Titanium 6Al-4V

Aging Procedure

Age at 538 C (1000 F) for 4 hours, air cool.

Annealing Procedure

Hold at 732 C(1350 F) between 1/4 and 4 hours, Furnace cool to 566 C(1050 F) then air cool. Furnace cooling is not required for forgings and bars.

Applications

6-4 is widely used in the aircraft industry in a variety of turbine and "hot" structural applications. It is generally employed in applications up to 400 C(750 F).

Cold Workability

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.

Forgeability

Rough forge at 982 C(1800 F), finish at @ 968 C (1750 C).

Formability

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.

Heat Treatability

Solution treat at 904-954 C(1660-1750 F) for 2 hours followed by water quench.

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) 1830

Principle Design Features

This alpha-beta grade is the most widely available and heavily used of all the titanium grades. The alloy is heat treatable and combines excellent strength and corrosion resistance with weld and fabricability. Beta Transus (F +/- 25) 1830.

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

Powder

Powder

Ring

Ring

Rod

Rod

Round Bar

Round Bar

Round Tube

Round Tube

Sheet

Sheet

Specialty Form

Specialty Form

Square Bar

Square Bar

Strip

Strip

Wire Round

Wire Round

Additional Data

Specifications

4905,4906,4911,4920,4928,4930,4934,4935,4954,4965,4967,B265,B348,B381,3.7164,1570,C50TF12,F-83142,T-81556,T-81915,T-9046,T-9047,M618,R56400

Chemical Elements

Aluminum5.5 - 6.75
Carbon0.08 max
Hydrogen0.015 max
Iron0.25 max
Nitrogen0.05 max
Oxygen0.2 max
TitaniumBalance
Vanadium3.5 - 4.5

Physical Properties

Density: 0.16lb/in³Density

Electrical Resistivity: 171µΩ·cmElectrical Resistivity

Melting Point: 3200°FMelting Point

Specific Gravity: 4.43Specific Gravity

Specific Heat: 0.135BTU/lb·°FSpecific Heat

Mechanical Properties

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

Reduction of Area: 25%Reduction of Area

Thermal Conductivity: 0.325BTU/hr·ft·°FThermal Conductivity

Thermal Expansion

ConditionMinMaxExpansion Coefficient
Annealed32 °F212 °F5 μin/in·°F
Annealed32 °F600 °F5.3 μin/in·°F
Annealed32 °F1000 °F5.6 μin/in·°F
Annealed32 °F1200 °F5.9 μin/in·°F
Annealed32 °F1500 °F6.1 μin/in·°F

Mechanical Test Data

FormSheet
ConditionSolution Annealed & Aged
Temperature70°F
Elongation10%
Reduction of Area25%
Tensile Strength130 KSI
Yield Strength120 KSI