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Versatile Nickel Based Superalloy 90 Fatigue Resistant / Creep Resistant
| 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
Alloy 90
Composition:
Nickel (Ni): 57-59%, Chromium (Cr): 13-15%, Iron (Fe): 13-15%, Cobalt (Co): 2.5-3.5%, Molybdenum (Mo): 2.5-3.5%, Tungsten (W): 1.5-2.5%, Titanium (Ti): 1.0-2.0%, Aluminum (Al): 1.0-2.0%
Application:
Gas Turbines, Aerospace Components, Industrial Processes
Density:
8.24 G/cm³
Tensile Strength:
760-1035 MPa
Yield Strength:
420-690 MPa
Modulus Of Elasticity:
205-215 GPa
Thermal Conductivity:
11-13 W/(m·K)
Melting Point:
Approximately 1320-1380°C
Corrosion Resistance:
Excellent Resistance To Oxidation And High Temperatures
Fatigue Resistance:
High Fatigue Resistance
Creep Resistance:
Excellent At Elevated Temperatures
Hardness:
28-35 HRC
Highlight:
Versatile Nickel Based Superalloy
,Nickel Based Superalloy 90
,Nickel Based Superalloy Fatigue Resistant
Product Description
Versatile Nickel Based Superalloy 90 Fatigue Resistant / Creep Resistant
Product Attributes
| Attribute | Value |
|---|---|
| Composition | Nickel (Ni): 57-59%, Chromium (Cr): 13-15%, Iron (Fe): 13-15%, Cobalt (Co): 2.5-3.5%, Molybdenum (Mo): 2.5-3.5%, Tungsten (W): 1.5-2.5%, Titanium (Ti): 1.0-2.0%, Aluminum (Al): 1.0-2.0% |
| Application | Gas turbines, aerospace components, industrial processes |
| Density | 8.24 g/cm³ |
| Tensile Strength | 760-1035 MPa |
| Yield Strength | 420-690 MPa |
| Modulus of Elasticity | 205-215 GPa |
| Thermal Conductivity | 11-13 W/(m·K) |
| Melting Point | Approximately 1320-1380°C |
| Corrosion Resistance | Excellent resistance to oxidation and high temperatures |
| Fatigue Resistance | High fatigue resistance |
| Creep Resistance | Excellent at elevated temperatures |
| Hardness | 28-35 HRC |
Product Description
Alloy 90: Advanced Nickel-Based Superalloy For High-Temperature Applications
Alloy 90, a nickel-based superalloy, is engineered for high-performance applications requiring exceptional strength, heat resistance, and corrosion resistance. Composed primarily of nickel with significant additions of chromium, iron, cobalt, molybdenum, tungsten, titanium, and aluminum, this alloy exhibits outstanding mechanical properties at elevated temperatures.
Key Features:
- High Temperature Strength: Alloy 90 offers impressive tensile and yield strengths, maintaining integrity under extreme heat conditions.
- Corrosion Resistance: Exhibits excellent resistance to oxidation, corrosion, and degradation in aggressive environments.
- Fatigue and Creep Resistance: Demonstrates superior fatigue and creep resistance, crucial for prolonged service life under cyclic and sustained loads.
- Thermal Stability: Retains mechanical properties at temperatures exceeding 1000°C, ideal for gas turbines and aerospace components.
- Versatile Application: Widely used in aerospace propulsion systems, industrial gas turbines, and high-temperature processing equipment.
- Machinability and Weldability: Though challenging to machine, Alloy 90 can be welded using appropriate techniques, ensuring versatility in fabrication.
Alloy 90 remains a cornerstone in industries demanding reliability, durability, and performance under demanding operational conditions, making it a preferred choice for critical components in aerospace and industrial sectors worldwide.
Detailed Composition:
| Element | Weight Percentage (%) |
|---|---|
| Nickel (Ni) | 57-59 |
| Chromium (Cr) | 13-15 |
| Iron (Fe) | 13-15 |
| Cobalt (Co) | 2.5-3.5 |
| Molybdenum (Mo) | 2.5-3.5 |
| Tungsten (W) | 1.5-2.5 |
| Titanium (Ti) | 1.0-2.0 |
| Aluminum (Al) | 1.0-2.0 |
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