Titanium 10-2-3

10V-2Fe-3Al

Material Data Sheet

Titanium 10-2-3 is a near-beta alloy developed primarily for high-strength applications in the 180 KSI (1241 MPa) UTS range, in order to provide weight savings over steels used in airframe forging applications. Titanium 10-2-3 also possesses the best hot-die forgeability of any commercial titanium alloy and is suitable for near-net-shape forging applications and isothermal forging. It possesses a high strength/toughness combination and is deep-hardenable. The mechanical properties of Titanium 10-2-3 can be adjusted through heat treatment to achieve different strength, plasticity and toughness levels.

This enables Titanium 10-2-3 to meet the requirements of damage tolerant designs with high structural efficiency, solid reliability and decreased manufacturing cost.

Chemical Composition
Chemistry Content %
Titanium, Ti 85.0
Vanadium, V 10.0
Iron, Fe 2.0
Aluminum, Al 3.0
Oxygen, O ≤ 0.13
Carbon, C ≤ 0.05
Nitrogen, N ≤ 0.05
Hydrogen, H ≤ 0.015
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
Tensile Strength, Ultimate 1260 MPa 183000 psi
Tensile Strength, Yield 1170 MPa 170000 psi
Elongation at Break 10% 10%
Modulus of Elasticity 107 GPa 15500 ksi
Compressive Yield Strength 1145 MPa 166000 psi
Ultimate Bearing Strength 1613 MPa 234000 psi
Bearing Yield Strength 1565 MPa 227000 psi
Poisson’s Ratio 0.32 0.32
Fatigue Strength 945 MPa 137000 psi
Fracture Toughness 44 MPa-m½ 40 ksi-in½
Shear Modulus 42.1 GPa 6110 ksi
Shear Strength 669 MPa 97000 psi
Applications
  • Landing Gear
  • Actuators
  • Fittings
  • Flap Tracks
  • Fasteners
  • Rotor Heads
Specifications
  • AMS 4983
  • AMS 4984
  • AMS 4986
  • AMS 4987
  • UNS R56410

Key Words: Ti10-2-3, 10-2-3, ti 10V-2Fe-3Al

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