# AM Post-Processing — Complete Technical Guide ## Principle: post-processing is part of the process, not an afterthought In AM, final properties depend on the post-processing sequence as much as on the printing process. Plan post-processing BEFORE printing (it affects orientation, tolerances, and geometry). --- ## Metal AM — Sequence and Treatments ### General LPBF sequence (mandatory) ``` 1. STRESS RELIEF (on the build plate, before any other operation) 2. Removal from build plate (EDM wire cutting / saw / milling) 3. Support removal (manual + tools + milling where necessary) 4. Heat treatment / aging (if required by the material) 5. HIP (if critical application) 6. Post-machining of critical surfaces 7. Surface finishing 8. Inspection / quality control ``` ### Stress Relief — Conditions by alloy | Alloy | Temperature | Time | Atmosphere | Purpose | |---|---|---|---|---| | AlSi10Mg | 270–300°C | 2h | Air / Argon | Reduce residual stresses; does not alter microstructure | | Ti-6Al-4V | 600–650°C | 2–4h | Vacuum / Argon | Critical — without this, severe distortions upon removal | | 316L | 900–1050°C | 1–2h | Vacuum / Argon | Solution annealing + stress relief | | 17-4PH | 1040°C (solution) + 480°C (H900) | 1h + 1h | Vacuum | Mandatory aging sequence | | Inconel 718 | 980°C + 720°C + 620°C | 1h + 8h + 8h | Vacuum | Full precipitation hardening sequence | | Inconel 625 | 1050°C | 2h | Vacuum | Stress relief only, no precipitation | ### HIP (Hot Isostatic Pressing) - **Purpose:** Closes residual porosity (gas-phase pores, lack of fusion) → mechanical properties closer to wrought material - **Typical conditions:** - Ti-6Al-4V: 900°C / 100–200 MPa / 2–4h / Argon - IN718: 1170°C / 175 MPa / 4h - AlSi10Mg: 500°C / 100 MPa / 3h (rarely economically justified) - **When mandatory:** Biomedical (implants), aerospace fatigue-critical, pressure-bearing components - **Effect on microstructure:** May coarsen the AS-built microstructure → compensate with post-HIP heat treatment - **Cost:** €500–2000/batch depending on size and material ### Post-Machining Metal AM - Functional surfaces (seats, precision holes, sealing surfaces) → ALWAYS post-machine - Recommended machining allowance in design phase: 0.5–1.5mm on critical surfaces - Techniques: CNC milling, turning, grinding (for critical surfaces), EDM (for hard-to-reach features) - **Warning:** AM microstructure may differ from wrought material → cutting parameters may vary --- ## Metal Surface Finishing ### Methods and achievable Ra | Method | Achievable Ra | Cost | Notes | |---|---|---|---| | **As-built LPBF** | 5–25 µm | — | Baseline; depends on orientation | | **Shot peening** | 3–8 µm | Low | Introduces surface compression → improves fatigue | | **Sand/bead blasting** | 3–10 µm | Low | Uniform finish, matting | | **Vibratory finishing** | 1–4 µm | Medium | Good for batches of small parts | | **Barrel tumbling** | 1–3 µm | Medium | Parts without sharp edges | | **Electropolishing** | 0.5–2 µm | Medium-High | Excellent for 316L; possible for Ti; difficult for Al | | **CNC machining** | 0.1–1.6 µm | High | Specific surfaces, accessible geometries | | **Grinding / lapping** | 0.01–0.5 µm | High | Sealing surfaces, mating interfaces | | **Laser polishing** | 1–5 µm | High | Internal surfaces (channels), inaccessible areas | | **Chemical etching** | Varies | Low | Removal of oxidised surface layer, especially Ti | ### Shot peening — specific notes - Significantly improves fatigue resistance (compressive residual stress) - Standard AMS 2430 for aerospace - Parameters: shot size S110–S230, pressure 2–4 bar, coverage 100–200% --- ## Polymer AM — Post-Processing ### FDM Post-Processing | Operation | Purpose | Materials | Notes | |---|---|---|---| | **Support removal** | Access to geometries | All | Mechanical (pliers/cutters) or dissolution (PVA in water, HIPS in limonene) | | **Sanding** | Surface finishing | PLA, ABS, ASA, PETG | Grits: 120 → 220 → 400 → 800 progressive; wet sanding for best results | | **Primer + filler** | Covering layer lines | All | Primer surfacer + sanding before painting | | **Acetone