2014A
Grade 2014A aluminium is a heat treatable high strength alloy with a 4-5% copper addition. Produced in bar and profile it is supplied in the fully heat-treated condition for the optimum mechanical properties.
Normally stocked in the T6 condition (stress relieved and artificially aged) the2014A offers a high strength vs. density and is commonly used in the aerospace and defence industries for the manufacture of aircraft structures, and truck frames. The general resistance to atmospheric attack is low, especially in marine environments. To improve the resistance against corrosion 2014A can be hard or protective anodised, coated or if in storage, lightly coat with Lanolin based protective Oil.
Chemical Composition
Aluminium |
Rem |
Silicon |
0.5-0.9% |
Copper |
3.9 - 5.0% |
Iron |
0.5% max |
Manganese |
0.4 – 1.2% |
Magnesium |
0.2-0.8% |
Zinc |
0.25% max |
Nickel |
0.1% max |
Titanium |
0.15% max |
Zirconium + Titanium |
0.2% max |
Chromium |
0.1% max |
Total Others |
0.15 max |
Related Specifications
2014A |
HE15 |
L168 |
BS H15 |
A92014 |
W Nr. 3.1254 / 3.1255 |
AlCu4SiMg |
AMS 4121 |
|
Key Features
- Very Good Machining Properties
- Good Hard Anodising Capability
- Easily Plated
- Good Strength Levels after heat treatment.
Typical Physical Properties
Melting Range |
530-610°C |
Density |
2.80 g/cm³ |
Thermal conductivity |
159 W/m°K |
Thermal expansion coefficient |
22 x 10-6 |
Electrical Conductivity |
38.3 IACS |
Electrical resistivity |
0.045 microhm m |
Modulus of elasticity |
74 GPa |
Fabrication Properties
Cold Formability |
Fair |
Machinability |
Excellent |
Brazing & Soldering |
Not recommended |
Oxygen Welding |
Not recommended |
Inert Gas Welding |
Not recommended |
Resistance Welding Spot & Beam |
Excellent |
Typical Applications
High strength structural components: aircraft (e.g. fittings and wheels), military vehicles and bridges, forgings for trucks and machinery (hydraulic etc.). Weapons manufacture, structural applications.
This technical information is given by Holme Dodsworth Metals without charge and the user shall employ such information at their own discretion and risk. For more detailed technical advice on temper selection, fabrication, joining, machining, physical and mechanical data please contact us as space does not permit the listing of every feature of the material.