7050 T7451 aircraft aluminum plate is a zinc alloy aluminum alloy, mainly used for structural parts that require high strength and corrosion resistance.
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.
7075 aerospace aluminum contains zinc as the main alloying element, has excellent mechanical properties and corrosion resistance, and is suitable for manufacturing structural and load-bearing parts.
7068 aluminum alloy is renowned for its excellent strength-to-weight ratio, making it ideal for applications requiring high strength and low weight.
7055 aluminum is a high-strength alloy mainly composed of aluminum, zinc, commonly used in aerospace applications, military vehicles, and other high-performance structures.
7150 aluminum plate is a high-strength alloy primarily used in aerospace applications due to its excellent strength-to-weight ratio and good resistance to stress corrosion cracking.
7014 aluminum alloy is a commonly used material in the aerospace and military fields, belonging to the aluminum-zinc-magnesium alloy series.
7010 aerospace aluminum plate is a high-strength, making it particularly suitable for lightweight, high-strength structural materials.
The 7049 aerospace aluminum plate is a high-strength aluminum alloy material widely used in aerospace, military, and high-performance industrial applications.
7178 aircraft aluminum plate is a high-strength aluminum alloy mainly used in aerospace, military, and high-performance engineering applications. It belongs to the aluminum-zinc alloy series and is typically strengthened through heat treatment processes.
7150-T7751 aluminum plate belongs to the 7000 series high-strength aluminum alloys, making it particularly suitable for the aerospace industry, especially for aircraft structures, airframe components, and other critical parts requiring high strength and corrosion resistance.
7178 O aluminum sheet is the annealed state of the 7178 aluminum alloy. This state features lower strength but higher ductility, making it easy to form and process.
7178 T6 and T651 aluminum alloys are both suitable for aerospace applications, but T651, which undergoes stress-relief and stabilization treatments, is more suited for applications requiring precise dimensions and long-term stability.
7178 T76 aluminum alloy is a version of the 7178 alloy in the T76 condition, which has undergone solution heat treatment and artificial aging stabilization to maximize its resistance to exfoliation corrosion.
7178-T7651 aluminum alloy is a high-strength aluminum material that undergoes specific heat treatment and aging processes to enhance its corrosion resistance and mechanical properties.
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.
7075 T651 is one of the most popular high-strength aluminum alloys in the aerospace sector, combining lightweight, strength, and excellent machinability, making it an ideal material choice.
7050-T7651 aluminum plate is a specially treated high-strength aerospace-grade aluminum alloy sheet, offering outstanding advantages in performance and durability.
The 7050 T7451 aluminum plate is a specially treated high-strength aluminum alloy, belonging to the 7050 series. This alloy is mainly used in applications requiring excellent strength and corrosion resistance, particularly in aerospace and other high-performance structures.
7049 T73 aluminum alloy is a material with high strength and excellent corrosion resistance, particularly suitable for high-strength structural components in aerospace and military applications.
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.
7049-T73 aluminum alloy is a variant of the 7049 aluminum alloy, with most properties being similar between the two, with the only significant difference in some mechanical properties and toughness.
7049 aluminum alloy is a high-strength aluminum alloy mainly composed of aluminum, zinc, copper, and magnesium, offering excellent strength. However, due to the addition of zinc and copper, its corrosion resistance and weldability are relatively poor.
7010 and 7075 aluminum alloys are widely used in the aerospace industry due to their high strength, light weight, and structural reliability.
7005 aluminum alloy is a high-strength, weldable, and heat-treatable forged aluminum alloy, widely used in lightweight and high-strength applications such as bicycle frames, transportation structures, and sports equipment.
The main difference between 7075 and 7005 aluminum is that 7075 has higher strength, making it more suitable for high-performance applications, while 7005 is easier to weld and is commonly used in bicycle frames and automotive components.
7005-O aluminum alloy is the version of 7005 aluminum in the annealed state. Compared to other 7005 series aluminum alloys, 7005-O aluminum has relatively lower strength but very high ductility. Its annealed state means that the alloy has a softer microstructure after being heated and slowly cooled, making it easier to form and weld during the processing.
7005 aluminum in T5 condition exhibits superior mechanical properties, especially in terms of strength, corrosion resistance, and fatigue resistance, making it widely used in high-demand structural components and industries.
7005-T53 aluminum alloy is an aluminum alloy with high tensile strength and shear strength, suitable for high-strength structural applications. Although its ductility is relatively low, it excels in corrosion resistance and mechanical performance.
7005 T6 Aluminum is an aluminum alloy that has undergone solution heat treatment and artificial aging. After this treatment, the mechanical properties of the metal are significantly enhanced, especially in terms of strength and heat resistance.
7050-T74 Aluminum offers higher tensile strength and toughness, while 7050-T7452 Aluminum provides improved fracture toughness and stability through stress relief processing.
7175-T74 aluminum is suitable for applications requiring higher ductility and fatigue strength, while 7175-T7452 aluminum performs better in terms of stress corrosion resistance, crack resistance, and shear strength.
7050 T74 aluminum alloy is a high-strength, excellent corrosion-resistant, and good fracture toughness aerospace material, widely used in aircraft structural components, especially suitable for applications under high stress and harsh environments.
7050-T7452 aluminum alloy is a high-strength, excellent stress corrosion cracking resistance, exfoliation corrosion resistance, and fracture toughness aerospace material, widely used in aircraft structural components.
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.
7475-T76 aluminum alloy is a high-strength aluminum alloy, belonging to the 7000 series of aluminum alloys, particularly suitable for structural components in the aerospace field, especially in applications that require high strength and corrosion resistance.
7068 T6511 is known for its outstanding mechanical properties, with tensile strength comparable to some steels, while retaining the lightweight advantage of aluminum.
7068 aluminum alloy combines high strength, good ductility, and excellent corrosion resistance, making it the preferred choice for applications requiring lightweight yet strong materials.
7475 aluminum alloy, a high strength 7xxx series material known for its excellent fracture toughness, fatigue resistance and aerospace applications. Ideal for critical structural components in aviation, defense and high stress engineering.