Aerospace TC4 Titanium Alloy Ti-6Al-4V Steel Rod Alloy Plate
| Attribute | Value |
|---|---|
| Name | Titanium Alloy Ti-6Al-4V |
| Density | 4.51g/cm³ |
| Component | Ti-6Al-4V |
| Different Names | TC4, Ti-6Al-4V, BT6, IMI318 |
| Application Area | Aerospace, automotive manufacturing, chemical industry, shipbuilding, etc. |
| Alloy Type | (α+β) type titanium alloy |
| Delivery Status | Shiny |
| Corrosion Resistance | Excellent |
Aerospace High Performance TC4 Titanium Alloy Workpiece Light Rod Ti-6Al-4V Steel Rod Alloy Plate
Chemical composition (%):
| Ti | Al | V | Fe | C | N | H | O |
|---|---|---|---|---|---|---|---|
| Margin | 5.5~6.8 | 3.5~4.5 | ≤0.30 | ≤0.10 | ≤0.05 | ≤0.015 | ≤0.20 |
The composition of titanium alloy TC4 material is Ti-6Al-4V, which belongs to the (α+β) type titanium alloy and has good comprehensive mechanical properties. Greater than intensity. The strength of TC4 is sb=1.012GPa, the density is g=4.51g/cm³, and the specific strength is sb/g=23.5, while the specific strength of alloy steel is sb/g less than 18. Titanium alloy has low thermal conductivity. The thermal conductivity of titanium alloy is 1/5 of iron and 1/10 of aluminum, and the thermal conductivity of TC4 is l=7.955W/m·K.
- Aerospace: Used in aircraft engines, missiles, satellites, and structural components for weight reduction and performance enhancement
- Shipbuilding: Hulls and propellers due to excellent corrosion resistance
- Automotive Manufacturing: Engine components and suspension systems for weight reduction and improved fuel economy
- Medical Field: Artificial joints and dental implants thanks to biocompatibility
- Chemical Industry: Reactors and heat exchangers for corrosion resistance
- Ocean Engineering: Seawater desalination equipment and submarine pipelines
TC4 titanium alloy has been widely used in fields such as aerospace, automotive manufacturing, and medical devices due to its excellent comprehensive mechanical properties and good processability. Its tensile strength is σ b/MPa ≥ 895, the predetermined residual tensile stress is σ r0.2/MPa ≥ 18, the elongation rate is δ 5 (%) ≥ 10, and the area shrinkage is ψ (%) ≥ 25.
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