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Titanium Alloys

TC4 / Ti-6Al-4V (ASTM Grade 5)

TC4 / Ti-6Al-4V (ASTM Grade 5) Alpha-Beta Titanium AlloyTC4 is the most widely used α+β titanium alloy in the world, of nominal composition Ti-6Al-4V, corresponding to international ASTM Grade 5

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TC4 / Ti-6Al-4V (ASTM Grade 5)

TC4 / Ti-6Al-4V (ASTM Grade 5) Alpha-Beta Titanium AlloyTC4 is the most widely used α+β titanium alloy in the world, of nominal composition Ti-6Al-4V, corresponding to international ASTM Grade 5

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

TC4 / Ti-6Al-4V (ASTM Grade 5) Alpha-Beta Titanium Alloy

TC4 is the most widely used α+β titanium alloy in the world, of nominal composition Ti-6Al-4V, corresponding to international ASTM Grade 5 / UNS R56400 / AMS 4911 / ISO 5832-3. It combines high specific strength, good fracture toughness, excellent corrosion resistance and proven biocompatibility, and is the benchmark titanium alloy for aerospace, medical, marine and high-performance consumer applications.

Overview

  • Material: TC4 — Ti-6Al-4V α+β titanium alloy
  • International equivalents: ASTM Gr.5 / UNS R56400 / AMS 4911 / ISO 5832-3 (medical)
  • Available forms: Bar, plate, sheet, strip, tube, wire, forgings and fasteners

Chemical Composition (wt%)

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 %.

Physical Properties

PropertyTypical Value
Density4.51 g/cm³
Melting rangeapprox. 1660–1690 °C
Thermal conductivityapprox. 7.95 W/m·K
Coefficient of thermal expansion (0–100 °C)approx. 8.6 ×10-6 /°C
Modulus of elasticityapprox. 110 GPa
Poisson's ratio0.34

Mechanical Properties

ConditionTensile strengthYield strengthElongationReduction of area
Annealed (room temp.)≥ 895 MPa≥ 825 MPa≥ 10 %≥ 25 %
At 400 °C≥ 585 MPa≥ 490 MPa——
Rupture strength (100 h, 400 °C)≥ 440 MPa—

Key Features

  • Excellent all-round properties: high strength combined with good ductility;
  • High specific strength — low density yet high strength, ideal for lightweighting;
  • Strong corrosion resistance against many media;
  • Good hot strength for long-term service at 400 °C;
  • Good cryogenic toughness, retained at low temperature;
  • Excellent biocompatibility for medical implants.

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 to avoid overheating / burning.
  • Cold working: cold rolled and cold drawn; intermediate annealing at approx. 650–700 °C at high cold-reduction levels.
  • Welding: TIG welding after thorough cleaning, with suitable parameters and inert-gas 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: wing spars, fuselage frames, wing panels, engine fan discs and blades, landing-gear components; spacecraft structures and engine parts;
  • Medical: artificial joints, bone-fixation devices and dental implants (per ISO 5832-3 / ASTM F136 where applicable);
  • Chemical: reaction towers, heat exchangers, piping and valves;
  • Sports & consumer: high-end bicycle frames, tennis rackets and golf-club components;
  • Marine: vessel and offshore-platform structures and seawater piping systems.

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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