Titanium Alloy 6-2-4-2 /6Al-2Sn-4Zr-2Mo

Technical Data Sheet

Titanium 6-2-4-2 (6Al-2Sn-4Zr-2Mo) is an alpha-beta titanium alloy capable of being heat treated to higher strengths in greater section sizes that 6Al-4V. Widely used in forged components, 6-2-4-2 beta forged material has enhanced strength, ductility and a combination of good low-cycle fatigue and fatigue-crack growth resitance. This alloy is used in the intermediate compressor stages of turbine engines for disks and blades, seals and for airframe parts.

Chemical Composition Limits
Weight % Al Sn Zr Mo Fe C N H O Others (total)
5.5-6.5 1.8-2.2 3.6-4.4 1.8-2.2 0.25 0.05 0.04 0.015 0.15 0.30

Typical Mechanical Properties

Material Thickness Tensile Strength min Yield Strength min Elongation in 4D (%)
ksi Mpa ksi Mpa
Titanium 6Al-2Sn-4Zr-2Mo
Sheet (duplex annealed) Room temp
0.025"-0.062" 135 931 125 862 8
Titanium 6Al-2Sn-4Zr-2Mo
Sheet (duplex annealed) Room temp
0.062"-1.0" 135 931 125 862 10
Titanium 6Al-2Sn-4Zr-2Mo
Sheet (duplex annealed) Room temp
1.0"-3.0" 130 896 120 827 10

Titanium 6Al-2Sn-4Zr-2Mo is available in sheet, strip, plate, bar and forgings. For all stock and size availability of Titanium 6Al-2Sn-4Zr-2Mo contact Sales.

AMS 4919 sheet, strip, plate (duplex annealed)
AMS 4975 bars, wire, rings (solution and precipitation heat treated)
AMS 4981 bars, wire, forgings (solution and precipitation heat treated)
AMS 6905 bars, wire, forgings (duplex annealed
AMS-T-9046 AB4 sheet, strip, plate
AMS-T-9047 6Al-2Sn-4Zr-2Mo bar
MIL-T-9046J AB-4 sheet, strip, plate
MIL-T-9047 6Al-2Sn-4Zr-2Mo bar
MIL-T-9046H Type III Comp G sheet, strip, plate
TA18 (w/drawn)
TA19 (w/drawn)
TA20 (w/drawn)
TA25 (w/drawn)
TA26 (w/drawn)
TA27 (w/drawn)

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Every effort is made to ensure that technical specifications are accurate. However, technical specifications included herein should be used as a guideline only. All specifications are subject to change without notice.