Ti-6Al-4V made by laser powder bed fusion, then hot isostatically pressed at 926 °C and annealed at 704 °C, is a fully post-processed condition of the printed alloy. As built, it has a fine martensitic microstructure, residual stress, some internal porosity and anisotropy between build directions. Pressing closes most internal pores and converts the martensite to a coarser alpha-beta structure, and the anneal stabilises it, improving ductility and fatigue resistance at some cost in strength. Surface roughness from the process remains, so fatigue-critical surfaces are usually machined or polished. Parts are used for aerospace structures and load-bearing medical hardware.
Compliance & Regulations
1 interactive curve for this material
Stress-strain, S-N fatigue and environmental knockdown curves are free with an account.
Create free account| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Elongation at Break(εf) | 16.10 range 15.00–17.20 | % | 20°C · specimen ASTM E8, machined after heat treatment · HIP ~926 °C, 100 MPa, then annealed 704 °C 2 h · Z (vertical cylinder | ||
Stress–Strain Curve(σ–ε) | Curve (22 pts) | Pa | 20°C · specimen ASTM E8, machined after heat treatment · HIP ~926 °C, 100 MPa, then annealed 704 °C 2 h · Z (vertical cylinder | ||
Ultimate Tensile Strength(σUTS) | 1.089 range 1.080–1.098 | GPa | 20°C · specimen ASTM E8, machined after heat treatment · HIP ~926 °C, 100 MPa, then annealed 704 °C 2 h · Z (vertical cylinder | ||
Yield Strength (0.2% offset)(σy) | 1.039 range 1.030–1.048 | GPa | 20°C · specimen ASTM E8, machined after heat treatment · HIP ~926 °C, 100 MPa, then annealed 704 °C 2 h · Z (vertical cylinder |
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Density(ρ) | 4.400 range 4.395–4.405 | kg/m³ | 20°C · specimen ASTM E8, machined after heat treatment · HIP ~926 °C, 100 MPa, then annealed 704 °C 2 h · Z (vertical cylinder |
Reference data from cited sources. Not verified or certified by MatWorld Inc. Verify against the source before use in design. Terms: engineering data