Aluminum alloy 7050 is a high-strength, heat-treatable alloy known for its excellent strength-to-weight ratio and good corrosion resistance. It belongs to the 7000 series of aluminum alloys and is commonly used in aerospace and military applications.
| Properties: |
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Density: 2.78 g/cm³ Melting Point: Approximately 490°C (914°F) Tensile Strength: Varies based on temper and processing. Yield Strength: Varies based on temper and processing. Elongation at Break: Varies based on temper and processing. Modulus of Elasticity: Approximately 71.7 GPa (10,400 ksi) Corrosion Resistance: Good |
| Details and Characteristics: |
Corrosion Resistance: 7050 offers good corrosion resistance, and its properties can be further enhanced through appropriate surface treatments. Heat Treatment: This alloy is heat-treatable, and different temper options (T6, T651, etc.) are available to achieve specific mechanical properties. Applications: Commonly used in aerospace and military applications, such as aircraft components, missile parts, and other high-strength structural components. |
Alloy : 7050 Aluminium Alloy
Temper:
O H14 H18 / T351 T3 T4 / H24 H26 H16 / H32 H111 H321 H116 H112 / T6 T651 / T7451 T6511
Diameter: 10mm-500mm
Length: 500mm-6000mm
Standard: GB/T 3880-2012 ASTMB209 EN485
Surface Treatment: Mill Finish / Brush PSolish / Bright Finish
MOQ: The inventory has no MOQ 2mt-3mt
Packing: Standard Export Packing
Port of Dispatch: It depends on the supplier's location and shipping arrangements
Delivery Time: The inventory is 5-7 days . 25-30 days for customized products
Payment: TT / LC / TT+LC
Chemical Composition |
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| Aluminum (Al): | 87.1% |
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| Zinc (Zn): | 7.1% |
| Copper (Cu): | 2.0% - 2.6% |
| Magnesium (Mg): | 1.9% - 2.6% |
| Chromium (Cr): | 1.9% - 2.6% |
| Manganese (Mn): | 0.1% |
| Iron (Fe): | 1.9% |
| Silicon (Si): | 0.12% |
| Titanium (Ti): | 1.2% - 2.0% |
| Other | 0.05%(each) 0.15(total) |
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