2xxx Series
2XXXHeat Treatable

2xxx Series

Aluminum-Copper Alloys

Overview

High strength-to-weight ratio, good machinability, heat treatable

Requires surface protection in corrosive environments

Applications

Aircraft structures
Automotive components
Military equipment
Truck frames
Suspension components

Common Alloys

201420172024

Properties

Strength
High
Corrosion Resistance
Poor
Weldability
Poor
Heat Treatable
Yes

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Manufacturing Process

Step 1

Material Preparation

Primary aluminum and copper/magnesium master alloys are weighed to hit precise target compositions (Cu 3.5–5.0%).

Step 2

Melting & Alloying

Elements dissolved in sequence at 720–760 °C. Ti-B grain refiner and flux treatments ensure a clean melt.

Step 3

DC Casting

Direct Chill casting into billets or rolling ingots; homogenisation soak at 480–500 °C for 12–24 h equalises composition.

Step 4

Hot Working

Billets are rolled or forged at 400–450 °C through multiple reduction passes to the required shape and gauge.

Step 5

Solution Heat Treatment

Rapid heating to 490–503 °C fully dissolves alloying elements, followed immediately by cold-water quench to lock the supersaturated state.

Step 6

Precipitation Hardening

Artificial aging at 120–130 °C (T6 temper) precipitates fine CuAl₂ particles for peak strength. Final tensile and hardness inspection.

Chemical Composition

EN 573-3 / AA

Max % unless range shown. Balance: Al.

Swipe to see all columns
AlloyChem. SymbolSiFeCuMnMgCrZnTi
2014AlCu4SiMg0.50–1.20.703.9–5.00.40–1.20.20–0.800.100.250.15
2017AlCu4MgSi0.20–0.800.703.5–4.50.40–1.00.40–0.800.100.250.15
2024AlCu4Mg10.500.503.8–4.90.30–0.91.2–1.80.100.250.15