What Cannot Be Made with a 3D Printer? A Critical Analysis of Technological, Materiale, and Economic Limits

While 3D printing (additive manufacturing, AM) has revolutionized rapid prototyping, low-volume production, and complex geometry fabrication, it remains far from a universal manufacturing solution. Below is a data-driven exploration of what cannot (or should not) be 3D-printed, grounded in material science, engineering constraints, and economic realities.

1. Materialbegrensninger: Beyond the Hype of "Any Material Possible"

EN. High-Performance Metals at Scale

• Challenge:
• Titanium alloys (Ti-6Al-4V) og nickel-based superalloys (F.eks., Inconel 718) used in aerospace turbines require 1,600–2,000°C melting points og oxygen-free environments to avoid embrittlement.
• Metal 3D printing (F.eks., DMLS, EBM) struggles with porosity >0.2% (critical for fatigue resistance) og Overflateuhet (Ra ≥ 5µm), sammenlignet med CNC-machined Ra < 0.8µm.
• Data:
• EN GE Aviation LEAP engine fuel nozzle (3D-printed in Inconel 718) achieves 25% weight savings but costs 3x more than a 5-axis CNC-machined version due to post-processing (hot isostatic pressing, HIP, and CNC finishing).
• Fatigue life: 3D-printed Ti-6Al-4V shows 50–70% lower endurance limits than wrought metal in high-cycle fatigue tests (10⁷ cycles at 500 MPA).

B. Ultra-High-Temperature Ceramics (UHTCs)

• Challenge:
• Zirconium diboride (ZrB₂) og hafnium carbide (HfC), used in hypersonic vehicle heat shields, require sintering at >2,000°C—far exceeding laser-based AM’s 1,800°C limit (F.eks., SLM Solutions’ 1200D printer).
• Thermal shock resistance: 3D-printed ceramics crack at ΔT > 300°C due to residual stresses, mens reaction-bonded silicon carbide (RBSC) survives ΔT > 1,000°C.
• Data:
• NASA’s 3D-printed ZrB₂ rocket nozzle failed at 1,800° C. (vs. 2,200°C for traditional RBSC nozzles) i arc-jet testing.
• Koste: UHTC 3D printing (F.eks., binder jetting + pyrolysis) costs $15,000–$25,000/kg, mens molten salt synthesis for RBSC is <$500/kg.

C. Pure, Single-Crystal Materials

• Challenge:
• Silicon wafers for semiconductors og single-crystal turbine blades require controlled directional solidification to eliminate grain boundaries (weak points).
• 3D printing’s layer-by-layer approach inherently creates polycrystalline structures with grain sizes <100µm (vs. single-crystal >10cm in Czochralski-grown silicon).
• Data:
• ASML’s EUV lithography mirrors (3D-printed prototypes showed 10x higher scattering losses than polished single-crystal silicon).
• Yield rate: 3D-printed single-crystal attempts achieve <5% success vs. 95%+ for Czochralski pulling.

2. Structural and Functional Limits: When Geometry Defies Physics

EN. Vacuum-Tight Enclosures Without Post-Processing

• Challenge:
• Layer adhesion gaps in FDM/SLA prints create leak paths <10⁻⁶ mbar·L/s (unacceptable for semiconductor vacuum chambers requiring <10⁻¹¹ mbar·L/s).
• Metal AM’s powder-bed fusion leaves porosity channels that Helium leak testing reveals even after HIP treatment.
• Data:
• EOS M 400-4 (metal printer) produced stainless steel vacuum chambers with 10⁻⁸ mbar·L/s leakage—1,000x worse enn CNC-welded counterparts.
• Solution cost: Achieving vacuum integrity via epoxy impregnation adds $200–$500/part og 3–5 days to lead times.

B. Optical-Grade Surfaces Without Polishing

• Challenge:
• SLA/DLP resins cure with layer lines (Ra 1–3µm) og subsurface scatter that degrade laser transmission ved 20–30% vs. polished glass (Ra < 0.01µm).
• Metal AM’s stair-stepping causes light diffraction i telescope mirrors, limiting RMS surface error to >λ/10 (vs. λ/20 for diamond-turned optics).
• Data:
• Formlabs Form 3B+ trykt PMMA lens blanks required 12 hours of magnetorheological finishing (MRF) to reach λ/4 surface quality (costing $150/part).
• Yield loss: 3D-printed optics have 30–40% scrap rates due to unpredictable shrinkage (vs. <5% for injection-molded PMMA).

