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Aluminium Alloy 7075 T651
This is prepared to give high quality as created by heat treating. This is a very high strength aircraft alloy, which also has excellent properties at low temperatures. Commonly used in the manufacture of aircraft and other aerospace applications not requiring the corrosion resistance of Clad 7075. Good machinability and hardness and not for welding and stress-corrosion cracking. Because of its superior strength, Alloy 7075 is heavily utilized by the aircraft and ordnance industries.
Aluminium Alloy 7075 T651 Rounds is available in Bars, Sheets, Plates, Discs, Etc
Round Bar – 20mm to 300mm Dia
Sheet/Plate – 3mm Thickness to 250mm Thickness
Chemical Composition of Aluminium Alloy 2014 Plate
Chemical Element |
% Present |
Silicon (Si) |
0.0 - 0.12 |
Iron (Fe) |
C0.0 - 0.15 |
Copper (Cu) |
2.00 - 2.60 |
Manganese (Mn) |
0.0 - 0.10 |
Magnesium (Mg) |
1.90 - 2.60 |
Chromium (Cr) |
0.0 - 0.04 |
Zinc (Zn)) |
5.70 - 6.70 |
Zirconium (Zr) |
0.08 - 0.15 |
Titanium (Ti) |
0.0 - 0.06 |
Other (Each) |
0.0 - 0.05 |
Others (Total) |
0.0 - 0.15 |
Aluminium (Al) |
Balance |
Mechanical Properties of Aluminium Alloy 2014 Plate
| Thickness (mm) |
Proof Strength (Min) |
Tensile Strength (Min) |
Elongation % (Min) |
| Over 6.3 up to & incl. 51 |
441 |
510 |
9 |
| Over 51 up to & incl. 76 |
434 |
503 |
8 |
| Over 76 up to & incl. 102 |
427 |
496 |
6 |
| Over 102 up to & incl. 127 |
421 |
490 |
5 |
| Over 127 up to & incl. 152 |
414 |
483 |
4 |
| Over 152 up to & incl. 178 |
407 |
476 |
4 |
| Over 178 up to & incl. 203 |
400 |
469 |
4 |
Physical Properties of Aluminium Alloy 2014 Plate
| Characteristic |
English |
Metric |
| Nominal Density (68° F / 20°C) |
0.101 lbs./ in ³ |
2.80 Mg/m³ |
| Melting Range |
990° F - 1175° F |
532°C - 635 °C |
| Specific Heat (212 °F / 100°C |
0.23 BTU/lb - °F |
960 J/kg-°K |
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