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Product Details:
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| Shape: | Bar | Produc Tname: | 7075 Aluminum Bar High Strength For Aerospace Engineering |
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| Material: | Aluminum Alloy | Density: | 2.7 G/cm³ |
| Surfacefinish: | Mill Finish, Anodized, Polished | Yieldstrength: | E.g. 190-500 MPa Depending On Alloy |
| Applications: | Construction, Automotive, Aerospace, Machinery | Alloytype: | E.g. 6061, 7075, 2024 |
| Corrosionresistance: | High | Length: | Customizable, Typically 1m To 6m |
| Heattreatment: | T3, T4, T6 (depending On Alloy) | Diameter: | Varies, E.g. 10mm To 200mm |
| Thermalconductivity: | Approximately 150-170 W/m·K | Tensilestrength: | E.g. 240-570 MPa Depending On Alloy |
| Highlight: | 7075-T651 Aluminum Bar,7075-T651 Aerospace Aluminum Bar,Precision Engineering Aluminum Bar |
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7075 aluminum bar is developed for aerospace engineering, high-load industrial equipment, defense systems, and precision mechanical structures requiring high tensile strength. The alloy provides excellent strength-to-weight ratio and stable mechanical properties.
Heavy-load engineering applications require:
7075 aluminum bars provide:
| Item | Specification |
|---|---|
| Alloy | 7075-T651 |
| Diameter | 10-250 mm |
| Surface | Mill Finish |
| Standard | ASTM B211 |
| Tensile Strength | ≥510 MPa |
Zinc alloy elements improve hardness and strength after heat treatment processing.
2024 aluminum bar is commonly used in aerospace structures, aircraft engineering, and high-fatigue industrial components. The alloy provides reliable fatigue resistance and lightweight structural performance.
Aerospace structures require:
2024 aluminum bars provide:
| Item | Specification |
|---|---|
| Alloy | 2024-T4 |
| Diameter | 10-180 mm |
| Surface | Mill Finish |
| Standard | AMS / ASTM |
Copper alloy composition improves fatigue resistance for structural applications.
Contact Person: Johnny
Tel: 13395131255