GH3230 Powder

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GH3230 Powder

Product	GH3230 Powder
CAS No.	3230-94-2
Appearance	Metallic 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-Mo-W-Fe
Density	7.8g/cm3
Molecular Weight	N/A
Product Codes	NCZ-DCY-285/25

GH3230 Description:

GH3230 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

GH3230 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.

GH3230 is a W-Mo reinforced nickel-based high-temperature alloy, which is usually used in an environment of 700-1000°C. GH3230 alloy has high high-temperature strength and good fatigue properties. And due to its excellent organizational stability, it has good anti-oxidation and anti-hot corrosion properties.

GH3230 Powder is a W-Mo reinforced nickel-based high-temperature alloy, which is usually used in an environment of 700-1000°C. GH3230 alloy has high high-temperature strength and good fatigue properties. And due to its excellent organizational stability, it has good anti-oxidation and anti-hot corrosion properties, and is widely used in aerospace engine combustion chambers, ground gas turbine combustion chambers, and some high-temperature and corrosion-resistant components in the chemical industry.

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	≥4.60g/cm³	≥5.20g/cm³

Heat Treatment Recommendations

Hot isostatic pressing: 1200±20°C/160Mpa/3h
Solution treatment: 1200±20°C/1h/AC

Mechanical Behavior

Test temperature	Tensile strength (σb/Mpa)	Yield strength (σp0.2/Mpa)	Elongation (δ5/%)
25℃	840	450	35
815℃	250	200	35
1000℃	160	130	30

Chemical Composition Range (Wt,-%)

Element	C	Cr	Ni	Co	W	Mo
wt％	0.05-0.15	20.00-24.00	Bal	≤5.00	13.00-15.00	3.15-4.15
Element	Al	Ti	Fe	La	B	Mn
wt％	2.20-0.50	≤0.10	≤3.00	0.005-0.05	≤0.015	0.30-1.00
Element	Si	P	S	Cu	O	N
wt％	0.25-0.75	≤0.01	≤0.010	≤0.50	≤0.025	≤0.015

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Category: High Temperature Alloy Powder

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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Alloy Series Powder

Product	Alloy Series Powder
CAS No.	12069-94-2
Appearance	Silver-White 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	NiCrCoMoFeAl
Density	2.6-2.8g/cm3
Molecular Weight	N/A
Product Codes	NCZ-DCY-290/25

Alloy Series Description:

Alloy Series 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

Alloy Series Powder Related Information :

Product	Specification	Apparent Density	Flow Ability	Oxygen Content	Tensile Strength	Yield Strength	Elongation
GH3625	15-53µm 45-105µm 75-150µm	≥4.40g/cm³	≤20s/50g	≤300ppm	1000±50Mpa	600±50Mpa	35±5%
GH4169		≥4.20g/cm³	≤20s/50g	≤300ppm	1250±30Mpa	1000±30Mpa	18±3%
GH3230		≥4.40g/cm³	≤20s/50g	≤300ppm	930±30Mpa	930±30Mpa	25±5%
GH3536		≥4.40g/cm³	≤20s/50g	≤300ppm	850±30Mpa	550±20Mpa	42±5%

Process: Vacuum air atomization method Advantages: high sphericity, small satellite powder, good fluidity, and high bulk density. The printed product has good fatigue resistance, anti-oxidation performance and structural stability Applications: aerospace and industrial turbine discs, rings, blades, machine and other structures, aerospace engine combustion chambers Packaging: ordinary packaging such as aluminum foil bags/plastic bottles/iron drums, vacuum packaging or inert gas-filled packaging, etc.

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GH 3625 Powder

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GH 3625 Powder

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.
Ingredient	Ni-Fe-Cr-Mo
Density	N/A
Molecular Weight	213.28g/mol
Product Codes	NCZ-DCY-283/25

GH 3625 Description:

GH 3526 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

GH 3625 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. GH 3625 Powder GH3625 powder is an age-hardenable nickel-iron base alloy containing 25% chromium along with additions of molybdenum and aluminum. It provides an exceptional combination of high strength, hardness, corrosion resistance, and oxidation resistance at elevated temperatures. Overview of GH3625 Powder GH 3625 powder is an age-hardenable nickel-iron base alloy containing 25% chromium along with additions of molybdenum and aluminum. It provides an exceptional combination of high strength, hardness, corrosion resistance, and oxidation resistance at elevated temperatures. Key properties and advantages of GH3625 powder include: GH3625 Powder Properties and Characteristics

Properties	Details
Composition	Ni-25Cr-4.5Mo-3.5Al alloy
Density	8.2 g/cc
Particle shape	Predominantly spherical
Size range	15-45 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

GH3625 is widely used in aerospace, oil and gas, chemical processing, and power generation sectors needing high strength and corrosion resistance at elevated temperatures. GH3625 Powder Composition

Element	Weight %
Nickel	Balance
Chromium	24-27%
Molybdenum	4-5%
Aluminum	3-4%
Carbon	0.1% max
Manganese	1% max
Silicon	0.5% max
Sulfur	0.015% max

Nickel provides corrosion resistance and aids precipitation hardening Chromium significantly improves oxidation and corrosion resistance Molybdenum and aluminum facilitate precipitation strengthening Carbon and other elements limited as impurities The composition is optimized to provide peak strengthening from precipitation hardening as well as excellent corrosion and oxidation resistance. GH3625 Powder Physical Properties

Property	Values
Density	8.2 g/cc
Melting point	1390-1440°C
Thermal conductivity	11 W/mK
Electrical resistivity	52 μΩ-cm
Coefficient of thermal expansion	13.0 x 10^-6 /K

High density compared to steels and titanium alloys Retains high strength at temperatures exceeding 1000°C Relatively low thermal conductivity necessitates design considerations CTE is moderate and similar to stainless steels These properties make GH3625 suitable for high strength applications at elevated temperatures needing corrosion resistance. GH3625 Powder Mechanical Properties

