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GH136 Alloy is a nickel-based superalloy with high strength and excellent oxidation resistance at elevated temperatures

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GH136 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

GH136 Alloy

Density:

~8.8 G/cm³ (0.317 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

Highlight:

high strength nickel based alloys

high strength nickel based superalloy

Product Description

GH136 Alloy is a high-performance nickel-based superalloy engineered for superior strength and oxidation resistance at elevated temperatures. This alloy is designed to perform reliably in extreme environments, making it suitable for demanding applications in aerospace and high-temperature industrial processes.

Key Properties and Features:

High-Temperature Strength: GH136 Alloy maintains excellent mechanical properties, including high tensile strength (~900 MPa or 130 ksi) and yield strength (~700 MPa or 102 ksi), at temperatures up to approximately 1300-1400°C (2370-2550°F). This capability makes it ideal for components exposed to intense heat.
Oxidation and Corrosion Resistance: The alloy offers robust resistance to oxidation and high-temperature corrosion, ensuring long-term durability and performance in harsh environments. This feature is crucial for applications in gas turbines, jet engines, and other high-stress applications.
Mechanical Properties: Provides good elongation (~15%), which contributes to its ability to withstand mechanical stress without compromising integrity.
Thermal Conductivity: With a thermal conductivity of approximately 13 W/m·K (9 BTU·in/hr·ft²·°F), GH136 effectively manages heat dissipation, which is important in high-performance systems.
Applications: Commonly used in aerospace components, gas turbines, and other high-temperature structural parts where high strength and resistance to thermal degradation are required.

GH136 Alloy’s combination of high strength, oxidation resistance, and thermal stability ensures it is a reliable choice for advanced engineering applications demanding exceptional performance under extreme conditions.

Here’s a composition table for GH136 Alloy:

Element	Composition Range (%)
Nickel (Ni)	60.0 - 65.0
Chromium (Cr)	14.0 - 16.0
Cobalt (Co)	8.0 - 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 provide general guidelines. For precise specifications or applications, consult specific standards or suppliers.

GH136 Alloy is a nickel-based superalloy with high strength and excellent oxidation resistance at elevated temperatures 0

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nickel based superalloys,

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GH136 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

GH136 Alloy

Density:

~8.8 G/cm³ (0.317 Lb/in³)

Melting Point:

~1300-1400°C (2370-2550°F)

Tensile Strength:

~900 MPa (130 Ksi)

Yield Strength:

~700 MPa (102 Ksi)

Elongation:

~15%

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

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

Product Description

Key Properties and Features:

High-Temperature Strength: GH136 Alloy maintains excellent mechanical properties, including high tensile strength (~900 MPa or 130 ksi) and yield strength (~700 MPa or 102 ksi), at temperatures up to approximately 1300-1400°C (2370-2550°F). This capability makes it ideal for components exposed to intense heat.
Oxidation and Corrosion Resistance: The alloy offers robust resistance to oxidation and high-temperature corrosion, ensuring long-term durability and performance in harsh environments. This feature is crucial for applications in gas turbines, jet engines, and other high-stress applications.
Mechanical Properties: Provides good elongation (~15%), which contributes to its ability to withstand mechanical stress without compromising integrity.
Thermal Conductivity: With a thermal conductivity of approximately 13 W/m·K (9 BTU·in/hr·ft²·°F), GH136 effectively manages heat dissipation, which is important in high-performance systems.
Applications: Commonly used in aerospace components, gas turbines, and other high-temperature structural parts where high strength and resistance to thermal degradation are required.

Here’s a composition table for GH136 Alloy:

Element	Composition Range (%)
Nickel (Ni)	60.0 - 65.0
Chromium (Cr)	14.0 - 16.0
Cobalt (Co)	8.0 - 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 provide general guidelines. For precise specifications or applications, consult specific standards or suppliers.

GH136 Alloy is a nickel-based superalloy with high strength and excellent oxidation resistance at elevated temperatures 0

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