GH4145 Alloy
GH4145 is a high-performance nickel-based superalloy renowned for its exceptional strength, thermal stability, and resistance to oxidation and corrosion. It is designed for use in demanding high-temperature environments where reliability and durability are critical.
Key Features:
- Composition: The alloy primarily consists of nickel, with substantial amounts of chromium, iron, and cobalt, alongside molybdenum, titanium, and aluminum. This composition provides a balance of mechanical strength, thermal stability, and corrosion resistance.
- Temperature Resistance: GH4145 performs effectively at high temperatures up to approximately 1390°C (2530°F), maintaining its mechanical properties and structural integrity under extreme thermal conditions.
- Mechanical Strength: It offers high yield and tensile strength, ensuring durability and performance under significant stress and load conditions.
- Oxidation and Corrosion Resistance: The alloy is highly resistant to oxidation and high-temperature corrosion, which prolongs the life of components and minimizes maintenance needs.
- Applications: GH4145 is commonly used in aerospace applications, including gas turbines, as well as in high-temperature industrial processes where its strength, stability, and resistance to harsh environments are essential.
GH4145 alloy’s superior combination of strength, thermal resistance, and corrosion protection makes it an ideal material for critical applications that require reliable performance in challenging conditions.
Here’s a detailed composition table for GH4145 alloy:
Element | Content Range |
Nickel (Ni) | Balance |
Chromium (Cr) | 18.0-21.0% |
Iron (Fe) | 14.0-17.0% |
Cobalt (Co) | 8.0-10.0% |
Molybdenum (Mo) | 2.0-3.0% |
Titanium (Ti) | 1.5-2.5% |
Aluminum (Al) | 1.0-1.5% |
Boron (B) | 0.005-0.015% |
This table provides a clear overview of the chemical composition of GH4145 alloy, detailing the content ranges of its key elements.
