When sourcing high-strength aluminum alloys on Alibaba.com, understanding the fundamental differences between alloy grades is critical for making informed procurement decisions. 7075 aluminum alloy belongs to the 7XXX series, characterized by zinc as the primary alloying element (5.1-6.1%), along with magnesium (2.1-2.9%), copper (1.2-2.0%), and chromium (0.18-0.28%) [4]. This chemical composition gives 7075 its exceptional strength-to-weight ratio, making it the material of choice for aerospace structural components, military equipment, and high-performance sporting goods.
For B2B buyers selling on Alibaba.com, it's essential to recognize that 7075 aluminum is not a one-size-fits-all solution. The alloy comes in multiple temper variants (O, T4, T6, T651, T73), each offering different mechanical properties suited to specific applications. T6 temper provides peak strength through solution heat treatment and artificial aging, while T73 temper sacrifices some strength for improved stress corrosion cracking resistance [5]. Understanding these distinctions helps buyers match material specifications to their exact requirements, avoiding both under-specification (safety risks) and over-specification (unnecessary cost).
7075 Aluminum Alloy: Common Temper Variants and Their Properties
| Temper Designation | Heat Treatment Process | Yield Strength (MPa) | Tensile Strength (MPa) | Hardness (HB) | Best For |
|---|---|---|---|---|---|
| O (Annealed) | Full annealing, softest condition | 140-180 | 220-280 | 60-80 | Forming operations, deep drawing |
| T4 | Solution heat treated + natural aging | 320-370 | 380-440 | 100-120 | Moderate strength applications |
| T6 | Solution heat treated + artificial aging | 470-540 | 540-620 | 150-190 | Peak strength aerospace components |
| T651 | T6 + stress relieved by stretching | 470-540 | 540-620 | 150-190 | Precision machined parts, reduced distortion |
| T73 | Overaged for SCC resistance | 410-470 | 480-550 | 130-160 | Marine environments, stress corrosion prone applications |

