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Titanium Alloys

TC12

TC12 Alpha-Beta Titanium AlloyTC12 is a Chinese high-zirconium α+β titanium alloy. After solution treatment and ageing it reaches high strength (≥ 1100 MPa) with good ductility and heat resistanc

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TC12

TC12 Alpha-Beta Titanium AlloyTC12 is a Chinese high-zirconium α+β titanium alloy. After solution treatment and ageing it reaches high strength (≥ 1100 MPa) with good ductility and heat resistanc

  • Bars
  • Plates
  • Tubes
  • Forgings
  • Wires
  • strips
  • Special Shapes

TC12 Alpha-Beta Titanium Alloy

TC12 is a Chinese high-zirconium α+β titanium alloy. After solution treatment and ageing it reaches high strength (≥ 1100 MPa) with good ductility and heat resistance up to about 450 °C, used for high-load aerospace structures, engine components and corrosion-resistant equipment.

Overview

  • Material: TC12 — high-Zr α+β titanium alloy
  • Nominal composition: Ti-(5.5–7.0)Al-(0.8–2.0)Mn-(0.8–2.0)Cr-(4.0–6.0)Zr-B (trace)
  • Available forms: Bar, plate, forgings and custom profiles

Chemical Composition (wt%)

ElementTiAlMnCrZrB
Content Bal.5.5–7.00.8–2.00.8–2.04.0–6.0trace

Fe / C / N / H / O limits are not stated on the source page — to be confirmed from the mill certificate.

Physical Properties

PropertyTypical Value
Densityapprox. 4.55 g/cm³
Melting range1660–1670 °C
Thermal conductivityapprox. 7 W/m·K
Modulus of elasticityapprox. 110 GPa

Mechanical Properties (heat treated)

PropertyTypical Value
Tensile strength≥ 1100 MPa
Yield strength≥ 1000 MPa
Elongation≥ 10 %
Reduction of area≥ 25 %
HardnessHRC 30–40

Key Features

  • High specific strength and hardness with lightweight design;
  • Good heat resistance, stable service at 450 °C;
  • Good corrosion resistance, especially in aerospace environments;
  • Can be formed into required shapes by various processes.

Fabrication & Heat Treatment

  • Machining: due to high hardness and wear resistance, use carbide or PCD tools at low speed with heavy cooling.
  • Welding: moderate weldability; inert-gas-shielded welding recommended.
  • Annealing: 750–800 °C, air or furnace cool, to relieve stress and refine structure.
  • Solution treatment & ageing: solution treat at 950–980 °C, then age at 480–550 °C for 4–8 h to raise strength and hardness.

Typical Applications

  • Aerospace: airframe structures, engine parts and turbine blades;
  • Chemical equipment: corrosion-resistant piping and vessels;
  • Other: high-performance sports equipment and automotive components.

For detailed datasheets, mill certificates (EN 10204 3.1) or inquiries on specific sizes and tolerances, please contact our sales & engineering team.

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