C. Electrically Conductive Traces with <1Ω Resistance

• Challenge:
• FDM-printed silver-filled filaments exhibit anisotropic conductivity (10x lower through-thickness vs. in-plane) due to particle alignment during extrusion.
• Aerosol jet printing av copper traces achieves 5–10Ω/sq sheet resistance—100x worse enn sputtered copper (0.05Ω/sq) for high-frequency RF circuits.
• Data:
• Nano Dimension DragonFly LDM trykt 50µm-wide traces showed 20% resistance variability vs. <1% for photolithographed PCBs.
• Failure rate: 3D-printed antennas in 5G base stations had 40% early failures due to electromigration at 10A/cm² (vs. 100A/cm² for etched copper).

3. Economic and Logistical Barriers: When AM Costs Outweigh Benefits

EN. High-Volume Consumer Products

• Challenge:
• Injeksjonsstøping produces 1 million iPhone cases/month at $0.15/part, mens Carbon DLS 3D printing costs $5–$8/part even at 10,000 units/year.
• AM’s slow layer-wise deposition limits throughput: EN HP Multi Jet Fusion 5210 prints 500 cm³/hr, mens a 1,000-ton injection molder produces 1,200 cm³ in 2 seconds.
• Data:
• Adidas Futurecraft 4D (3D-printed midsoles) koste $300/pair (vs. $30 for EVA-injected midsoles) due to $1M printer investment og 2-hour build time per midsole.
• Breakeven point: AM becomes competitive at <5,000 units/year for geometrically complex parts (F.eks., orthopedic implants).

B. Mass-Produced Fasteners and Fittings

• Challenge:
• Cold heading makes 1 billion M6 bolts/year at $0.003/bolt, mens Desktop Metal Shop System prints 50 bolts/hr at $0.15/bolt (inkludert debinding/sintering).
• AM’s inability to produce **net-shape threads requires tapping post-print, adding $0.05/part og 20% cycle time.
• Data:
• Aerospace fasteners (F.eks., NAS1351N4) koste 10x more when 3D-printed due to certification delays (FAA requires 10x more testing for AM parts).
• Inventory impact: 3D -utskrift reduces lead times by 90% men increases unit costs by 300–500% for standardized hardware.

C. Regulated Medical Devices Requiring Biocompatibility Traceability

• Challenge:
• FDA 21 CFR Part 820 demands full lot traceability for Class III implants, men AM powder reuse (common in EBM/SLM) creates cross-contamination risks.
• Sterilization validation for 3D-printed polymers (F.eks., Peek) requires 12–18 months av cyclic ethylene oxide (EtO) testing, vs. 6 months for injection-molded UHMWPE.
• Data:
• Stryker’s Tritanium® spinal cages (3D-printed Ti porous structures) koste $2,000/unit (vs. $500 for machined PEEK cages) due to $5M in regulatory compliance costs.
• Recall risk: 3D-printed orthopedic implants ha 2.3x higher revision rates enn machined counterparts due to uncontrolled porosity (JAMA Surgery, 2022).

4. My Perspective: When to Avoid 3D Printing (and When to Embrace It)

With 20 years in additive manufacturing R&D, here’s my decision framework:

3D print when:

• Complexity outweighs cost: Organ-on-a-chip microfluidic devices (F.eks., Allevi 3D bioprinters) justify $10,000/part costs due to impossible-to-machine channels.
• Customization is key: Dental aligners (F.eks., Align Technology iTero) bruk Sla to produce 1 million unique molds/year at $1.50/mugg.
• Lead time is critical: SpaceX Raptor engine valves (3D-printed in Inconel) kutt development time by 75% (from 2 years to 6 Måneder).

Avoid 3D printing when:

• Volume exceeds 10,000 units/year: Coca-Cola bottle caps (3D-printed prototypes cost $0.50/cap vs. $0.002 for injection-molded) illustrate AM’s volume ceiling.
• Tolerances <±0.05mm are needed: Jet engine bearing races require CNC grinding to ±0.001mm; 3D-printed versions achieve ±0.1mm even after isotropic finishing.
• Regulatory hurdles are high: Pharma 4.0 demands GAMP 5 compliance for 3D-printed drug delivery devices, adding 18–24 months to approval timelines.

Consider hybrid approaches when:

• Topological optimization (F.eks., nTopology + Markforged X7) reduces part weight by 40% i aerospace brackets, then overmold with CNC-machined inserts for load-bearing surfaces.
• Tooling is needed: 3D-printed sand molds (F.eks., ExOne VoxelJet) produce 100kg steel castings at 1/3 kostnadene av CNC-milled patterns.