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Titanium Alloys

TC6 (Ti-6Al-2.5Mo-2Cr)

TC6 (Ti-6Al-2.5Mo-2Cr) Alpha-Beta Titanium AlloyTC6 is a Chinese α+β two-phase titanium alloy of nominal composition Ti-6Al-2.5Mo-2Cr (with Si), broadly comparable to the Russian BT3-1 family. It

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TC6 (Ti-6Al-2.5Mo-2Cr)

TC6 (Ti-6Al-2.5Mo-2Cr) Alpha-Beta Titanium AlloyTC6 is a Chinese α+β two-phase titanium alloy of nominal composition Ti-6Al-2.5Mo-2Cr (with Si), broadly comparable to the Russian BT3-1 family. It

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

TC6 (Ti-6Al-2.5Mo-2Cr) Alpha-Beta Titanium Alloy

TC6 is a Chinese α+β two-phase titanium alloy of nominal composition Ti-6Al-2.5Mo-2Cr (with Si), broadly comparable to the Russian BT3-1 family. It offers high strength, good hot strength for long-term service at 400–450 °C and good oxidation resistance, and is used mainly for aero-engine discs / blades and highly stressed aircraft structures.

Overview

  • Material: TC6 — Ti-6Al-2.5Mo-2Cr-Si α+β titanium alloy
  • Nominal composition: Ti-6Al-2.5Mo-2Cr-Si (approx. BT3-1-type)
  • Available forms: Bar, plate, forgings and custom profiles

Chemical Composition (wt%)

ElementTiAlMoCrFeSiCNHO
Content Bal.5.5–7.02.0–3.00.8–2.30.2–0.70.15–0.40≤ 0.10≤ 0.05≤ 0.015≤ 0.18

Physical Properties

PropertyTypical Value
Densityapprox. 4.50 g/cm³
Electrical resistivity (room temp.)approx. 1.36 μΩ·m (appears high for titanium — verify)
α/β transus960–1000 °C
OxidationA thin protective oxide forms after long exposure at 400 °C; oxidation becomes severe above 550 °C

Mechanical Properties

ConditionTensile strengthYield strengthElongationReduction of area
Annealed (room temp.)≥ 980 MPa≥ 840 MPa≥ 10 %≥ 25 %
At 400 °C≥ 685 MPa≥ 590 MPa——
Rupture strength (100 h, 400 °C)≥ 540 MPa—

Key Features

  • Good all-round mechanical properties: high strength and reasonable ductility;
  • Good hot strength for long-term service at 400–450 °C;
  • Corrosion resistance better than stainless steel in most environments;
  • Reasonable oxidation resistance within its service range.

Fabrication & Heat Treatment

  • Melting: vacuum arc remelting (VAR) for uniform composition and quality.
  • Hot working: forged, rolled or extruded at 850–1050 °C with controlled heating.
  • Cold working: moderate cold ductility; cold rolled and cold drawn with intermediate annealing at approx. 650–750 °C.
  • Welding: TIG and electron-beam welding are possible, but as a highly alloyed α+β alloy it is sensitive to the weld thermal cycle; post-weld heat treatment is required to restore the weld and HAZ properties.
  • Standard annealing: 800–850 °C for 1–2 h, air cool.
  • Double annealing: 950–1000 °C for 1–2 h air cool, then 550–600 °C for 4–6 h air cool, for best balance.
  • Solution treatment & ageing: solution treat at 950–1000 °C then rapid cool; age at 500–550 °C to raise strength.

Typical Applications

  • Aerospace: aero-engine blades, turbine discs, compressor discs and blades; airframe bulkheads, joints, load-bearing clamps, actuator cylinders and tail rods;
  • Chemical: reactors, piping and columns for high-temperature, high-pressure, highly corrosive service.

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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