GH3536 Alloy Powder
$0.00
GH3536 Alloy Powder
| Product | GH3536 Alloy Powder |
| CAS No. | N/A |
| Appearance | Â Gray to 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-Cr-Mo-Co-W |
| Density | 8.3g/cm3 |
| Molecular Weight | N/A |
| Product Codes | NCZ-DCY-286/25 |
GH3536 Alloy Description:
GH3536 Alloy 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
GH3536 Alloy 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.
GH3536 Alloy Powder
GH3536 alloy powder is a nickel-based superalloy powder used for additive manufacturing applications requiring high strength and corrosion resistance at elevated temperatures. As an advanced powder metallurgy product, GH3536 allows complex geometries to be fabricated using laser or electron beam-based metal 3D printing processes.
GH3536 alloy powder was designed specifically for additive manufacturing, using composition optimization and powder atomization techniques to achieve superior properties compared to conventional nickel superalloys. The key features of GH3536 alloy powder include:
High strength at temperatures up to 760°C (1400°F)
Oxidation and corrosion resistance in harsh environments
Excellent thermal fatigue life and crack growth resistance
Good printability and low porosity in printed parts
Can be age hardened to optimize strength and ductility
The combination of properties make GH3536 suitable for aerospace, power generation, oil & gas, and chemical processing components exposed to extreme temperatures and stresses. Both new part fabrication and repair of worn components can benefit from using this advanced powder.
GH3536 Alloy Powder Composition
GH3536 has a complex composition designed to provide an optimal balance of properties. The nominal composition is shown below:
| Element | Weight % |
| Nickel (Ni) | Balance |
| Chromium (Cr) | 13.5 – 16.0 |
| Cobalt (Co) | 12.0 – 15.0 |
| Tungsten (W) | 5.0 – 7.0 |
| Tantalum (Ta) | 3.0 – 5.0 |
| Aluminum (Al) | 2.8 – 3.8 |
| Titanium (Ti) | 0.5 – 1.5 |
| Niobium (Nb) | 0.5 – 1.5 |
| Hafnium (Hf) | 0.2 – 0.8 |
| Carbon (C) | 0.05 – 0.15 |
| Boron (B) | 0.01 – 0.03 |
| Zirconium (Zr) | 0.01 – 0.05 |
Nickel forms the matrix, while elements like chromium, cobalt, and aluminum improve oxidation resistance. Refractory elements tantalum, tungsten, niobium, and hafnium contribute to strength at elevated temperatures. Titanium and niobium strengthen the alloy through carbide formation. Trace amounts of carbon, boron, and zirconium enhance precipitation hardening.
The powder composition is designed to limit segregation and maintain composition uniformity during printing, ensuring consistent properties in the final part. The spherical powder morphology also improves flowability and packing density for good printability.
GH3536 Alloy Powder Properties
GH3536 exhibits an excellent combination of strength, ductility, and environmental resistance owing to its tailored composition and optimized production process. The key properties are summarized below:
Mechanical Properties
| Property | As-printed | Aged |
| Tensile Strength | 1050 – 1250 MPa (152 – 181 ksi) | 1275 – 1400 MPa (185 – 203 ksi) |
| Yield Strength (0.2% offset) | 900 – 1100 MPa (131 – 160 ksi) | 1150 – 1300 MPa (167 – 189 ksi) |
| Elongation | 25 – 35% | 16 – 22% |
| Hardness | 32 – 38 HRC | 36 – 43 HRC |
Physical Properties
| Property | Typical Value |
| Density | 8.3 g/cm3 |
| Melting Point | 1310°C (2390°F) |
Thermal Properties
| Property | Temperature |
| Coefficient of Thermal Expansion | 12.8 x 10-6/°C at 20-100°C |
| Thermal Conductivity | 11.4 W/m-K at 20°C |
| Specific Heat | 0.43 J/g-°C at 20°C |
Oxidation Resistance
Resists oxidation in air up to ~980°C. Protective Cr2O3 oxide scale forms.
Better oxidation resistance than Inconel 718 and many other Ni alloys.
Corrosion Resistance
Excellent resistance to hot corrosion and sulfidation.
Resists many organic acids, chlorides, caustics.
Other Properties
Retains strength and ductility after prolonged exposures up to 760°C.
Excellent thermal fatigue life. Resists crack growth.
Low coefficient of friction and galling resistance.
The strength of GH3536 in the aged condition exceeds that of conventional nickel superalloys like Inconel 718 while maintaining robust ductility. The alloy is stronger than many stainless steels at high temperatures. Oxidation resistance approaches that of nickel-chromium alloys like Inconel 601. Overall, GH3536 provides an exceptional balance of properties for critical applications.
