Aluminum alloy 7020 is a high-strength, heat-treatable alloy primarily used in aerospace applications, particularly in the construction of aircraft structures. It offers a good combination of strength, toughness, and corrosion resistance. Here are some details about 7020 aluminum alloy:
Mechanical Properties: |
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Tensile Strength: 52,000 psi (360 MPa) Yield Strength: 44,000 psi (305 MPa) Elongation: 9% |
Physical Properties: |
Density: 2.78 g/cm³ (0.100 lb/in³) Melting Range: 655°C-695°C (1211°F-1283°F) |
Welding: |
7020 is generally considered weldable using standard welding methods, including gas tungsten arc welding (GTAW/TIG) and gas metal arc welding (GMAW/MIG). However, welding should be approached with care, and special precautions may be necessary to avoid heat-affected zone issues. |
Corrosion Resistance: |
7020 offers good corrosion resistance, especially when compared to other high-strength aluminum alloys. However, its primary use in aerospace applications often involves protective coatings for additional corrosion protection. |
Alloy : 7020 Aluminium Alloy
Temper :
O H14 H24 H18 / T351 T3 T4 T651 T6 / H14 H24 H26 H16 / H32 H111 H321 H116 H112 / T6 T651 / T651 T6 T7451
T6: Solution heat-treated and artificially aged. This is the most common temper for 7020, providing high strength and toughness.
Thickness : 0.2mm-300mm
Width : 500mm-3000mm
Standard : GB/ 3880-2012 ASTMB209 EN485
Surface Treatment : Mill finish / Brush polish
PVC Coated : One side or two side PVC
MOQ : The inventory has no MOQ
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
Alloy 7020 Composition: |
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Aluminum (Al): | 91.9% |
Copper (Cu): | 1.4%-2.0% |
Manganese (Mn): | 0.10%-0.40% |
Magnesium (Mg): | 1.2%-2.1% |
Chromium (Cr): | 0.10% |
Zinc (Zn): | 5.8%-6.8% |
Titanium (Ti): | 0.10% |
Others: | 0.05% (each) 0.15% (total) |
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