7475 aluminum plate is a high-strength aluminum alloy, it has excellent strength and corrosion resistance, and is often used to manufacture aircraft structures and parts.
7475 aluminum alloy is known for its excellent mechanical properties, including high strength, toughness, and resistance to stress corrosion cracking.
Alloys 7050 and 7475 are used in the construction of wing attach structures, ensuring safety and durability during flight.
7050, 7475, and 7099 high-strength aluminum alloys are used to manufacture wing ribs, providing structural support to the wings and enhancing structural integrity.
7050, 7475, and 7099 have outstanding strength-to-weight ratios and fatigue resistance, making these high-strength aluminum alloys ideal materials for manufacturing wing spars.
2024, 7075, and 7475 combinations exhibit excellent strength and fatigue resistance, making them suitable for wing skins to withstand deformation under stress.
7475 and 7050 aluminum alloys are high-strength aerospace aluminum alloys widely used in the aerospace industry, especially in aircraft structures.
7475 aluminum alloy is a high-strength, ultra-pure aluminum-zinc-magnesium-copper alloy with excellent strength and toughness. Its core feature is significantly enhanced exfoliation corrosion resistance.
T651 7475 aluminum is a high-performance material that undergoes special treatment. The 7475 aluminum alloy requires three steps: solution heat treatment, stress relief, and artificial aging.
7475-T7351 aluminum alloy is a high-strength aluminum alloy, which belongs to the T7351 temper of the 7475 series. Its manufacturing process involves a series of complex heat treatment steps designed to optimize its properties, especially in terms of stress corrosion resistance.
7475 T761 aluminum sheet is a widely used aluminum alloy material in the aerospace industry, particularly suitable for applications that require high strength, excellent corrosion resistance, and some toughness.
7475-T61 aluminum alloy is a high-strength alloy that is widely used in aerospace and other fields that require high material performance.
The two alloys are very similar in terms of general composition and thermal properties, but 7475 may have slight advantages in fatigue resistance, elongation, and thermal diffusivity in certain aspects, making it more versatile in high-performance or high-stress applications.