Titanium 6-2-4-2

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Aging Procedure

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

Annealing Procedure

For duplex annealing, hold at 900 C(1670 F) for 1/2 hour, air cool to 788 C(1465 F) and air cool. For beta anneal, hold at 1024 C(1900 F) for 1/2 hour, air cool to 593 C(1100 F) for 8 hours and air cool.

Applications

Most commonly found in gas turbine compressor components, such as blades, discs and impellers. It is also used for sheet metal components in afterburners and "hot" airframe sections.

Cold Workability

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.

Forgeability

Rough forge at 1038-1066 C(1929-1980 F), finish at 954-982 C(1770-1825 F).

Formability

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.

Heat Treatability

Beta minus 14 C(25 F).

Hot Workability

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

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.

Other Physical Properties

Beta Transus (F +/- 25) 1820

Principle Design Features

This near alpha alloy is designed primarily for high temperature applications (up to 538 C). It combines excellent strength and corrosion resistance with relatively good weld and fabricability. Beta Transus (F +/- 25) 1820.

Weldability

Rated as "fair" in terms of weldability.

Known Forms

Billet

Billet

Coil

Coil

Disc

Disc

Flat Bar

Flat Bar

Foil

Foil

Hollow Bar

Hollow Bar

Ingot

Ingot

Pipe

Pipe

Plate

Plate

Ring

Ring

Rod

Rod

Round Bar

Round Bar

Round Tube

Round Tube

Sheet

Sheet

Square Bar

Square Bar

Strip

Strip

Additional Data

Specifications

4919,4952,4975,4976,3.7164,B50 TF22,B50TF21,B50TF22,C50TF7,F-83142,T-81915,T-9046,T-9047,1220,R54620

Chemical Elements

Aluminum5.5 - 6.5
Carbon0.1 max
Hydrogen 20.15 max
Iron0.25 max
Molybdenum1.8 - 2.2
Nitrogen0.5 max
Oxygen 20.15 max
Silicon0.06 - 0.1
Tin1.8 - 2.2
TitaniumBalance
Zirconium3.6 - 4.4

Physical Properties

Density: 0.164lb/in³Density

Electrical Resistivity: 171µΩ·cmElectrical Resistivity

Melting Point: 3100°FMelting Point

Specific Gravity: 4.54Specific Gravity

Mechanical Properties

Modulus of Elasticity – Tension: 16.5MSIModulus of Elasticity – Tension

Reduction of Area: 25%Reduction of Area

Thermal Expansion

ConditionMinMaxExpansion Coefficient
Annealed32 °F212 °F4.3 μin/in·°F
Annealed32 °F600 °F4.5 μin/in·°F
Annealed32 °F1000 °F4.5 μin/in·°F
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