Aluminum alloy 7075 is a high-strength, heat-treatable alloy that belongs to the 7000 series of aluminum alloys. It is widely used in aerospace applications and other industries where high strength and low density are critical requirements.
Properties: |
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Density: 2.78 g/cm³ Melting Point: Approximately 635°C (1175°F) Tensile Strength: Varies based on temper and thickness. Yield Strength: Varies based on temper and thickness. Elongation at Break: Varies based on temper and thickness. Modulus of Elasticity: Approximately 71 GPa (10,300 ksi) Thermal Conductivity: 130 W/m·K |
Details and Characteristics: |
Fatigue Resistance: It exhibits good fatigue resistance, contributing to its use in applications such as aircraft structures. High Strength: 7075 alloy is known for its exceptionally high strength, making it one of the strongest aluminum alloys available. Anodizing Compatibility: 7075 alloy is generally compatible with anodizing processes, providing options for surface treatment and enhancement. Weldability: It has fair weldability, but welding should be performed with caution, and post-weld heat treatment may be required to restore properties. |
Alloy: 7075 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
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
Chemical Composition |
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Aluminium (Al): | 90.7% |
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Iron (Fe): | 0.5% |
Copper (Cu): | 5.1% - 6.1% |
Titanium (Ti): | 0.10% |
Manganese (Mn): | 2.1% - 2.9% |
Magnesium (Mg): | 2.1% - 2.9% |
Zinc (Zn): | 1.2% - 2.0% |
Chromium (Cr): | 0.18% - 0.28% |
other | 0.05%(each) 0.15(total) |
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