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DMLS titanium parts contain two categories of defects that post-processing must address: residual stress (from rapid thermal cycling during sintering) and microporosity (from incomplete fusion, gas entrapment, or lack-of-fusion defects). Stress relief and HIP address these separately.

Stress Relief: Required for All Structural Parts

Residual stress in DMLS titanium reaches 600–900 MPa — comparable to the yield strength of the material itself. Without stress relief, parts will distort on support removal and may fail prematurely under cyclic loading.

Standard cycle: 800°C / 2 hours / vacuum furnace / controlled cooling at 5°C/min.

This is the minimum post-processing requirement for any structural DMLS titanium part. It does not eliminate porosity.

HIP: Required for Fatigue-Critical Applications

Hot isostatic pressing (HIP) applies simultaneous heat and pressure to close subsurface porosity. The standard cycle for Ti6Al4V: 900°C / 100 MPa argon / 2 hours.

HIP increases fatigue life by 3–5× versus stress-relief-only parts by eliminating the stress concentrations at pores that initiate fatigue cracks. It is mandatory for:

  • Rotating aerospace components (fan blades, impellers)
  • Structural flight hardware with defined fatigue life
  • Orthopedic implants subjected to millions of load cycles

HIP does not eliminate surface porosity (open pores). Surface finish post-processing (machining, electropolishing) is required separately.

Decision Matrix

ApplicationStress ReliefHIPRationale
Non-structural bracketsOptionalDistortion control only
Static structuralRecommendedImproved ultimate strength
Fatigue-critical (aerospace)RequiredFatigue life mandate
Medical implantsRequiredCyclic loading in vivo
Research/prototypeOptionalCost optimization

Cost Consideration

HIP adds $200–$800 per batch (not per part) depending on furnace size. For small runs of high-value parts, the per-part cost premium is modest relative to part value. For prototype quantities, HIP is often deferred until design validation.

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