Property	Condition	Values
Hardness	Solution annealed	35 HRC
Hardness	Peak aged	50-56 HRC
Tensile strength	Annealed	1000 MPa
Tensile strength	Aged	1500-1800 MPa
Yield strength	Aged	1200-1600 MPa
Elongation	Aged	10-15%

Ages to very high strength levels exceeding other precipitation hardening alloys Retains reasonable ductility in peak aged condition Hardness increases substantially after aging treatment Strength can be tailored through aging time and temperature These properties make GH3625 suitable for components needing high strength combined with corrosion resistance. GH3625 Powder Applications

Industry	Uses
Aerospace	Turbine blades, bolts, fasteners
Oil and gas	Wellhead valves, downhole tools
Chemical processing	Extruder screws, valve parts
Power generation	Boiler components, steam and gas turbines

Some specific product applications include: Aerospace turbine engine blades, discs and fasteners Bolting for high temperature petrochemical piping Valve components used in corrosive chemical environments Boiler superheater tubes and headers Steam turbine blades and fasteners GH3625 provides exceptional strength and corrosion resistance for critical components used at elevated temperatures across demanding industries. GH3625 Powder Standards

Standard	Description
AMS 5815	Nickel alloy powder compositions
AMS 5408	Wire, rods, and bars of precipitation hardening nickel alloys
AMS 5698	Investment castings of PH nickel alloys
AMS 5772	Nickel alloy forgings
AMS 5634	Nickel alloy extruded shapes

These define: Chemical composition limits of GH3625 Required mechanical properties in different heat treatment conditions Approved powder production method – inert gas atomization Impurity limits for critical elements Compliance testing protocols Proper handling and storage instructions Meeting these certification requirements ensures optimal performance. GH3625 Powder Particle Size Distribution

Particle Size	Characteristics
15-25 microns	Ultrafine powder used in laser AM processes
25-45 microns	Size range for most powder bed AM systems
45-75 microns	Larger sizes used in laser cladding

Finer powder provides higher resolution and surface finish Coarser powder suitable for high deposition rate processes Size distribution tailored based on AM method used Spherical morphology maintained in all sizes Controlling particle size distribution and morphology is critical for AM performance, final part properties and quality. GH3625 Powder Apparent Density

Apparent Density	Details
Up to 60% of true density	For spherical powder morphology
4.5 – 5.2 g/cc	Improves with greater packing density

Spherical powder shape provides high apparent density Higher density improves powder flow and bed packing in AM Reduces entrapped gas porosity in final part Maximizing density minimizes press cycle time Higher apparent density results in better manufacturing productivity and part performance. GH3625 Powder Production Method

Method	Details
Gas atomization	High pressure inert gas breaks up molten metal stream into fine droplets
Vacuum induction melting	High purity input materials melted under vacuum
Multiple remelting	Improves chemical homogeneity
Sieving	Classifies powder into different particle size fractions

Gas atomization with inert gas produces clean spherical powder Vacuum processing minimizes gaseous impurities Multiple remelts improve uniformity of composition Post-processing provides particle size distribution control Automated methods combined with strict quality control result in consistent GH3625 powder suitable for critical applications. GH3625 Powder Handling and Storage

Recommendation	Reason
Ensure proper ventilation	Avoid exposure to fine metallic particles
Use appropriate PPE	Prevent accidental inhalation or ingestion
Follow safe protocols	Reduce health and fire hazards
Store sealed containers	Prevent contamination or oxidation

GH3625 powder is relatively stable but general precautions are still recommended for safe handling and maintaining purity. Storage Recommendations Store in stable containers in a dry, cool area Limit exposure to moisture which can degrade properties Maintain temperatures below 30°C Proper precautions preserve powder condition and prevent safety issues. GH3625 Powder Inspection and Testing

Test	Details
Chemical analysis	OES or XRF spectroscopy used to verify composition
Particle size distribution	Laser diffraction analysis
Apparent density	Measured as per ASTM B212 standard
Powder morphology	SEM imaging of particle shape
Flow rate analysis	Gravity flow rate through specified nozzle
Moisture measurement	Loss on drying analysis

Testing ensures the powder meets the required chemical purity, particle characteristics, density specifications, morphology and flowability per relevant standards. GH3625 Powder Pros and Cons Advantages of GH3625 Powder Exceptional high temperature strength and creep resistance Retains strength and hardness up to 1100°C Excellent corrosion resistance across environments Good fatigue strength and fracture toughness High hardness combined with reasonable ductility Less dense than nickel superalloys Limitations of GH3625 Powder More expensive than stainless steel powders Requires controlled heat treatment for optimal properties Lower wear resistance than cobalt alloys Difficult to machine after sintering Limited cold heading and forming capability Subject to pitting in strongly oxidizing acids Comparison With Inconel 718 Powder GH3625 vs Inconel 718 Powder

Parameter	GH3625	Inconel 718
Density	8.2 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

GH3625 provides higher tensile strength Inconel 718 offers better overall corrosion resistance GH3625 is more cost effective Inconel 718 is preferred for extreme environments GH3625 provides optimal strength and cost balance GH3625 Powder FAQs Q: What are the main applications of GH3625 nickel alloy powder? A: Main applications include aerospace turbine components, oil and gas wellhead valves and downhole tools, power generation parts, chemical processing equipment, and other high temperature components needing strength and corrosion resistance. Q: Why is GH3625 preferred over stainless steel powders in high temperature applications? A: GH3625 retains significantly higher strength compared to stainless steels at temperatures exceeding 650°C. It also provides excellent corrosion resistance in hot corrosive environments. Q: What precautions should be taken when working with GH3625 powder? A: Recommended precautions include ventilation, appropriate PPE, avoiding ignition sources, following safe handling protocols, and storing sealed containers away from moisture, air, and contamination. Q: How does aluminum affect the properties of GH3625 alloy? A: Aluminum enhances precipitation hardening by forming nickel-aluminum precipitates during aging treatment. This provides substantial strengthening while maintaining reasonable ductility.