Applications of GH3536 Alloy Powder
The combination of strength, environmental resistance, printability, and ease of post-processing makes GH3536 suitable for:
Aerospace Components
Turbine blades, vanes, combustors
Structural parts, landing gear
Rocket engine nozzles, thrusters
Hypersonic vehicle hot structures
Power Generation
Gas turbine hot section parts
Heat exchangers, recuperators
Heat shields, thermowells
Oil & Gas
Downhole tools, wellhead parts
Valves, pumps for corrosive services
Automotive
Turbocharger wheels and housings
Exhaust components
Chemical Processing
Valves, pumps, reaction vessels
Heat exchanger tubing
Tooling
Injection molds with conformal cooling
Die casting dies, hot stamping tools
Others
Heating elements
Radioactive waste containers
Specialty fasteners and springs
GH3536 can replace existing parts made of lower performance materials to improve durability and efficiency. The powder is also ideal for fabricating new designs not possible with conventional manufacturing. Both new part production and repair/refurbishment of worn components are enabled.
Printing GH3536 Alloy Powder
GH3536 powder can be successfully printed using laser powder bed fusion (L-PBF) and electron beam powder bed fusion (E-PBF) processes. The spherical powder morphology provides good flow and packing. Key considerations include:
Printing Process
Laser and electron beam powder bed technologies applicable.
Process parameters require development for new machines.
Inert gas chamber atmosphere (argon or nitrogen).
Powder specification
Particle size range 10-45 μm, D50 ~25 μm typical.
Apparent density 2.5-3.5 g/cm3.
Flow rate 25-35 s (Hall flowmeter).
Printing Recommendations
Preheating baseplate to ~150°C reduces thermal stresses.
Scan speeds from 400-1000 mm/s are typical.
Hatch spacing 0.08-0.12 mm for good densification.
100% fresh powder for reuse.
Post Processing
Stress relieving: 1080°C/2hr, air cool.
Aging: 760°C/8-16 hr, air cool.
Hot isostatic pressing can further reduce porosity.
With parameter optimization, densities over 99.8% are possible. The microstructure consists of fine, uniform grains suitable for critical applications.
Specifications of GH3536 Powder
GH3536 alloy powder is commercially available in the standard size distribution and classes summarized below. Custom variations can also be produced.
| Powder Size Distribution | |
| D10 | 10 μm |
| D50 | 25 μm |
| D90 | 45 μm |
| Powder Classes | Nominal Flow Rate | Apparent Density |
| Class I | 25 s | 2.5 g/cm3 |
| Class II | 28 s | 2.8 g/cm3 |
| Class III | 32 s | 3.2 g/cm3 |
Other specifications:
Spherical morphology with satellite fraction under 1%.
Oxygen content under 100 ppm.
No binders or lubricants added.
Each powder lot is provided with a Certificate of Analysis detailing composition, particle characteristics, flow rate, and other parameters.
Handling and Storage of GH3536
To maintain powder quality during handling and storage:
Store sealed powder containers in a cool, dry environment. Desiccant is recommended.
Avoid exposing powder to moisture which can cause clumping and flow issues.
Limit temperature excursions during transport and storage.
Open containers only in an inert atmosphere glove box or argon chamber.
Immediately process open containers to limit oxidation. Do not reuse exposed powder.
Use appropriate PPE and avoid inhalation or contact with skin and eyes.
With proper handling, GH3536 powder has a shelf life exceeding one year from manufacture date. FIFO inventory management is recommended.
As an alloy powder containing nickel and other elements, standard safety precautions should be taken during handling:
Use PPE: Powder suitable respirator, gloves, eye protection, protective clothing.
Avoid skin contact or inhalation of dusts during handling.
Properly ground all powder handling equipment. Inert gas glove boxes recommended.
Use dust collection during cleanup. Avoid generating airborne dust.
Dispose of excess powder and cleanup debris appropriately.
Refer to SDS document for additional safety information.
Nickel powder is classified as a suspected carcinogen. Follow all laws and regulations for safe metal powder handling.
