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Anti Oxidation GH39 Alloy Nickel Based Superalloy High Temperature Strength

Anti Oxidation GH39 Alloy Nickel Based Superalloy High Temperature Strength

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
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
Highlight:

GH39 Nickel Based Superalloy

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Anti Oxidation Nickel Based Superalloy

Product Description
Anti Oxidation GH39 Alloy Nickel Based Superalloy High Temperature Strength
Material Specifications
Attribute Value
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
Product Overview

GH39 Alloy is a high-performance nickel-based superalloy engineered for exceptional strength and oxidation resistance at elevated temperatures. Designed for reliability in extreme environments, it excels in aerospace and industrial applications where thermal and mechanical stress are prevalent.

Key Properties and Features
  • High-Temperature Strength: Maintains excellent mechanical properties at elevated temperatures, with tensile strength of ~900 MPa (130 ksi) and yield strength of ~750 MPa (109 ksi). Capable of withstanding temperatures up to 1350-1450°C (2460-2640°F).
  • Oxidation and Corrosion Resistance: Superior resistance to oxidation and high-temperature corrosion ensures long-term durability in harsh environments, making it ideal for gas turbines and jet engines.
  • Mechanical Properties: Good elongation (~15%) enhances ability to handle mechanical stresses without failure, contributing to structural integrity.
  • Thermal Conductivity: Approximately 14 W/m·K (10 BTU·in/hr·ft²·°F) effectively manages heat, maintaining thermal stability in high-performance systems.
  • Applications: Aerospace components, high-temperature gas turbines, and industrial applications requiring strength, oxidation resistance, and thermal stability.
Chemical Composition
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.
Anti Oxidation GH39 Alloy Nickel Based Superalloy High Temperature Strength 0
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