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GH3230 Powder

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GH3230 Powder

Product	GH3230 Powder
CAS No.	3230-94-2
Appearance	Metallic 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-Mo-W-Fe
Density	7.8g/cm3
Molecular Weight	N/A
Product Codes	NCZ-DCY-284/25

GH3230 Description:

GH3230 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. GH3230 Powder GH3230 powder is an age-hardenable nickel-iron base alloy containing 30% chromium along with additions of molybdenum and aluminum. It offers an exceptional combination of high strength, hardness, corrosion resistance, and oxidation resistance at elevated temperatures. Overview of GH3230 Powder GH3230 powder is an age-hardenable nickel-iron base alloy containing 30% chromium along with additions of molybdenum and aluminum. It offers an exceptional combination of high strength, hardness, corrosion resistance, and oxidation resistance at elevated temperatures. GH3230 Powder Properties and Characteristics

Properties	Details
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
Corrosion resistance	Excellent including pitting and crevice corrosion

GH3230 Powder Composition

Element	Weight %
Nickel	Balance
Chromium	28-32%
Molybdenum	3-5%
Aluminum	1-3%
Carbon	0.1% max
Manganese	1% max
Silicon	0.5% max
Sulfur	0.015% max

Nickel provides corrosion resistance and facilitates precipitation hardening Chromium significantly enhances oxidation and corrosion resistance Molybdenum and aluminum enable precipitation strengthening Carbon and other elements limited as impurities The composition is designed to achieve peak strengthening from precipitation hardening along with excellent corrosion and oxidation resistance. GH3230 Powder Physical Properties

Property	Values
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

High density compared to steels and titanium alloys Retains high strength at temperatures exceeding 1000°C Relatively low thermal conductivity necessitates design considerations CTE is moderate and similar to stainless steels These properties make GH3230 suitable for high strength applications at elevated temperatures needing corrosion resistance. GH3230 Powder Mechanical Properties

Property	Condition	Values
Hardness	Solution annealed	37 HRC
Hardness	Peak aged	52-58 HRC
Tensile strength	Annealed	1100 MPa
Tensile strength	Aged	1600-2000 MPa
Yield strength	Aged	1400-1800 MPa
Elongation	Aged	8-12%

Ages to very high strength levels exceeding other precipitation hardening alloys Retains reasonable ductility in peak aged condition Hardness increases substantially after aging treatment Strength can be tailored through aging time and temperature These exceptional properties make GH3230 suitable for components needing very high strength combined with corrosion resistance. GH3230 Powder Applications

Industry	Uses
Aerospace	Turbine blades, bolts, fasteners
Oil and gas	Wellhead valves, downhole tools
Chemical processing	Extruder screws, valve parts
Power generation	Boiler components, steam and gas turbines

Some specific product applications include: Aerospace turbine engine blades, discs and fasteners Bolting for high temperature petrochemical piping Valve components used in corrosive chemical environments Boiler superheater tubes and headers Steam turbine blades and fasteners GH3230 provides exceptional strength and corrosion resistance needed for critical components used at extreme temperatures across demanding industries. GH3230 Powder Standards

Standard	Description
AMS 5815	Nickel alloy powder compositions
AMS 5408	Wire, rods, bars of precipitation hardening nickel alloys
AMS 5698	Investment castings of PH nickel alloys
AMS 5772	Nickel alloy forgings
AMS 5634	Nickel alloy extruded shapes

These define: Chemical composition limits of GH3230 Required mechanical properties in different heat treatment conditions Approved powder production method – inert gas atomization Impurity limits for critical elements Compliance testing protocols Proper handling and storage instructions Meeting these certification requirements ensures optimal performance. GH3230 Powder Particle Sizes

Particle Size	Characteristics
10-22 microns	Ultrafine powder used in laser AM processes
22-45 microns	Size range for most powder bed AM systems
45-75 microns	Larger sizes used in laser cladding or thermal spraying

Finer powder provides higher resolution and surface finish in AM Coarser powder suitable for high deposition rate processes Size distribution tailored based on AM or other method used Spherical morphology maintained in all sizes Controlling particle size distribution and shape is critical for optimizing processing method performance and final part properties. GH3230 Powder Apparent Density

Apparent Density	Details
Up to 60% of true density	For spherical powder morphology
4.8 – 5.5 g/cc	Improves with greater packing density

Method	Details
Gas atomization	High pressure inert gas breaks up molten metal stream into fine droplets
Vacuum induction melting	High purity input materials melted under vacuum
Multiple remelting	Improves chemical homogeneity
Sieving	Classifies powder into different particle size fractions

Gas atomization with inert gas produces clean spherical powder Vacuum processing minimizes gaseous impurities Multiple remelts improve uniformity of composition Post-processing provides particle size distribution control Automated methods combined with strict quality control result in consistent GH3230 powder suitable for critical applications. GH3230 Powder Handling and Storage

Recommendation	Reason
Ensure proper ventilation	Avoid exposure to fine metallic particles
Use appropriate PPE	Prevent accidental inhalation or ingestion
Follow safe protocols	Reduce health and fire hazards
Store sealed containers	Prevent contamination or oxidation

GH3230 powder is relatively stable but general precautions are still recommended for safe handling and maintaining purity. Storage Recommendations Store in stable containers in a dry, cool area Limit exposure to moisture which can degrade properties Maintain temperatures below 30°C Proper precautions preserve powder condition and prevent safety issues. GH3230 Powder Inspection and Testing

Test	Details
Chemical analysis	OES or XRF spectroscopy used to verify composition
Particle size distribution	Laser diffraction analysis
Apparent density	Measured as per ASTM B212 standard
Powder morphology	SEM imaging of particle shape
Flow rate analysis	Gravity flow rate through specified nozzle
Moisture measurement	Loss on drying analysis

