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) |
Titanium | 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 | 0.025"-0.062" | 135 | 931 | 125 | 862 | 8 |
Titanium 6Al-2Sn-4Zr-2Mo | 0.062"-1.0" | 135 | 931 | 125 | 862 | 10 |
Titanium 6Al-2Sn-4Zr-2Mo | 1.0"-3.0" | 130 | 896 | 120 | 827 | 10 |
Availability
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.
Specifications
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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