Product Details:
|
Name: | Nickel Based Superalloy | Density: | ~8.6 G/cm³ (0.310 Lb/in³) |
---|---|---|---|
Melting Point: | ~1300-1400°C (2370-2550°F) | Tensile Strength: | ~950 MPa (138 Ksi) |
Yield Strength: | ~750 MPa (109 Ksi) | Elongation: | ~15% |
Thermal Conductivity: | ~12 W/m·K (8.4 BTU·in/hr·ft²·°F) | Modulus Of Elasticity: | ~210 GPa (30 X 10³ Ksi) |
Corrosion Resistance: | Good Oxidation And Corrosion Resistance At High Temperatures | Applications: | Aerospace Components, Gas Turbines, High-temperature Structural Parts |
Highlight: | Nickel Based Superalloy Oxidation Resistant,High Strength Nickel Based Superalloy |
Attribute | Value |
---|---|
Name | Nickel Based Superalloy |
Density | ~8.6 g/cm³ (0.310 lb/in³) |
Melting Point | ~1300-1400°C (2370-2550°F) |
Tensile Strength | ~950 MPa (138 ksi) |
Yield Strength | ~750 MPa (109 ksi) |
Elongation | ~15% |
Thermal Conductivity | ~12 W/m·K (8.4 BTU·in/hr·ft²·°F) |
Modulus of Elasticity | ~210 GPa (30 x 10³ ksi) |
Corrosion Resistance | Good oxidation and corrosion resistance at high temperatures |
Applications | Aerospace components, gas turbines, high-temperature structural parts |
GH132 Alloy is a high-performance nickel-based superalloy designed for demanding high-temperature applications. It is known for its exceptional strength and stability under elevated temperatures, making it ideal for use in aerospace and industrial environments.
Element | Composition Range (%) |
---|---|
Nickel (Ni) | 60.0 - 65.0 |
Chromium (Cr) | 14.0 - 16.0 |
Cobalt (Co) | 8.0 - 10.0 |
Molybdenum (Mo) | 2.5 - 4.0 |
Iron (Fe) | ≤ 6.0 |
Titanium (Ti) | 1.0 - 2.0 |
Aluminum (Al) | 1.0 - 2.0 |
Carbon (C) | ≤ 0.10 |
Manganese (Mn) | ≤ 0.5 |
Silicon (Si) | ≤ 0.5 |
Sulfur (S) | ≤ 0.01 |
These values are general guidelines. For specific applications or precise compositions, consult with industry standards or suppliers.
Contact Person: John zhou
Tel: +8613306184668
Fax: 86-510-88232386