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GH44 Alloy is a high-strength nickel-based superalloy with excellent high-temperature stability and oxidation resistance

GH44 Alloy is a high-strength nickel-based superalloy with excellent high-temperature stability 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
Place of Origin
China
Brand Name
Zhonggong Special Metallurgy
Certification
ISO Certificate
Model Number
GH44 Alloy
Density:
~8.8 G/cm³ (0.317 Lb/in³)
Melting Point:
~1350-1450°C (2460-2640°F)
Tensile Strength:
~950 MPa (138 Ksi)
Yield Strength:
~800 MPa (116 Ksi)
Elongation:
~15%
Thermal Conductivity:
~12 W/m·K (8.4 BTU·in/hr·ft²·°F)
Modulus Of Elasticity:
~210 GPa (30 X 10³ Ksi)
Corrosion Resistance:
Excellent Oxidation And Corrosion Resistance At High Temperatures
Applications:
Aerospace Components, Gas Turbines, High-temperature Structural Parts
Highlight:

aerospace components nickel based alloys

,

aerospace components nickel based superalloy

Product Description

GH44 Alloy is a high-performance nickel-based superalloy designed for exceptional strength and durability in extreme high-temperature environments. It is engineered to meet the rigorous demands of aerospace and industrial applications, providing reliable performance under intense thermal and mechanical stress.

Key Properties and Features:

  • High-Temperature Strength: GH44 Alloy maintains impressive mechanical properties at elevated temperatures, offering high tensile strength (~950 MPa or 138 ksi) and yield strength (~800 MPa or 116 ksi). It can withstand temperatures up to approximately 1350-1450°C (2460-2640°F), making it suitable for critical components subjected to extreme heat.

  • Oxidation and Corrosion Resistance: The alloy is highly resistant to oxidation and corrosion at high temperatures, ensuring long-term durability and reliability in harsh environments. This resistance is crucial for applications in gas turbines, jet engines, and other high-temperature processes where exposure to aggressive conditions is common.

  • Mechanical Properties: GH44 Alloy exhibits good elongation (~15%), which enhances its ability to handle mechanical stress and strain without failure. This property is essential for maintaining structural integrity and performance in demanding applications.

  • Thermal Conductivity: With a thermal conductivity of approximately 12 W/m·K (8.4 BTU·in/hr·ft²·°F), GH44 efficiently manages heat, which is beneficial for maintaining thermal stability and preventing overheating in high-performance systems.

  • Applications: Commonly used in aerospace components, high-temperature gas turbines, and other industrial applications where high strength, oxidation resistance, and thermal stability are required. GH44’s robust performance in extreme conditions makes it a preferred material for advanced engineering tasks that demand exceptional performance and durability.

GH44 Alloy’s combination of high strength, excellent oxidation resistance, and thermal stability ensures its reliability and performance in critical applications exposed to severe conditions.

 

Here’s a composition table for GH44 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 specific applications or precise compositions, consult detailed material specifications or supplier data.

 

GH44 Alloy is a high-strength nickel-based superalloy with excellent high-temperature stability and oxidation resistance 0

products
PRODUCTS DETAILS
GH44 Alloy is a high-strength nickel-based superalloy with excellent high-temperature stability 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
Place of Origin
China
Brand Name
Zhonggong Special Metallurgy
Certification
ISO Certificate
Model Number
GH44 Alloy
Density:
~8.8 G/cm³ (0.317 Lb/in³)
Melting Point:
~1350-1450°C (2460-2640°F)
Tensile Strength:
~950 MPa (138 Ksi)
Yield Strength:
~800 MPa (116 Ksi)
Elongation:
~15%
Thermal Conductivity:
~12 W/m·K (8.4 BTU·in/hr·ft²·°F)
Modulus Of Elasticity:
~210 GPa (30 X 10³ Ksi)
Corrosion Resistance:
Excellent Oxidation And Corrosion Resistance At High Temperatures
Applications:
Aerospace Components, Gas Turbines, 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

aerospace components nickel based alloys

,

aerospace components nickel based superalloy

Product Description

GH44 Alloy is a high-performance nickel-based superalloy designed for exceptional strength and durability in extreme high-temperature environments. It is engineered to meet the rigorous demands of aerospace and industrial applications, providing reliable performance under intense thermal and mechanical stress.

Key Properties and Features:

  • High-Temperature Strength: GH44 Alloy maintains impressive mechanical properties at elevated temperatures, offering high tensile strength (~950 MPa or 138 ksi) and yield strength (~800 MPa or 116 ksi). It can withstand temperatures up to approximately 1350-1450°C (2460-2640°F), making it suitable for critical components subjected to extreme heat.

  • Oxidation and Corrosion Resistance: The alloy is highly resistant to oxidation and corrosion at high temperatures, ensuring long-term durability and reliability in harsh environments. This resistance is crucial for applications in gas turbines, jet engines, and other high-temperature processes where exposure to aggressive conditions is common.

  • Mechanical Properties: GH44 Alloy exhibits good elongation (~15%), which enhances its ability to handle mechanical stress and strain without failure. This property is essential for maintaining structural integrity and performance in demanding applications.

  • Thermal Conductivity: With a thermal conductivity of approximately 12 W/m·K (8.4 BTU·in/hr·ft²·°F), GH44 efficiently manages heat, which is beneficial for maintaining thermal stability and preventing overheating in high-performance systems.

  • Applications: Commonly used in aerospace components, high-temperature gas turbines, and other industrial applications where high strength, oxidation resistance, and thermal stability are required. GH44’s robust performance in extreme conditions makes it a preferred material for advanced engineering tasks that demand exceptional performance and durability.

GH44 Alloy’s combination of high strength, excellent oxidation resistance, and thermal stability ensures its reliability and performance in critical applications exposed to severe conditions.

 

Here’s a composition table for GH44 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 specific applications or precise compositions, consult detailed material specifications or supplier data.

 

GH44 Alloy is a high-strength nickel-based superalloy with excellent high-temperature stability and oxidation resistance 0

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