Titanium 6-2-4-2

6Al-2Sn-4Zr-2Mo

Material Data Sheet

Titanium 6Al-2Sn-4Zr-2Mo, also known as 6-2-4-2, is an alpha-beta Titanium. Primarily used for its combination of tensile strength, creep strength, and toughness, Ti 6-2-4-2 has good creep resistance up to 550°C and up to 0.1% Silicon is frequently added to further improve the creep resistance of the alloy. Ti 6-2-4-2 alloy is produced by primary melting under vacuum (VAR), electron beam (EB) melting or plasma arc cold hearth melting (PAM). Primary melting is followed by single or double vacuum arc re-melting (VAR).

The forging and machining characteristics of Ti 6-2-4-2 are similar to those of Ti 6Al-4V and weldability of Ti 6-2-4-2 is fair, using AMS 4952 weld wire. Several different treatments are also available. Ti 6-2-4-2 is capable of being heat-treated to higher strengths in greater section sizes than 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.

Chemical Composition
Element Content %
Titanium, Ti 88.0
Aluminum, Al 6.0
Tin, Sn 2.0
Zirconium, Zr 4.0
Molybdenum, Mo 2.0
Nitrogen, N ≤ 0.5
Iron,Fe ≤0.25
Oxygen, O ≤ 0.15
Hydrogen, H ≤ 0.15
Carbon, C ≤ 0.1
Silicon, Si ≤ 0.06 – 0.1
Physical Properties
Properties Metric Imperial
Density 4.54 g/cm3 0.164 lbs/in3
Melting Point 1588-1716 °C 2890-3120 °F
Mechanical Properties
Properties Metric Imperial
Modulus of Elasticity 16.5 x 103 11.4 x 103
Ultimate Tensile Strength 135 930
Yield Strength(0.2% offset) 135 930
Elongation 8% 8%
Applications
  • Compressor blades
  • Turbine engine components
  • Discs
  • Impellers
  • Afterburner structures
  • Airframe skins
  • Seals
Specifications
  • AMS 4919
  • AMS 4952
  • AMS 4975
  • AMS 4976
  • DIN 3.7164
  • GE B50 TF22
  • GE B50TF21
  • GE B50TF22
  • GE C50TF7
  • MIL F-83142
  • MIL T-81915
  • MIL T-9046
  • MIL T-9047
  • PWA 1220
  • UNS R54620

Key Words: Ti6Al2Sn4Zr2Mo, Ti-6242; Ti-6-2-4-2; UNS R54620

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