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Gh3039 Corrosion Resistant Nickel Based Superalloy 8.23 g/cm3 high performance
| 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
GH3039 alloy
Composition:
Nickel-based Superalloy Containing Chromium, Cobalt, Iron, And Other Elements
Density:
8.23 G/cm³
Melting Point:
1320-1370°C (2408-2498°F)
Tensile Strength:
850-1100 MPa (at Room Temperature)
Yield Strength (0.2% Offset):
450-700 MPa
Elongation:
30-50%
Thermal Conductivity:
9.8 W/m·K (at 100°C)
Specific Heat Capacity:
Specific Heat Capacity
Coefficient Of Thermal Expansion:
13.6 µm/m·K (20-100°C)
Electrical Resistivity:
1.10 µΩ·m (at 20°C)
Magnetic Properties:
Non-magnetic
Highlight:
Gh3039 nickel based superalloy
,Corrosion Resistant nickel based superalloy
,Nickel Based Superalloy 8.23 g/cm3
Product Description
GH3039 Corrosion Resistant Nickel Based Superalloy
High-performance nickel-based superalloy with 8.23 g/cm³ density, designed for extreme temperature and corrosive environments.
Key Attributes
| Attribute | Value |
|---|---|
| Composition | Nickel-based superalloy containing Chromium, Cobalt, Iron, and other elements |
| Density | 8.23 g/cm³ |
| Melting Point | 1320-1370°C (2408-2498°F) |
| Tensile Strength | 850-1100 MPa (at room temperature) |
| Yield Strength (0.2% offset) | 450-700 MPa |
| Elongation | 30-50% |
| Thermal Conductivity | 9.8 W/m·K (at 100°C) |
| Coefficient of Thermal Expansion | 13.6 µm/m·K (20-100°C) |
| Electrical Resistivity | 1.10 µΩ·m (at 20°C) |
| Magnetic Properties | Non-magnetic |
Product Description
GH3039 is a premium nickel-based superalloy engineered for demanding applications requiring exceptional mechanical strength, oxidation resistance, and corrosion resistance. Its unique composition maintains structural integrity at temperatures up to 1370°C (2498°F), making it ideal for extreme environments.
Primary Applications: Gas turbine components, aerospace parts, chemical processing equipment, and other high-temperature industrial applications where reliability under prolonged stress is critical.
Detailed Composition
| Element | Composition (%) |
|---|---|
| Nickel (Ni) | 51.0 - 55.0 |
| Chromium (Cr) | 19.0 - 22.0 |
| Cobalt (Co) | 15.0 - 20.0 |
| Iron (Fe) | 5.0 - 9.0 |
| Molybdenum (Mo) | 2.5 - 3.5 |
| Titanium (Ti) | ≤ 0.70 |
| Aluminum (Al) | ≤ 0.60 |
| Carbon (C) | ≤ 0.08 |
| Manganese (Mn) | ≤ 0.50 |
| Silicon (Si) | ≤ 0.50 |
| Phosphorus (P) | ≤ 0.015 |
| Sulfur (S) | ≤ 0.010 |
| Boron (B) | ≤ 0.006 |
Performance Advantages
- Exceptional creep and fatigue resistance for prolonged service life
- Maintains mechanical properties at extreme temperatures
- Superior resistance to oxidation and corrosion
- Non-magnetic properties for specialized applications
- Reliable performance in aggressive chemical environments
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