Testing ensures the powder meets the required chemical purity, particle characteristics, density specifications, morphology and flowability per relevant standards. GH3230 Powder Pros and Cons Advantages of GH3230 Powder Excellent high temperature strength and creep resistance Retains strength and hardness up to 1150°C Outstanding corrosion resistance across environments Good fatigue strength and fracture toughness High hardness combined with reasonable ductility Less dense than nickel superalloys Limitations of GH3230 Powder More expensive than stainless steel powders Requires controlled heat treatment for optimal properties Lower wear resistance than cobalt alloys Difficult to machine after sintering Limited cold heading and forming capability Subject to pitting in strongly oxidizing acids Comparison With Inconel 718 Powder GH3230 vs Inconel 718 Powder

Parameter	GH3230	Inconel 718
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 provides higher tensile strength Inconel 718 offers better overall corrosion resistance GH3230 is more cost effective Inconel 718 is preferred for extreme environments GH3230 provides optimal strength and cost balance GH3230 Powder FAQs Q: What are the main applications of GH3230 nickel alloy powder? A: Main applications include aerospace turbine components, oil and gas wellhead valves and downhole tools, chemical processing equipment, power generation parts, and other high temperature components needing exceptional strength and corrosion resistance. Q: Why is GH3230 preferred over stainless steel powders in high temperature applications? A: GH3230 retains significantly higher strength compared to stainless steels at temperatures exceeding 650°C. It also provides excellent corrosion resistance in hot corrosive environments. Q: What precautions should be taken when working with GH3230 powder? A: Recommended precautions include ventilation, appropriate PPE, avoiding ignition sources, following safe handling protocols, and storing sealed containers away from moisture, air, and contamination. Q: How does chromium improve the properties of GH3230 alloy? A: Chromium provides substantial improvement in oxidation and corrosion resistance. It also forms fine precipitates during aging treatment which contribute to precipitation hardening and strengthening.

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GH4169 Powder

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GH4169 Powder

Product	GH4169 Powder
CAS No.	7440-02-0
Appearance	Gray Dull 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	NiCr22Mo9Nb
Density	8.19g/cm3
Molecular Weight	N/A
Product Codes	NCZ-DCY-290/25

GH4169 Description:

GH4169 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

GH4169 Powder Related Information :

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

GH4169 is a Nb-Mo reinforced nickel-based high-temperature alloy. Its normal working environment is 253-650C. It has good mechanical properties below 650C. Under special circumstances, GH4169 can be used at 800°C for a short period of time. GH4169 is suitable for many high temperature applications, such as gas turbine components. 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	≥4.20g/cm³	≥4.80g/cm³

Heat treatment recommendations 980-1060°C/1h/AC+720°C±10°C/8h/F一620C10C/8h/AC Mechanical behavior

815°C high temperature durability performance
Constant stress (δ/Mpa)	Duration(t/h)	Elongation after break(δ5/%)
690	80	5
Test temperature	Tensile strength (σb/Mpa)	Yield strength (σp0.2/Mpa)	Elongation (δ5/%)
25℃	1270	1030	12
650℃	1000	860	12

Chemical composition range (wt,-%)

Element	C	Cr	Ni	Co	Nb	Mo
wt％	0.02-0.06	17.00-21.00	50.00-55.00	≤1.00	4.75-5.50	2.80-3.30
Element	Al	Ti	Fe	B	Mg	Mn
wt％	0.20-0.80	0.65-1.15	Bal	≤0.006	≤0.010	≤0.35
Element	Si	P	S	Cu	O	N
wt％	≤0.35	≤0.015	≤0.015	≤0.30	≤0.020	≤0.015

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Inconel 625 Powder

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Inconel 625 Powder

Product	Inconel 625 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	NiCr22Mo9Nb
Density	8.4g/cm3
Molecular Weight	N/A
Product Codes	NCZ-DCY-292/25

Inconel 625 Description:

Inconel 625 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

Inconel 625 Powder Related Information :

Metal Powder	Size	Quantity	Price/kg	Size	Quantity	Price/kg
Inconel 625	0-20μm	1KG	$59	20-63μm	1KG	$98.30
		10KG	$39		10KG	$69.10
		100KG	$34		100KG	$64.50

Overview GH3625 powder Inconel 625 powder is an alloy powder used for metal additive manufacturing processes like selective laser sintering (SLS) and direct metal laser sintering (DMLS). It is a nickel-based superalloy that offers high strength, corrosion resistance, and excellent high-temperature properties. GH3625 is designed specifically for additive manufacturing to produce complex, dense parts with exceptional mechanical properties comparable to wrought materials. It enables the production of lightweight components with complex geometries for aerospace, automotive, medical, and industrial applications. This guide provides a detailed overview of GH3625 powder covering its composition, properties, applications, specifications, pricing, advantages, and limitations. Comparisons are made to other common alloys like Inconel 718 and Stellite 21 to highlight the performance and suitability of GH3625 for different uses. An FAQ section addresses key questions about this material. GH3625 powder Inconel 625 powder Composition GH3625 has a complex chemical composition designed to provide a combination of high strength, resistance to thermal fatigue, oxidation, and corrosion resistance. Here is an overview of its composition:

Element	Weight %
Nickel	Balance
Chromium	15-17%
Cobalt	10%
Molybdenum	8-10%
Tantalum	5-6%
Aluminum	1.2-1.7%
Titanium	0.5-1.2%
Boron	0.01%

Nickel forms the base of this superalloy providing ductility and toughness. Elements like chromium, cobalt, and molybdenum contribute to high temperature strength through solid solution strengthening. Tantalum provides solid solution strengthening and forms carbide particles for precipitation hardening. Aluminum and titanium form the gamma prime phase Ni3(Al,Ti) to give excellent high temperature mechanical properties. Boron enhances grain boundary strength. The balanced composition gives GH3625 powder excellent weldability compared to precipitation hardening stainless steels. It can be easily post-processed through hot isostatic pressing (HIP), heat treatment, and machining. GH3625 powder Inconel 625 powder Properties

Property	Value
Density	8.1-8.5 g/cc
Melting Point	1260-1335°C
Thermal Conductivity	11-12.5 W/mK
Coefficient of Thermal Expansion	12.5-13.5 x 10<sup>-6</sup>/K
Modulus of Elasticity	156-186 GPa
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

