개요 inconel 3d printed part
Inconel 3D printed parts refer to components fabricated from Inconel superalloy powders using additive manufacturing (AM) methods. Inconel grades offer exceptional heat and corrosion resistance combined with high strength, making them ideally suited to aerospace, power generation, and other demanding applications.
Key properties of Inconel 3D printed parts:
- High strength maintained to over 700°C
- Withstand aggressive environments including oxidation, corrosion
- Complex geometries produced directly from CAD models
- Reduced lead times and buy-to-fly ratios vs subtractive machining
- Choice of Inconel 625, 718 alloys and others to suit needs
- Requires hot isostatic pressing (HIP) to eliminate internal voids
Continue reading to learn more about popular Inconel alloys, mechanical properties, post-processing, uses and part qualification.
Alloy Types
Common Inconel grades used in additive manufacturing include:
| 합금 | 니켈 함량 | 주요 기능 |
|---|---|---|
| 인코넬 625 | 60% min | Exceptional corrosion resistance, oxidation resistance to 980°C |
| 인코넬 718 | 50-55% | Highest strength maintained to 700°C, age hardening response |
| 인코넬 939 | N/A | High end service temperature from excellent coarsened grain structure stability |
표 1: Popular Inconel superalloys available for AM processing
These alloys offer exceptional performance under heat and corrosion exposure better than stainless steels. Inconel 718 sees widest adoption today but new grades will expand capabilities further.
속성 inconel 3d printed part
Key properties exhibited by Inconel 3D printed parts:
| 속성 | 설명 |
|---|---|
| 고온 강도 | Strength maintained up to 700°C for age-hardened alloys |
| Thermal Resistance | Service temperatures over 1000°C possible |
| 내식성 | Excellent is variety of acidic, marine environments |
| 산화 저항 | Protective surface chromium oxide layer |
| 크리프 저항 | Deformation resistance under loads at high temps |
| 경도 | Up to Rockwell C 40-45 when age hardened |
표 2: Overview of mechanical and physical properties offered by Inconel AM alloys
The combination of strength, environmental resistance and stability under extreme temperatures makes Inconel an exceptionally versatile material system for critical applications.
Printed Part Accuracy
Dimensional accuracy and tolerances achievable with Inconel AM alloys:
| 매개변수 | Capability |
|---|---|
| 치수 정확도 | ±0.3% to ±0.5% as printed |
| 최소 벽 두께 | 0.020 inches to 0.040 inches |
| 허용 오차 | ±0.005 inches common |
| 표면 마감 | Up to Ra 3.5 μm (140 μin) finish as printed |
표 3: Overview of printed accuracy and surface finish for Inconel AM parts
Post-processing like machining and finishing can further improve accuracy and surface finish. Data above is indicative – discuss specific requirements with candidate vendors for your application needs.
Part Testing of inconel 3d printed part
Qualifying Inconel AM components for end use requires standard testing protocols:
| 테스트 | 목적 | Sample Methods |
|---|---|---|
| 화학 분석 | Verify alloy chemistry and microstructure | Optical emission spectrometry, image analysis |
| 인장 테스트 | Measure tensile and yield strengths | ASTM E8, ISO 6892 |
| Stress rupture testing | Determine rupture strength over time | ASTM E292 |
| 골절 인성 | Understand crack propagation resistance | ASTM E1820 |
| Corrosion testing | Evaluate material mass loss in environments | ASTM G31, ASTM G48 |
| 비파괴 테스트 | Detect surface/subsurface defects | Penetrant testing, CT scans |
표 4: Common test methods for qualifying Inconel AM printed parts
Data must comply with applicable industry specifications like AMS, ASME, AWS, etc. as dictated by the end application and operating environment. Discuss needed validation testing with AM vendors.
