Inconel 718 in 3D Metal Printing

High-temperature resistant, high-strength, and corrosion-resistant. Inconel 718 is a nickel-based alloy for components that must withstand high temperatures and mechanical stresses over the long term.

  • Strength is maintained at high temperatures
  • Very good resistance to corrosion and oxidation
  • Suitable for demanding high-temperature applications

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Product Visualization, AI-Generated

Is Inconel 718 the right material for your component?

Inconel is particularly suitable when …
  • sustained high operating temperatures occur
  • high strength is required even at elevated temperatures
  • Corrosion or oxidation resistance is required under demanding conditions
  • complex, heavily loaded components are planned
  • the technical benefits justify the high material and manufacturing costs
Consider alternatives if …
  • the lowest component price is the deciding factor
  • The focus is on component weight
  • moderate temperatures are sufficient
  • Thermal or electrical conductivity is the primary requirement
  • high hardness is required for tooling or mold making

Suitable Alternatives

  • Titanium, when weight is more important than maximum temperature resistance. Learn more about titanium
  • Stainless steel 1.4404, when moderate temperatures are sufficient. About stainless steel
  • Tool steel 1.2709, when hardness is more important than temperature resistance. About tool steel

Inconel: A Comparison

Decision criterionInconel 718Titanium TiAl6V4Stainless steel 1.4404Tool steel 1.2709
Weighthighvery lowhighhigh
Strengthvery highvery highhighvery high (hardened)
Corrosion Resistancevery goodvery highvery goodlow without coating
Temperature Resistancevery highmediummediummedium
Thermal Conductivitylowrather lowlowlow
Cost itemhighhighmediummedium–high
A typical decisionHigh-Temperature ApplicationLightweight Construction Plus Strengthrobust standard applicationTool and Mold Making for High-Hardness Applications

In short: Inconel 718 is the right choice when components need to withstand high temperatures over the long term. For lightweight construction without temperature requirements, titanium or aluminum are usually the more cost-effective solution.

Inconel 718 at a Glance

High-temperature-resistant nickel-based alloy with excellent strength and corrosion resistance—for the most demanding operating conditions.

Typical components made of Inconel:

  • Turbine and Engine Components
  • Components for High-Temperature Process Technology
  • Combustion Chamber and Exhaust System Components
  • Heavy-duty functional components in power generation and turbine technology
  • Components subject to corrosion in a chemical environment
  • Custom High-Temperature Small-Batch Production

Typical applications:

  • Aerospace,
  • Energy and Turbine Technology,
  • Chemical and Process Engineering,
  • Motorsports,
  • Mechanical Engineering.
Density~ 8.19 g/cm³
Tensile strengthRm (heat-treated)~ 1250 MPa
Yield strengthRp0.2 (heat-treated)~ 1080 MPa
Elongation at break A~ 16 %
Modulus of Elasticity E~ 200,000 MPa
Hardness~ 40 HRC
Max. Operating Temperature~ 650 °C
Installation space (Inconel)280 × 280 × 360 mm
Tolerances (Approximate Values)±0.2 mm or ±0.2% (whichever is greater)
Surfaceblasted / shot-blasted; CNC precision machining available upon request

The values listed are approximate. Actual properties may depend on factors such as component orientation, wall thickness, process parameters, and heat treatment, among others.

Designing Inconel Components for 3D Printing

In 3D printing with Inconel 718, the design affects not only manufacturability but also part quality, costs, and the amount of post-processing required. Therefore, part orientation, support structures, powder removal, and functional surfaces that will require machining later on should be taken into account as early as the development stage.

Cavities and internal channels

Internal channels and complex cavities are among the particular strengths of additive manufacturing. However, it must be possible to completely remove any unmelted metal powder after the manufacturing process.

Enclosed cavities should therefore be avoided. For internal structures, sufficiently large and easily accessible powder inlets must be provided. The shape, length, and configuration of the channels must allow for reliable emptying.

Wall thicknesses and delicate areas

Wall thicknesses must be tailored to the size, geometry, and load-bearing requirements of the component. Structures that are too thin or have a large surface area may deform during manufacturing. Solid sections, on the other hand, increase material usage, construction time, and thermal stress.

