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.
Buy high-quality 7050 aluminum round bar stock for extreme durability and fatigue resistance. Ideal for structural components, military hardware, and marine environments. Includes competitive pricing, volume discounts, and tailor-made cutting services.
As a trusted 7075 aluminum manufacturer, we specialize in producing premium ASTM/AMS certified aluminum flat bars with excellent strength-to-weight ratio.
Manufacturer of premium 7075-T6 aluminum round bars, offering unmatched strength, corrosion resistance, and durability. Ideal for aerospace, automotive, and military applications.
We offer direct sales of high-strength 7075 aluminum bars, supporting customization of round bars, square bars, and hexagonal bars (Φ3mm-250mm). Precision machining and surface treatment services are available. In-stock supply with quality compliant with national standards.
As a leading manufacturer, we offer 7075 T73 aluminum round bars that comply with ASTM B211, AMS 4122, and AMS 4124 standards, ensuring reliability in critical environments.
As a professional 7075 aluminum alloy square tube manufacturer, we provide high-strength, corrosion-resistant seamless aluminum square tube customization services. Through cold treatment forging process, it has excellent fatigue resistance and machining characteristics.
Our factory specializes in the supply of 7075-T7351 aluminum alloy round bars, which meet the ASTM B211 standard, with a diameter of 1/4"-3" and available for direct shipment. Customized cutting and technical solution optimization are supported.
Our 7075 aluminum hex bars are manufactured according to ASTM B211/B221 and AMS-QQ-A-225/9 standards, with custom sizes (imperial and metric) and cold-finished surfaces to ensure strict tolerances and smooth processing.
As a professional manufacturer of 7075 aluminum alloy round tubes, we provide high-strength, lightweight, and fatigue-resistant aerospace-grade seamless aluminum tube solutions.
As a high-strength aerospace-grade aluminum alloy manufacturer, 7075-T73511 extruded rectangular bars are designed for demanding conditions. By choosing our products, you get aerospace-certified solutions that help propel your project efficiently.
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.
7010 aluminum alloy is a high-strength, good fatigue strength, and excellent stress corrosion resistance forged aluminum alloy.
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.
7049 and 7050 aluminum alloys are both designed for high-performance applications in aerospace and other demanding industries, but they offer slightly different advantages based on their composition and specific properties.
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.
7175-T74 aluminum alloy is a high-strength aluminum alloy commonly used in aerospace and military fields. Its characteristic is that after solution heat treatment and artificial aging, it achieves an excellent balance of mechanical properties.
7175-T7452 aluminum alloy is a special treatment condition of the 7175 series aluminum alloy, offering excellent mechanical properties and corrosion resistance, making it particularly suitable for high-strength aerospace and other high-demand applications.
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.
7178 T651 and 7178-T6510 aluminum alloys are different heat treatment states of the 7178 aluminum alloy, which improve the mechanical properties of the metal through solution heat treatment, stress relief, and artificial aging.
7178-T651 aluminum alloy is a high-strength aluminum alloy that undergoes specific heat treatment and stress-relief processes. It is commonly used in applications requiring high fatigue strength and multiple stress cycles, such as aerospace and automotive industries.
7178 T6510 aluminum is a high-strength aluminum alloy that has undergone solution heat treatment, stress relief, and artificial aging to achieve specific mechanical properties.
7075 T6 and 7075-T62 aluminum alloys both belong to the 7000 series of aluminum alloys and are commonly used in aerospace, military, and high-strength structural applications.
7075-T6 aluminum alloy is widely used in the aerospace and automotive industries due to its good strength-to-density ratio, fracture toughness and resistance to stress corrosion cracking (SCC).
7075-T62 aluminum is a specific heat-treated version of the 7075 aluminum alloy, offering excellent mechanical properties. It is widely used in aerospace, military, and high-end industrial fields.
7075 T651 and 7075-T6510 are both high-strength aluminum alloys, but they have slightly different characteristics, making them suitable for different application fields.
7075 T6510 is a high-strength aluminum alloy, widely used in fields that require extremely high strength, durability, and good mechanical properties.
7075-T6 aluminum and 7075-T6511 aluminum are two common tempers of 7075 aluminum alloy. The main difference between them lies in the heat treatment process, stress relief, and the stretching process applied to the metal during manufacturing.
7075-T6511 aluminum alloy, while meeting high strength requirements, offers excellent machinability, weldability, and structural stability after fine processing and treatment. It is highly suitable for high-performance structures and high-load applications.
The difference between 7075-T651 and 7075-T652 aluminum mainly lies in the way they release stress and the resulting mechanical properties.
7075 T652 aluminum alloy belongs to the 7075 series aluminum alloy, which is usually composed of aluminum, zinc, magnesium and copper elements. Its alloying composition gives it very high strength and hardness.
7075-T6 aluminum and 7075-T7 aluminum are two common variants of 7075 aluminum alloy, which are obtained through different heat treatment processes and processing methods, resulting in certain differences in their mechanical properties.
7075-T7 aluminum alloy is a variant of the 7075 series that has undergone special treatment, offering unique properties, especially suitable for applications requiring high ductility and stability.
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.
7075-T6 and 7075-T651 are both high-strength temper grades of 7075 aluminum alloy, but their main differences lie in the heat treatment process and the resulting mechanical and manufacturing properties.
7075-T73 aluminum is a high-strength alloy belonging to the Al-Zn-Mg-Cu series, a heat-treatable strengthened alloy, widely applied in aerospace, military, and high-end manufacturing fields for its excellent overall performance.
7075 T7451 is a high-strength aluminum alloy in the 7xxx series, known for its outstanding mechanical properties and suitability for critical aerospace and industrial applications.
7075 T76 is a high-strength aluminum alloy in the 7000 series, known for its excellent mechanical properties and enhanced corrosion resistance due to a specific heat treatment process.
The differences between 7075-T6 and 7075-T73 aluminum alloys primarily stem from their heat treatment processes, which result in varying mechanical properties, corrosion resistance, and suitability for specific applications.