
Alloy Portfolio
Nickel X
Hastelloy X, also known as Alloy X, is a high-temperature nickel-chromium-iron-molybdenum alloy with excellent oxidation resistance and high-temperature strength. Composed of approximately 47.5% nickel, 22% chromium, 18.5% iron, and significant amounts of molybdenum and cobalt, Hastelloy X is designed for use in extreme environments.
This alloy is particularly well-suited for applications in gas turbine engines, where it withstands high temperatures and thermal cycling. Hastelloy X exhibits good resistance to oxidation and carburization in high-temperature atmospheres, making it suitable for components such as combustion chambers, afterburner parts, and other critical aerospace and industrial applications. Its combination of high-temperature strength and corrosion resistance makes Hastelloy X a valuable material for use in challenging environments where both mechanical and chemical properties are crucial.
Key Characteristics of Hastelloy X:
- High Temperature Strength: Hastelloy X exhibits excellent strength and stability at elevated temperatures, making it suitable for use in high-temperature applications.
- Oxidation Resistance: The alloy has remarkable resistance to oxidation at high temperatures, making it suitable for environments with exposure to air and oxygen.
- Good Fabricability: Hastelloy X is known for its good fabricability, allowing for various manufacturing processes such as welding, forging, and machining.
- High Creep Resistance: The alloy shows resistance to creep deformation, making it suitable for applications involving sustained loads at high temperatures.
- Excellent Weldability: Hastelloy X can be welded using various welding techniques, which adds to its versatility in fabrication processes.
- Corrosion Resistance: It provides good corrosion resistance in a variety of corrosive environments, including strong acids and reducing agents.
- Thermal Stability: Hastelloy X maintains its mechanical properties even after prolonged exposure to high temperatures.
Applications of Hastelloy X:
- Aerospace Industry: Hastelloy X is commonly used in gas turbine engine components, such as combustion chambers, afterburners, and tailpipes, due to its high-temperature strength and oxidation resistance.
- Chemical Processing: The alloy is employed in chemical processing equipment, including reactors, catalyst support grids, and piping, where resistance to high temperatures and corrosive chemicals is crucial.
- Industrial Furnaces: Hastelloy X is used in the construction of industrial furnaces and heating elements where exposure to high temperatures and oxidative atmospheres is prevalent.
- Superalloys: It is used as a superalloy in various applications that demand high-temperature strength, corrosion resistance, and stability, such as in the production of aerospace components.
- Nuclear Reactors: Hastelloy X finds applications in nuclear reactors and related components due to its resistance to high-temperature and corrosive conditions.
- Automotive Industry: Some high-performance automotive applications, particularly in exhaust systems, may use Hastelloy X due to its ability to withstand high temperatures and corrosive exhaust gases.
- Power Generation: The alloy is employed in components of power generation systems, including turbine blades and combustion chambers.
- Petrochemical Industry: Hastelloy X is utilized in various petrochemical applications, including components for processing units and equipment where exposure to corrosive substances is common.
Here is the chemical composition of Hastelloy X, presented in a tabular format:
-
Nickel
(Ni)
47.5%
-
Chromium
(Cr)
22.0%
-
Iron
(Fe)
18.5%
-
Cobalt
(Co)
9.0%
-
Molybdenum
(Mo)
1.5%
-
Silicon
(Si)
0.5% max
-
Carbon
(C)
0.1% max
-
Manganese
(Mn)
0.1% max
-
Sulfur
(S)
0.03% max
-
Phosphorus
(P)
0.02% max
Here are the typical mechanical properties of Hastelloy X, presented in tabular form:
Property | Value |
---|---|
Tensile Strength | 760 MPa (110,000 psi) minimum |
Yield Strength (0.2% offset) | 340 MPa (49,300 psi) minimum |
Elongation | 40% minimum |
Hardness (Brinell) | Not typically specified |
Modulus of Elasticity | 217 GPa (31,500 ksi) |