
| Standard | Designation |
| UNS (USA) | A92014 (Commonly AA2014) |
| UNI (Italy) | P-AlCu4.4SiMnMg |
| ISO | Al Cu4 Si Mg |
| EN | EN AW-2014 / 2014A |
The Italian UNI designation explicitly lists the primary alloying elements in order of their concentration:
Al: Aluminium (Base)
Cu (4.4%): Copper is the primary alloying element, providing high strength through precipitation hardening.
Si: Silicon improves fluidity and hardness.
Mn: Manganese increases recrystallization temperature and strengthens the matrix.
Mg: Magnesium enhances the strength-to-weight ratio and response to heat treatment.
When sourcing this material, the distinction between "Sheet" and "Plate" often dictates the manufacturing process and the final temper.
Thickness: Generally < 6mm.
Form: Cold-rolled.
Common State: Often supplied as Alclad. Because 2014 is prone to corrosion, sheets are frequently "clad" with a thin layer of high-purity aluminum (usually alloy 1050 or 1230) on both sides to provide galvanic protection.
Application: Aircraft fuselage skins, wing skins, and fairings.
Thickness: Generally > 6mm (up to several hundred mm).
Form: Hot-rolled or forged.
Common State: Usually T651. This indicates the plate has been solution heat-treated, artificially aged, and stress-relieved by stretching to ensure dimensional stability during machining.
Application: Structural bulkheads, military bridge components, and heavy-duty forged parts.
| Property | Value |
| Yield Strength | $\approx 415 \text{ MPa}$ |
| Ultimate Tensile Strength | $\approx 485 \text{ MPa}$ |
| Shear Strength | $\approx 290 \text{ MPa}$ |
| Fatigue Strength | $\approx 125 \text{ MPa}$ |
Do Not Weld: Like its WNr 3.1255 counterpart, this alloy is generally considered non-weldable by traditional fusion methods. It is sensitive to "hot cracking." If joining is required, use mechanical fasteners or friction stir welding.
Machining: This is where the alloy shines. It allows for high-speed cutting with excellent surface finishes. However, carbide-tipped tools are recommended due to the Silicon content.
Surface Protection: If the material is not "Alclad," it must be anodized (Chromic or Sulfuric acid anodizing) or primed with a zinc-chromate primer to prevent rapid oxidation in industrial or marine environments.
Note: If your design requires high strength but also needs to be welded, you might consider switching to a 7000-series alloy (like 7075) or a high-strength 6000-series (like 6082), though neither perfectly matches the specific machining characteristics of AA2014.
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