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Titanium 3Al-8V-6Cr-4Mo-4Zr

Annealing Procedure
Heat to 704 C (1300 F),hold for 2 hours follow by air cooling. For intermediate stress relieving, heat to 482-538 C(900-1000 F) and hold for 45 minutes.
Applications
Commonly employed in a variety of spring and fastener applications. Also found in tubulars in oil and gas wells.
Cold Workability
The cold work characteristics of this material is similar to that of a moderately tempered austenitic stainless steel. In multiple cold forming operations, intermediate stress relief is recommended to prevent tearing or other material damage. Post-work annealing is required to reattain optimum performance characteristics.
Forgeability
Rough work can be performed at 900 C (1650 F), while finishing operations should be performed at 843 C (1550 F).
Formability
May be hot or cold formed using hydropress, power brake, stretch or drop hammer methods. Similar in characteristics to 300 series stainless steels.
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) 1460
Principle Design Features
This beta alloy is similar in performance to 13-11-3, but is easier to melt. It is mainly available in bar and wire forms. Beta Transus (F +/- 25) 1460

Known Forms

Bar-Hollow
Flat Bar
Forgings-Discs
Hexagon Bar
Open Die Forgings
Pipe-Seamless
Pipe-Welded
Plate
Round Bar
Sheet
Square Bar
Strip
Tube-Round (Seamless)
Tube-Round (Welded)
Wire-Flat
Wire-Round
Wire-Welding
Billet
Coil
Contour Rings
Mandrel Rings
Shafts
Shapes-Extruded
Welded Rings

Additional Data

Specifications

R58640

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Chemical Elements

Aluminum3 - 4
Carbon0.05 max
Chromium5.5 - 6.5
Iron0.03 max
Molybdenum3.5 - 4.5
Nitrogen0.03 max
Oxygen0.14 max
TitaniumBalance
Vanadium7.5 - 8.5
Zirconium3.5 - 4.5

Physical Properties

Density: 0.174lb/in³
Melting Point: 3000°F
Specific Heat: 0.125BTU/lb·°F

Mechanical Properties

Modulus of Elasticity – Tension: 15MSI

Thermal Expansion

ConditionMinMaxExpansion Coefficient
Annealed32 °F212 °F4.9 µin/in/°F
Annealed32 °F600 °F5.2 µin/in/°F
Annealed32 °F1000 °F5.4 µin/in/°F

Rupture Test Data

ConditionFormTemperatureTimeRupture Strength
Test Specimen AnnealedSheet600 °F100 Hours140 KSI

Creep Test Data

ConditionFormTemperatureTimeApplied StressCreep Strain
Test Specimen AnnealedSheet600 °F100 Hours0.2 %100 mil/in

Mechanical Test Data

FormSheet
ConditionHeat treated 1600F 1 Hr AC+ 925 F 8 Hrs
Measurement Temperature70°F
Elongation6%
Tensile Strength180KSI
Yield Strength170KSI
FormPlate
ConditionHeat treated 1600F 1 Hr AC+ 925 F 8 Hrs
Measurement Temperature70°F
Elongation8%
Tensile Strength180KSI
Yield Strength170KSI
FormSheet
ConditionSolution Annealed & Aged
Measurement Temperature70°F
Elongation6%
Tensile Strength170KSI
Yield Strength160KSI
FormSheet
ConditionTest Specimen Annealed
Measurement Temperature70°F
FormSheet
ConditionTest Specimen Annealed
Measurement Temperature600°F
FormSheet
ConditionTest Specimen Annealed
Measurement Temperature800°F
Elongation10%
Tensile Strength145KSI
Yield Strength125KSI
FormSheet
ConditionTest Specimen Annealed
Measurement Temperature1000°F
Tensile Strength125KSI
Yield Strength110KSI
Periodic Table
Pipe Sizes
Hardness Conversion
Sheet Gauges
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