インコネル718 3Dプリンティング

目次

概要

Inconel 718 is a high-strength nickel-chromium superalloy widely used for extreme temperature applications such as gas turbine components, rocket engines, and nuclear reactors. The combination of excellent mechanical properties, corrosion resistance, and workability make Inconel 718 a versatile material across industries like aerospace, oil and gas, power generation, and automotive.

In recent years, additive manufacturing (AM) of Inconel 718 has emerged as a transformative production method to fabricate complex, high-performance metal parts. Also known as 3D printing, AM builds up components layer-by-layer directly from a 3D model without the constraints of traditional machining or casting.

This guide provides an in-depth look at Inconel 718 3D printing, including alloy properties, popular AM process types, parameters, microstructures, mechanical behavior, post-processing, applications, and suppliers. It aims to assist engineers, designers, and technical program managers in implementing Inconel 718 3D printing and qualifying printed parts for production use.

インコネル718 3D印刷

Inconel 718 Alloy Overview

Inconel 718 is a precipitation hardened nickel-chromium alloy containing important alloying elements like niobium, molybdenum, aluminum and titanium.

Inconel 718 Composition

エレメント重量 %目的
ニッケル50-55%Corrosion resistance, ductility
クロム17-21%耐酸化性
バランス費用対効果
ニオビウム4.75-5.5%Precipitation strengthening
モリブデン2.8-3.3%固溶体強化

Nickel and chromium provide corrosion resistance and high temperature stability. Hardening elements like niobium and molybdenum give superior strength through precipitation and solid solution strengthening mechanisms.

Inconel 718 Properties

  • 700℃までの優れた強度
  • High impact toughness and fatigue resistance
  • 優れた耐酸化性と耐食性
  • 高いクリープ破断強度
  • Easily formed and welded with standard techniques
  • Density of 8.19 g/cm3

This combination of properties makes Inconel 718 suitable for extreme environments beyond the capabilities of steels and aluminum alloys.

インコネル718 3Dプリンティング プロセス

Several additive manufacturing processes have demonstrated success with Inconel 718 and are seeing increasing adoption for production applications:

Popular AM Processes for Inconel 718

プロセス説明密度微細構造機械的特性
レーザー粉末床融合 (L-PBF)Laser melts powder layers99.5%+Columnar grains, some porosityTensile strength within wrought range
電子ビーム粉末床融合(E-PBF)Electron beam melts powder99.5%+Columnar grains, some porosityTensile strength within wrought range
指向性エネルギー蒸着(DED)Focused heat source melts powder or wire feed99%Epitaxial grains, some porosityVariable based on process parameters
バインダー・ジェットLiquid binder selectively joins powder particles60%+Porous, requires infiltrationLow as-printed, improves with infiltration

L-PBF and E-PBF can achieve densities over 99.5% with properties approaching wrought Inconel 718. DED and binder jetting require post-processing to reach full density.

Each process requires optimization of print parameters to achieve desired microstructure and properties.

Inconel 718 3D Printing Parameters

Printing parameters significantly influence the resulting microstructure, defects, and mechanical performance of printed Inconel 718 parts.

Key Inconel 718 Print Parameters

パラメータ典型的な範囲インパクト
層厚20-100 μmDensity, surface finish
Laser/beam power100-500 WMelt pool size, heating rate
スキャン速度100-1000 mm/sCooling rate, solidification
ハッチの間隔50-200 μmBonding between hatches
ビームフォーカス30-100 μmMelt pool width, depth
パウダーサイズ10-45 μmPowder flowability, surface finish

Thinner layers and narrower hatches enhance density and bonding but reduce build speeds. Faster scanning gives finer grains but can cause hot cracking. Small powder sizes improve surface finish.

Careful optimization of parameters tailors grain structure strength, ductility, surface quality, and printing productivity.

Inconel 718 3D Printing Microstructures

Inconel 718 exhibits diverse microstructures when printed using AM processes:

Microstructural Features in Printed Inconel 718

  • Columnar grains parallel to build direction
  • Epitaxial grains matching base plate orientation
  • Typical grain width of 100-400 μm
  • Solidification segregation between dendrite cores and interdendritic regions
  • Lack of texture compared to wrought product
  • Precipitation of strengthening phases like γ” and γ’
  • Porosity and microcracks from incomplete fusion

Grain morphology follows heat flow and solidification patterns during printing. Segregation leads to chemical variations which can cause cracking. Careful processing is needed to achieve a uniform, controlled microstructure.

Heat treatments dissolve unfavorable phases and promote hardening precipitates like Ni3Nb gamma-double-prime for optimal strength.

