IN738LC Powder
$0.00
IN738LC Powder
| Product | INC738LC Powder |
| CAS No. | N/A |
| Appearance | Gray or Metallic Silver Powder |
| Purity | ≥99%,  ≥99.9%,  ≥95%(Other purities are also available) |
| APS | 1-5 µM, 10-53 µM  (Can be customized),  Ask for other available size range. |
| Ingredient | Ni-16Cr-8.5Co-2.4Al-3.4Ti-1.75Mo-1.75w-0.9Nb-0.6Zr-0.1C |
| Density | 8.19g/cm3 |
| Molecular Weight | N/A |
| Product Codes | NCZ-DCY-278/25 |
IN738LC Description:
INC738LC Powder is one of the numerous advanced ceramic materials manufactured by Nanochemazone. Nanochemazone produces too many standard grades when applicable, including Mil Spec (military grade); ACS, Reagent and Technical Grade; Food, Agricultural and Pharmaceutical Grade; Optical Grade, USP and EP/BP (European Pharmacopoeia/British Pharmacopoeia) and follows applicable ASTM testing standards. Typical and custom packaging is available. Additional technical, research and safety (MSDS) information are available. Please request a quote above for more information on lead time and pricing
IN738LC Powder Related Information :
Storage Conditions:
Airtight sealed, avoid light and keep dry at room temperature.
Please contact us for customization and price inquiry
Email:Â contact@nanochemazone.com
Note: We supply different size ranges of Nano and micron as per the client’s requirements and also accept customization in various parameters.
Best IN738LC powder for 3D printing in 2024
| Alloy | Nominal Composition (wt%) |
| IN738LC | Ni – 16Cr – 8.5Co – 3.4Al – 3.4Ti – 1.7Mo – 2.6W – 1.7Ta – 0.9Nb – 0.05C – 0.03Zr – 0.001B |
Characteristics of IN738LC Powder
| Property | Value |
| Density | 8.19 g/cm³ |
| Melting Range | 1260-1335°C |
| Yield Strength (at 650°C) | >758 MPa |
| Tensile Strength (at 650°C) | >1035 MPa |
| Elongation (at 650°C) | >12% |
| Grain Size | Fine-grained |
| Gamma Prime Phase | High volume fraction |
IN738LC powder exhibits exceptional high-temperature strength, creep resistance, and oxidation resistance due to its unique composition and microstructure. The presence of aluminum, titanium, and refractory elements like tungsten and tantalum contributes to the formation of a high volume fraction of gamma prime (γ’) precipitates, which are responsible for its superior mechanical properties at elevated temperatures.
Benefits of Using IN738LC Powder for 3D Printing
Additive manufacturing with IN738LC powder offers numerous benefits over traditional manufacturing methods, making it an attractive choice for various industries. Let’s explore some of the key advantages:
Design Flexibility: 3D printing allows for the production of complex geometries and intricate internal structures that would be challenging or impossible to manufacture using conventional methods. This design freedom enables the creation of optimized components with improved functionality and performance.
Weight Reduction: By leveraging the design flexibility of additive manufacturing, engineers can produce lightweight yet robust components with optimized topologies, resulting in significant weight savings, particularly in aerospace and automotive applications.
Rapid Prototyping: The ability to quickly produce prototypes and functional parts from IN738LC powder accelerates the product development cycle, enabling faster iterations and reducing time-to-market.
Material Efficiency: Additive manufacturing processes like SLM and EBM have higher material utilization rates compared to subtractive manufacturing methods, leading to less waste and improved resource efficiency.
Customization: 3D printing enables the production of customized components tailored to specific requirements, making it ideal for applications with low-volume or unique demands.
Repair and Remanufacturing: IN738LC powder can be used to repair or remanufacture worn or damaged components, extending their service life and reducing replacement costs.
Applications of IN738LC Powder in 3D Printing
| Application | Industry | Examples |
| Turbine Components | Aerospace, Energy | Blades, Vanes, Nozzles |
| Automotive Components | Automotive | Turbochargers, Exhaust Manifolds |
| Tooling and Molds | Manufacturing | Injection Molds, Die Casting Molds |
| Heat Exchangers | Energy, Chemical | High-Temperature Recuperators |
| Medical Implants | Healthcare | Orthopedic Implants, Dental Restorations |
The exceptional high-temperature properties and corrosion resistance of IN738LC make it suitable for a wide range of applications across various industries. In the aerospace and energy sectors, this superalloy is widely used for producing turbine components, such as blades, vanes, and nozzles, which are subject to extreme temperatures and high stresses. The automotive industry also benefits from IN738LC powder in the manufacturing of turbochargers and exhaust manifolds.
Additionally, IN738LC powder finds applications in tooling and mold making, where its high strength and wear resistance are invaluable. Heat exchangers and recuperators in the energy and chemical industries also utilize this material due to its ability to withstand elevated temperatures and corrosive environments. Moreover, the biocompatibility of IN738LC makes it a promising candidate for medical implants and dental restorations.