The high melting point, thermal conductivity, and low coefficient of thermal expansion enable good dimensional stability under high temperature service environments up to 1000°C for limited periods. The alloy has excellent tensile and yield strength comparable to wrought materials along with good ductility and fracture toughness. It exhibits high hardness, resistance to wear, galling, and abrasion. The properties allow GH3625 to outperform stainless steels, cobalt alloys, and even rival precipitation hardening nickel superalloys in high temperature strength. It also offers better weldability than Inconel 718. GH3625 powder Inconel 625 powder Applications The combination of high strength, hardness, toughness, and thermal stability makes GH3625 suitable for: GH3625 powder Inconel 625 powder Applications

Industry	Components
Aerospace	Turbine blades, combustor parts, nozzle guide vanes
Automotive	Turbocharger wheels, manifolds, valves
Oil and Gas	Wellhead parts, downhole tools, valves
Power Generation	Heat exchangers, burner components
Chemical Processing	Pump impellers, valves, reaction vessels
Medical	Dental implants, prosthetics, surgical instruments

The ability to 3D print complex geometries allows consolidating multiple parts into single components and lightweight lattice structures. This enables faster printing of single-piece components versus assembling multiple sections. GH3625 is used to print blades, impellers, plates, discs, tubes with conformal cooling channels, and other mission-critical components working under high pressures and temperatures. GH3625 powder Inconel 625 powder Specifications GH3625 powder for AM processes is available in different size distributions, shapes, and formulations from various powder manufacturers. GH3625 Powder Types

Specification	Details
Particle Size Distribution	15-45 μm, 15-53 μm, 53-150 μm
Particle Shape	Spherical, satellite, polyhedral
Alloy Modifications	With B, C, Zr, Nb, Ta
Manufacturing Method	Gas atomization, plasma atomization

Gas atomization and plasma atomization produce spherical powders optimal for SLS/DMLS processes. Satellite powders have higher tap density and improve powder flowability. Smaller 15-45 μm powders provide high resolution and surface finish while larger 53-150 μm allow faster build speeds. Different alloying additions like boron, carbon, zirconium, niobium, and tantalum are used to tailor material properties. GH3625 powder Inconel 625 powder Standards

Standard	Description
ASTM F3056	Standard specification for additive manufacturing nickel alloy
AMS7016	Nickel alloy powder for high temperature service
ASME B46.1	Surface texture requirements

GH3625 powder is qualified based on composition limits, particle size distribution, morphology, flowability, apparent density, and microstructure per ASTM F3056. Additional testing as per application standards is required. GH3625 powder Inconel 625 powder Pros and Cons GH3625 has the following advantages that make it a popular choice: GH3625 Pros Excellent strength and hardness up to 1000°C Good corrosion and oxidation resistance Weldable for post-processing Higher ductility than Inconel 718 Can be age hardened by heat treatment Complex geometries enabled by AM Faster and cheaper than castings Reduces part count through consolidation GH3625 Cons More expensive than stainless steels Lower strength than Inconel 718 above 550°C Susceptible to strain-age cracking Requires hot isostatic pressing (HIP) Difficult to machine – requires specialist tools Limited supplier data on long term performance Proper selection of AM process parameters and post-processing mitigates some of the limitations of GH3625 powder. Comparison of GH3625 powder Inconel 625 powder with Inconel 718 and Satellite 21 GH3625 occupies a niche between Inconel 718 and Satellite 21 in terms of properties and cost: Alloy Comparison

Property	GH3625	Inconel 718	Satellite 21
Cost	Medium	High	Low
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
Weldability	Good	Poor	Medium
Manufacturability	Medium	Difficult	Easy

GH3625 matches or exceeds the performance of Satellite 21 cobalt alloys in wear and corrosion resistance but at lower cost. It approaches the strength of Inconel 718 up to 550°C and offers better weldability and manufacturability. This makes it a cost-effective alternative for many applications requiring performance between these standard alloys. The ability to 3D print complex geometries also gives it an edge. GH3625 powder Inconel 625 powder – FAQs Q: What is GH3625 powder? A: GH3625 is a nickel-based superalloy powder specifically designed for additive manufacturing processes like selective laser sintering (SLS) and direct metal laser sintering (DMLS). It provides an excellent combination of high temperature strength, hardness, wear and corrosion resistance. Q: What is GH3625 powder used for? A: GH3625 powder is used to 3D print critical components like turbine blades, manifolds, impellers, heat exchangers that require high mechanical properties, dimensional stability, and thermal resistance up to 1000°C. It finds applications across aerospace, automotive, energy, chemical processing, and medical industries. Q: What metal 3D printing processes use GH3625 powder? A: Selective laser sintering (SLS) and direct metal laser sintering (DMLS) are powder bed fusion 3D printing processes commonly used with GH3625 powder. Binder jetting is also suitable for GH3625. Q: What are the material properties of GH3625? A: GH3625 has excellent tensile strength 1050-1280 MPa, yield strength 860-1050 MPa, and hardness 32-38 HRC similar to wrought materials. It has good ductility of 8-15% elongation and high resistance to wear, galling, abrasion, and corrosion. Thermal properties allow use up to 1000°C. Q: Does GH3625 powder require heat treatment? A: Yes, GH3625 parts printed using SLS/DMLS require hot isostatic pressing (HIP) followed by heat treatment to achieve optimal mechanical properties, material consolidation, and microstructure. HIP helps close internal pores and voids. Q: Is GH3625 weldable? A: GH3625 is designed to have excellent weldability compared to precipitation hardening stainless steels and Inconel 718. This allows repairing and joining AM GH3625 parts through welding. Stress relieving may be required after welding to prevent cracking. Q: Is GH3625 machinable? A: GH3625 is difficult to machine compared to stainless steel and requires high-speed machining with specialist carbide tools. Tool wear is higher so optimal feeds, speeds, and tool paths are necessary. Q: How much does GH3625 powder cost? A: GH3625 typically costs between $90-250 per kg based on order size, particle size distribution, manufacturing method, and additional testing/qualification requirements. It is more expensive than stainless steel powders but lower cost than Inconel 718.

