GH136 Alloy Nickel Alloy Pipe With High Strength And Excellent Oxidation Resistance
| Attribute | Value |
|---|---|
| Density | ~8.8 g/cm³ (0.317 lb/in³) |
| Melting Point | ~1300-1400°C (2370-2550°F) |
| Tensile Strength | ~900 MPa (130 ksi) |
| Yield Strength | ~700 MPa (102 ksi) |
| Elongation | ~15% |
| Thermal Conductivity | ~13 W/m·K (9 BTU·in/hr·ft²·°F) |
| Modulus of Elasticity | ~210 GPa (30 x 10³ ksi) |
| Corrosion Resistance | Good oxidation and corrosion resistance at high temperatures |
GH136 Alloy is a high-performance nickel-based superalloy engineered for superior strength and oxidation resistance at elevated temperatures. This alloy is designed to perform reliably in extreme environments, making it suitable for demanding applications in aerospace and high-temperature industrial processes.
- High-Temperature Strength: Maintains excellent mechanical properties, including high tensile strength (~900 MPa or 130 ksi) and yield strength (~700 MPa or 102 ksi), at temperatures up to approximately 1300-1400°C (2370-2550°F). Ideal for components exposed to intense heat.
- Oxidation and Corrosion Resistance: Offers robust resistance to oxidation and high-temperature corrosion, ensuring long-term durability in harsh environments. Crucial for applications in gas turbines, jet engines, and other high-stress applications.
- Mechanical Properties: Provides good elongation (~15%), contributing to its ability to withstand mechanical stress without compromising integrity.
- Thermal Conductivity: Approximately 13 W/m*K (9 BTU*in/hr*ft²*°F), effectively managing heat dissipation in high-performance systems.
- Applications: Commonly used in aerospace components, gas turbines, and other high-temperature structural parts where high strength and resistance to thermal degradation are required.
GH136 Alloy's combination of high strength, oxidation resistance, and thermal stability ensures it is a reliable choice for advanced engineering applications demanding exceptional performance under extreme conditions.
| Element | Composition Range (%) |
|---|---|
| Nickel (Ni) | 60.0 - 65.0 |
| Chromium (Cr) | 14.0 - 16.0 |
| Cobalt (Co) | 8.0 - 10.0 |
| Molybdenum (Mo) | 3.0 - 5.0 |
| 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 provide general guidelines. For precise specifications or applications, consult specific standards or suppliers.
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