Inspection of GH3536 Powder
To ensureGH3536 powder meets application requirements, the following inspection procedures can be used:
Particle Size Distribution
Laser diffraction analysis (ISO 13320)
Sieve analysis (ASTM B214)
Morphology & Microstructure
Scanning electron microscopy
Optical microscopy of mounted and polished specimens
Powder Composition
Inductively coupled plasma mass spectrometry (ASTM E1097)
Inert gas fusion for O and N (ASTM E1019)
Powder Density
Apparent density (Hall flowmeter)
Tap density (ASTM B527)
Powder Flowability
Hall flowmeter (ASTM B213)
Revolution powder analyzer
Lot Acceptance
Sampling per ASTM B215
Verify powder meets size, composition, morphology specifications
Testing should be conducted for each powder lot to verify conformance to applicable ASTM standards. This ensures consistent, high quality powder feedstock for printing.
FAQs
Q: What makes GH3536 better than other Ni superalloys for AM?
A: GH3536 has higher strength than workhorse alloys like Inconel 718 while maintaining ductility. The powder composition and atomization process minimize segregation and porosity.
Q: Does GH3536 require hot isostatic pressing (HIP) after printing?
A: HIP can further reduce internal porosity but is not required to achieve high densities (>99.5%) with optimized AM parameters. HIP may allow higher service temperatures.
Q: What post processing is required after printing GH3536?
A: A simple stress relief heat treatment can be used after printing. For optimal strength, an aging heat treatment is recommended.
Q: What are the lead times for purchasing GH3536 powder?
A: Small lots can ship in 2-4 weeks. Allow 3-5 months for large production volumes depending on availability.
Q: Does GH3536 contain aluminum or titanium to cause issues during printing?
A: The Al and Ti concentrations are balanced to avoid powder oxidation or excessive reaction with the melt pool during printing.
Q: What particle size distribution is recommended for printing GH3536?
A: A distribution with D10 of 10 μm, D50 of 25 μm, and D90 of 45 μm provides a good balance of flowability and printing.
Q: Can GH3536 be used for printing parts with overhangs and complex geometries?
A: Yes, GH3536 has demonstrated excellent printability for parts with overhangs exceeding 45° overhang angle.
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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| Product | GH 3625 Powder |
| CAS No. | 3526-43-0 |
| 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. |
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| Molybdenum | 8-10% |
| Tantalum | 5-6% |
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| Thermal Conductivity | 11-12.5 W/mK |
| Coefficient of Thermal Expansion | 12.5-13.5 x 10<sup>-6</sup>/K |
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| Poission’s Ratio | 0.29-0.33 |
| Tensile Strength | 1050-1280 MPa |
| Yield Strength (0.2% offset) | 860-1050 MPa |
| Elongation | 8-15% |
| Hardness | 32-38 HRC |
| Industry | Components |
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| Alloy Modifications | With B, C, Zr, Nb, Ta |
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| Density | High | Medium | High |
| Strength | Medium | Very High | Medium |
| Hardness | High | Medium | Very High |
| Wear Resistance | Medium | Low | Very High |
| Corrosion Resistance | Medium | High | Medium |
| Oxidation Resistance | Medium | High | Medium |
| Thermal Stability | Up to 1000°C | Up to 700°C | Up to 900°C |
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GH3230 Powder
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| Appearance | Metallic Gray Powder |
| Purity | ≥99%,  ≥99.9%,  ≥95%(Other purities are also available) |
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| Size range | 10-45 microns |
| Apparent density | Up to 60% of true density |
| Flowability | Good |
| Strength | Very high after aging treatment |
| Corrosion resistance | Excellent including pitting and crevice corrosion |
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| 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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| 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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| Yield strength | Aged | 1400-1800 MPa |
| Elongation | Aged | 8-12% |
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| Chemical processing | Extruder screws, valve parts |
| Power generation | Boiler components, steam and gas turbines |
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| Appearance | Gray Dull Silver Powder |
| Purity | ≥99%,  ≥99.9%,  ≥95%(Other purities are also available) |
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| Size range | Size distribution | Hall flow rate | Bulk density | Tap density | ||
| D10(μm) | D50(μm) | D90(μm) | ||||
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| 815°C high temperature durability performance | |||
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| 690 | 80 | 5 | |
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| 25℃ | 1270 | 1030 | 12 |
| 650℃ | 1000 | 860 | 12 |
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| Product | GH5188 Powder |
| CAS No. | N/A |
| Appearance | Metallic Gray or Dark Gray Powder |
| Purity | ≥99%,  ≥99.9%,  ≥95%(Other purities are also available) |
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| 650℃ | 650 | 280 | ≥50 |
| 900℃ | 300 | 240 | ≥50 |
| 950℃ | 200 | 170 | ≥50 |
| 1000℃ | 160 | 130 | ≥50 |
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| Element | B | La | Mn | Si | P | S |
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| wt％ | ≤0.07 | ≤0.025 | ≤0.015 | – | – | – |
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| 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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