7050 T73510 T73511 Aluminum

7050 aluminum alloy is a high-strength aluminum alloy commonly used in the aerospace field, especially suitable for applications that require high stress and corrosive environments. 7050 aluminum alloy exhibits significant performance differences in its various heat-treated states, with T73510 and T73511 being two common states.

Both 7050 T73510 and T73511 Aluminum alloys have excellent stress corrosion resistance and high strength, making them widely used in the aerospace field for structural components that meet different design requirements.

• 7050-T73510 aluminum: The main feature is enhanced stress corrosion resistance through over-aging without straightening. It is suitable for aerospace structural components and environments requiring high strength.
• 7050-T73511 aluminum: Compared to T73510, over-aging is more complete, and it is straightened after stretching. It is more suitable for structural components with higher shape accuracy requirements.

Comparison table of 7050-T73510 and 7050-T73511 aluminum alloys

7050-T73510 Aluminum Alloy

7050-T73510 Aluminum Alloy Heat Treatment and State

• Solution Heat Treatment: The 7050 aluminum alloy undergoes solution heat treatment during the manufacturing process to dissolve the alloying elements and achieve a uniform distribution. This process enhances the strength and toughness of the material.
• Stress Relief: After solution heat treatment, the aluminum undergoes a stress relief process. This process relieves internal stress by stretching the metal a certain amount, with the amount of stretching depending on the type of product being produced (e.g., extrusions or tubes).
• Artificial Over-aging: To further stabilize the aluminum alloy, 7050-T73510 aluminum undergoes artificial over-aging. The degree of over-aging is selected to maximize stress corrosion resistance, which is especially important for aerospace structural components.

7050-T73510 Aluminum Alloy Stretching Characteristics

After the stretching operation, the aluminum is not straightened, which is different from the T73511 state. The T73510 state is particularly suitable for applications where straightening is not a critical requirement, such as certain load-bearing structural components.

7050-T73510 Aluminum Alloy Applications

7050-T73510 aluminum is mainly used for aerospace structural components, especially those requiring high strength, excellent stress corrosion resistance, and durability, such as aircraft fuselage, wings, and high-pressure components.

7050-T73511 Aluminum Alloy

7050-T73511 Aluminum Alloy Heat Treatment and State

• Solution Heat Treatment: Like the T73510 state, 7050-T73511 aluminum also undergoes solution heat treatment to ensure uniform distribution of alloying elements and to improve material strength.
• Stress Relief: Similarly, 7050-T73511 aluminum undergoes stress relief by stretching, with the amount of stretching adjusted based on the form of the alloy (e.g., extrusions or tubes).
• Artificial Over-aging: Compared to T73510, 7050-T73511 aluminum undergoes more extensive over-aging, which helps further improve the alloy's stress corrosion resistance, especially under more severe environmental conditions.

7050-T73511 Aluminum Alloy Stretching Characteristics

In the T73511 state, the aluminum alloy is straightened after stretching, which is one of the main differences from the T73510 state. The straightening process makes 7050-T73511 aluminum more suitable for applications requiring higher shape accuracy.

7050-T73511 Aluminum Alloy Applications

The applications of 7050-T73511 aluminum are similar to those of T73510, but it is especially suitable for structural components that require higher shape accuracy, such as wing spars, long rod structures, and landing gear. With superior stress corrosion resistance in the T73511 state, it is suitable for use in components exposed to high stress and corrosive environments.

7050 T73510 T73511 Aluminum Mechanical Properties

7050 T73510 T73511 Aluminum Physical Properties

7050 T73510 T73511 Aluminum Electrical Properties

7050 T73510 T73511 Aluminum Thermal Properties

7050 T73510 T73511 Aluminum Processing Properties

Chemical Composition of 7050 Aluminum Alloy