TIMET TIMETAL® 10-2-3 Titanium Alloy (Ti-10V-2Fe-3Al), Solution Treated and Aged 950°F (510°C)

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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.
Vendors:

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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