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Blog · Materials Engineering

Additive manufacturing in titanium

Freedom-to-design in Ti-6Al-4V structural components via LPBF.

Jul 2026 · 11 min read · Materials Engineering

Beyond machining

Ti-6Al-4V is the workhorse of titanium: 60% of global production. Excellent strength-to-weight ratio (UTS ~ 950 MPa, density 4.43 g/cm3), full biocompatibility, seawater corrosion resistance. But machining it is expensive: titanium is a poor thermal conductor, heat concentrates on the tool, and cutting speeds are 5-10x lower than for steel.

LPBF (Laser Powder Bed Fusion) additive manufacturing changes the rules: instead of starting from a block of material and removing the excess (subtractive), it builds layer by layer (30-60 micrometers) by selectively melting powder with a laser.

Geometries machining cannot touch

LPBF enables shapes that would be impossible or prohibitively expensive to machine:

  • Internal conformal channels: cooling ducts that follow the part geometry, impossible to drill
  • Lattice structures: periodic lattices (BCC, FCC, gyroid) with 10-30% solid density, designed to absorb impact energy or reduce weight while maintaining stiffness
  • Assembly consolidation: a part of 23 machined and welded components printed in a single operation
  • Thin walls: minimum thicknesses of 0.3 mm, impossible by machining

Microstructure rules

The microstructure of LPBF-printed Ti-6Al-4V is radically different from forged material. High cooling rates (10^3 - 10^6 K/s) produce a fine-grained acicular martensitic matrix (alpha-prime phase), with higher hardness and strength than forged material but lower ductility.

  • As-built: UTS ~ 1100-1200 MPa, elongation ~ 6-10%, alpha-prime martensite
  • After HIP (Hot Isostatic Pressing, 920C, 100 MPa, 2h): UTS ~ 950-1000 MPa, elongation ~ 14-18%, equiaxed alpha+beta structure. Closes internal porosity
  • After annealing (800C, 2h): UTS ~ 1000-1050 MPa, elongation ~ 12-15%, partially decomposes alpha-prime

Residual stresses: the hidden enemy

Each deposited layer undergoes an extreme thermal cycle: the laser locally melts powder at ~1660C, it solidifies in microseconds, and upon contraction generates tensile stresses that warp the part. Thin parts or those with asymmetric sections deform visibly; non-visible internal stresses can cause premature failure in service.

Mitigation strategies:

  • Build plate preheating (200-500C): reduces the thermal gradient and thus the stresses
  • Orientation optimization: orient the part to minimize cross-sectional area per layer and keep stresses symmetric about the build axis
  • Scan strategy: island (chessboard) patterns of 5-10 mm rotated 67 degrees between layers distribute stresses
  • Post-process heat treatment: stress relief at 600-800C before cutting from the build plate is practically mandatory for complex geometries

Process simulation

Simulating LPBF requires solving coupled phenomena at multiple scales: thermal (melting/solidification), fluid (melt pool flow), mechanical (stresses), and metallurgical (phase change). Commercial codes (Simufact Additive, Amphyon, Netfabb) use a simplified layer-by-layer approach:

  • An inherent thermal strain is applied for each activated layer
  • The quasi-static mechanical problem is solved (not the full thermal one)
  • Distortion prediction is qualitatively correct and quantitatively within 15-25%

Simulation enables iterating over supports, orientation, and scan strategy without printing physical parts. A typical analysis of a 100 mm part takes 2-4 hours on a workstation.

Real-world applications

  • Aerospace: GE9X engine brackets with 300 parts reduced to 7 printed ones. 25% weight savings and 50% cost savings
  • Medical: hip and cranial implants with controlled surface porosity for osseointegration
  • Motorsport: suspension brackets and brake components with internal lattice for energy absorption
  • Defense: heat exchangers with internal surfaces optimized by CFD and manufactured by LPBF

Conclusions

LPBF titanium does not replace machining — it complements it where geometries are complex, production runs are short, or functional integration justifies the cost. The key lies in understanding the resulting microstructure, managing residual stresses, and designing for the process — not simply printing a part designed for machining.