3D Printing Processes for IN738LC Powder
Additive manufacturing processes compatible with IN738LC powder include selective laser melting (SLM) and electron beam melting (EBM). These powder bed fusion techniques offer excellent control over the microstructure and properties of the final component.
Selective Laser Melting (SLM): In the SLM process, a high-powered laser selectively melts and fuses the IN738LC powder layer by layer, according to the 3D model data. The build chamber is typically filled with an inert gas, such as argon or nitrogen, to prevent oxidation and maintain the desired material properties.
Electron Beam Melting (EBM): EBM utilizes a focused electron beam to selectively melt the IN738LC powder in a vacuum environment. This process allows for higher build rates and can produce parts with excellent mechanical properties and reduced residual stresses.
Both SLM and EBM processes require careful control of process parameters, such as laser or electron beam power, scan speed, hatch spacing, and layer thickness, to ensure optimal densification, microstructure, and mechanical properties of the final component.
To achieve the desired properties, post-processing steps like stress relief heat treatments, hot isostatic pressing (HIP), and surface finishing may be necessary, depending on the application requirements.
| Powder Specifications |
| Particle Size Distribution: 15-53 μm |
| Flowability: Excellent |
| Sphericity: High |
| Apparent Density: 4.2-4.6 g/cm³ |
| Standards: AMS 5832, AMS 5385 |
| Typical Grades |
| IN738LC – Standard Grade |
| IN738LC-LG – Low Gauge Grade |
| IN738LC-HG – High Gauge Grade |
Pros and Cons of Using IN738LC Powder for 3D Printing
| Pros | Cons |
| Excellent high-temperature strength and creep resistance | Higher material cost compared to some other alloys |
| Superior oxidation and corrosion resistance | Potential for cracking and distortion during printing |
| Ability to produce complex geometries | Strict process control required for optimal properties |
| Lightweight and high strength-to-weight ratio | Limited availability of qualified suppliers |
Advantages of IN738LC Powder for 3D Printing
When compared to traditional manufacturing methods, additive manufacturing with IN738LC powder offers several distinct advantages:
Design Optimization: The ability to produce complex geometries and internal features enables the design of components with optimized topologies, leading to weight reduction and improved performance. For instance, in the aerospace industry, lightweight yet strong turbine blades can be created, resulting in increased fuel efficiency and reduced emissions.
Rapid Prototyping and Iteration: The additive manufacturing process allows for rapid prototyping and iterative design cycles, significantly shortening the product development timeline. This advantage is particularly valuable in industries with stringent testing and certification requirements, such as aerospace and automotive.
Customization and Personalization: 3D printing with IN738LC powder enables the production of customized or patient-specific components, catering to unique requirements in fields like medical implants, tooling, and specialized industrial applications.
Material Efficiency and Waste Reduction: Additive manufacturing processes have higher material utilization rates compared to subtractive methods, resulting in less waste and improved resource efficiency. This not only reduces material costs but also contributes to a more sustainable manufacturing approach.
Repair and Remanufacturing: IN738LC powder can be used to repair or remanufacture worn or damaged components, extending their service life and reducing replacement costs. This capability is particularly beneficial in industries with high-value assets, such as aerospace and energy.
While additive manufacturing with IN738LC powder offers numerous advantages, it is essential to consider potential limitations and challenges. Process control, post-processing requirements, and the availability of qualified suppliers can impact the overall feasibility and cost-effectiveness of using this material for specific applications.
Limitations of IN738LC Powder for 3D Printing
Despite its numerous benefits, using IN738LC powder for 3D printing also presents some limitations and challenges:
Higher Material Cost: Nickel-based superalloys like IN738LC are generally more expensive compared to some other alloys used in additive manufacturing, which can increase the overall cost of production.
Strict Process Control: Achieving optimal mechanical properties and part quality with IN738LC powder requires precise control over various process parameters, such as laser or electron beam power, scan speed, hatch spacing, and layer thickness. Deviations from the optimal parameters can lead to defects or suboptimal performance.
Potential for Cracking and Distortion: Due to the high thermal gradients and residual stresses involved in the additive manufacturing process, IN738LC components can be susceptible to cracking and distortion. Careful design, process optimization, and post-processing techniques like stress relief heat treatments and hot isostatic pressing (HIP) may be necessary to mitigate these issues.
Limited Availability of Qualified Suppliers: While several suppliers offer IN738LC powder, the number of qualified and experienced suppliers may be limited compared to more widely used materials. This can impact the availability, lead times, and pricing of the powder.
Post-Processing Requirements: Depending on the application and performance requirements, post-processing steps like hot isostatic pressing (HIP), heat treatments, and surface finishing may be necessary to achieve the desired mechanical properties and surface quality. These additional steps can increase the overall cost and lead time.
