

0.04 max

Oxygen

0.15 max

Tin

1.75 - 2.25

Titanium

Balance

Zirconium

3.5 - 4.5


Principal Design Features This is a heat treatable, alpha-beta alloy which was designed primarily for high temperature applications requiring higher strength than alloy 6-2-4-2 at similar temperatures. It combines good corrosion resistance and strength with weldability and fabricability. The alloy is generally available at the mill level in bar and billet form.

Applications Generally selected over 6-2-4-2 for applications requiring strength at temperatures up to 454 C(850 F). Found in gas turbine discs and impellers and has been evaluated for use in deep sour well applications.

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" limited" in terms of weldability.

Heat Treatment Solution treat at 843-913 C(1550-1675 F), air, oil or water quench.

Forging Work at 843-927 C(1565-1725 F) from bar and billet.

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 Triplex-Beta minus 14 C(25 F), 1-2 hours, air cool, plus 801-857 C(1490-1595 F), 1-4 hours, air cool plus 593 C(1100 F) 4-8 hours, air cool. For stress relief, heat to 482-649 C(900-1200 F), hold for 1-4 hours and air cool.

Aging Hold at 579-607 C(1075-1125 F) for 8 hours and air cool.

Other Physical Props Beta Transus (F+/- 25) 1710

Physical Data : [top]

Density (lb / cu. in.) 0.169
Specific Gravity 4.65
Melting Point (Deg F) 1635
Thermal Conductivity 4.1
Modulus of Elasticity Tension 16


Mechanical Data : [top]

Form

Sheet

Condition

Solution Annealed & Aged

Temper

70

Tensile Strength

170

Yield Strength

160

Elongation

10

Reduction of Area

20


Form

Sheet

Condition

Test Specimen Annealed

Temper

600

Tensile Strength

150

Yield Strength

125

Elongation

10

Reduction of Area

30


Form

Sheet

Condition

Test Specimen Annealed

Temper

800

Tensile Strength

140

Yield Strength

110

Elongation

10

Reduction of Area

30


Form

Sheet

Condition

Test Specimen Annealed

Temper

900


Form

Sheet

Condition

Test Specimen Annealed

Temper

1000

Tensile Strength

125

Yield Strength

95

Elongation

15

Reduction of Area

50



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