Properties of Printed Inconel 718

AM processing can achieve mechanical properties comparable to wrought Inconel 718 with proper optimization:

Inconel 718 Mechanical Properties

プロパティAs-PrintedWrought Mill-Annealed
引張強度1000-1300 MPa1000-1200 MPa
降伏強度500-1100 MPa500-900 MPa
伸び10-35%20-35%
疲労強度100-600 MPa300-500 MPa
硬度25-50 HRC25-35 HRC

Strength meets or exceeds wrought levels, although elongation and fatigue properties remain lower and more variable.

Tensile anisotropy is observed between vertical and horizontal build orientations. Properties are heavily influenced by the specific AM process parameters used.

Post-Processing of Printed Inconel 718

Post-print processes are often required to improve surface finish, dimensional accuracy, and material properties:

Common Post-Processing Methods

  • 熱処理 – Develops optimal microstructure and precipitate hardening
  • 熱間静水圧プレス – Closes internal voids and porosity
  • 表面加工 – Reduces surface roughness for critical finishes
  • ショットピーニング – Induces compressive stresses to improve fatigue life
  • コーティング – Provide wear or corrosion resistance when needed

Standard Inconel 718 age hardening is commonly used, though some modify heat treatment for AM microstructures. Machining, grinding or polishing are used where surface finish requirements are stringent.

Applications of Printed Inconel 718

Inconel 718 3D printing is well suited for:

  • 航空宇宙 – Turbine components, rocket nozzles, engine assemblies
  • 発電 – Gas turbine hot section parts, nuclear fuel cladding
  • 自動車 – Turbocharger wheels and housings
  • 石油化学 – Downhole tools, valves, pumps
  • Space – Satellite and launchpad components
  •  – Dental implants, surgical instruments

Benefits versus conventional methods:

  • 複雑な形状の設計自由度
  • Weight reduction through lattices and topology optimization
  • Part consolidation, reduced assembly
  • Shorter lead times for on-demand production
  • Customized shapes, digitally driven inventories

Limitations include process costs for low production volumes and certification challenges in regulated industries.

Suppliers of Printed Inconel 718

Many manufacturers offer Inconel 718 3D printing services worldwide:

Select Service Providers

会社概要AM ProcessesAdditional Materials生産能力
GEアディティブDED, Binder JettingTitanium alloys, steels, superalloysLarge volumes
マテリアライズレーザーPBFチタン、アルミニウム、スチールMedium volumes
3DシステムズレーザーPBF、バインダージェッティングTitanium, stainless steel, CoCr, AlSi10MgPrototyping to mid volumes
EquispheresレーザーPBFTitanium, steels, aluminumSmall volumes
カーペンター添加剤Laser PBF, E-PBFTitanium, stainless, tool steelsMedium volumes

Both large OEMs and niche AM service bureaus offer Inconel 718 printing. Many provide secondary finishing operations.

Part costs range from an estimated $100-500/lb depending on order size, quality requirements, and processing method used.

Qualifying Printed Inconel 718 Parts

Stringent qualification protocols apply for aerospace and other regulated applications:

  • Mechanical testing over range of print orientations
  • Chemical analysis for composition conformance
  • Non-destructive evaluation (NDE) for defect detection
  • Long-term performance evaluation through heat treating, hot isostatic pressing, machining trials
  • Process reproducibility assessments
  • Documentation of parameter optimization, microstructures, defect prevention

Test artifacts like tensile bars, fatigue samples, and material coupons optimize characterization of printed properties.

Complying with applicable industry specifications supports certification and production approval.

よくあるご質問

What particle size is recommended for printing Inconel 718?

10-45 micron powder is typical, with finer ~15 micron powder improving density and surface finish but compromising flow and recovery.

What causes porosity when printing Inconel 718?

Insufficient melting, lack of fusion between layers, and entrapped gas cause voids. Optimizing energy input, scan patterns, layer thickness, and gas flow reduces porosity.

What post-processing improves fatigue life of printed Inconel 718?

Shot peening induces beneficial compressive stresses that inhibit crack initiation and growth. HIP and machining also help by closing surface pores.

How does printed Inconel 718 compare to cast and forged 718?

AM approaches mechanical properties of cast and forged material but with finer, more segregated microstructure. Heat treatment can achieve precipitation strengthening comparable to wrought product.

What are some alternatives to Inconel 718 for 3D printing?

Cobalt chrome, nickel superalloys like 625 and 686, and precipitation hardening stainless steels offer similar high temperature properties. Titanium alloys excel where lower density is critical.

Can you 3D print a Inconel 718 and stainless steel bimetal part?

Yes, directed energy deposition is capable of transitioning between dissimilar alloys by precise powder or wire switching to build multi-material components.

結論

In summary, Inconel 718 3D printing unleashes exceptional design freedom and performance improvements utilizing this high strength superalloy. Matching part requirements to process capabilities and optimizing printing parameters is key to exploiting benefits versus conventional methods. Ongoing advances in quality, properties, multi-material structures, and cost continue to expand adoption of Inconel 718 AM across demanding industrial applications.

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