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Rulon Bearings
TIMET TIMETAL® 10-2-3 Titanium Alloy (Ti-10V-2Fe-3Al), Solution Treated and Aged 950°F (510°C)
Categories: Metal; Nonferrous Metal; Titanium Alloy; Beta Titanium Alloy

Material Notes: High-Strength Forging Alloy. Mechanical property data after solution treatment and aging 950°F (510°C) for 8 hours then air cool.

Features: A readily forgeable alloy that offers excellent combinations of strength, ductility, fracture toughness and high cycle fatigue strength. Typically used for critical aircraft structures, such as landing gear, actuators, flap tracks, and rotor heads.

Typical heat treatment for this alloy: Solution heat treat: 28-56°C below beta transus for a minimum for 30 mins, then water quench. Age then air cool.

Data provided by TIMET.

Available Properties
  • Density, Typical
  • Tensile Strength, Ultimate
  • Tensile Strength, Ultimate
  • Tensile Strength, Ultimate
  • Tensile Strength, Yield
  • Tensile Strength, Yield
  • Tensile Strength, Yield
  • Elongation at Break, in 2"
  • Elongation at Break, in 2"
  • Elongation at Break, in 2"
  • Reduction of Area
  • Reduction of Area
  • Reduction of Area
  • Tensile Modulus
  • Tensile Modulus
  • Tensile Modulus
  • Compressive Modulus
  • Poissons Ratio
  • Fatigue Strength, Limit; test specifics not reported
  • Fatigue Strength, Notched (Kt = 3); Stress Ratio = 0.1; Axial Loading;
  • Fatigue Strength, Smooth (Kt = 1); Stress Ratio = 0.1; Axial Loading
  • Fracture Toughness, ST then Aged 8 hrs
  • Shear Modulus
  • CTE, linear
  • Beta Transus
  • Aluminum, Al
  • Carbon, C
  • Hydrogen, H
  • Iron, Fe
  • Nitrogen, N
  • Other, each
  • Other, total
  • Oxygen, O
  • Titanium, Ti, Calculated as remainder
  • Vanadium, V
Property Data

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Ensinger PEI
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