GH333 Alloy Nickel Based Superalloy With High Strength Excellent Oxidation Resistance
| Attribute | Value |
|---|---|
| Material Type | Nickel-based Superalloy |
| Density | ~8.3 g/cm³ |
| Tensile Strength | ~850 MPa |
| Yield Strength | ~700 MPa |
| Temperature Range | Up to 950°C (1742°F) |
| Oxidation Resistance | Excellent |
| Corrosion Resistance | Good |
| Applications | Aerospace, power generation, chemical processing |
| Heat Treatment | Solution treated and aged |
GH333 Alloy is a high-performance nickel-based superalloy engineered for demanding high-temperature applications. It is designed to deliver exceptional strength, durability, and resistance to harsh environments, making it suitable for critical components in aerospace and industrial sectors.
- Composition: Primarily nickel with chromium, molybdenum, titanium, and aluminum, tailored to enhance its mechanical properties and resistance to heat.
- Temperature Resistance: Effective in environments up to 950°C (1742°F), where it maintains structural integrity and performance.
- Mechanical Properties: Provides high tensile and yield strength, ensuring reliability and stability under extreme stress conditions.
- Oxidation and Corrosion Resistance: Excellent resistance to oxidation and corrosion, extending the lifespan of components in aggressive environments.
- Applications: Ideal for use in aerospace engine components, industrial gas turbines, exhaust systems, and chemical processing equipment, where high-temperature stability and durability are crucial.
- Heat Treatment: Capable of being heat-treated to achieve optimal mechanical properties, including improved strength and toughness, offering flexibility in manufacturing processes.
GH333 Alloy's advanced properties make it an ideal choice for applications requiring high performance, resistance to extreme temperatures, and reliable long-term operation. Its robust nature ensures dependable service in some of the most challenging industrial and aerospace environments.
| Element | Composition (%) |
|---|---|
| Nickel (Ni) | Balance |
| Chromium (Cr) | 14.0 - 16.0 |
| Molybdenum (Mo) | 3.0 - 4.0 |
| Titanium (Ti) | 1.0 - 2.0 |
| Aluminum (Al) | 0.8 - 1.2 |
| Iron (Fe) | ≤ 4.0 |
| Carbon (C) | ≤ 0.08 |
| Silicon (Si) | ≤ 0.50 |
| Manganese (Mn) | ≤ 0.50 |
| Boron (B) | ≤ 0.01 |
These values are approximate and can vary slightly based on the specific production standards and requirements of the alloy.
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