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GH169 Alloy is a high-strength, heat-resistant nickel-based superalloy for turbine engines
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GH169 Alloy is a high-strength, heat-resistant nickel-based superalloy for turbine engines
| 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
GH169 Alloy
Density:
8.4 G/cm³
Melting Point:
1260-1360°C
Tensile Strength:
950-1150 MPa
Yield Strength:
750-900 MPa
Hardness:
15-25%
Thermal Conductivity:
11.0 W/m·K
Oxidation Resistance:
Good
Applications:
Turbine Engines, Aerospace Components
Highlight:
aerospace components nickel based alloys
,aerospace components nickel based superalloy
Product Description
GH169 Alloy is a high-performance, nickel-based superalloy designed for applications requiring exceptional strength and heat resistance. Key features include:
- High Temperature Strength: GH169 Alloy maintains superior mechanical properties at high temperatures, typically up to 1,300°C (2,372°F), making it ideal for extreme environments.
- Exceptional Strength: The alloy exhibits high tensile and yield strength, ensuring durability and reliability in high-stress applications such as turbine engines.
- Good Oxidation and Corrosion Resistance: Offers solid resistance to oxidation and corrosion, enhancing the longevity and performance of components in aggressive environments.
- Thermal Stability: Demonstrates stability under thermal cycling, reducing the risk of deformation and maintaining structural integrity.
- Applications: Widely used in turbine engines, aerospace components, and other high-temperature applications where strength, durability, and resistance to extreme conditions are critical.
GH169 Alloy is engineered to meet the demanding requirements of advanced engineering and aerospace industries, providing reliable performance in challenging conditions.
Here's a table summarizing the typical chemical composition of GH169 Alloy:
| Element | Content (%) |
|---|---|
| Nickel (Ni) | 60.0-65.0 |
| Chromium (Cr) | 14.0-16.0 |
| Cobalt (Co) | 6.0-8.0 |
| Molybdenum (Mo) | 4.0-5.0 |
| Aluminum (Al) | 0.8-1.2 |
| Titanium (Ti) | 1.5-2.0 |
| Carbon (C) | 0.08-0.15 |
| Iron (Fe) | Balance |
| Others | Trace elements |
This composition provides GH169 Alloy with its desired properties of high strength, heat resistance, and durability. Let me know if you need any further details.
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