2014 Aluminium Sheet
Aluminum alloy 2014 is a high-strength, heat-treatable alloy with good machinability. It is often used in aerospace applications, structural components, and other high-stress applications.
| Mechanical Properties: |
|---|
Tensile Strength:68,000 psi (469 MPa) Yield Strength:47,000 psi (324 MPa) Elongation:12% |
| Physical Properties: |
Density: 2.78 g/cm³ (0.100 lb/in³) Melting Range: 500°C-640°C (932°F-1184°F) |
| Welding: |
| 2014 is generally considered weldable using standard methods, although caution is needed due to its high copper content. Welding processes like gas tungsten arc welding (GTAW/TIG) or gas metal arc welding (GMAW/MIG) are commonly used. |
| Corrosion Resistance: |
| 2014 has moderate corrosion resistance. It is not as corrosion-resistant as some other aluminum alloys but is suitable for many applications. Its primary use is in situations where high strength and toughness are required. |
| Considerations |
| 2014 is known for its excellent machinability, making it suitable for applications requiring intricate or precise machining. |
2014 Aluminium Sheets
Alloy: 2014 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
T3: Solution heat-treated and then cold worked.
T351: Solution heat-treated, stress-relieved by stretching, and then artificially aged.
T4: Solution heat-treated and then naturally aged to a substantially stable condition.
T6: Solution heat-treated and then artificially aged.
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 2014 Composition: |
|
| Aluminum (Al): | 90.7% |
| Silicon (Si): | 0.7% |
| Iron (Fe): | 0.7% |
| Copper (Cu): | 3.9%-5.0% |
| Manganese (Mn): | 1.2%-1.8% |
| Magnesium (Mg): | 1.2%-1.8% |
| Titanium (Ti): | 0.2%-0.8% |
| Zinc (Zn) | 1.2%-1.8% |
| Others: | 0.15% (each), 0.15% (total) |
Typical Uses: Aerospace components | Aircraft structures | Truck frames | Structural components in construction | High-stress applications
