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Titanium Alloys

TC17 / Ti-17

TC17 / Ti-17 (Ti-5Al-2Sn-2Zr-4Mo-4Cr) Titanium AlloyTC17 is a Chinese near-β / quasi-β titanium alloy of nominal composition Ti-5Al-2Sn-2Zr-4Mo-4Cr, directly corresponding to the Western Ti-17 (G

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TC17 / Ti-17

TC17 / Ti-17 (Ti-5Al-2Sn-2Zr-4Mo-4Cr) Titanium AlloyTC17 is a Chinese near-β / quasi-β titanium alloy of nominal composition Ti-5Al-2Sn-2Zr-4Mo-4Cr, directly corresponding to the Western Ti-17 (G

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

TC17 / Ti-17 (Ti-5Al-2Sn-2Zr-4Mo-4Cr) Titanium Alloy

TC17 is a Chinese near-β / quasi-β titanium alloy of nominal composition Ti-5Al-2Sn-2Zr-4Mo-4Cr, directly corresponding to the Western Ti-17 (GE) alloy. It offers high strength, excellent fracture toughness, deep hardenability and a wide forging window, and is the standard material for large aero-engine fan and compressor discs up to about 450 °C.

Overview

  • Material: TC17 / Ti-17 — Ti-5Al-2Sn-2Zr-4Mo-4Cr near-β titanium
  • International equivalent: Ti-17 (GE), China GB TC17
  • Available forms: Bar, disc forgings, rings and custom profiles

Chemical Composition (wt%)

ElementTiAlSnZrMoCrFeCNHO
Content Bal.4.5–5.51.5–2.51.5–2.53.5–4.53.5–4.5≤ 0.30≤ 0.10≤ 0.05≤ 0.015≤ 0.15

Other elements: each ≤ 0.10 %, total ≤ 0.40 %.

Physical Properties

PropertyTypical Value
Densityapprox. 4.55 g/cm³
Melting rangeapprox. 1580–1630 °C
Thermal conductivityapprox. 7–9 W/m·K
Coefficient of thermal expansion (20–100 °C)approx. 8.8 ×10-6 /°C
Modulus of elasticityapprox. 110–120 GPa
α/β transus850–900 °C

Mechanical Properties

ConditionTensile strengthYield strengthElongationReduction of area
Annealed (room temp.)≥ 980 MPa≥ 840 MPa≥ 10 %≥ 25 %
At 450 °C≥ 635 MPa≥ 540 MPa——
Rupture strength (100 h, 450 °C)≥ 540 MPa—

Good fracture toughness.

Key Features

  • High strength (UTS > 800 MPa, yield around 700 MPa and above);
  • Excellent fracture toughness in complex stress states;
  • Deep hardenability — suitable for large-section discs;
  • Wide forging window and good hot-work flexibility;
  • Tunable strength / ductility / toughness balance via heat treatment;
  • Good hot strength up to 450 °C.

Fabrication & Heat Treatment

  • Melting: typically triple VAR melting for uniform composition and high purity.
  • Hot working: forged, rolled or extruded at 850–1000 °C; wide forging window.
  • Cold working: moderate cold ductility; intermediate annealing at approx. 650–750 °C.
  • Welding: TIG and electron-beam welding after thorough cleaning and suitable shielding.
  • Machining: relatively difficult; select appropriate tool material and parameters to control tool wear and surface quality.
  • Solution treatment: 800±10 °C / 4 h / water quench (β-forged material); or 840±10 °C / 1 h air cool + 800±10 °C / 4 h water quench (α+β-forged material).
  • Ageing: 585–685 °C, typical 630 °C / 8 h, air cool.
  • Stress-relief annealing: 480–650 °C / 1–4 h, air or furnace cool; typical 550 °C / 4 h air cool.

Typical Applications

  • Aerospace: aero-engine fan and compressor discs and blades; airframe structures and landing gear;
  • Shipbuilding: hull structures and propellers;
  • Chemical: chemical equipment and piping.

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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