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Anti Corrosion Oxidation Hastelloy X Alloy Nickel Chromium Molybdenum Alloy
| MOQ: | 100KG |
| Price: | Price is negotiated based on the required specifications and quantity |
| Standard Packaging: | Standard export packaging, or packaging as required |
| Delivery Period: | 5-8 working days, depending on the parameters required for negotiation |
| Payment Method: | Payment Terms: Mainly T/T.. L/C, D/A, D/P, |
| Supply Capacity: | 5000 tons per month |
Detail Information
Place of Origin
China
Brand Name
Zhonggong Special Metallurgy
Certification
ISO Certificate
Model Number
HastelloyX
Name:
Hastelloy X Alloy
Applications:
Gas Turbines, Aerospace Components, High-temperature Industrial Processes
Density:
~8.72 G/cm³ (0.315 Lb/in³)
Melting Point:
~1260-1330°C (2300-2425°F)
Tensile Strength:
~930 MPa (135 Ksi)
Yield Strength:
~690 MPa (100 Ksi)
Elongation:
~20%
Thermal Conductivity:
~12.2 W/m·K (8.4 BTU·in/hr·ft²·°F)
Modulus Of Elasticity:
~207 GPa (30 X 10³ Ksi)
Corrosion Resistance:
Excellent, Especially In High-temperature Environments
Highlight:
Anti Corrosion Hastelloy X Alloy
,Nickel Chromium Molybdenum Alloy
,Anti oxidation Hastelloy X Alloy
Product Description
Anti Corrosion Oxidation Hastelloy X Alloy Nickel Chromium Molybdenum Alloy
Product Attributes
| Attribute | Value |
|---|---|
| Name | Hastelloy X Alloy |
| Applications | Gas turbines, aerospace components, high-temperature industrial processes |
| Density | ~8.72 g/cm³ (0.315 lb/in³) |
| Melting Point | ~1260-1330°C (2300-2425°F) |
| Tensile Strength | ~930 MPa (135 ksi) |
| Yield Strength | ~690 MPa (100 ksi) |
| Elongation | ~20% |
| Thermal Conductivity | ~12.2 W/m·K (8.4 BTU·in/hr·ft²·°F) |
| Modulus of Elasticity | ~207 GPa (30 x 10³ ksi) |
| Corrosion Resistance | Excellent, especially in high-temperature environments |
Product Description
Hastelloy X Is A High-Performance Nickel-Chromium-Molybdenum Alloy For High-Temp Applications
Hastelloy X Alloy is a high-performance nickel-chromium-molybdenum superalloy designed to deliver exceptional performance in extreme environments. This alloy is engineered to maintain its mechanical strength and structural integrity at temperatures up to 2200°F (1200°C), making it ideal for high-temperature applications such as gas turbines, jet engines, and industrial heat exchangers.
Key Properties and Features:
- Temperature Resistance: Capable of withstanding extreme temperatures while retaining excellent strength and resistance to thermal degradation.
- Corrosion Resistance: Offers superior resistance to oxidation, carburization, and sulfidation, ensuring longevity and reliability in harsh environments.
- Mechanical Strength: Maintains high tensile and yield strength, coupled with excellent creep and fatigue resistance, under severe operational conditions.
- Applications: Commonly used in aerospace components, high-temperature gas turbines, jet engines, and other critical industrial processes requiring robust high-temperature performance.
- Stability: Provides consistent performance and dimensional stability, even in the most demanding applications, reducing the need for frequent maintenance or replacement.
Hastelloy X's combination of strength, resistance to thermal and chemical degradation, and reliability makes it a preferred choice for high-stress, high-temperature applications where durability and long-term performance are essential.
Chemical Composition
| Element | Composition Range (%) |
|---|---|
| Nickel (Ni) | 47.0 - 52.0 |
| Chromium (Cr) | 19.0 - 21.0 |
| Molybdenum (Mo) | 8.0 - 9.5 |
| Iron (Fe) | Balance |
| Cobalt (Co) | 1.0 - 2.5 |
| Titanium (Ti) | 0.6 - 1.0 |
| Aluminum (Al) | 0.2 - 0.8 |
| Carbon (C) | ≤ 0.1 |
| Manganese (Mn) | ≤ 1.0 |
| Silicon (Si) | ≤ 0.5 |
| Sulfur (S) | ≤ 0.01 |
Please verify with specific standards or suppliers for precise values as they may vary slightly.
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