Description
Description
Note: For pricing & ordering information, please get in touch with us at sales@nanochemazone.com
Please contact us for quotes on Larger Quantities and customization. E-mail: contact@nanochemazone.com
Customization:
If you are planning to order large quantities for your industrial and academic needs, please note that customization of parameters (such as size, length, purity, functionalities, etc.) is available upon request.
NOTE:
Images, pictures, colors, particle sizes, purity, packing, descriptions, and specifications for the real and actual goods may differ. These are only used on the website for the purposes of reference, advertising, and portrayal. Please contact us via email at sales@nanochemazone.com or by phone at (+1 780 612 4177) if you have any questions.
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GH3230 Powder
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| CAS No. | 3230-94-2 |
| Appearance | Metallic Gray Powder |
| Purity | ≥99%,  ≥99.9%,  ≥95%(Other purities are also available) |
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GH3230 Description:
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| Composition | Ni-30Cr-4Mo-2Al alloy |
| Density | 8.3 g/cc |
| Particle shape | Predominantly spherical |
| Size range | 10-45 microns |
| Apparent density | Up to 60% of true density |
| Flowability | Good |
| Strength | Very high after aging treatment |
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| Chromium | 28-32% |
| Molybdenum | 3-5% |
| Aluminum | 1-3% |
| Carbon | 0.1% max |
| Manganese | 1% max |
| Silicon | 0.5% max |
| Sulfur | 0.015% max |
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| Density | 8.3 g/cc |
| Melting point | 1370-1420°C |
| Thermal conductivity | 12 W/mK |
| Electrical resistivity | 70 μΩ-cm |
| Coefficient of thermal expansion | 12.5 x 10^-6 /K |
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| Hardness | Peak aged | 52-58 HRC |
| Tensile strength | Annealed | 1100 MPa |
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| Elongation | Aged | 8-12% |
| Industry | Uses |
| Aerospace | Turbine blades, bolts, fasteners |
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| Chemical processing | Extruder screws, valve parts |
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| 4.8 – 5.5 g/cc | Improves with greater packing density |
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| Ensure proper ventilation | Avoid exposure to fine metallic particles |
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| Store sealed containers | Prevent contamination or oxidation |
| Test | Details |
| Chemical analysis | OES or XRF spectroscopy used to verify composition |
| Particle size distribution | Laser diffraction analysis |
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| Flow rate analysis | Gravity flow rate through specified nozzle |
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| Density | 8.3 g/cc | 8.2 g/cc |
| Strength | Higher | Lower |
| Corrosion resistance | Excellent | Outstanding |
| Cost | Moderate | Very high |
| Uses | Oil and gas, chemical processing | Aerospace, nuclear |
GH3230 Powder
GH3230 Powder
| Product | GH3230 Powder |
| CAS No. | 3230-94-2 |
| Appearance | Metallic Gray Powder |
| Purity | ≥99%,  ≥99.9%,  ≥95%(Other purities are also available) |
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GH3230 Description:
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| D10(μm) | D50(μm) | D90(μm) | ||||
| 15-53μm | 17-22 | 32-38 | 52-58 | ≤18s/50g | ≥4.60g/cm³ | ≥5.20g/cm³ |
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| 25℃ | 840 | 450 | 35 |
| 815℃ | 250 | 200 | 35 |
| 1000℃ | 160 | 130 | 30 |
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| wt％ | 0.05-0.15 | 20.00-24.00 | Bal | ≤5.00 | 13.00-15.00 | 3.15-4.15 |
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| wt％ | 2.20-0.50 | ≤0.10 | ≤3.00 | 0.005-0.05 | ≤0.015 | 0.30-1.00 |
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| Product | GH4169 Powder |
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| Appearance | Gray Dull Silver Powder |
| Purity | ≥99%,  ≥99.9%,  ≥95%(Other purities are also available) |
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GH4169 Description:
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| Form | Spherical | Spherical |
| Flow Ability | ≤25s | |
| Apparent Density | ≥4.0 g/c㎡ | |
| Oxygen Content | ≤200 ppm | |
| Nitrogen Content | ≤150ppm | |
| Properties | Details |
| Composition | Fe-17Cr-4Ni-1.5Ti-0.7Al-0.25Nb alloy |
| Density | 7.9 g/cc |
| Particle shape | Irregular, angular |
