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.
7050 aerospace aluminum bar is a high-strength aluminum alloy, widely used in the aerospace, military, and high-performance industrial sectors.
Due to its excellent mechanical properties and good corrosion resistance, 7A09 aluminum alloy is widely used in the aerospace industry, especially suitable for manufacturing high-strength structural components such as aircraft frames, fuselage skins, and beams.
7A04 aluminum alloy is a high-strength, corrosion-resistant aerospace aluminum material that is widely used in the aerospace industry.
7014 aluminum is a high-strength alloy primarily used in applications that require excellent mechanical properties and corrosion resistance.
7075 aluminum belongs to the 7000 series and is one of the strongest aluminum alloys available. Its primary alloying element is zinc, along with small amounts of magnesium and copper.
7050 aluminum forgings are widely used in the manufacture of fuselage structural parts, wing beams, landing gear components, etc. due to their excellent strength, corrosion resistance and weldability.
7075 belongs to the aluminum-zinc alloy series. 7075 aluminum forgings are particularly suitable for aerospace, military and high-performance engineering fields.
During the forging process of 7175 alloy, the material is heated to a certain temperature and then deformed by mechanical force to achieve the desired shape and properties.
The casting and heat treatment processes of 7014 can further enhance its strength and toughness, making it suitable for extreme operating conditions.
7A09 aerospace aluminum forgings are a type of forged product based on 7A09 aluminum alloy, commonly used in the aerospace field.
7475 aluminum alloy is known for its excellent mechanical properties, including high strength, toughness, and resistance to stress corrosion cracking.
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.
The 7000 series aluminum alloys are one of the preferred materials in the aerospace field due to their excellent strength and good corrosion resistance.
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.
Yes, 7075 aluminum is generally stronger than 6061 aluminum. 6061 aluminum is more versatile and has good mechanical properties, but its strength is not as high as 7075.
7150 is more suitable for high-performance applications that require higher strength and corrosion resistance, while 7075 is popular in standard applications where high strength is required.
7150 aluminum alloy is a high-strength aerospace-grade aluminum alloy, commonly used in the structural components of aircraft and spacecraft, particularly in critical areas that require high strength and excellent 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.
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.
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.
Both 2124 and 7075 alloys are widely used in aerospace and structural applications. 2124 is favored for its fatigue resistance and thermal conductivity, while 7075 is the ideal choice for high-strength requirements.
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.
7049-T7352 aluminum alloy is a high-strength alloy that undergoes special heat treatment and aging processes, offering excellent mechanical properties, corrosion resistance, and high-temperature stability. It is commonly used in aerospace and other high-performance structural 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.
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.