Uniform material distribution and smooth transitions are generally preferable to sharp changes in cross-sectional dimensions. Fillet radii can help reduce local stress peaks.

Overhangs and Support Structures

Overhanging areas require additional support structures, depending on their angle, length, and orientation. These structures stabilize the component during the construction process and dissipate process heat.

Since support structures must be removed after manufacturing, they should be placed on easily accessible and non-critical surfaces whenever possible. The orientation of the component therefore has a direct impact on:

  • the number of support structures required
  • the surface quality
  • the amount of post-processing required
  • the construction time and, consequently, the production costs
  • the location of mechanically and visually relevant surfaces

Holes, Threads, and Fits

Holes and threads can be incorporated into the design. If tight dimensional tolerances, defined fits, or load-bearing threads are required, mechanical finishing is often recommended.

To ensure this, the relevant areas should be designed with an appropriate machining allowance. This applies in particular to:

  • Fit holes
  • Thread
  • Bearing and Seal Seats
  • Planned Areas
  • Connection surfaces
  • precise contours

A technical drawing that includes tolerances and functional surfaces makes production planning easier.

Distortion and Thermal Stresses

Layer-by-layer melting and solidification result in significant local temperature differences. These can cause residual stresses and warping. Large, flat surfaces, abrupt changes in cross-section, and uneven material distribution are particularly critical.

These effects can be reduced through proper component orientation, design adjustments, and subsequent heat treatment.

Design data for testing

For the manufacturing review, you can submit your 3D model in STEP, STL, or 3MF format. For fits, threads, sealing surfaces, and geometric and dimensional tolerances, a technical drawing in PDF format should also be provided.

Are you still in the design phase? We review component orientation, critical geometries, post-processing, and potential cost optimizations before manufacturing begins.

Manufacturing, Build Volume, and Tolerances: Important Information for Optimal 3D Printing

Rapidobject uses Inconel 718 in powder-bed-based metal 3D printing. This material is particularly well-suited for high-stress components that must withstand high temperatures over the long term.

Materials and Manufacturing Processes:

  • Manufacturing process: powder-bed-based metal 3D printing
  • Typical finish: sandblasted
  • Further processing: stress-relief annealing/aging, HIP, Trowal finishing, and CNC machining according to technical specifications

Post-processing Options

3D Printing
Heat Treatment/HIPSolution annealing and aging; HIP, if necessary, to reduce porosity
Blasting/Trowalizingeven, matte finish
CNC FinishFlat surfaces, holes, threads, sealing grooves
LabelingSerial number/logo available
DocumentationTest report/measurement report available upon request
  • Mating surfaces,
  • Drilling,
  • Thread,
  • Seal Grooves

– Everything from a single source. Just upload your drawing.

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Frequently Asked Questions About 3D Metal Printing with Inconel

When is Inconel 718 a better choice than titanium?

Inconel 718 is the right choice when components must withstand high temperatures over the long term—an area where titanium reaches its limits.

If, on the other hand, weight is the primary consideration and temperatures remain moderate, titanium (TiAl6V4) is the lighter and usually more economical choice.

Inconel 718 retains its strength even at significantly higher temperatures than 1.4404 stainless steel and offers even greater corrosion resistance under demanding conditions.

For standard applications without extreme temperature exposure, stainless steel is usually the more economical solution due to its lower cost.

Inconel 718 is particularly well-suited for components subjected to high loads in high-temperature environments. Typical examples include:

  • Turbine and Engine Components
  • Combustion Chamber and Exhaust System Components
  • Components for High-Temperature Process Technology
  • Components subject to corrosion in a chemical environment

For applications that do not involve high temperatures or corrosion, another material is usually more cost-effective.

For Inconel 718, a maximum continuous operating temperature of approximately 650 °C is specified. This value should be considered a general guideline.

The permissible operating temperature of a specific component also depends on the load, duration of use, environment, and safety requirements.

After additive manufacturing, Inconel components have a rough surface due to the manufacturing process. At Rapidobject, the components are sandblasted as standard, resulting in a uniform, matte finish.

