2024 aluminum alloy is one of the most widely used high-strength materials in aerospace structural applications. The "T4" temper designation indicates the material has undergone solution heat treatment followed by natural aging at room temperature, achieving an optimal balance of strength, fatigue resistance, and formability. For manufacturers looking to sell on Alibaba.com, understanding the precise specifications of this alloy is essential for meeting buyer expectations in the aerospace sector.
The copper content (3.8-4.9%) is what gives 2024 alloy its exceptional strength-to-weight ratio, but it also creates a vulnerability: corrosion susceptibility. This is why "bare" 2024-T4 is typically specified for applications where the material will be clad (Alclad) or coated, or where the part will be protected from environmental exposure. For B2B buyers sourcing on Alibaba.com, suppliers who can explain these trade-offs demonstrate technical competence that builds trust.
Mechanical Properties: 2024-T4 Bare Aluminum Specifications
| Property | Value | Test Standard | Application Relevance |
|---|---|---|---|
| Ultimate Tensile Strength (UTS) | 469-480 MPa (68,000-69,000 psi) | ASTM B209 | Maximum load before failure |
| Yield Strength (0.2% offset) | 310-324 MPa (45,000-47,000 psi) | ASTM B209 | Permanent deformation threshold |
| Elongation at Break | 16-20% | ASTM B209 | Formability and ductility indicator |
| Brinell Hardness | 120 HB | ASTM E10 | Wear resistance and machinability |
| Fatigue Strength | 138-140 MPa | Rotating beam test | Critical for cyclic load applications |
| Density | 2.78 g/cm³ (0.100 lb/in³) | ASTM B209 | Weight-to-strength ratio calculation |
| Thermal Conductivity | 130 W/m-K | ASTM E1461 | Heat dissipation in structural assemblies |
| Modulus of Elasticity | 73.1 GPa (10,600 ksi) | ASTM E111 | Stiffness under load |
The T4 temper is particularly significant for aerospace applications. After solution heat treatment at approximately 495°C, the material is quenched and then allowed to naturally age at room temperature for 4-5 days. This natural aging process allows copper-magnesium precipitates to form uniformly throughout the aluminum matrix, enhancing strength without the distortion risks associated with artificial aging (T6 temper). For suppliers on Alibaba.com, being able to explain this process—and why T4 is preferred over T6 for certain aerospace applications—positions you as a knowledgeable partner rather than just a commodity vendor.

