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Inconel X-750 Round Bar High Performance Nickel Chromium 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
InconelX-750 Alloy
Chemical Composition:
Ni (70.0-76.0%), Cr (14.0-17.0%), Fe (6.0-10.0%), Mo (2.8-3.3%), Ti (0.6-1.0%), Al (0.2-0.6%), C (0.08% Max), Mn (1.0% Max), Si (0.5% Max), S (0.015% Max), P (0.015% Max)
Density:
8.38 G/cm³
Melting Point:
1290-1350°C
Tensile Strength:
965 MPa (140 Ksi)
Yield Strength:
690 MPa (100 Ksi)
Elongation:
30% (minimum)
30% (minimum):
210 GPa
Thermal Conductivity:
11.7 W/m·K
Specific Heat Capacity:
0.43 J/g·K
Corrosion Resistance:
Excellent Resistance To Oxidation And Carburization At High Temperatures
Applications:
Gas Turbines, Rocket Engines, Industrial Furnaces, Nuclear ReactorsGas Turbines, Rocket Engines, Industrial Furnaces, Nuclear ReactorsGas Turbines, Rocket Engines, Industrial Furnaces, Nuclear ReactorsGas Turbines, Rocket Engines, Industrial Furnaces, Nucl
Highlight:
Inconel X-750
,Inconel X750 Round Bar
,Inconel Alloy X-750
Product Description
Inconel X-750 Round Bar High Performance Nickel Chromium Alloy
Product Specifications
| Attribute | Value |
|---|---|
| Chemical Composition | Ni (70.0-76.0%), Cr (14.0-17.0%), Fe (6.0-10.0%), Mo (2.8-3.3%), Ti (0.6-1.0%), Al (0.2-0.6%), C (0.08% max), Mn (1.0% max), Si (0.5% max), S (0.015% max), P (0.015% max) |
| Density | 8.38 g/cm³ |
| Melting Point | 1290-1350°C |
| Tensile Strength | 965 MPa (140 ksi) |
| Yield Strength | 690 MPa (100 ksi) |
| Elongation | 30% (minimum) |
| Modulus of Elasticity | 210 GPa |
| Thermal Conductivity | 11.7 W/m·K |
| Specific Heat Capacity | 0.43 J/g·K |
| Corrosion Resistance | Excellent resistance to oxidation and carburization at high temperatures |
| Applications | Gas turbines, rocket engines, industrial furnaces, nuclear reactors |
Product Overview
Inconel X-750: Nickel-Chromium Alloy With High Strength And Excellent Oxidation Resistance At Elevated Temperatures
Inconel X-750 is a high-performance nickel-chromium alloy designed for exceptional strength and oxidation resistance at elevated temperatures. This alloy is specifically engineered to withstand harsh environments and maintain mechanical properties under extreme conditions, making it ideal for aerospace, industrial, and nuclear applications.
Key Features
- High-Temperature Strength: Maintains excellent tensile and yield strength at temperatures up to 2200°F (1204°C).
- Superior Corrosion Resistance: Outstanding resistance to oxidation, carburization, and sulfidation.
- Mechanical Properties: Tensile strength of 965 MPa (140 ksi) and yield strength of 690 MPa (100 ksi) with 30% minimum elongation.
- Thermal Conductivity: Approximately 11.7 W/m·K for effective heat distribution.
- Fabrication Versatility: Available in sheets, plates, bars, pipes, and welding wire.
Applications
- Gas turbine components (blades, vanes)
- Rocket engine parts
- Industrial furnace components
- Nuclear reactor cores and high-stress components
Standard Specifications
- ASTM B333
- ASTM B805
- ASTM B829
Detailed Composition
| Element | Range | Typical Value |
|---|---|---|
| Nickel (Ni) | 70.0 - 76.0% | 72.0% |
| Chromium (Cr) | 14.0 - 17.0% | 15.0% |
| Iron (Fe) | 6.0 - 10.0% | 8.0% |
| Molybdenum (Mo) | 2.8 - 3.3% | 3.0% |
| Titanium (Ti) | 0.6 - 1.0% | 0.8% |
| Aluminum (Al) | 0.2 - 0.6% | 0.4% |
| Carbon (C) | ≤0.08% | 0.05% |
| Manganese (Mn) | ≤1.0% | 0.8% |
| Silicon (Si) | ≤0.5% | 0.4% |
| Sulfur (S) | ≤0.015% | 0.01% |
| Phosphorus (P) | ≤0.015% | 0.01% |
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