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GH169 Alloy High Strength Heat Resistant Nickel Based Superalloy For Turbine Engines
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GH169 Alloy 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:
GH169 Nickel Based Superalloy
,Heat Resistant Nickel Based Superalloy
,GH169 Alloy Heat Resistant
Product Description
GH169 Alloy High Strength Heat Resistant Nickel Based Superalloy For Turbine Engines
Product Attributes
| Attribute | Value |
|---|---|
| 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 |
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: Maintains superior mechanical properties at temperatures up to 1,300°C (2,372°F), ideal for extreme environments.
- Exceptional Strength: Exhibits high tensile and yield strength for durability in high-stress applications like turbine engines.
- Good Oxidation and Corrosion Resistance: Enhances longevity and performance in aggressive environments.
- Thermal Stability: Resists deformation under thermal cycling while maintaining structural integrity.
- Applications: Widely used in turbine engines, aerospace components, and other high-temperature applications.
Engineered to meet demanding requirements of advanced engineering and aerospace industries, GH169 Alloy provides reliable performance in challenging conditions.
Chemical Composition
| 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.
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