애플리케이션
Industries using Inconel 3D printed parts for demanding environments:
| 산업 | 구성 요소 | 혜택 |
|---|---|---|
| 항공우주 | 터빈 블레이드, 로켓 노즐 | Maintains strength at high operating temps |
| 전력 생성 | Heat exchangers, valves | Corrosion resistance with high temp strength |
| 석유 및 가스 | Wellhead parts, fracturing components | Withstand harsh downhole conditions |
| 자동차 | Turbocharger housings | Handles exhaust heat and gases |
| 화학 처리 | Reaction vessels, conduits | Resilience against corrosive reactions |
Table 5: Overview of Inconel AM parts usage across industries
Inconel alloys produce lightweight, high-performance components replacing conventionally fabricated hardware not capable of meeting application demands.
후처리 inconel 3d printed part
Common secondary operations for Inconel AM printed parts:
| 프로세스 | 목적 | 방법 |
|---|---|---|
| 열간 등방성 프레스 | Eliminate internal voids and improve density | High pressure, high temp inert gas |
| 열처리 | Adjust microstructure and finalize properties | Solution annealing, aging profiles specific to alloy |
| 가공 | Improve dimensional accuracy and surface finish | CNC milling/turning centers |
| 코팅 | Enhance wear, corrosion and thermal resistance | Thermal spray, PVD, CVD coatings |
표 6: Recommended post-processing techniques for Inconel AM printed parts
Nearly all parts will undergo HIP and heat treatment before use. Additional subsurface checks like penetrant testing or CT scans also inform certification. Discuss protocols tailored to your component with AM vendors.
비용 분석
| 매개변수 | 일반적인 값 |
|---|---|
| Inconel Powder Cost | $100-500 per kg |
| 구매 대 비행 비율 | 1.5 : 1 |
| 리드 타임 | 4-8 weeks for printed parts |
| Printer Utilization | 50-75% |
| Finishing Allowance | 30% of printed part cost |
Table 7: Cost factors for Inconel AM part production
Significant powder reuse helps cost efficiency. Finishing steps like machining and coatings also add expense – budget 30% or more above printing costs depending on complexity.
Pros and Cons
장점
- Withstand much higher operating temps than stainless or titanium alloys
- Components maintain high strength across temperature range
- Unprecedented coolant channel geometries for enhanced heat transfer
- As-printed parts rival or exceed mechanical properties of cast Inconel
- Significantly lighter printed hardware than traditionally manufactured
- Buy-to-fly ratios near 100% with very little wasted powder
- Reduced lead times from on-demand digital inventories
단점
- Very high material costs starting around $100 per kg for powder
- Low system productivity around 5 kg powder used per day
- Significant parameter optimization required for new parts and alloys
- Extensive qualification testing mandated for aerospace and nuclear
- High operator skill level needed on specialized AM equipment
- Powder reuse up to only 10-20 cycles before refresh
- Porosity and residual stresses require HIP and finish machining
자주 묻는 질문
Q: What size Inconel parts can be 3D printed?
A: State-of-the-art systems accommodate build volumes up to 1,000 mm diameter by 600 mm height. Larger components must be segmented into sub-assemblies. Multi-laser platforms continue expanding part sizes further.
Q: Does Inconel printing require special facilities or equipment?
A: Inconel generally prints in inert argon gas chambers rather than with filters or vacuum systems. Otherwise standard metal AM machines apply without exotic additions. Handling fine powders dictates care without specific room requirements.
Q: What lead time can be expected for Inconel AM part orders?
A: Typical quoted lead times fall around 4-10 weeks depending on part size, post-processing and testing selected. Digital inventories mitigate delays so printed components ship faster than castings with supply shortages.
Q: What industries offer the best Inconel AM business opportunities?
A: Aerospace, space, petrochemical and nuclear sectors push adoption of performance alloys like Inconel. Medical also offers growth designing certified implants. Standard stainless and tool steel parts now commoditized so more exotic alloys gain interest.
Q: Does AM enable any novel Inconel applications not possible previously?
A: AM facilitates formerly impossible conformal cooling channels and hollow internal structures to enhance heat transfer in tight spaces. Parts also see use atop rockets and satellites where weights were traditionally prohibitive or machining inaccessible. Continued R&D expands future capabilities further still.
