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Aerospace Components Inconel 751 Alloy High Strength Nickel Chromium Alloy 8.25g/Cm3
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Aerospace Components Inconel 751 Alloy High Strength Nickel Chromium Alloy 8.25g/Cm3
| 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
Inconel 751 Alloy
Name:
Inconel 751 Alloy
Density:
8.25g/cm3
Melting Point:
1300-1350°C
Tensile Strength:
965 MPa (140 Ksi)
Yield Strength:
620 MPa (90 Ksi)
Elongation:
20% (minimum)
Modulus Of Elasticity:
210 GPa
Chemical Composition:
Ni (60.0-65.0%), Cr (17.0-22.0%), Co (10.0-15.0%), Mo (2.8-3.3%), Ti (0.9-1.2%), Al (0.3-0.6%), C (0.08% Max), Mn (1.0% Max), Si (0.5% Max), S (0.015% Max), P (0.015% Max)
Thermal Conductivity:
12.0 W/m·K
Specific Heat Capacity:
0.43 J/g·K
Corrosion Resistance:
Excellent Resistance To Oxidation And Carburization At High Temperatures
Highlight:
Inconel 751 Alloy
,Nickel Chromium Alloy 8.25g/Cm3
,High Strength Nickel Chromium Alloy
Product Description
Aerospace Components Inconel 751 Alloy High Strength Nickel Chromium Alloy 8.25g/Cm3
Product Specifications
| Attribute | Value |
|---|---|
| Name | Inconel 751 Alloy |
| Density | 8.25g/cm3 |
| Melting Point | 1300-1350°C |
| Tensile Strength | 965 MPa (140 ksi) |
| Yield Strength | 620 MPa (90 ksi) |
| Elongation | 20% (minimum) |
| Modulus of Elasticity | 210 GPa |
| Chemical Composition | Ni (60.0-65.0%), Cr (17.0-22.0%), Co (10.0-15.0%), Mo (2.8-3.3%), Ti (0.9-1.2%), Al (0.3-0.6%), C (0.08% max), Mn (1.0% max), Si (0.5% max), S (0.015% max), P (0.015% max) |
| Thermal Conductivity | 12.0 W/m·K |
| Specific Heat Capacity | 0.43 J/g·K |
| Corrosion Resistance | Excellent resistance to oxidation and carburization at high temperatures |
Product Overview
Inconel 751: Nickel-Chromium Alloy With High Strength And Excellent High-Temperature Oxidation Resistance
Inconel 751 is a high-performance nickel-chromium-cobalt alloy designed for superior strength and stability at elevated temperatures. It is engineered to offer exceptional resistance to oxidation, carburization, and high-temperature degradation, making it ideal for demanding applications in aerospace and industrial environments.
Key Features
- High-Temperature Strength: Maintains excellent mechanical properties at temperatures up to 1300°C (2372°F) with tensile strength of 965 MPa (140 ksi) and yield strength of 620 MPa (90 ksi).
- Outstanding Oxidation Resistance: Specifically formulated to resist oxidation and carburization, extending component lifespan in high-temperature environments.
- Thermal Properties: Features thermal conductivity of 12.0 W/m·K and specific heat capacity of 0.43 J/g·K for effective heat distribution and stability.
- Mechanical Flexibility: Provides minimum elongation of 20% to accommodate deformation while maintaining structural integrity.
- Fabrication Versatility: Available in sheets, plates, bars, pipes, and welding wire for diverse industrial applications.
Applications
- Gas turbine components (blades, vanes)
- Aerospace applications requiring high strength and temperature resistance
- High-temperature industrial equipment and processes
Standard Specifications
- ASTM B166
- ASTM B167
- ASTM B168
Inconel 751 combines high strength, excellent oxidation resistance, and thermal stability, making it an ideal choice for critical applications in extreme environments where reliability and performance are paramount.
Chemical Composition
| Element | Range | Typical Value |
|---|---|---|
| Nickel (Ni) | 60.0 - 65.0% | 62.0% |
| Chromium (Cr) | 17.0 - 22.0% | 19.0% |
| Cobalt (Co) | 10.0 - 15.0% | 12.0% |
| Molybdenum (Mo) | 2.8 - 3.3% | 3.0% |
| Titanium (Ti) | 0.9 - 1.2% | 1.0% |
| Aluminum (Al) | 0.3 - 0.6% | 0.5% |
| 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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