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Inconel 718 Powder

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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 pricing

Inconel 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

inconel 718 powder Applications Inconel 718 powder finds applications in various industries due to its unique properties. Some of its key applications include:

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

Specifications, Sizes, and Grades Inconel 718 powder is available in various specifications, sizes, and grades to meet specific application requirements. The table below provides an overview of these parameters:

Parameter	Details
Specifications	ASTM B163, AMS 5848, ISO 2076
Sizes	15-150 microns (typical)
Grades	Inconel 718, Inconel 718Plus

in718 powder Pros and Cons Like any material, Inconel 718 powder has its advantages and disadvantages. The table below summarizes the pros and cons:

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

IN718 powder Specific Metal Powder Models Various metal powder models of Inconel 718 are available in the market. Some of the notable models include: Met3DP Inconel 718: Optimized for LPBF and EBPBF processes, offering high density and excellent mechanical properties. Praxair Incoloy 718: Designed for LPBF applications, known for its fine particle size and consistent flowability. Carpenter Technology Carpenter 718: Suitable for both LPBF and EBPBF, providing high strength and corrosion resistance. ATI 718Plus: Developed for LPBF, featuring improved strength and ductility compared to standard Inconel 718. Sandvik Osprey 718: Produced using the Osprey process, resulting in spherical particles with high flowability and packing density. Höganäs AM 718: Optimized for LPBF, offering high density and excellent mechanical properties. LPW Technology LPW 718: Specifically designed for LPBF, known for its consistent particle size and low oxygen content. Arcam AB Arcam 718: Suitable for EBPBF, offering high density and fine particle size. Renishaw Ren AM 718: Developed for LPBF, providing high strength and corrosion resistance. EOS GmbH EOS 718: Optimized for LPBF, known for its high density and excellent surface finish. FAQ Q: What is the difference between Inconel 718 powder and other nickel-based alloys? A: Inconel 718 powder is known for its exceptional strength, corrosion resistance, and high-temperature capabilities compared to other nickel-based alloys. It contains a higher percentage of chromium, which contributes to its enhanced corrosion resistance. Q: How is Inconel 718 powder used in additive manufacturing? A: Inconel 718 powder is used in LPBF and EBPBF processes. In LPBF, a laser beam selectively melts the powder particles to create the desired shape, while in EBPBF, an electron beam is used for melting. Q: What are the advantages of using Inconel 718 powder in AM? A: Using Inconel 718 powder in AM offers advantages such as design flexibility, reduced lead times, and the ability to create complex geometries. It also allows for the production of lightweight components with high strength and durability. Q: What are the future trends in Inconel 718 powder technology? A: Research and development efforts are focused on improving the powder’s flowability, packing density, and mechanical properties. Additionally, there is a growing interest in developing new alloys based on Inconel 718 with enhanced performance characteristics.

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Inconel 718 Powder

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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 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

Overview of Inconel 718 Powder Inconel 718 is a precipitation hard enable nickel-based superalloy powder widely used for additive manufacturing across aerospace, oil & gas, power generation and automotive industries. This article provides a detailed guide to Inconel 718 powder. Key aspects covered include composition, properties, AM print parameters, applications, specifications, suppliers, handling, inspection methods, comparisons to alternatives, pros and cons, and FAQs. Tables are used to present information in an easy-to-reference format. Composition of Inconel 718 Powder The composition of Inconel 718 is:

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

Trace amounts of cobalt, boron, copper and magnesium are also added to enhance properties. Key properties of Inconel 718 include:

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

Typical parameters for printing Inconel 718 powder include:

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

The parameters depend on factors like build geometry, temperature management and post-processing needs. Applications of 3D Printed Inconel 718 Parts Inconel 718 parts made by AM are used in:

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

Benefits over wrought parts include complex geometries and reduced buy-to-fly ratios. Specifications of Inconel 718 Powder for AM Inconel 718 powder must meet the following specifications for 3D printing:

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

Handling and Storage of Inconel 718 Powder As a reactive material, Inconel 718 powder requires controlled handling: Store sealed containers in a cool, dry inert atmosphere Prevent exposure to moisture, air, temperature extremes Use properly grounded equipment during transfer Avoid dust accumulation and ignition sources Local exhaust ventilation recommended Follow applicable safety guidelines Correct storage/handling prevents composition changes or hazards. Inspection and Testing of Inconel 718 Powder Inconel 718 powder batches are validated using:

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

Testing per ASTM standards ensures batch-to-batch quality consistency. Comparing Inconel 718 to Alternative Superalloy Powders Inconel 718 compares with other alloys as:

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

For balanced properties at lower cost, Inconel 718 supersedes other Ni superalloys for many applications. Pros and Cons of Inconel 718 Powder for AM

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

Inconel 718 enables high performance AM at a reasonable cost. Frequently Asked Questions about Inconel 718 Powder Q: What particle size range works best for printing Inconel 718 alloy? A: A range of 15-45 microns provides the optimum combination of flowability, high resolution, and high density parts. Q: What post processing is typically required for Inconel 718 AM parts? A: Hot isostatic pressing, heat treatment, and machining are commonly needed to eliminate voids, optimize properties, and achieve tolerances. Q: Is Inconel 718 easier to 3D print than other Ni superalloys? A: Yes, its excellent weldability and lower cracking susceptibility make Inconel 718 one of the easier Ni-based superalloys to process by AM. Q: What industries use Inconel 718 alloy for metal 3D printing? A: Aerospace, oil & gas, power generation, automotive, and medical sectors are major applications benefiting from additively manufactured Inconel 718. Q: Does Inconel 718 require supports when 3D printing? A: Minimal supports are recommended on overhangs and bridged sections to prevent deformation and allow easy removal after printing. Q: What defects can occur when printing Inconel 718 powder? A: Potential defects are cracking, porosity, distortion, incomplete fusion, and surface roughness. Most can be prevented with optimized parameters. Q: What hardness can be expected with Inconel 718 AM components? A: Hardness after printing is typically 30-35 HRC. Post-processes like aging can increase it to 40-50 HRC for higher wear resistance. Q: What accuracy can be obtained with Inconel 718 printed parts? A: Comparable dimensional tolerances and surface finishes to CNC machined components can be achieved after post-processing. Q: Is hot isostatic pressing mandatory for Inconel 718 3D printed parts? A: HIP eliminates internal voids and improves fatigue life. It may not be required for non-critical applications. Q: What alloy powder has properties closest to Inconel 718 for AM? A: Inconel 625 has comparable corrosion resistance and weldability to 718 but lower strength. Inconel 939 trades weldability for higher strength.

