Polished 7075 Aluminum Alloy Plates for Aircraft
Aircraft Aluminium sheets (2024 , 2014, 2017, 7075,7475)
Classic alloy:2024, 2324, 2524, 7075, 7475, 7050, 7150.
Product characters:high strength, high ductility, high damage tolerance.
| Specifications |
| Alloys (AA) |
Temper |
Thickness range (mm) |
Length range (mm) |
Width range (mm) |
| 2024, 2324, 2524, 7075, 7475, 7050, 7150 |
F and O
H111, H112, T4, T6 (For 6061, 6063), T651(Stretched plate) |
6 - 300 |
1000 - 10000 |
500 - 2700 |
| Stretched aluminumplate |
| Thickness limit |
6 - 70 mm |
| Length limit |
2000 - 10000 mm |
| Chemical composition |
| Alloy (%) |
2024 |
7075 |
7050 |
7475 |
6061 |
7075 |
| Si |
0.50 |
0.40 |
0.12 |
0.10 |
0.40- 0.80 |
0.40 |
| Fe |
0.50 |
0.50 |
0.15 |
0.12 |
0.70 |
0.50 |
| Cu |
3.8~4.9 |
1.2~2.0 |
2.0~2.6 |
1.2~1.9 |
0.15- 0.40 |
1.2- 2.0 |
| Mn |
0.30~0.9 |
0.30 |
0.10 |
0.06 |
0.15 |
0.30 |
| Mg |
1.2~1.8 |
2.1~2.9 |
1.9~ 2.6 |
1.9~2.6 |
0.8- 1.2 |
2.1- 2.9 |
| Cr |
0.10 |
0.18~0.28 |
0.04 |
0.18~0.25 |
0.04- 0.35 |
0.18- 0.28 |
| Zr |
- |
- |
0.08~0.15 |
- |
- |
- |
| Zn |
0.25 |
5.1~6.1 |
5.7~6.7 |
5.2~6.2 |
0.25 |
5.1- 6.1 |
| Ti |
0.15 |
0.20 |
0.06 |
0.06 |
0.15 |
0.20 |
| Each (Others) |
0.05 |
0.05 |
0.05 |
0.05 |
0.05 |
0.05 |
| Total (Others) |
0.15 |
0.15 |
0.15 |
0.15 |
0.15 |
0.15 |
| Al |
Remaining |
Remaining |
Remaining |
Remaining |
Remaining |
Remaining |
| Single number indicates maximum content. |
| Packing |
| Aluminum Plate : Aluminum Plates are placed in wooden boxes on wooden skids with runners along the length of the sheet. They are wrapped in HDPE with hardboard on top and bottom of the stack. Hoop iron strapping runs along the length of the sheets. Silica gel packets are put in the boxes for moisture protection.(Aluminum plate) |
Contact information:
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Phone:86-0371-55083768 FAX:86-0371-55685982
MOB:86-173-3717-6360
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