smoothing** | Partial surface dissolution | ABS ONLY | Ra from ~30µm to ~2–5µm; caution: modifies dimensions ±0.1–0.3mm | | **IPA smoothing (XTC-3D resin)** | Surface encapsulation | All | Adds ~0.3–0.5mm — account for this in tolerances | | **Painting** | Aesthetics, UV protection | All (with primer) | Polyurethane or acrylic paints | | **Annealing** | Reduction of internal stresses, HDT | PLA, PETG, ABS | PLA: 60–80°C / 1h; PETG: 80°C / 2h; improves thermal resistance | | **Heat-set inserts** | Reliable metal threads | All thermoplastics | M2–M12; insert with soldering iron/heat station; pull-out strength >>printed thread | | **Epoxy impregnation** | Impermeability, rigidity | All | Low-viscosity resins (West System, Smooth-On) penetrate the structure | ### SLS / MJF Post-Processing | Operation | Purpose | Notes | |---|---|---| | **Breakout + cleaning** | Remove excess powder | Shot/sand blasting standard; compressed air for internals | | **Bead blasting** | Uniform finish, improved Ra | Ra from 12µm → 6–8µm; uniform satin appearance | | **Dyeing** | Uniform colouring | PA12: excellent dyeing capability (standard black or colours with dedicated dyes); hot process 80–95°C | | **Vibratory finishing** | Ra < 4µm | Good for batches; caution with thin features | | **SLS coating (e.g. Ceracoat, Duracoat)** | Impermeability + colour | Specific coatings for SLS; slightly increases Ra | | **Impregnation** | Impermeability | Epoxy resins or low-viscosity cyanoacrylate | | **Painting** | Aesthetics | With PA-specific primer | | **Machining** | Critical tolerances | PA12 machines well; watch for cutting heat | ### SLA / DLP / MSLA Post-Processing — MANDATORY ``` MANDATORY SEQUENCE: 1. Removal from the build plate 2. Wash in IPA (10–15 min agitation or dedicated washing machine) → IPA 90%+ for optimal cleaning → Alternative: Form Wash solution or equivalent 3. Air drying (5–10 min) for IPA evaporation 4. UV post-curing (MANDATORY) → 405nm, 900–1200 mJ/cm² or follow manufacturer specifications → Time: 15–60 min depending on resin and part size → Elevated temperatures (40–60°C) accelerate and improve uniformity 5. Support removal (post-curing for standard resins; pre-curing for flexible resins) 6. Optional finishing: sanding, painting, coating ``` **Warning:** Uncured resin is toxic — mandatory PPE (nitrile gloves, goggles, ventilation) --- ## Ceramic AM — Post-Processing ### SLA/DLP ceramics (Lithoz, 3DCeram) ``` 1. Wash (IPA or supplier-specific solvent) 2. UV post-curing (same as standard SLA) 3. Thermal DEBINDING: 200–600°C / slow ramp (1–5°C/min) to eliminate organic binder → Critical phase: ramp too fast → cracking 4. PRE-SINTERING (brown body): ~1000°C / 2h → brittle but handleable ceramic 5. Final SINTERING: → Alumina: 1550–1600°C / 2h → Zirconia: 1450–1550°C / 2h → Shrinkage: 20–25% linear (compensate in CAD) 6. Optional HIP for dense zirconia (density >99.9%) 7. Grinding/lapping for functional surfaces ``` --- ## Inspection and Qualification ### Inspection methods for AM parts | Method | Applies to | Detects | When to use | |---|---|---|---| | **Visual + dimensional (CMM)** | All | Dimensions, tolerances | Standard, always | | **CT scan (tomography)** | Metal AM, ceramics | Internal porosity, cracks, inclusions | Critical parts, biomedical, aerospace | | **Ultrasound (UT)** | Metals | Cracks, delaminations | Large parts | | **X-ray radiography** | Metals | Porosity, defects | Cost-effective alternative to CT | | **Hardness (HV, HRC)** | Metals | Heat treatment state | Verify post-HT | | **Metallography** | Metals (coupon) | Microstructure, porosity | Initial process qualification | | **Tensile testing** | All (coupon) | Rm, E, elongation | Batch qualification | | **Profilometer** | All | Ra, Rz | Verify surface finish | ### Acceptable porosity by application | Application | Max acceptable porosity | |---|---| | Prototypes / non-structural | <5% | | Structural parts (non-critical) | <1% | | Fatigue-critical applications | <0.1% (HIP often required) | | Biomedical (implants) | <0.05% (HIP mandatory) | | Pressure vessels / sealings | <0.01% → HIP + CT scan |