TC21 Damage-Tolerance Alpha-Beta Titanium AlloyTC21 is a Chinese high-strength, high-toughness α+β titanium alloy of nominal composition Ti-6Al-2Sn-2Zr-3Mo-1Cr-2Nb-Si. It is engineered for damage
TC21 is a Chinese high-strength, high-toughness α+β titanium alloy of nominal composition Ti-6Al-2Sn-2Zr-3Mo-1Cr-2Nb-Si. It is engineered for damage tolerance — high strength (≥ 1100 MPa) combined with high fracture toughness (KIC 70–90 MPa·m1/2) and low crack growth rate — and is used for critical load-bearing airframe and engine components.
| Element | Ti | Al | Sn | Zr | Mo | Cr | Nb | Si | Fe | C | N | H | O |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| Content | Bal. | 5.5–6.5 | 1.5–2.5 | 1.5–2.5 | 2.5–3.5 | 0.8–1.5 | 1.5–2.5 | 0.10–0.25 | ≤ 0.30 | ≤ 0.10 | ≤ 0.05 | ≤ 0.015 | ≤ 0.15 |
Other elements: each ≤ 0.10 %, total ≤ 0.40 %.
| Property | Typical Value |
|---|---|
| Density | approx. 4.52 g/cm³ |
| Melting range | approx. 1600–1650 °C |
| Thermal conductivity | approx. 7–9 W/m·K |
| Coefficient of thermal expansion (20–100 °C) | approx. 8.6 ×10-6 /°C |
| Modulus of elasticity | approx. 110–120 GPa |
| α/β transus | 950 ± 5 °C |
| Property | Typical Value |
|---|---|
| Tensile strength | ≥ 1100 MPa |
| Yield strength | ≥ 1000 MPa |
| Elongation | ≥ 10 % |
| Reduction of area | ≥ 25 % |
| Fracture toughness KIC | 70–90 MPa·m1/2 |
Low crack growth rate; retains good properties at 400 °C with good elevated-temperature strength and creep resistance.
For detailed datasheets, mill certificates (EN 10204 3.1) or inquiries on specific sizes and tolerances, please contact our sales & engineering team.