Product Details:
|
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 |
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 |
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 |
Contact Person: John zhou
Tel: +8613306184668
Fax: 86-510-88232386