| Size range | 10-150 microns |
| Apparent density | Up to 50% of true density |
| Flowability | Moderate |
| Strength | Very high after aging treatment |
| Corrosion resistance | Excellent, including marine environments |
| Element | Weight % |
| Iron (Fe) | Balance |
| Chromium (Cr) | 16-18% |
| Nickel (Ni) | 3.5-5.5% |
| Titanium (Ti) | 1.2-1.8% |
| Aluminum (Al) | 0.3-1.2% |
| Niobium (Nb) | 0.15-0.45% |
| Carbon (C) | 0.04% max |
| Silicon (Si), Manganese (Mn) | 1% max each |
| Property | Values |
| Density | 7.9 g/cc |
| Melting point | 1400-1450°C |
| Electrical resistivity | 0.80 μΩ-m |
| Thermal conductivity | 12 W/mK |
| Thermal expansion | 12 x 10^-6 /K |
| Maximum service temperature | 650°C |
| Property | Condition | Values |
| Hardness | Solution annealed | 90 HRB |
| Hardness | Peak aged | 40-45 HRC |
| Tensile strength | Annealed | 550-750 MPa |
| Tensile strength | Peak aged | 1300-1600 MPa |
| Yield strength | Peak aged | 1100-1400 MPa |
| Elongation | Peak aged | 8-13% |
| Industry | Example Uses |
| Aerospace | Airframe and engine components, fasteners |
| Marine | Shafts, fixtures, solenoids, valves |
| Nuclear | Fuel element cladding, internal structures |
| Oil and gas | Structural parts for wellheads, offshore platforms |
| Chemical | Process equipment like vessels and pipes |
| Standard | Description |
| AMS 5922 | Precipitation hardening stainless steel powder for aerospace parts |
| ASTM A580 | Standard for precipitation hardening stainless steel wire |
| ASTM A638 | Standard for precipitation hardening iron-based superalloys |
| AMS 5898 | Bars, forgings, rings of precipitation hardening stainless steels |
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| 10-22 microns | Ultrafine grade for high density |
| 22-75 microns | Most commonly used size range |
| 75-150 microns | Coarser sizes for improved flowability |
| Apparent density | Details |
| Up to 50% of true density | For irregular powder morphology |
| 4.5-5.5 g/cc | Higher for spherical powders |
| Method | Details |
| Gas atomization | High pressure inert gas breaks up molten metal stream into fine droplets |
| Water atomization | High pressure water jet breaks metal into fine particles |
| Vacuum induction melting | High purity input materials melted under vacuum |
| Multiple remelting | Improves chemical homogeneity |
| Sieving | Classifies powder into different particle size ranges |
| Recommendation | Reason |
| Ensure proper ventilation | Prevent exposure to fine metallic particles |
| Avoid ignition sources | Powder can combust in oxygen atmosphere |
| Follow safe protocols | Reduce health and fire hazards |
| Use non-sparking tools | Prevent possibility of ignition |
| Store sealed containers | Prevent contamination or oxidation |
| Test | Details |
| Chemical analysis | ICP and XRF verify composition |
| Particle size analysis | Determines particle size distribution |
| Apparent density | Measured as per ASTM B212 standard |
| Powder morphology | SEM imaging of particle shape |
| Flow rate testing | Gravity flow rate through specified funnel |
| Loss on ignition | Determines moisture content |
| Parameter | GH4169 | 17-4PH | 15-5PH |
| Density | 7.9 g/cc | 7.7 g/cc | 7.8 g/cc |
| Hardness | 40-45 HRC | 38-45 HRC | 36-42 HRC |
| Tensile strength | 1300-1600 MPa | 1200-1450 MPa | 1050-1400 MPa |
| Corrosion resistance | Excellent | Very good | Good |
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GH5188 Powder
GH5188 Powder
| Product | GH5188 Powder |
| CAS No. | N/A |
| Appearance | Metallic Gray or Dark Gray Powder |
| Purity | ≥99%,  ≥99.9%,  ≥95%(Other purities are also available) |
| APS | 1-5 µM, 10-53 µM  (Can be customized),  Ask for other available size range. |
| Ingredient | CoCrNiW |
| Density | 9.10g/cm3 |
| Molecular Weight | N/A |
| Product Codes | NCZ-DCY-291/25 |
GH5188 Description:
GH5188 Powder is one of the numerous advanced ceramic materials manufactured by Nanochemazone. Nanochemazone produces too many standard grades when applicable, including Mil Spec (military grade); ACS, Reagent and Technical Grade; Food, Agricultural and Pharmaceutical Grade; Optical Grade, USP and EP/BP (European Pharmacopoeia/British Pharmacopoeia) and follows applicable ASTM testing standards. Typical and custom packaging is available. Additional technical, research and safety (MSDS) information are available. Please request a quote above for more information on lead time and pricingGH5188 Powder Related Information :
