7050 7475 Aerospace Aluminum for Wing Attach Structure
7050 and 7475 are high-strength aluminum alloys commonly used in aerospace applications, particularly in the manufacturing of wing attach structures and other critical components.
Wing Attach Structure Aerospace Aluminum 7050
Properties of Aerospace Aluminum 7050
- 7050 is known for its high strength-to-weight ratio, excellent stress corrosion resistance, and good toughness.
- 7050 alloy is typically heat-treatable, significantly enhancing its mechanical properties.
- 7050 is often used in the T7451 temper, which offers better stress corrosion cracking resistance compared to other tempers.
Applications of Aerospace Aluminum 7050
- Commonly used in aircraft structures, particularly in areas where high strength and low weight are required.
- Very suitable for wing skins, fuselage frames, and other load-bearing components.
- Frequently used in military aircraft and aerospace applications, where durability and performance are critical.
Chemical Composition of Aerospace Aluminum 7050
Element | Composition % |
Si | 0.12 |
Fe | 0.15 |
Cu | 2.0-2.6 |
Mn | 0.10 |
Mg | 1.9-2.6 |
Cr | 0.04 |
Zr | 0.08-0.15 |
Zn | 5.7-6.7 |
Ti | 0.06 |
Al | Remainder |
Wing Attach Structure Aerospace Aluminum 7475
Properties of Aerospace Aluminum 7475
- The 7475 alloy is characterized by excellent mechanical properties and high stress corrosion cracking resistance.
- 7475 is also heat-treatable, typically used in the T761 temper, providing a balance of strength and toughness.
Applications of Aerospace Aluminum 7475
- 7475 is commonly used in aerospace structures that require high strength and lightweight characteristics.
- Common applications include wing structures, fuselage components, and other areas requiring high performance.
- It is especially popular in applications needing high fatigue resistance and strong performance under varying load conditions.
Chemical Composition of Aerospace Aluminum 7475
Chemical composition of 7475 alloy | |
Si | 0.10 |
Fe | 0.12 |
Cu | 1.20-1.90 |
Mn | 0.06 |
Mg | 1.9-2.60 |
Cr | 0.18-0.25 |
Ni | - |
Zn | 5.2-6.20 |
Ti | 0.06 |
Al | Remainder |
Comparison of Aerospace Aluminum 7050 and 7475
- Strength: Both 7050 and 7475 exhibit high tensile and yield strength, making them suitable for aerospace structural applications.
- Corrosion Resistance: 7050 has slightly better stress corrosion cracking resistance, making it the preferred choice in environments prone to such issues.
- Weight: Both alloys offer a good strength-to-weight ratio, which is critical for aerospace applications.
- Manufacturing: Both alloys can be fabricated using standard processes, including machining, welding (with appropriate filler materials), and forming.
When selecting between 7050 and 7475 aluminum alloys for wing attach structures, engineers must consider specific mechanical performance requirements, environmental conditions, and manufacturing methods. Both alloys provide excellent performance for aerospace applications, with 7050 slightly ahead in corrosion resistance, while 7475 may be favored in certain applications due to its overall strength and toughness.
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