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Titanium Alloys

TC10

TC10 Alpha-Beta Titanium AlloyTC10 is a Chinese α+β titanium alloy. (Note: the source page lists a Ti-6Al-4V-type composition identical to TC4, which appears to be a copy-paste error — the actual

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TC10

TC10 Alpha-Beta Titanium AlloyTC10 is a Chinese α+β titanium alloy. (Note: the source page lists a Ti-6Al-4V-type composition identical to TC4, which appears to be a copy-paste error — the actual

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

TC10 Alpha-Beta Titanium Alloy

TC10 is a Chinese α+β titanium alloy. (Note: the source page lists a Ti-6Al-4V-type composition identical to TC4, which appears to be a copy-paste error — the actual TC10 grade is a higher-alloyed near-β titanium. Verify composition against the mill certificate before publication.)

Overview

  • Material: TC10 — α+β / near-β titanium alloy
  • Available forms: Bar, plate, sheet, tube, wire and forgings

Chemical Composition (wt%) — PER SOURCE, PLEASE VERIFY

ElementTiAlVFeCNHO
Content Bal.5.5–6.83.5–4.5≤ 0.30≤ 0.10≤ 0.05≤ 0.015≤ 0.20

Other elements: each ≤ 0.10 %, total ≤ 0.40 %. This matches TC4 / Ti-6Al-4V and is likely incorrect for TC10 — replace with actual TC10 (Ti-5Al-4Mo-2Cr-2.5Fe-type) composition.

Physical Properties

PropertyTypical Value
Densityapprox. 4.5 g/cm³
Melting rangeapprox. 1600–1650 °C
Thermal conductivityapprox. 7–10 W/m·K
Coefficient of thermal expansion (20–100 °C)approx. 8.6 ×10-6 /°C
Modulus of elasticityapprox. 110–120 GPa

Mechanical Properties (annealed)

PropertyTypical Value
Tensile strength≥ 900 MPa
Proof strength σr0.2≥ 825 MPa
Elongation (δ5)≥ 10 %
At 400 °C tensile strength≥ 635 MPa
Rupture strength (100 h, 400 °C)≥ 540 MPa

Key Features

  • High strength with good ductility and high specific strength;
  • Strong corrosion resistance against many media;
  • Good hot strength for long-term service at 400 °C;
  • Good cryogenic toughness;
  • Good weldability.

Fabrication & Heat Treatment

  • Melting: vacuum arc remelting (VAR) for uniform composition and low impurities.
  • Hot working: forged, rolled or extruded at 850–1000 °C with controlled heating.
  • Cold working: cold rolled and cold drawn; intermediate annealing at approx. 650–700 °C.
  • Welding: TIG welding after thorough cleaning and with suitable shielding.
  • Annealing: 700–800 °C for 1–2 h, air cool.
  • Solution treatment & ageing: solution treat at 900–950 °C then rapid cool; age at 500–550 °C to raise strength.

Typical Applications

  • Aerospace: spars, frames, wing panels, engine fan discs and blades, landing gear; spacecraft structures and engine parts;
  • Petrochemical: reaction towers, heat exchangers, piping and valves;
  • Shipbuilding: propellers, shafting and seawater piping;
  • Medical: artificial joints and bone-fixation devices.

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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