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GH39 Alloy is a nickel-based superalloy known for its excellent high-temperature strength and oxidation resistance

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GH39 Alloy is a nickel-based superalloy known for its excellent high-temperature strength and oxidation resistance

MOQ:	100KG
Price:	Price is negotiated based on the required specifications and quantity
Standard Packaging:	Standard export packaging, or packaging as required
Delivery Period:	5-8 working days, depending on the parameters required for negotiation
Payment Method:	Payment Terms: Mainly T/T.. L/C, D/A, D/P,
Supply Capacity:	5000 tons per month

Details Information

Product Description

Detail Information

Place of Origin

China

Brand Name

Zhonggong Special Metallurgy

Certification

ISO Certificate

Model Number

GH39 Alloy

Density:

~8.9g/cm³ (0.321 Lb/in³)

Melting Point:

~1350-1450°C (2460-2640°F)

Tensile Strength:

~900 MPa (130 Ksi)

Yield Strength:

~750 MPa (109 Ksi)

Elongation:

Thermal Conductivity:

~14 W/m·K (10 BTU·in/hr·ft²·°F)

Modulus Of Elasticity:

~210 GPa (30 X 10³ Ksi)

Corrosion Resistance:

Good Resistance To Oxidation And Corrosion At High Temperatures

Applications:

Aerospace Components, Gas Turbines, High-temperature Industrial Parts

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aerospace components nickel based alloys

aerospace components nickel based superalloy

Product Description

GH39 Alloy is a high-performance nickel-based superalloy engineered for exceptional strength and oxidation resistance at elevated temperatures. It is specifically designed to perform reliably in extreme environments, making it ideal for aerospace and industrial applications where high thermal and mechanical stress is common.

Key Properties and Features:

High-Temperature Strength: GH39 Alloy maintains excellent mechanical properties at elevated temperatures, with high tensile strength (~900 MPa or 130 ksi) and yield strength (~750 MPa or 109 ksi). It is capable of withstanding temperatures up to approximately 1350-1450°C (2460-2640°F) without significant loss of strength.
Oxidation and Corrosion Resistance: The alloy exhibits superior resistance to oxidation and high-temperature corrosion, ensuring long-term durability and performance in harsh environments. This property is crucial for applications in gas turbines, jet engines, and other high-temperature processes.
Mechanical Properties: GH39 provides good elongation (~15%), which enhances its ability to handle mechanical stresses and strains without failure, contributing to structural integrity in demanding applications.
Thermal Conductivity: With a thermal conductivity of approximately 14 W/m·K (10 BTU·in/hr·ft²·°F), GH39 effectively manages heat, helping to maintain thermal stability and reduce overheating in high-performance systems.
Applications: Commonly used in aerospace components, high-temperature gas turbines, and other industrial applications requiring high strength, oxidation resistance, and thermal stability. GH39’s robust performance in extreme conditions ensures it is a reliable choice for advanced engineering tasks.

GH39 Alloy's combination of high strength, excellent oxidation resistance, and thermal stability makes it a preferred material for critical applications where reliability and durability are paramount.

Here’s a composition table for GH39 Alloy:

Element	Composition Range (%)
Nickel (Ni)	60.0 - 65.0
Chromium (Cr)	15.0 - 20.0
Cobalt (Co)	5.0 - 10.0
Molybdenum (Mo)	3.0 - 5.0
Iron (Fe)	≤ 6.0
Titanium (Ti)	1.0 - 2.0
Aluminum (Al)	1.0 - 2.0
Carbon (C)	≤ 0.10
Manganese (Mn)	≤ 0.5
Silicon (Si)	≤ 0.5
Sulfur (S)	≤ 0.01

These values are general guidelines. For precise specifications or detailed applications, consult specific standards or suppliers.

GH39 Alloy is a nickel-based superalloy known for its excellent high-temperature strength and oxidation resistance 0

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GH39 Alloy is a nickel-based superalloy known for its excellent high-temperature strength and oxidation resistance

MOQ:	100KG
Price:	Price is negotiated based on the required specifications and quantity
Standard Packaging:	Standard export packaging, or packaging as required
Delivery Period:	5-8 working days, depending on the parameters required for negotiation
Payment Method:	Payment Terms: Mainly T/T.. L/C, D/A, D/P,
Supply Capacity:	5000 tons per month

Detail Information

Product Description

Detail Information

Place of Origin

China

Brand Name

Zhonggong Special Metallurgy

Certification

ISO Certificate

Model Number

GH39 Alloy

Density:

~8.9g/cm³ (0.321 Lb/in³)

Melting Point:

~1350-1450°C (2460-2640°F)

Tensile Strength:

~900 MPa (130 Ksi)

Yield Strength:

~750 MPa (109 Ksi)

Elongation:

~15%

Thermal Conductivity:

~14 W/m·K (10 BTU·in/hr·ft²·°F)

Modulus Of Elasticity:

~210 GPa (30 X 10³ Ksi)

Corrosion Resistance:

Good Resistance To Oxidation And Corrosion At High Temperatures

Applications:

Aerospace Components, Gas Turbines, High-temperature Industrial Parts

Minimum Order Quantity:

100KG

Price:

Price is negotiated based on the required specifications and quantity

Packaging Details:

Standard export packaging, or packaging as required

Delivery Time:

5-8 working days, depending on the parameters required for negotiation

Payment Terms:

Payment Terms: Mainly T/T.. L/C, D/A, D/P,

Supply Ability:

5000 tons per month

Highlight

aerospace components nickel based alloys

aerospace components nickel based superalloy

Product Description

Key Properties and Features:

High-Temperature Strength: GH39 Alloy maintains excellent mechanical properties at elevated temperatures, with high tensile strength (~900 MPa or 130 ksi) and yield strength (~750 MPa or 109 ksi). It is capable of withstanding temperatures up to approximately 1350-1450°C (2460-2640°F) without significant loss of strength.
Oxidation and Corrosion Resistance: The alloy exhibits superior resistance to oxidation and high-temperature corrosion, ensuring long-term durability and performance in harsh environments. This property is crucial for applications in gas turbines, jet engines, and other high-temperature processes.
Mechanical Properties: GH39 provides good elongation (~15%), which enhances its ability to handle mechanical stresses and strains without failure, contributing to structural integrity in demanding applications.
Thermal Conductivity: With a thermal conductivity of approximately 14 W/m·K (10 BTU·in/hr·ft²·°F), GH39 effectively manages heat, helping to maintain thermal stability and reduce overheating in high-performance systems.
Applications: Commonly used in aerospace components, high-temperature gas turbines, and other industrial applications requiring high strength, oxidation resistance, and thermal stability. GH39’s robust performance in extreme conditions ensures it is a reliable choice for advanced engineering tasks.

Here’s a composition table for GH39 Alloy:

Element	Composition Range (%)
Nickel (Ni)	60.0 - 65.0
Chromium (Cr)	15.0 - 20.0
Cobalt (Co)	5.0 - 10.0
Molybdenum (Mo)	3.0 - 5.0
Iron (Fe)	≤ 6.0
Titanium (Ti)	1.0 - 2.0
Aluminum (Al)	1.0 - 2.0
Carbon (C)	≤ 0.10
Manganese (Mn)	≤ 0.5
Silicon (Si)	≤ 0.5
Sulfur (S)	≤ 0.01

These values are general guidelines. For precise specifications or detailed applications, consult specific standards or suppliers.

GH39 Alloy is a nickel-based superalloy known for its excellent high-temperature strength and oxidation resistance 0

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