Storage Conditions: Airtight sealed, avoid light and keep dry at room temperature. Please contact us for customization and price inquiry Email: contact@nanochemazone.com Note: We supply different size ranges of Nano and micron as per the client’s requirements and also accept customization in various parameters. GH5188 Powder GH5188 is a W-strengthened diamond-based high-temperature alloy. GH5188 has good mechanical properties and excellent high temperature oxidation resistance. It is suitable for aviation parts that require tensile strength below 980°C and oxidation resistance below 1100°C. GH5188 is a W-strengthened diamond-based high-temperature alloy. GH5188 has good mechanical properties and excellent high temperature oxidation resistance. It is suitable for aviation parts that require tensile strength below 980°C and oxidation resistance below 1100°C. Physical Properties| Size range | Size distribution | Hall flow rate | Bulk density | Tap density | ||
| D10(μm) | D50(μm) | D90(μm) | ||||
| 15-53μm | 17-22 | 32-38 | 52-58 | ≤18s/50g | ≥4.80g/cm³ | ≥5.40g/cm³ |
| Test temperature | Tensile strength (σb/Mpa) | Yield strength (σp0.2/Mpa) | Elongation (δ5/%) |
| 25℃ | 900 | 400 | ≥45 |
| 650℃ | 650 | 280 | ≥50 |
| 900℃ | 300 | 240 | ≥50 |
| 950℃ | 200 | 170 | ≥50 |
| 1000℃ | 160 | 130 | ≥50 |
| Element | C | Cr | Ni | Co | W | Fe |
| wt％ | 0.05-0.15 | 20.00-24.00 | 20.00-24.00 | Bal | 13.00-16.00 | ≤3.00 |
| Element | B | La | Mn | Si | P | S |
| wt％ | ≤0.015 | 0.03-0.12 | ≤1.25 | 0.20-0.50 | ≤0.02 | ≤0.015 |
| Element | Cu | O | N | – | – | – |
| wt％ | ≤0.07 | ≤0.025 | ≤0.015 | – | – | – |
IN939 Powder
IN939 Powder
| Product | IN939 Powder |
| CAS No. | N/A |
| Appearance | Gray Powder |
| Purity | ≥99%,  ≥99.9%,  ≥95%(Other purities are also available) |
| APS | 1-5 µM, 10-53 µM  (Can be customized),  Ask for other available size range. |
| Ingredient | C6H6N6O6 |
| Density | 8.15g/cm3 |
| Molecular Weight | N/A |
| Product Codes | NCZ-DCY-280/25 |
IN939 Description:
IN939 Powder is one of the numerous advanced ceramic materials manufactured by Nanochemazone. Nanochemazone produces too many standard grades when applicable, including Mil Spec (military grade); ACS, Reagent and Technical Grade; Food, Agricultural and Pharmaceutical Grade; Optical Grade, USP and EP/BP (European Pharmacopoeia/British Pharmacopoeia) and follows applicable ASTM testing standards. Typical and custom packaging is available. Additional technical, research and safety (MSDS) information are available. Please request a quote above for more information on lead time and pricingIN939 Powder Related Information :
Storage Conditions: Airtight sealed, avoid light and keep dry at room temperature. Please contact us for customization and price inquiry Email: contact@nanochemazone.com Note: We supply different size ranges of Nano and micron as per the client’s requirements and also accept customization in various parameters. Best IN939 Powder for 3D Printing in 2024 IN939 powder is a nickel-based superalloy that exhibits exceptional mechanical properties and high resistance to corrosion and oxidation. It is primarily composed of nickel, chromium, cobalt, molybdenum, and tantalum. This composition gives IN939 powder its remarkable strength, heat resistance, and stability at elevated temperatures. Overview of IN939 Powder for 3D Printing IN939 is a high-performance nickel-based superalloy powder designed for additive manufacturing of critical components needing exceptional mechanical properties at high temperatures. This article provides a comprehensive guide to IN939 powder for 3D printing applications across aerospace, automotive, energy and industrial sectors. Key aspects covered include IN939 composition, properties, print parameters, applications, specifications, suppliers, handling, inspection, comparisons to alternatives, advantages and limitations, and frequently asked questions. Quantitative data is presented in easy-to-reference tables. Composition of IN939 Powder IN939 has a complex precipitation hardening alloy composition:| Element | Weight % | Purpose |
| Nickel | Balance | Principal matrix element |
| Chromium | 15 – 18 | Oxidation resistance |
| Aluminum | 3.8 – 4.8 | Precipitation hardening |
| Titanium | 0.9 – 1.4 | Precipitation hardening |
| Cobalt | 12 – 15 | Solid solution strengthening |
| Tantalum | 3.8 – 4.8 | Carbide former |
| Carbon | 0.05 – 0.15 | Carbide former |
| Boron | 0.006 – 0.012 | Grain boundary strengthener |
| Property | Description |
| High strength | Excellent tensile and creep rupture strength up to 1050°C |
| Thermal stability | Strength maintained up to 1000°C |
| Creep resistance | High stress-rupture life at high temperatures |