Depending on the requirements, additional processes such as Trowalizing, HIP, or CNC finishing may be performed.

Threads, holes, and fits can be incorporated into the 3D model. However, if specific dimensions or tight tolerances are required, subsequent machining is often recommended.

The relevant areas should therefore be designed with a machining allowance and marked on a technical drawing. For example, threads can be cut, holes can be reamed, or mating surfaces can be milled.

STL, STEP, and 3MF. For CNC machining, please also provide a technical drawing as a PDF.

Usually immediately after upload—complex assemblies are analyzed automatically.

Solution annealing/aging, HIP, blasting, tumbling, milling/planing, drilling, threading, surface marking.

Yes. For orders of more than 2 units, we offer automated volume-based pricing; for recurring orders, framework agreements are available.

Do you have any questions?

We’d be happy to provide you with personalized advice on your 3D printing project—from the initial idea to the finished part. 

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Is Inconel not the best fit for your needs?

Compare Inconel with Other Metals

Inconel 718 combines high-temperature resistance with high strength and corrosion resistance. However, for components that are not subject to extreme temperature requirements, this effort is not always necessary.

Therefore, determine which property is most important for your application.

Do you need maximum strength with minimal weight?
Titanium

Titanium TiAl6V4 combines very high strength with relatively low weight and excellent corrosion resistance. It is particularly well-suited for demanding, weight-optimized functional components.

Typical decision-making criteria:

  • low component weight combined with high strength
  • high corrosion resistance
  • complex, weight-optimized geometries
  • Aerospace, Motorsports, Medical Technology
Would you like to reduce weight and manufacturing costs?
Aluminum

Aluminum is suitable for lightweight functional components that require only moderate mechanical strength. Compared to titanium, aluminum can be more cost-effective and also offers good thermal conductivity.

Typical decision-making criteria:

  • low component weight
  • good thermal conductivity
  • Economical prototypes and production runs
  • moderate mechanical stress
Do you need a durable and corrosion-resistant standard material?
Stainless steel 1.4404

Stainless steel 1.4404 is suitable for robust functional components where corrosion resistance and cost-effectiveness are more important than maximum weight reduction.

Typical decision-making criteria:

  • high corrosion resistance
  • Heavy-duty industrial components
  • good machinability
  • Component weight is not a deciding factor
Do you need a curable material for tooling or mold making?
Tool steel 1.2709

Tool steel 1.2709 is suitable for high-strength and hardenable components. In additive toolmaking, it is possible to create complex geometries or cooling channels that closely follow the part’s contours—features that would require significant effort to produce using conventional methods.

Typical decision-making criteria:

  • high hardness
  • components subjected to high mechanical stress
  • contour-following cooling
  • Subsequent heat treatment and CNC machining
Do you need corrosion resistance or a surface that can be machined to a high standard?
Bronze CuSn10

CuSn10 bronze is suitable for components subject to corrosion and wear, as well as for applications that require a surface that can be easily machined or polished.

Typical decision-making criteria:

  • corrosive environmental conditions
  • Functional components subject to mechanical stress
  • components subject to wear and tear
  • polishable or decorative surfaces
Is thermal or electrical conductivity more important?
Copper

Copper and copper alloys are suitable for components where heat transfer or electrical conductivity are key considerations. Additive manufacturing enables the creation of complex geometries and internal cooling structures.

Typical decision-making criteria:

  • Heat Transfer
  • electrical conductivity
  • complex cooling channels
  • Inductors and Electronic Applications
Still unsure about which material to choose?

Have Your Metal Component Inspected

The right metal alloy is not determined solely by its maximum strength. The key factor is the interplay of:

  • mechanical stress
  • Component weight
  • Operating Temperature
  • Corrosion Requirements
  • Thermal or electrical conductivity
  • Geometry
  • Post-processing
  • Quantity and Target Costs

Please send us your 3D model and the key requirements for the component. We will determine whether Inconel 718 is suitable or whether an alternative metal would be more appropriate from a technical or economic standpoint.

Markus Prokscha

SLM expert

Bachelor of Arts: Integrated Design

+49 (0) 341 231 837 32 metall@rapidobject.com