Understanding Inconel Alloys
Inconel refers to a family of nickel-chromium superalloys engineered for demanding applications. Common grades include:
• Inconel 625: Known for exceptional corrosion resistance and weldability.
• Inconel 718: Favored for high-strength, creep-resistant parts up to 700 °C.
• Inconel 738LC: Designed for gas-turbine blades requiring thermal fatigue life.
Key properties that make these alloys stand out:
High tensile strength across 20–950 °C.
Superior oxidation and corrosion resistance in harsh media.
Excellent creep and fatigue performance under cyclic loads.
These attributes stem from carefully balanced nickel-chromium bases, reinforced by elements like molybdenum, niobium, and titanium. Understanding each grade’s microstructure and phase stability is critical for optimizing 3D-printed parts in service.
Why Choose Inconel for 3D Printing?
Inconel’s compatibility with powder-bed fusion and directed energy deposition unlocks unprecedented design freedom:
• Strength-to-weight optimization: Thin walls and lattice cores reduce mass without sacrificing load capacity.
• Thermal stability: Maintains mechanical integrity in 600–800 °C environments—ideal for exhaust, turbine, and heat-exchanger components.
• Complex geometries: Internal channels, topology-optimized shapes, and consolidated assemblies become one-piece prints, eliminating welds and fasteners.
• Rapid iteration: From CAD model to final part in days, designers can test multiple configurations with minimal lead time.
Compared to machining or casting, additive production of Inconel shortens the supply chain, lowers inventory costs, and slashes assembly overhead. When performance margins are tight and downtime is costly, 3D printed Inconel often delivers the best value proposition.
Post-Processing Techniques
Even with precise powder-bed fusion, Inconel parts require careful post-processing to meet stringent specifications:
Stress Relief Heat Treatment
• Typical cycles: 980 °C for 1–2 hours, slow furnace cooling.
• Purpose: Reduces residual stresses and minimizes crack risk.
Hot Isostatic Pressing (HIP)
• Conditions: ~120 MPa and 1150 °C for several hours.
• Outcome: Nearly eliminates internal porosity, boosting fatigue life.
Surface Finishing
• Shot peening: Introduces compressive surface stresses for fatigue resistance.
• Machining & polishing: Achieves tight tolerances and surface roughness down to Ra 0.2 µm.
Protective Coatings
• Thermal barrier or oxidation coatings extend service life in extreme heat.
Selecting the right sequence and parameters ensures that mechanical properties meet or exceed wrought-alloy standards, even for mission-critical applications.
Key Applications
Aerospace
• Combustion-chamber liners, turbine blades, and fuel nozzles.
• Weight reduction through lattice structures improves fuel efficiency.
Oil & Gas
• Downhole drilling tools, subsea manifolds, and heat exchangers.
• Corrosion resistance in sour environments (H₂S, CO₂).
Power Generation
• Gas-turbine vanes, diffusers, and heat-recovery steam-generator tubes.
• High-temperature creep resistance under continuous operation.
Chemical Processing
• Reactor internals and piping for corrosive media (acids, chlorides).
Medical & Automotive (Emerging)
• Surgical instruments, customized implants, turbocharger turbine wheels.
Cost Analysis
Cost Component |
Inconel 718 |
Aluminum (AlSi10Mg) |
Stainless Steel (316L) |
Titanium (Ti6Al4V) |
Raw Material ($/kg) |
200–400 |
50–80 |
80–150 |
250–350 |
Build Rate (g/hr) |
10–15 |
40–60 |
20–30 |
6–10 |
Machine Cost ($/hr) |
100–150 |
75–100 |
80–120 |
120–160 |
Post-Processing ($/kg) |
50–100 |
30–60 |
40–80 |
60–120 |
Powder Reuse Rate (%) |
70–80 |
60–70 |
70–80 |
60–70 |
Lead Time |
Days–weeks |
Days |
Days–weeks |
Weeks |
Raw Material
• Aluminum powder is the most cost-effective but offers lower high-temperature strength.
• Stainless steel sits in the middle, combining moderate cost with corrosion resistance.
• Titanium and Inconel command a premium, reflecting their superior strength-to-weight and thermal stability.
Build Rate & Machine Cost
• Aluminum’s high build rates reduce hourly overhead, making it ideal for larger batches of non-critical parts.
• Inconel and titanium require slower scan speeds and more energy, driving up machine runtime costs.
Post-Processing
• Inconel and titanium often need Hot Isostatic Pressing and extensive stress relief, increasing per-kilogram expenses.
• Stainless steel and aluminum typically need simpler stress relief and fewer finishing passes.
Powder Reuse
• Alloys with stable chemistries (Inconel, stainless) support higher reuse rates, recouping material costs.
• Aluminum and titanium powders degrade faster under repeated reuse, slightly raising effective material spend.
SLM 3D Printing Inconel Service at 3DSPRO
3DSPRO’s specialized SLM offering caters to the exacting demands of Inconel parts. Service highlights include:
Industrial-Grade SLM Systems
• More than 80 machines are operating.
• Build envelopes up to 280*280*35mm for 3D printed inconel parts.
Powder Management & Quality Control
• ISO-certified labs monitor particle size (15–45 µm) and composition.
• Closed-loop recycling preserves powder integrity over 5+ reuse cycles.
Advanced Post-Processing
• In-house furnaces for dual-stage stress relief and HIP.
• Various surface finishing options for industrial use.
Key Properties of SLM Printed Inconel 718 at 3DSPRO:
Property |
Testing Method |
Value |
Hardness |
ISO 6597-1:03-2006 |
300 HV |
Density |
WGE-Prod-067EN |
8.15 g/cm³ |
Relative density |
WGE-Prod-067EN |
99.5% |
Tensile strength |
DIN EN ISO 6892-1:2009 |
980MPa |
Elongation at Break |
DIN EN ISO 6892-1:2009 |
13% |
Yield strength |
DIN EN ISO 6892-1:2009 |
700MPa |
Elastic modulus |
DIN EN ISO 6892-1:2009 |
200GPa |
Roughness Ra |
ISO 4287 / AITM 1-00070 |
15 µm |
Roughness Rz |
ISO 4287 / AITM 1-00070 |
60 µm |
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