| Oxidation resistance | Forms protective Cr2O3 oxide scale |
| Thermal fatigue resistance | Resists cracking during thermal cycling |
| Phase stability | Microstructure stable after prolonged exposures |
| Corrosion resistance | Resistant to hot corrosion, oxidation, sulfidation |
| Parameter | Typical value | Purpose |
| Layer thickness | 20-50 μm | Resolution vs build speed |
| Laser power | 250-500 W | Sufficient melting without evaporation |
| Scan speed | 800-1200 mm/s | Density vs production rate |
| Hatch spacing | 100-200 μm | Mechanical properties |
| Support structure | Minimal | Easy removal |
| Hot isostatic pressing | 1160°C, 100 MPa, 3h | Eliminate porosity |
| Industry | Components |
| Aerospace | Turbine blades, vanes, combustors |
| Power generation | Hot gas path parts, heat exchangers |
| Automotive | Turbocharger wheels, valves |
| Chemical processing | Pumps, valves, reaction vessels |
| Parameter | Specification |
| Particle size | 15-45 μm typical |
| Particle shape | Spherical morphology |
| Apparent density | > 4 g/cc |
| Tap density | > 6 g/cc |
| Hall flow rate | > 23 sec for 50 g |
| Purity | >99.9% |
| Oxygen content | <100 ppm |
| Method | Parameters Tested |
| Sieve analysis | Particle size distribution |
| SEM imaging | Particle morphology |
| EDX | Chemistry and composition |
| XRD | Phases present |
| Pycnometry | Density |
| Hall flow rate | Powder flowability |
| Alloy | High Temperature Strength | Cost | Printability | Ductility |
| IN939 | Excellent | High | Excellent | Low |
| IN738 | Good | Medium | Excellent | Medium |
| IN718 | Fair | Low | Good | Excellent |
| Hastelloy X | Excellent | High | Fair | Medium |
| Pros | Cons |
| Exceptional high temperature strength | Expensive compared to IN718 |
| Excellent oxidation and creep resistance | Significant parameter optimization needed |
| Complex geometries feasible | Limited room temperature ductility |
| Faster processing than cast/wrought | Controlled storage and handling environment |
| Comparable properties to cast alloy | Difficult to machine after printing |
Inconel 718 Powder
Inconel 718 Powder
| Product | Inconel 718 Powder |
| CAS No. | 7440-02-0 |
| Appearance | Gray Metallic  Powder |
| Purity | ≥99%,  ≥99.9%,  ≥95%(Other purities are also available) |
| APS | 1-5 µM, 10-53 µM  (Can be customized),  Ask for other available size range. |
| Ingredient | Ne-Fe-Cr |
| Density | 8.19g/cm3 |
| Molecular Weight | N/A |
| Product Codes | NCZ-DCY-277/25 |
Inconel 718 Description:
Inconel 718 Powder is one of the numerous advanced ceramic materials manufactured by Nanochemazone. Nanochemazone produces too many standard grades when applicable, including Mil Spec (military grade); ACS, Reagent and Technical Grade; Food, Agricultural and Pharmaceutical Grade; Optical Grade, USP and EP/BP (European Pharmacopoeia/British Pharmacopoeia) and follows applicable ASTM testing standards. Typical and custom packaging is available. Additional technical, research and safety (MSDS) information are available. Please request a quote above for more information on lead time and pricingInconel 718 Powder Related Information :
Storage Conditions: Airtight sealed, avoid light and keep dry at room temperature. Please contact us for customization and price inquiry Email: contact@nanochemazone.com Note: We supply different size ranges of Nano and micron as per the client’s requirements and also accept customization in various parameters. Best in718 powder inconel 718 powder for metal 3D printing inconel 718 powder Overview Inconel 718 powder is a high-performance alloy powder used in additive manufacturing (AM) processes, such as laser powder bed fusion (LPBF) and electron beam powder bed fusion (EBPBF). It is renowned for its exceptional strength, corrosion resistance, and high-temperature capabilities. Inconel 718 powder is widely employed in demanding industries like aerospace, energy, and medical. inconel 718 powder Composition and Characteristics Inconel 718 powder is an alloy primarily composed of nickel (Ni), chromium (Cr), iron (Fe), and niobium (Nb). Its specific composition varies slightly depending on the manufacturer and application requirements. The table below highlights the typical composition and characteristics of Inconel 718 powder:| Property | Value |
| Nickel (Ni) | 50-55% |
| Chromium (Cr) | 17-21% |
| Iron (Fe) | 17-21% |
| Niobium (Nb) | 4.75-5.5% |
| Molybdenum (Mo) | 2.8-3.3% |
| Titanium (Ti) | 0.65-1.15% |
| Aluminum (Al) | 0.2-0.8% |
| Carbon (C) | 0.08% max |
| Silicon (Si) | 0.35% max |
| Manganese (Mn) | 0.35% max |
| Sulfur (S) | 0.015% max |
