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Aluminum
7075
Aluminium 7075
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Aluminium
7075 Sheet, Rod, Bar and Plate
| Chemical
Composition Limits Aluminium Alloy 7075 |
Others |
| Weight
% |
Si |
Fe |
Cu |
Mn |
Mg |
Cr |
Zn |
Ti |
Each |
Total |
| Minimum |
- |
- |
1.2 |
- |
2.1 |
0.18 |
5.1 |
- |
- |
- |
| Maximum |
0.40 |
0.50 |
2.0 |
0.30 |
2.9 |
0.28 |
6.1 |
0.20 |
0.05 |
0.15 |
| Typical
Physical Properties |
| 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 |
Available in: Bar, Sheet,
Strip, Plate, Tube, Extrusion, Sections, Wire.
|
Applicable
Specifications
Aluminum Alloy
7075
|
| American Specifications |
European Specifications |
|
ASTM B211
ASTM B221
QQ-A-200/11
QQ-A-200/15
QQ-A-225/9
QQ-A-250/12
QQ-A-250/13
QQ-A-250/18
QQ-A-250/24
QQ-A-250/25
AMS 4038
AMS 4039
AMS 4045
AMS 4046
AMS 4048
AMS 4049
AMS 4078
AMS 4122
AMS 4123
AMS 4124
AMS 4154
AMS 4166
AMS 4167
AMS 4168
AMS 4169
|
2L88
Clad T6 Sheet
2L95
Plate
L160
Bars and Sections
L161
Forging stock
L162
Forging stock
L170
Extruded Sections
DTD
5124
3.4364
A-Z5GU
|
Alloy Description
|
This alloy offers the
highest strength of the common screw machine alloys. The superior stress
corrosion resistance of the T173 and T7351 tempers makes it a logical replacement
for 2024, 2014 and 2017 in many of the most critical applications. The
T6 and T651 tempers have fair machinability. This alloy is heavily utilized
by the aircraft and ordnance industries because of its superior strength.
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Disclaimer
Every effort is made to ensure that
technical specifications are accurate. However, technical specifications
included herein should be used as a guideline only. All specifications are
subject to change without notice.
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