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
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.
| Element | Ti | Al | Sn | Zr | Mo | Cr | Fe | C | N | H | O |
|---|---|---|---|---|---|---|---|---|---|---|---|
| Content | Bal. | 4.5–5.5 | 1.5–2.5 | 1.5–2.5 | 3.5–4.5 | 3.5–4.5 | ≤ 0.30 | ≤ 0.10 | ≤ 0.05 | ≤ 0.015 | ≤ 0.15 |
Other elements: each ≤ 0.10 %, total ≤ 0.40 %.
| Property | Typical Value |
|---|---|
| Density | approx. 4.55 g/cm³ |
| Melting range | approx. 1580–1630 °C |
| Thermal conductivity | approx. 7–9 W/m·K |
| Coefficient of thermal expansion (20–100 °C) | approx. 8.8 ×10-6 /°C |
| Modulus of elasticity | approx. 110–120 GPa |
| α/β transus | 850–900 °C |
| Condition | Tensile strength | Yield strength | Elongation | Reduction 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.
For detailed datasheets, mill certificates (EN 10204 3.1) or inquiries on specific sizes and tolerances, please contact our sales & engineering team.