| Phosphorus (P) | 0.015% max |
| Industry | Applications |
| Aerospace | Turbine blades, engine components, structural parts |
| Energy | Gas turbine components, heat exchangers, pressure vessels |
| Medical | Surgical instruments, implants, dental prosthetics |
| Automotive | High-performance engine components, exhaust systems |
| Defense | Armor, weapons, aerospace components |
| Parameter | Details |
| Specifications | ASTM B163, AMS 5848, ISO 2076 |
| Sizes | 15-150 microns (typical) |
| Grades | Inconel 718, Inconel 718Plus |
| Pros | Cons |
| High strength and hardness | Expensive compared to other alloys |
| Excellent corrosion resistance | Difficult to machine |
| High-temperature capabilities | Requires specialized welding techniques |
| Good weldability and formability | Can be susceptible to stress corrosion cracking |
Inconel 718 Powder
Inconel 718 Powder
| Product | Inconel 718 Powder |
| CAS No. | N/A |
| Appearance | Gray Metallic Powder |
| Purity | ≥99%,  ≥99.9%,  ≥95%(Other purities are also available) |
| APS | 1-5 µM, 10-53 µM  (Can be customized),  Ask for other available size range. |
| Ingredient | Ne-Fe-Cr |
| Density | 8.192g/cm3 |
| Molecular Weight | N/A |
| Product Codes | NCZ-DCY-281/25 |
Inconel 718 Description:
Inconel 718 Powder is one of the numerous advanced ceramic materials manufactured by Nanochemazone. Nanochemazone produces too many standard grades when applicable, including Mil Spec (military grade); ACS, Reagent and Technical Grade; Food, Agricultural and Pharmaceutical Grade; Optical Grade, USP and EP/BP (European Pharmacopoeia/British Pharmacopoeia) and follows applicable ASTM testing standards. Typical and custom packaging is available. Additional technical, research and safety (MSDS) information are available. Please request a quote above for more information on lead time and pricingInconel 718 Powder Related Information :
Storage Conditions:. Airtight sealed, avoid light and keep dry at room temperature. Please contact us for customization and price inquiry Email: contact@nanochemazone.com Note: We supply different size ranges of Nano and micron as per the client’s requirements and also accept customization in various parameters. Best inconel 718 powder for 3D printing Inconel 718 powder (IN718) is a well-known nickel-based superalloy powder that is extensively used in high-value-added engineering applications such as jet engines in aerospace and steam generators in nuclear power plants, as well as in the defense and marine sectors.| Metal Powder | Size | Quantity | Price/kg | Size | Quantity | Price/kg |
| Inconel 718 | 0-20μm | 1KG | 60.9 | 53-105μm | 1KG | 59 |
| 10KG | 39.8 | 10KG | 38 | |||
| 100KG | 34.5 | 100KG | 33 |
| Element | Weight % | Purpose |
| Nickel | 50 – 55 | Principal matrix element |
| Chromium | 17 – 21 | Oxidation resistance |
| Iron | Balance | Solid solution strengthener |
| Niobium | 4.75 – 5.5 | Precipitation hardening |
| Molybdenum | 2.8 – 3.3 | Solid solution strengthening |
| Titanium | 0.65 – 1.15 | Carbide former |
| Aluminum | 0.2 – 0.8 | Precipitation hardening |
| Carbon | 0.08 max | Carbide former |
| Property | Description |
| High strength | Tensile strength 1050 – 1350 MPa |
| Phase stability | Retains strength after prolonged use up to 700°C |
| Corrosion resistance | Resistant to aqueous corrosion and oxidation |
| Weldability | Readily weldable with matching filler |
| Fabricability | Easy to form and machine |
| Creep resistance | High stress rupture strength at high temperatures |
| Parameter | Typical value | Purpose |
| Layer height | 20 – 50 μm | Balance speed and resolution |
| Laser power | 195 – 350 W | Sufficient melting without evaporation |
| Scan speed | 700 – 1300 mm/s | Density versus build rate |
| Hatch spacing | 80 – 160 μm | Mechanical properties |
| Support structure | Minimal | Easy removal |
| Hot isostatic pressing | 1120°C, 100 MPa, 3h | Eliminate internal voids |
| Industry | Components |
| Aerospace | Turbine blades, disks, hot section parts |
| Oil & gas | Downhole tools, valves, pumps |
| Power generation | Combustion cans, transition ducts |
| Automotive | Turbocharger wheels, exhaust valves |
| Medical | Orthopedic implants, surgical tools |
| Parameter | Specification |
| Particle size range | 10 – 45 μm |
| Particle shape | Spherical morphology |
| Apparent density | > 4 g/cc |
| Tap density | > 6 g/cc |
| Hall flow rate | > 23 sec for 50 g |
| Purity | >99.9% |
| Oxygen content | <100 ppm |
| Method | Parameters Tested |
| Sieve analysis | Particle size distribution |
| SEM imaging | Particle morphology |
| EDX | Chemistry and composition |
