INC.
Aluminum Alloy 7075 Sheets and Plates is an aluminum-zinc alloy with 1%-8% zinc notwithstanding little measures of magnesium and little amounts of copper and chromium. Because of its high erosion protection properties, Aluminum Alloy 7075 Sheets and Plates are normally utilized as a part of marine and aviation applications. Aluminum Alloy 7075 Sheets and Plates is utilized as a part of airframe structures and other exceptionally focused on segments because of its high quality levels. Our 7075 plate has T651 temper, indicating it has been solution heat treated followed by a minimal stretching to reduce stresses in the material. The material was then artificially aged to allow the alloying elements to precipitate out of the material, to give immediate maximum strength.
| UNS | EN | DIN,WNr | JIS | AFNOR | ISO | BS | GOST |
|---|---|---|---|---|---|---|---|
| A97075 | ENAW-AlZn5.5MgCu EN AW-7075 | 3.4365 AlZnMgCu1.5 | 7075 | 7075 A-Z5GU | AlZn6MgCu | 7075 L95 L96 | V95 |
| Grade | Element | |||||||
|---|---|---|---|---|---|---|---|---|
|
|
Si
|
Fe
|
Cu
|
Mn
|
Mg
|
Cr
|
Zn
|
Ti
|
|
7075
|
0.40
|
0.50
|
1.2/2.0
|
0.30
|
2.1/2.9
|
0.18/0.28
|
5.1/6.1
|
0.20
|
| Properties | Metric |
|---|---|
| Tensile strength | 83-73 Ksi |
| Yield strength | 73-63 Ksi |
| Hardness Brinell | 150 |
| Elongation | 13-11% |