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K465 Alloy Powder

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K465 Alloy Powder

Product	K465 Alloy Powder
CAS No.	7440-02-0
Appearance	Silvery-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	NiCrMoCo
Density	8.1-8.3g/cm3
Molecular Weight	N/A
Product Codes	NCZ-DCY-293/25

K465 Alloy Description:

K465 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

K465 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. K465 Alloy Powder K465 alloy powder is a nickel-based superalloy that offers high strength and corrosion resistance at elevated temperatures. It is widely used in aerospace, power generation, and chemical processing industries. K465 Alloy Powder: Composition, Properties, Applications, and Specifications K465 has become a popular choice for aerospace, power generation, and chemical processing industries where components are subjected to high temperatures or aggressive environments. It allows complex geometries to be 3D printed for optimal performance. This article provides detailed information on the composition, properties, applications, specifications, availability, processing, and comparisons of K465 superalloy powder for additive manufacturing. K465 Alloy Powder Composition The nominal composition of K465 nickel-based superalloy powder is given below:

Element	Weight %
Nickel (Ni)	Balance
Chromium (Cr)	15 – 17%
Cobalt (Co)	9 – 10%
Molybdenum (Mo)	3%
Tantalum (Ta)	4.5 – 5.5%
Aluminum (Al)	5 – 6%
Titanium (Ti)	0.5 – 1%
Boron (B)	0.01% max
Carbon (C)	0.03% max
Zirconium (Zr)	0.01% max
Niobium (Nb)	1% max

Nickel forms the base of the alloy and provides a face-centered cubic matrix for high temperature strength. Elements like chromium, cobalt, and molybdenum contribute to solid solution strengthening and enable precipitation hardening. Aluminum and titanium are added to form gamma prime precipitates Ni3(Al,Ti) to provide hardness and creep resistance up to 700°C. Tantalum provides solid solution strengthening and forms carbides for grain structure control. Boron facilitates precipitation of complex carbides. The balanced composition of K465 nickel superalloy powder results in a combination of strength, ductility, corrosion resistance, and weldability required for high performance additive manufactured components. The optimized levels of alloying elements can be tailored based on final part requirements. K465 Alloy Powder Properties K465 superalloy powder processed via laser powder bed fusion or electron beam melting exhibits the following properties in as-built and heat treated states: Mechanical Properties

Property	As-Built Condition	After Heat Treatment
Tensile Strength	1050 – 1250 MPa	1150 – 1350 MPa
Yield Strength	750 – 950 MPa	1000 – 1200 MPa
Elongation	10 – 25%	8 – 15%
Hardness	35 – 45 HRC	42 – 48 HRC

High strength levels comparable to cast and wrought Ni-based superalloys Ductility retained after heat treatment allows some forming/forging Precipitation hardening by gamma prime phase after solution treatment Physical Properties

Property	Value
Density	8.1 – 8.3 g/cc
Melting Point	1260 – 1350°C
Thermal Conductivity	11 – 16 W/m-K
Thermal Expansion Coefficient	12 – 16 x 10<sup>-6</sup> /K

High Temperature Properties

Property	Value
Service Temperature	Up to 700°C
Oxidation Resistance	Good up to 850°C
Phase Stability	Retains strength up to 70% of melting point
Creep Rupture Strength	140 MPa at 700°C for 1000 hours

Retains over half its strength at maximum service temperature Resists oxidation and hot corrosion in gas turbine environments Excellent creep rupture strength under load at high temperature Other Notable Properties Weldable using conventional fusion welding methods Good surface finish and dimensional accuracy in AM builds Customizable with different heat treatments High thermal fatigue and crack growth resistance The balanced set of mechanical, physical, and thermal properties make K465 suitable for extreme environments faced in aerospace engines, power generation systems, and chemical processing equipment. The properties can be fine-tuned based on application requirements. K465 Alloy Powder Applications The major applications of additive manufactured K465 superalloy parts include: Aerospace: Combustor liners, augmentors, flame holders in jet engines Structural brackets, frames, housings, fittings Hot section components like turbine blades and vanes Rocket propulsion systems and spacecraft engines Power Generation: Heat exchangers, piping, valves, manifolds in boilers and heat recovery systems Gas turbine hot gas path components like nozzles, shrouds Solar power receivers and collectors Automotive: Turbocharger wheels and housings Exhaust system manifolds and components Chemical Processing: Reformer tubes, reaction vessels, heat exchanger components Piping, valves, pumps for corrosive chemicals Tooling like mandrels, fixtures for composite parts Benefits: Withstands sustained use at over 700°C lower density than competing alloys Oxidation and corrosion resistance in hot gas environments Reduces component weight compared to cast nickel alloys Enables complex optimized geometries not possible with casting Consolidates multiple parts into one printed component Saves material waste relative to subtractive methods Shorter lead times compared to traditional processing K465 is frequently used as substitute for heavier, costlier superalloys in aerospace engines and land-based power systems. The alloy powder can be tailored to meet requirements in extreme temperature, pressure, and corrosive service conditions. K465 Alloy Powder Specifications K465 alloy powder for AM processes is supplied by various manufacturers to the following nominal specifications:

Parameter	Specification
Particle size distribution	15 – 53 microns
Oxygen content	0.05% max
Nitrogen content	0.05% max
Morphology	Spheroidal
Apparent density	4.0 – 4.5 g/cc
Tap density	4.5 – 5.0 g/cc
Flow rate	15 – 25 s/50g

