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Oxidation Resistance Nickel Based Superalloy GH131 Alloy For Aerospace Components
| 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
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
Highlight:
Nickel Based Superalloy GH131
,Oxidation Resistance Nickel Based Superalloy
Product Description
Oxidation Resistance Nickel Based Superalloy GH131 Alloy For Aerospace Components
Product Specifications
| Attribute | Value |
|---|---|
| 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 |
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: Maintains mechanical strength and dimensional stability at temperatures up to approximately 1300-1400°C (2370-2550°F).
- Oxidation Resistance: Exhibits strong resistance to oxidation and high-temperature corrosion for durability in harsh environments.
- Mechanical Properties: High tensile strength (~900 MPa or 130 ksi) and yield strength (~700 MPa or 102 ksi) with good elongation (~20%).
- Thermal Conductivity: Approximately 13 W/m·K (9 BTU·in/hr·ft²·°F) for effective heat dissipation.
- Applications: Aerospace components, gas turbines, and other high-temperature structural parts requiring 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.
Chemical Composition
| 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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