When sourcing aluminum alloy materials on Alibaba.com, buyers encounter multiple grade designations (5052, 6061, 7075, 2025, 2026, 8000 series) that significantly impact performance, cost, and application suitability. This section breaks down what these configurations actually mean—without marketing fluff—so you can make informed decisions based on your specific requirements.
Aluminum alloy grades are classified by series, each defined by primary alloying elements that determine mechanical properties, formability, weldability, and corrosion resistance. The four-digit designation system (e.g., 6061-T6) tells you both the alloy composition and heat treatment condition.
Common Aluminum Alloy Grades: Composition & Key Properties
| Alloy Grade | Series | Primary Alloying Elements | Typical Tensile Strength (MPa) | Yield Strength (MPa) | Thermal Conductivity (W/m·K) | Density (g/cm³) |
|---|---|---|---|---|---|---|
| 5052-H32 | 5xxx | Magnesium 2.2-2.8%, Chromium 0.15-0.35% | 228-280 | 193-240 | 138 | 2.68 |
| 6061-T6 | 6xxx | Magnesium 0.8-1.2%, Silicon 0.4-0.8% | 310-350 | 270-310 | 154-167 | 2.70 |
| 7075-T6 | 7xxx | Zinc 5.1-6.1%, Magnesium 2.1-2.9%, Copper 1.2-2.0% | 503-572 | 434-503 | 130-140 | 2.81 |
| 2025-T6 | 2xxx | Copper 3.9-5.0%, Magnesium 0.2-0.8% | 400 | 255 | 154 | 2.81 |
| 2026-T6 | 2xxx | Copper 3.4-4.5%, Magnesium 1.2-1.8% | 430-520 | 310-360 | 120-160 | 2.78 |
| 8000 Series | 8xxx | Iron 0.3-0.8%, Copper 0.1-0.3% | 90-150 | 40-120 | up to 237 | 2.70-2.80 |
Key Configuration Differences Explained:
5xxx Series (5052): Non-heat-treatable alloys with magnesium as the primary alloying element. These offer the best formability and corrosion resistance—especially in marine environments—but lower strength compared to heat-treatable grades. Ideal for applications requiring extensive bending, stamping, or welding.
6xxx Series (6061): Heat-treatable alloys containing magnesium and silicon. This is the most widely used structural aluminum alloy, offering an excellent balance of strength, formability, weldability, and corrosion resistance. The T6 temper (solution heat-treated and artificially aged) provides maximum strength.
7xxx Series (7075): Heat-treatable alloys with zinc as the primary alloying element. These deliver the highest strength-to-weight ratio among commercial aluminum alloys but sacrifice formability, weldability, and corrosion resistance. Commonly used in aerospace and high-performance automotive applications.
2xxx Series (2025, 2026): Copper-containing alloys originally developed for aerospace applications. These offer high strength and good machinability but lower corrosion resistance. Often used in structural components where strength is critical.
8xxx Series: Specialized alloys designed for specific applications like electrical conductivity or thermal management. The 8000 series can achieve thermal conductivity up to 237 W/m·K, making it ideal for heat exchangers and electronic cooling applications.

