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

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Titanium 6-6-2


Availability

Titanium 6-6-2 is stocked by 6 North American distributors and produced by 14 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 5 distributors but is also available to a lesser extent in Bar Products, Wire Products, Fasteners, Forging Products, Shapes, and Tubular Products.

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Specifications

The following specifications cover Titanium 6-6-2

  • AMS 4918
  • AMS 4936
  • AMS 4971
  • AMS 4978
  • AMS 4979
  • DMS 1870
  • DMS 1887
  • MIL F-83142
  • MIL T-81556
  • MIL T-9046
  • MIL T-9047
  • UNS R56620

Property Results

Related Metals:


Chemistry Data : [top]

Aluminum

5 - 6

Carbon

0.05 max

Copper

0.35 - 1

Hydrogen 2

0.015 max

Iron

0.35 - 1

Nitrogen

0.04 max

Oxygen

0.2 max

Tin

1.5 - 2.5

Titanium

Balance

Vanadium

5 - 6


Principal Design Features This alpha-beta alloy can be heat treated to higher strengths and heavier section sizes than alloy 6AL-4V. It combines excellent strength, corrosion resistance and moderately good fabricability. Beta Transus (F +/- 25) 1735.

Applications Used primarily in plate and forging applications for airframe sections, rocket cases and ordnance 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 may be hot or cold formed. Popular methods include hydropress, stretch or drop-hammer. This material responds similarly to 300 series stainless steels.

Welding Beta Transus (F +/- 25) 1735

Heat Treatment Solution treat at 843-913 C(1550-1675 F) for 1 hour and water cool.

Forging Rough at 932 C(1710 F), finish at 843 C(1550 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 material are similar to those of 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 required to re-attain optimum performance characteristics.

Annealing Hold at 704 C(1300 F) for 2 hours, air cool. For stress relieving, hold at 593 C(1100 F) for 2 hours and air cool.

Aging Age at 538-621 C(1000-1150 F) for 4-8 hours and air cool.

Other Physical Props Beta Transus (F +/- 25) 1735

Physical Data : [top]

Density (lb / cu. in.) 0.164
Specific Heat (Btu/lb/Deg F - [32-212 Deg F]) 0.155
Electrical Resistivity (microhm-cm (at 68 Deg F)) 157
Melting Point (Deg F) 3100
Thermal Conductivity 4.2
Modulus of Elasticity Tension 16.5
Reduction of Area 20


Mechanical Data : [top]

Form

Sheet

Condition

Solution Annealed & Aged

Temper

70

Tensile Strength

150

Yield Strength

140

Elongation

10

Reduction of Area

20


Form

Sheet

Condition

Test Specimen Annealed

Temper

70


Form

Sheet

Condition

Test Specimen Annealed

Temper

400

Tensile Strength

145

Yield Strength

127


Form

Sheet

Condition

Test Specimen Annealed

Temper

600

Tensile Strength

135

Yield Strength

117



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