7050 Aluminium Chequered Sheet & Plate
Aluminium alloy 7050 is a high-strength, heat-treatable alloy known for its exceptional strength-to-weight ratio and toughness. While it may not be the most common choice for chequered sheets or plates, it is widely used in aerospace and military applications where high strength and durability are critical.
| Details and Characteristics: |
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Strength: 7050 aluminium alloy is known for its high strength, particularly after heat treatment. Corrosion Resistance: While it has good corrosion resistance, it may not be as corrosion-resistant as some other aluminium alloys. Toughness: It exhibits good toughness and resistance to crack propagation, making it suitable for applications where fatigue resistance is critical. Applications: Aerospace components (aircraft structures, fuselage components) | Military and defense applications | High-performance structures requiring strength and toughness |
7050 Aluminium Chequered Sheet & Plate
Alloy : 7050 Aluminium Alloy |
Temper:
O / F / H12 / H14 / H16 / H18 / H19 / H22 / H24 / H26 / H32 / H34 / H36 / H38 / H111 / H112 / H321 / T3 / T4 / T5 / T6 / T7 / T351 / T451 / T651 / T851
Thickness: 0.2mm - 10mm
Width: 500mm-2000mm
Standard: GB/T 3880-2012 ASTMB209 EN485
Pattern: Big Five Bars / Small Five Bars / Two Bars/ Small Three Bars / Diamond
Surface Treatment: Mill Finish / Brush Polish / 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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| Aluminium (Al): | 89.7% |
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| Zinc (Zn): | 6.1% |
| Copper (Cu): | 2.1-2.9% |
| Magnesium (Mg): | 2.0-2.6% |
| Chromium (Cr): | 0.04-0.15% |
| Manganese (Mn): | 0.06% |
| Titanium (Ti): | 0.06% |
| Others: | 0.05% each, 0.15% total (max) |
