Aluminium 2014
Aluminium 2014 is a copper based, high strength aluminium. Machinability of the material is good in the annealed state but somewhat more difficult in heat treated conditions.
The alloy is easily cold worked in the T3 and T4 tempers. Aluminium 2014 is has the following uses…
-
Contribution to the manufacture of aircraft structures
-
Truck frames
Aluminium 2014 is available from us in bar, hexagon, tube and flats in a range of sizes… Round bars: from ¼” dia – 12” dia
Chemical & Physical Properties
Typical Chemical Composition
Elements |
Min % |
Max % |
Al |
Remainder |
|
Cr |
|
0.10 |
Cu |
3.9 |
5.0 |
Fe |
|
0.50 |
Mg |
0.20 |
0.8 |
Mn |
0.40 |
1.2 |
Ni |
|
0.10 |
Others each |
|
0.05 |
Others total |
|
0.15 |
Si |
0.50 |
0.9 |
Ti |
|
0.15 |
Zn |
|
0.25 |
Zr+Ti |
|
0.20 |
Typical Mechanical Properties
Property/unit | Condition | Temp | Size | Min | Max |
Tensile Strength (N/mm2) | H13 | RT | <= 18mm | 210 | 300 |
0.2% Proof Stress (N/mm2) | H13 | RT | <= 18mm | 190 | |
Elongation in 100mm % | H13 | RT | <= 18mm | 5 | |
Tensile Strength (N/mm2) | T4 | RT | <= 18mm | 380 | |
0.2% Proof Stress (N/mm2) | T4 | RT | <= 18mm | 255 | |
Elongation in 100mm % | T4 | RT | <= 18mm | 18 | |
Tensile Strength (N/mm2) | T6 | RT | <= 18mm | 440 | |
0.2% Proof Stress (N/mm2) | T6 | RT | <= 18mm | 415 | |
Elongation in 100mm % | T6 | RT | <= 18mm | 9 | |
Tensile Strength (N/mm2) | T62 | RT | <= 18mm | 440 | |
0.2% Proof Stress (N/mm2) | T62 | RT | <= 18mm | 415 | |
Elongation in 100mm % | T62 | RT | <= 18mm | 9 |
Tolerances
Diameter
|
Tolerance |
8mm – 18mm |
+/- 0.22mm |
18mm – 25mm |
+/- 0.25mm |
25mm – 40mm |
+/- 0.30mm |
40mm – 50mm |
+/- 0.35mm |
50mm – 65mm |
+/- 0.40mm |
65mm – 80mm |
+/- 0.45mm |
80mm – 100mm |
+/- 0.55mm |
100mm – 120mm |
+/- 0.65mm |
120mm – 150mm |
+/- 0.80mm |
150mm – 180mm |
+/- 1.00mm |
180mm – 220mm |
+/- 1.15mm |
220mm – 270mm |
+/- 1.30mm |
270mm – 320mm |
+/- 1.60mm |