TIMET TIMETAL® 10-2-3 Titanium Alloy (Ti-10V-2Fe-3Al), Aged Billet/Bar per ASTM 4984

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TIMET TIMETAL® 10-2-3 Titanium Alloy (Ti-10V-2Fe-3Al), Aged Billet/Bar per ASTM 4984
Categories:	Metal; Nonferrous Metal; Titanium Alloy; Beta Titanium Alloy
Material Notes:	High-Strength Forging Alloy. Mechanical property data reported per ASTM 4984 after solution treatment and aging 900°-950°F (482°-510°C) then air cool. Industry Specifications: USA Aerospace: AMS 4984. 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, Typical
Tensile Strength, Yield, Typical
Elongation at Break, Typical
Modulus of Elasticity, Typical
Tensile Modulus
Tensile Modulus
Compressive Yield Strength
Compressive Modulus
Ultimate Bearing Strength, e/D = 1.5
Ultimate Bearing Strength, e/D = 2.0
Bearing Yield Strength, e/D = 1.5
Bearing Yield Strength, e/D = 2.0
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
Shear Strength
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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