TIMETAL® 10-2-3 Titanium Alloy (Ti-10V-2Fe-3Al), Aged Billet/Bar per ASTM 4987
Subcategory: Titanium Alloy; Nonferrous Metal; Beta Titanium Alloy
Material Notes: Titanium content above is calculated as the remainder and may not reflect the actual range. High-Strength Forging Alloy. Industry Specifications: USA Aerospace: AMS 4987. 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. Typical heat treatment for this alloy: Solution heat treat: 28-56°C below beta transus for a minimum for 30 mins, then water quench. Aging heat treatment: 482-593°C for 8 hrs, air cool. Data provided by TIMET.
Available Properties |
- Density
- Tensile Strength, Ultimate
- Tensile Strength, Yield
- Elongation at Break
- Reduction of Area
- Modulus of Elasticity
- Compressive Yield Strength
- Ultimate Bearing Strength
- Bearing Yield Strength
- Poissons Ratio
- Fatigue Strength
- Fracture Toughness
- Shear Modulus
- Shear Strength
- CTE, linear 20°C
- Beta Transus
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Property Data |
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