When sourcing aerospace-grade aluminum alloys on Alibaba.com, understanding the specific characteristics of 7050-T7451 is essential for making informed procurement decisions. This high-strength aluminum-zinc-magnesium-copper alloy has become the material of choice for critical aircraft structural components, particularly in applications where thick sections and superior fracture toughness are paramount.
What Does 7050-T7451 Mean? The designation breaks down into two key components: 7050 indicates the alloy composition (aluminum with zinc as the primary alloying element, plus copper, magnesium, and zirconium), while T7451 specifies the temper condition (solution heat-treated, stress-relieved by stretching, and over-aged to achieve optimal toughness and stress corrosion resistance). This temper designation is critical because it directly impacts the material's mechanical performance in service.
The chemical composition of 7050-T7451 is precisely controlled: Aluminum (87.3-90.3%), Zinc (5.7-6.7%), Copper (2.0-2.6%), Magnesium (1.9-2.6%), and Zirconium (0.08-0.15%). The addition of zirconium is particularly important—it forms fine precipitates that inhibit recrystallization during heat treatment, resulting in improved fracture toughness compared to earlier 7000-series alloys like 7075.
7075-T6 has a yield strength of nearly 500 MPa, almost double that of 6061 (270 MPa). If your part is for aerospace or high-stress robotics where every gram counts, 7075 is your best friend. [5]
However, for thick-section applications exceeding 3 inches, 7050-T7451 becomes the preferred choice. The T7451 temper provides better stress corrosion cracking (SCC) resistance than T6 tempers, which is crucial for aircraft components exposed to harsh environmental conditions over decades of service life.