Powder particle size distribution optimized for AM processes High powder flowability ensures uniform layer spreading Low oxygen content minimizes risk of defects in builds Spherical morphology provides good packing and powder bed density Additional Requirements: Powder should be handled in an inert atmosphere to prevent contamination Moisture content must be kept below 0.1 wt% for good powder flow Temporary storage life up to 1 year in sealed containers with argon Open containers to be used within 1 week to avoid degradation Meeting powder specifications in terms of size, shape, chemistry, and handling is critical to achieving high density AM parts with expected mechanical properties. K465 Alloy Powder Availability K465 superalloy powder can be sourced from major suppliers like:

Manufacturer	Product Name
Praxair	TA1
Carpenter Additive	Car Tech K465
Sandvik Osprey	K465-TCP
Erasteel	Satellite AM K465

The alloy powder is sold in various sizes ranging from 1 kg containers for R&D purposes up to 1000 kg containers for production volumes. Prices range from $90-150 per kg based on quantity and manufacturer. Lead times for procurement typically range from 2-8 weeks after order confirmation. Customized particle size distributions and special handling may require a longer lead time. K465 powder inventory should be monitored closely and reordered well in advance of running out. Shortages can cause costly AM machine downtime. Consider spacing out orders over time to maintain stock. K465 Alloy Powder Processing Parameter Ranges for AM Processes:

Process	Preheating Temp	Layer Thickness	Laser Power	Scan Speed	Hatch Spacing
DMLS	150 – 180°C	20 – 60 μm	195 – 250 W	600 – 1200 mm/s	0.08 – 0.12 mm
EBM	1000 – 1100°C	50 – 200 μm	5 – 25 mA	50 – 200 mm/s	0.1 – 0.2 mm

DMLS = Direct metal laser sintering EBM = Electron beam melting A wider range of parameters allows flexibility to optimize for surface finish, build time, or mechanical properties Preheating reduces residual stresses; higher for EBM due to higher temperatures Slower scan speeds improve density but prolong build time Fine hatch spacing reduces porosity but requires more scan passes Post-Processing: Removal of parts from build plate using EDM wire cutting Removal of residual powder via glass bead blasting Stress relief heat treatment at 870°C for 1 hour HIP treatment at 1160°C under 100 MPa pressure for 4 hours Age hardening heat treatment at 760°C for 10 hours Benefits of Post-Processing: HIP closes internal voids and minimizes porosity Heat treatments relieve residual stress and achieve optimal hardness Yields close to 100% dense parts with mechanical properties equivalent to cast and wrought Additional hot isostatic pressing (HIP) and heat treatments can further enhance properties Parameter selection, support structures, build orientation, post-processing steps are all optimizable based on AM technology used and properties required. How K465 Compares with Other Superalloy Powders K465 vs Inconel 718

Alloy	K465	Inconel 718
Density	Higher	Lower
Tensile Strength	Similar	Similar
Service Temperature	100°C higher	Up to 650°C
Cost	2X more expensive	More economical

K465 chosen for higher temperature capability where cost increase is justified Inconel 718 more economical for lower temperature applications K465 vs Haynes 282

Alloy	K465	Haynes 282
Processability	Better	More difficult
Thermal conductivity	Higher	Lower
Service temperature	Similar	Similar
Cost	Similar	Similar

K465 easier to laser print and post-process without cracking Haynes 282 more prone to solidification cracks during builds K465 vs CM 247 LC

Alloy	K465	CM 247 LC
Density	Lower	Higher
Strength	Similar	Similar
Ductility	Higher	Lower
Cost	Lower	Higher

K465 has better combinaton of strength and ductility Lower cost alloy alternative to CM 247 LC K465 vs Inconel 625

Alloy	K465	Inconel 625
Service Temperature	Higher	Up to 700°C
Corrosion Resistance	Moderate	Excellent
Cost	Higher	Lower
Availability	More limited	Readily available

Inconel 625 chosen where corrosion resistance trumps high temperature capability K465 preferred for jet engine parts seeing extreme temperatures Understanding where K465 excels or falls short compared to alternatives aids material selection for AM components. The alloy can be tailored to shift the balance between cost, availability, processability, and properties. K465 Alloy Powder – Frequently Asked Questions Q: What pre-processing steps are required for K465 powder? A: K465 powder needs to be dried for 1-4 hours at 100-150°C to remove moisture absorbed during shipping and storage. Sieving between 20-63 microns will eliminate large particles that can cause recoater issues. Q: Does K465 require hot isostatic pressing (HIP) post-processing? A: HIP is recommended but not mandatory for K465. It helps close internal voids and achieve maximum density and mechanical properties. HIP at 1160°C under 100 MPa for 4 hours is typical. Q: What heat treatments can be used to tailor K465 properties? A: Solution treatment at 1150°C plus single or double aging between 700-850°C is used to optimize strength and ductility. Rapid cooling after solution treatment enhances properties. Q: Is K465 superalloy weldable for repair purposes? A: Yes, K465 can be welded using ER NiCrMo-10 filler metal. Solution treatment at 1175°C and aging at 845°C is required after welding to restore properties. Q: What manufacturing defects can occur with K465 builds? A: Lack of fusion porosity, cracking between layers, delamination, and distortion are potential defects requiring parameter optimization. Lower preheat and faster scan speeds increase risk. Q: What finishing methods can be used on additively manufactured K465 parts? A: Machining, shot peening, chemical etching, and electropolishing allow surface roughness improvement. This facilitates NDE inspection and improves fatigue life. Q: Does K465 alloy powder require special storage precautions? A: K465 powder rapidly absorbs moisture, so storage in sealed argon purged containers is required. Use within 1 week of opening container to prevent degradation. Q: What safety precautions are needed when handling K465 powder? A: K465 powder is not flammable but may cause skin/eye irritation. Use protective gloves, clothing, face shields. Avoid inhalation and install proper ventilation.

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