AMS Titanium Alloy 6-2-4-2 (6Al-2Sn-4Zr-2Mo) Bar and Rod

1.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.
2.Size: Φ7mm~Φ230mm;

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Product Details

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 resistance. This alloy is used in the intermediate compressor stages of turbine engines for disks and blades, seals and for airframe parts.

Standard Specification:

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-9047 6Al-2Sn-4Zr-2Mo bar;

MIL-T-9047 6Al-2Sn-4Zr-2Mo bar;

Standard	Werkstoff No.	UNS
Titanium Alloy 6-2-4-2 /6Al-2Sn-4Zr-2Mo	3.7144	R54620

Technical Data Sheet

Chemical Composition

Weight %

Other

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

Balance

5.5~6.5

3.6~4.4

1.8~2.2

0.05

0.25

0.04

0.15

0.0150

0.3Total Max.

Typical Mechanical Properties (Tensile Requirements)

Material	Tensile Strength, min		Yield Strength (0.2% Offset) min or range		Elongation in 4D,min%
Material	ksi	MPa	ksi	MPa	Elongation in 4D,min%
Titanium Alloy 6-2-4-2 /6Al-2Sn-4Zr-2Mo	135	931	125	862	4

AMS Titanium Alloy 6-2-4-2 (6Al-2Sn-4Zr-2Mo) Bar and Rod

Product Details

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