Ti-6Al-4V (TC4) is the most widely used titanium alloy for additive manufacturing, offering an exceptional combination of strength, corrosion resistance, and biocompatibility. It performs reliably in structural, aerospace, and medical environments due to its high fatigue strength and low density.
Using titanium 3D printing, TC4 enables production of complex, lightweight components including aerospace brackets, orthopedic implants, and high-performance mechanical parts. Additive manufacturing improves material efficiency, customization, and performance consistency in critical applications.
Country/Region | Standard | Grade or Designation |
---|---|---|
USA | ASTM | Grade 5 |
USA | UNS | R56400 |
China | GB | TC4 |
Russia | GOST | BT6 |
Category | Property | Value |
---|---|---|
Physical Properties | Density | 4.43 g/cm³ |
Melting Range | 1604–1660°C | |
Thermal Conductivity (20°C) | 6.7 W/(m·K) | |
Thermal Expansion (20–500°C) | 8.6 µm/(m·K) | |
Chemical Composition (%) | Titanium (Ti) | Balance |
Aluminum (Al) | 5.5–6.75 | |
Vanadium (V) | 3.5–4.5 | |
Oxygen (O) | ≤0.20 | |
Iron (Fe) | ≤0.30 | |
Mechanical Properties | Tensile Strength | ≥950 MPa |
Yield Strength (0.2%) | ≥880 MPa | |
Elongation at Break | ≥10% | |
Modulus of Elasticity | 110 GPa | |
Hardness (HRC) | 32–36 |
TC4 is compatible with Selective Laser Melting (SLM), Direct Metal Laser Sintering (DMLS), and Electron Beam Melting (EBM), making it one of the most accessible titanium alloys for high-performance 3D printed components.
Technology | Precision | Surface Quality | Mechanical Properties | Application Suitability |
---|---|---|---|---|
SLM | ±0.05–0.2 mm | Excellent | Excellent | Aerospace, Medical |
DMLS | ±0.05–0.2 mm | Very Good | Excellent | Consumer, Precision Parts |
EBM | ±0.1–0.3 mm | Good | Very Good | Large Aerospace and Industrial |
For high-precision aerospace or medical components with complex geometries and Ra 5–10 µm surface finishes, SLM is ideal for its dimensional accuracy and mechanical reliability.
DMLS is suitable for prototyping and high-volume functional parts that require strong fatigue performance and good machinability.
EBM is preferred for thicker components with good mechanical robustness and faster build rates, used in aircraft structural components or heavy-duty tools.
Residual stresses caused by thermal cycling are mitigated through robust support structures and Hot Isostatic Pressing (HIP), typically conducted at 920–950°C and 100–150 MPa to improve fatigue performance.
Porosity impacts strength and fatigue life. Laser parameter optimization (250–400 W, 600–1000 mm/s scan speed) and HIP post-processing increase part density above 99.9%.
Surface roughness (Ra 8–15 µm) impacts medical applications and mechanical contact surfaces. CNC machining or electropolishing improves surface finish to Ra 0.4–1.0 µm.
Powder must be protected from oxidation—storage and printing require oxygen <200 ppm and RH <5% to prevent embrittlement.
Ti-6Al-4V is widely used in:
Aerospace: Brackets, hinges, internal supports, and airframe components.
Medical: Orthopedic implants, bone plates, and surgical instruments.
Consumer & Industrial: Lightweight structural parts, robotics, and sporting equipment.
A recent aerospace application using SLM-produced TC4 brackets achieved a 30% reduction in weight and a 20% increase in fatigue life over forged components, enhancing fuel efficiency and part longevity.
Why is Ti-6Al-4V the most common titanium alloy in additive manufacturing?
What industries benefit most from 3D printed TC4 parts?
How does TC4 compare with other titanium alloys in fatigue performance?
What are the post-processing requirements for Ti-6Al-4V 3D printed parts?
Which 3D printing technology is best suited for manufacturing TC4 components?