7065 is high zinc containing aluminum alloy. It is used for making plate.
Chemical Composition
| Element[1]
|
Weight percentage
|
| Aluminum
|
87.02 - 89.45 %
|
| Chromium
|
<= 0.04 %
|
| Copper
|
1.9 - 2.3 %
|
| Iron
|
<= 0.08 %
|
| Magnesium
|
1.5 - 1.8 %
|
| Manganese
|
<= 0.04 %
|
| Other, each
|
<= 0.05 %
|
| Other, total
|
<= 0.15 %
|
| Silicon
|
<= 0.06 %
|
| Titanium
|
<= 0.06 %
|
| Zinc
|
7.1 - 8.3 %
|
| Zirconium
|
0.05 - 0.15 %
|
Properties
7065-T7451 alloy properties[2]
| Property
|
Value
|
| Ultimate Tensile strength
|
77 ksi
|
| Yield strength
|
71 ksi
|
| Elongation percentage
|
11%
|
Application
- Plate
- Aerospace
- The combination of high strength and fracture toughness properties and corrosion resistance makes 7065 suitable as a replacement for 7010, 7050, 7075, 7475 and other alloys for critical intermediate thickness applications.[3]
- Spar, rib, and integrally machined structural parts for new, derivative, or retrofit aircraft.[3]
References
Aluminum alloy table
|
|---|
| Introduction | |
|---|
| Al 1000 series (pure) | |
|---|
| Al-Cu 2000 series | |
|---|
| Al-Mn 3000 series | |
|---|
| Al-Si 4000 series |
- 4006
- 4007
- 4015
- 4032
- 4043
- 4047
- 4543
|
|---|
| Al-Mg 5000 series | |
|---|
| Al-Mg-Si 6000 series | |
|---|
| Al-Zn 7000 series | |
|---|
| 8000 series (misc.) | |
|---|
| Named alloys | |
|---|