| XRD | Phases present |
| Pycnometry | Density |
| Hall flow rate | Powder flowability |
| Alloy | Cost | Printability | Weldability | Strength |
| Inconel 718 | Low | Good | Excellent | Medium |
| Inconel 625 | Medium | Excellent | Excellent | Low |
| Inconel 939 | Very High | Fair | Limited | Excellent |
| Haynes 282 | High | Good | Limited | Excellent |
| Pros | Cons |
| Proven material credentials in AM | Lower high temperature strength than some alloys |
| Excellent weldability and machinability | Susceptible to solidification cracking during printing |
| Readily printed into complex shapes | Requires controlled atmosphere handling |
| Cost advantage over exotic superalloys | Significant post-processing often required |
| Available from range of suppliers | Relatively low hardness after printing |
Nickel-based K403 Powder
Nickel-based K403 Powder
| Product | Nickel-based K403 Powder |
| CAS No. | 7440-02-0 |
| Appearance | Gray Powder |
| Purity | ≥99%,  ≥99.9%,  ≥95%(Other purities are also available) |
| APS | 1-5 µM, 10-53 µM  (Can be customized),  Ask for other available size range. |
| Ingredient | Ni-Cr-Co-Al-Mo-W-Ti-C-B |
| Density | 8.2g/cm3 |
| Molecular Weight | N/A |
| Product Codes | NCZ-DCY-294/25 |
Nickel-based K403 Description:
Nickel-based K403 Powder is one of the numerous advanced ceramic materials manufactured by Nanochemazone. Nanochemazone produces too many standard grades when applicable, including Mil Spec (military grade); ACS, Reagent and Technical Grade; Food, Agricultural and Pharmaceutical Grade; Optical Grade, USP and EP/BP (European Pharmacopoeia/British Pharmacopoeia) and follows applicable ASTM testing standards. Typical and custom packaging is available. Additional technical, research and safety (MSDS) information are available. Please request a quote above for more information on lead time and pricingNickel-based K403 Powder Related Information :
Storage Conditions: Airtight sealed, avoid light and keep dry at room temperature. Please contact us for customization and price inquiry Email: contact@nanochemazone.com Note: We supply different size ranges of Nano and micron as per the client’s requirements and also accept customization in various parameters. Nickel-based K403 Powder K403 powder is a nickel-chromium-iron-molybdenum alloy powder. It offers excellent resistance to oxidation, corrosion and thermal fatigue cracking. K403 has good phase stability at high temperatures. K403 powder is designed for protective coatings, thermal spray, welding, brazing, and other high temperature applications. Overview of Nickel-based K403 Powder K403 powder is a nickel-chromium-iron-molybdenum alloy powder. It offers excellent resistance to oxidation, corrosion and thermal fatigue cracking. K403 has good phase stability at high temperatures. Key features of K403 powder include: Outstanding high temperature strength and creep resistance Resists oxidation and hot corrosion up to 1150°C Retains properties under cyclic heating conditions Compatible coefficient of expansion with common alloys Available in various size ranges and morphologies K403 powder is designed for protective coatings, thermal spray, welding, brazing, and other high temperature applications. This article provides a detailed look at the composition, properties, applications, specifications, pricing, safety, and other essential information about nickel-based K403 powder. Composition of Nickel-based K403 Powder The typical composition of nickel-based K403 powder is:| Element | Composition |
| Nickel (Ni) | Balance |
| Chromium (Cr) | 21-23% |
| Iron (Fe) | 17-20% |
| Molybdenum (Mo) | 8-10% |
| Tungsten (W) | 1-2% |
| Manganese (Mn) | ≤0.5% |
| Silicon (Si) | ≤0.5% |
| Carbon (C) | ≤0.1% |
| Property | Details |
| Density | 8.2 g/cm3 |
| Melting Point | 1350-1400°C |
| Thermal Conductivity | 11 W/m.K |
| Electrical Resistivity | 94 microhm-cm |
| Young’s Modulus | 207 GPa |
| Poisson’s Ratio | 0.29-0.30 |
| Tensile Strength | ≥ 550 MPa up to 1050°C |
| Elongation | 15-25% |
| Hardness | 30-35 HRC |
| Oxidation Resistance | Excellent isothermal up to 1150°C |
| Parameter | K403 Powder | IN738 Powder |
| Composition | Ni-Cr-Fe-Mo | Ni-Cr-Co-Al-Ti |
| Oxidation Resistance | Excellent up to 1150°C | Very Good up to 1100°C |
| Cost | Higher | Lower |
| Phase Stability | Very Good | Poor |
| Mechanical Strength | High up to 1050°C | Good up to 750°C |
| Fabrication | Medium | Easy |
| Applications | Thermal spray, welding | Turbine components, AM parts |
| Availability | Moderate | Readily available |
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