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Temperature Resistant Inconel 706 Nickel Alloy Rod For Aerospace Components
| 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
Inconel706 Alloy
Name:
Nickel Based Alloys
Alloy Type:
Nickel-Chromium Superalloy
Density:
~8.42 G/cm³ (0.305 Lb/in³)
Melting Point:
~1360-1410°C (2480-2570°F)
Tensile Strength:
~1100 MPa (160 Ksi)
Yield Strength:
~950 MPa (138 Ksi)
Elongation:
~20%
Thermal Conductivity:
~11.8 W/m·K (8.2 BTU·in/hr·ft²·°F)
Modulus Of Elasticity:
~207 GPa (30 X 10³ Ksi)
Corrosion Resistance:
Excellent In High-temperature Environments
Applications:
Aerospace Components, Gas Turbines
Highlight:
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Product Description
Temperature Resistant Inconel 706 Nickel Alloy Rod For Aerospace Components
Product Specifications
| Attribute | Value |
|---|---|
| Name | Nickel Based Alloys |
| Alloy Type | Nickel-Chromium Superalloy |
| Density | ~8.42 g/cm³ (0.305 lb/in³) |
| Melting Point | ~1360-1410°C (2480-2570°F) |
| Tensile Strength | ~1100 MPa (160 ksi) |
| Yield Strength | ~950 MPa (138 ksi) |
| Elongation | ~20% |
| Thermal Conductivity | ~11.8 W/m·K (8.2 BTU·in/hr·ft²·°F) |
| Modulus of Elasticity | ~207 GPa (30 x 10³ ksi) |
| Corrosion Resistance | Excellent in high-temperature environments |
| Applications | Aerospace components, gas turbines |
Product Description
Inconel 706 is a high-strength nickel-chromium alloy for aerospace and high-temperature applications. This superalloy is engineered to deliver exceptional performance under extreme conditions, combining superior mechanical properties with outstanding resistance to oxidation and corrosion.
Key Features
- High Strength: Maintains excellent tensile and yield strength even at elevated temperatures
- Temperature Resistance: Performs reliably in extreme heat while retaining structural integrity
- Corrosion Resistance: Superior oxidation and corrosion resistance for harsh environments
- Aerospace Applications: Ideal for gas turbines and critical structural components
Chemical Composition
| Element | Composition Range (%) |
|---|---|
| Nickel (Ni) | 50.0 - 55.0 |
| Chromium (Cr) | 13.0 - 15.0 |
| Iron (Fe) | Balance |
| Molybdenum (Mo) | 1.5 - 2.5 |
| Titanium (Ti) | 2.0 - 3.0 |
| Aluminum (Al) | 0.3 - 0.6 |
| Cobalt (Co) | 0.5 - 2.0 |
| Carbon (C) | ≤ 0.05 |
| Manganese (Mn) | ≤ 0.5 |
| Silicon (Si) | ≤ 0.5 |
| Sulfur (S) | ≤ 0.01 |
Note: Please verify with specific standards or suppliers for precise values.
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