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6-2-2-2-2-.25 titanium material property data sheet - product availability and request a quote

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Metal Suppliers Online: Material Property Data

Titanium 6-2-2-2-2-.25


Availability

Titanium 6-2-2-2-2-.25 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 Forging Products.

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Specifications

The following specifications cover Titanium 6-2-2-2-2-.25

No Specifications.


Property Results

Related Metals:


Chemistry Data : [top]

Aluminum

5.25 - 6.25

Carbon

0.05 max

Chromium

1.75 - 2.25

Hydrogen

0.0125 max

Iron

0.25 max

Molybdenum

1.75 - 2.25

Nitrogen

0.03 max

Oxygen

0.14 max

Silicon

0.2 - 0.3

Tin

1.75 - 2.25

Titanium

Balance

Zirconium

1.75 - 2.25


Principal Design Features This is an alpha-beta alloy generally selected for its high strength, fracture toughness and intermediate creep strength. Not generally available at the distributor level, it is widely available from producers in bar, billet, sheet and plate. Beta Transus (F +/- 25) 1780

Applications Typical applications include airframe and jet engine 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 Hot forming will reduce both the springback and required forming forces, and will increase the overall ductility of the material.

Welding Rated as" limited" in terms of weldability.

Forging Rough forge at 1650-1750 F, finish at 1600-1700 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 Soak at 1300-1500 F for 2 hours, air cool.

Other Comments

Other Physical Props Beta Transus (F +/- 25) 1780

Physical Data : [top]

Density (lb / cu. in.) 0.165
Modulus of Elasticity Tension 17.7


Mechanical Data : [top]

Form

Sheet

Condition

Solution Annealed & Aged

Temper

70

Tensile Strength

170

Yield Strength

160

Elongation

12

Reduction of Area

20


Form

Sheet

Condition

Test Specimen Annealed

Temper

70

Sharpy

12


Form

Sheet

Condition

Test Specimen Annealed

Temper

400

Tensile Strength

145

Yield Strength

117

Elongation

19

Reduction of Area

33


Form

Sheet

Condition

Test Specimen Annealed

Temper

600

Tensile Strength

140

Yield Strength

107

Elongation

20

Reduction of Area

35


Form

Sheet

Condition

Test Specimen Annealed

Temper

800

Tensile Strength

130

Yield Strength

102

Elongation

21

Reduction of Area

40



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