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GH131 Alloy is a nickel-based superalloy with high strength and excellent oxidation resistance at elevated temperatures

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GH131 Alloy is a nickel-based superalloy with high strength and excellent oxidation resistance at elevated temperatures

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

GH131 Alloy

Density:

~8.35 G/cm³ (0.302 Lb/in³)

Melting Point:

~1300-1400°C (2370-2550°F)

Tensile Strength:

~900 MPa (130 Ksi)

Yield Strength:

~700 MPa (102 Ksi)

Elongation:

Thermal Conductivity:

~13 W/m·K (9 BTU·in/hr·ft²·°F)

Modulus Of Elasticity:

~210 GPa (30 X 10³ Ksi)

Corrosion Resistance:

Good Oxidation And Corrosion Resistance At High Temperatures

Applications:

Aerospace Components, Gas Turbines, And High-temperature Structural Parts

Highlight:

high strength nickel based alloys

high strength nickel based superalloy

aerospace components nickel based alloys

Product Description

GH131 Alloy is a high-performance nickel-based superalloy designed for applications requiring exceptional strength and oxidation resistance at elevated temperatures. It is known for its excellent mechanical properties, including high tensile and yield strength, which make it suitable for demanding aerospace and industrial environments.

Key Properties and Features:

High-Temperature Strength: GH131 Alloy maintains its mechanical strength and dimensional stability at temperatures up to approximately 1300-1400°C (2370-2550°F), making it ideal for use in high-temperature applications.
Oxidation Resistance: The alloy exhibits strong resistance to oxidation and high-temperature corrosion, ensuring durability and longevity in harsh environments.
Mechanical Properties: Offers high tensile strength (~900 MPa or 130 ksi) and yield strength (~700 MPa or 102 ksi), along with good elongation (~20%), suitable for structural and load-bearing components.
Thermal Conductivity: With a thermal conductivity of approximately 13 W/m·K (9 BTU·in/hr·ft²·°F), it performs well in applications where heat dissipation is a factor.
Applications: Commonly used in aerospace components, gas turbines, and other high-temperature structural parts that demand high performance and reliability under extreme conditions.

GH131 Alloy's robust performance in severe environments, coupled with its excellent strength and resistance properties, makes it a preferred choice for advanced aerospace and industrial applications.

Here’s a composition table for GH131 Alloy:

Element	Composition Range (%)
Nickel (Ni)	60.0 - 70.0
Chromium (Cr)	14.0 - 16.0
Cobalt (Co)	8.0 - 10.0
Molybdenum (Mo)	2.5 - 4.5
Iron (Fe)	≤ 5.0
Titanium (Ti)	1.0 - 2.5
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; please verify with specific standards or suppliers for precise compositions.

Tags:

nickel based superalloys,

base alloy,

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Stainless Steel Plate Sheet

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Nickel Based Alloys

Nickel Alloy Plate

Nickel Alloy Rod

Nickel Alloy Pipe

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Hastelloy Plate

Hastelloy Rod

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Titanium Alloy

Titanium Alloy Plate

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Monel Alloy

Iron Nickel Alloy

Cobalt Based Alloys

GH131 Alloy is a nickel-based superalloy with high strength and excellent oxidation resistance at elevated temperatures

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

GH131 Alloy

Density:

~8.35 G/cm³ (0.302 Lb/in³)

Melting Point:

~1300-1400°C (2370-2550°F)

Tensile Strength:

~900 MPa (130 Ksi)

Yield Strength:

~700 MPa (102 Ksi)

Elongation:

~20%

Thermal Conductivity:

~13 W/m·K (9 BTU·in/hr·ft²·°F)

Modulus Of Elasticity:

~210 GPa (30 X 10³ Ksi)

Corrosion Resistance:

Good Oxidation And Corrosion Resistance At High Temperatures

Applications:

Aerospace Components, Gas Turbines, And High-temperature Structural 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

high strength nickel based alloys

high strength nickel based superalloy

aerospace components nickel based alloys

Product Description

Key Properties and Features:

High-Temperature Strength: GH131 Alloy maintains its mechanical strength and dimensional stability at temperatures up to approximately 1300-1400°C (2370-2550°F), making it ideal for use in high-temperature applications.
Oxidation Resistance: The alloy exhibits strong resistance to oxidation and high-temperature corrosion, ensuring durability and longevity in harsh environments.
Mechanical Properties: Offers high tensile strength (~900 MPa or 130 ksi) and yield strength (~700 MPa or 102 ksi), along with good elongation (~20%), suitable for structural and load-bearing components.
Thermal Conductivity: With a thermal conductivity of approximately 13 W/m·K (9 BTU·in/hr·ft²·°F), it performs well in applications where heat dissipation is a factor.
Applications: Commonly used in aerospace components, gas turbines, and other high-temperature structural parts that demand high performance and reliability under extreme conditions.

GH131 Alloy's robust performance in severe environments, coupled with its excellent strength and resistance properties, makes it a preferred choice for advanced aerospace and industrial applications.

Here’s a composition table for GH131 Alloy:

Element	Composition Range (%)
Nickel (Ni)	60.0 - 70.0
Chromium (Cr)	14.0 - 16.0
Cobalt (Co)	8.0 - 10.0
Molybdenum (Mo)	2.5 - 4.5
Iron (Fe)	≤ 5.0
Titanium (Ti)	1.0 - 2.5
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; please verify with specific standards or suppliers for precise compositions.

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