7050 aluminum alloy profiles are suitable for producing large structural components with thick cross-sections, such as aircraft wing beams, fuselage frames, landing gear, and supporting structures.
7075 aluminum extrusions are used in the aerospace field to ensure the reliability of aircraft structures in high-strength environments while meeting the demands of lightweight design.
7175 aluminum profiles are a high-strength aluminum alloy primarily composed of aluminum, zinc, magnesium, and copper, offering outstanding mechanical properties and corrosion resistance.
The 7049 aluminum alloy not only enhances the strength and safety of structures in the aerospace field but also effectively reduces the overall weight of aircraft, improving fuel efficiency and range performance.
The 7150 aluminum alloy has excellent mechanical properties, including high strength, good toughness, and fatigue resistance. Its tensile strength and yield strength are generally high, making it suitable for structures that bear heavy loads.
7014 aluminum alloy is a high-strength aluminum alloy. Its extruded profiles have excellent mechanical properties and good processability, and are suitable for key structural components of aircraft.
7178 T6511 is an aerospace-grade aluminum alloy from the 7XXX series. It primarily utilizes zinc as the principal alloying element, supplemented with magnesium and copper to enhance its properties.
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.
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.