GH4033 High-Temperature Alloy is a nickel-based superalloy commonly used in aerospace, power generation, and other industrial applications. It is characterized by its excellent oxidation resistance, superior thermal stability, and high mechanical strength, making it suitable for turbine components, combustion chambers, and other critical parts exposed to extreme heat and harsh environments.
Product Overview
GH4033 is a nickel-chromium-based high-temperature alloy with aluminum and titanium added to form γ-phase dispersion strengthening. This alloy demonstrates good high-temperature strength in the range of 700–750°C and excellent oxidation resistance below 900°C. GH4033 has good heating process performance and is mainly used for manufacturing engine rotor components. The alloy is ideal for parts that need to work stably in high-temperature environments for extended periods and offers excellent thermal processing properties, making it particularly suitable for hot rolling and billet supply.
Key Features
- Excellent High-Temperature Strength: The alloy offers sufficient high-temperature strength in the 700–750°C range, making it suitable for high-temperature operating environments.
- Good Oxidation Resistance: GH4033 demonstrates excellent oxidation resistance below 900°C, making it ideal for use in oxidative environments.
- Good Thermal Processing Performance: The alloy is easy to process, suitable for forging, welding, and surface treatment.
- Good Grain Size Control: The grain size is controlled through forging temperature and deformation, enhancing the alloy's microstructure and performance.
- Outstanding Welding Performance: The alloy can be arc-welded in a solution-treated state, but welding stress should be relieved promptly after welding.
Applications
- Aerospace Engines: Used in the production of engine rotor components, especially those that operate under high-temperature conditions.
- High-Temperature Components: Suitable for manufacturing components that must operate in the 700–750°C temperature range for extended periods.
- Gas Turbines: Ideal for manufacturing gas turbine components that require high strength and oxidation resistance.
- Other High-Temperature Applications: Suitable for various industrial devices and components requiring high-temperature resistance, oxidation resistance, and excellent mechanical properties.
C | Cr | Ni | Al | Ti | ||||
0.03~0.08 | 19.0~22.0 | Balance | 0.60~1.00 | 2.40~2.80 | ||||
Fe | Mn | Si | P | S | B | Ce | ||
Not more than | Not more than | Not more than | Not more than | Not more than | Not more than | Not more than | ||
4 | 0.35 | 0.65 | 0.015 | 0.007 | 0.01 | 0.01 |