Aluminum

7075 Aluminum
Maximum structural strength
7075-T651 aluminum is an aluminum-zinc-magnesium-copper alloy with very high mechanical strength. It stands out for its excellent strength-to-weight ratio, good machinability and ability to withstand high loads, although it has lower weldability and corrosion resistance than 6000-series alloys.
Main features
Very high mechanical strength
Excellent strength-to-weight ratio
High fatigue strength
Standards and equivalents
| Commercial | ASTM | UNS | EN | DIN |
|---|---|---|---|---|
| 7075-T651 | B209 y B211 | A97075 | AW-7075 | 3.4365 |
Chemical composition
| % | Si | Fe | Cu | Mn | Mg | Cr | Zn | Ti | Others, each | Others, total | Al |
|---|---|---|---|---|---|---|---|---|---|---|---|
| Min | — | — | 1.20 | — | 2.10 | 0.18 | 5.10 | — | — | — | Bal. |
| Max | 0.40 | 0.50 | 2.00 | 0.30 | 2.90 | 0.28 | 6.10 | 0.20 | 0.05 | 0.15 | Bal. |
Supply condition
Hot rolledT651Available package sizes
Plates1/4" – 6"6.35 mm – 152.4 mm
Round bars1" – 6"25.4 mm – 152.4 mm—
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Typical applications
- Aerospace components
- High-stress structural parts
- High-strength molds and tooling
- Axles, shafts and mechanical components
- Fixtures and bases for demanding applications
- Parts subject to high loads
- Racing and automotive components
- Precision base plates
- Precision machined components
Note: The information and values in this data sheet are provided for reference only and may vary depending on manufacturing, treatment and application conditions. They do not constitute guaranteed specifications, so use and interpretation of this data is the user's responsibility.
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