2024 T3 and T4 aluminum alloys are high-strength materials and are suitable for structural parts that require high strength and low weight, but they have certain limitations in corrosion resistance and weldability.
2219 aircraft aluminum plate has excellent mechanical properties and high temperature properties, and is suitable for manufacturing aircraft structural parts, fuel tanks and other parts that require high strength and corrosion resistance.
2124 alloy has high strength and hardness after heat treatment, and is suitable for manufacturing aircraft structural parts, spacecraft parts and other parts that require high strength and low weight.
2017 aluminum alloy is a high-strength aluminum alloy with lead and copper as the main components. It has excellent strength and good machinability and is commonly used in aerospace and military fields.
2A12 aluminum alloy is copper as the main alloying element. It is widely used in the aerospace field, especially structural parts that require high strength and good corrosion resistance.
6082 aluminum alloy has excellent mechanical properties and corrosion resistance, and is widely used in the aerospace industry and other high-performance fields.
6061 aircraft aluminum plate is a commonly used aluminum alloy material, widely used in aerospace, automobiles, ships, construction and machinery manufacturing.
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.
2014 aluminum alloy is a high-strength aluminum alloy widely used in aerospace, military, and other high-demand engineering fields.
2618 aluminum alloy is a high-strength aluminum alloy primarily composed of aluminum, copper, and small amounts of other elements such as magnesium, silicon, and manganese.
2004 Aerospace Aluminum Alclad Plate is known for its excellent strength-to-weight ratio and good machinability. It typically exhibits high fatigue resistance and is commonly used in aerospace structures.
5052 aerospace aluminum is an aluminum alloy with magnesium as the primary alloying element. It has good corrosion resistance, high strength, and machinability, making it widely used in the aerospace field.
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.
6063 aircraft-grade aluminum is a special aluminum alloy that belongs to the 6000 series, primarily alloyed with magnesium and silicon.
Aerospace aluminum-magnesium alloy refers to alloy materials primarily composed of aluminum and magnesium, widely used in the aerospace field. They are favored for their excellent mechanical properties, good corrosion resistance, and relatively light weight.
The use of aluminum alloys in the aerospace industry is very widespread, primarily because aluminum alloys have excellent strength-to-weight ratios, corrosion resistance, and workability.
Typical aerospace aluminum alloys include 2024 (UNS: A92024), 6061 (UNS: S96061), and 7075 (UNS: S97075).
Aerospace aluminum alloys have significant advantages in performance, processing, and applications, making them suitable for use in high-strength and high-corrosion environments. In contrast, ordinary aluminum alloys are more suitable for everyday life and general industrial uses, emphasizing cost and ease of processing.
Common high-strength aluminum alloys such as 2024, 7075, and 7010 have excellent mechanical strength, toughness, and corrosion resistance.
The 6000 series aluminum alloys are highly popular, primarily composed of magnesium and silicon. As a category, they are often regarded as "architectural" or "structural" aluminum. Among these, the 6061 and 6063 aluminum alloys stand out due to their wide applications.
7075 aluminum alloy is one of the most commonly used high-strength aluminum alloys in the aerospace field, making it particularly suitable for aircraft structures due to its excellent mechanical properties.
Aerospace aluminum products come in various forms, including sheets, forgings, extrusions, profiles, and tubes.
Aircraft aluminum alloys are widely used in the aerospace industry due to their superior strength, light weight, and durability, making them ideal materials for aircraft structures.
6063 aluminum alloy is not as widely used in critical structural components in the aerospace sector as high-strength alloys like 7075 or 2024, but its characteristics make it suitable for certain specialized applications.
Selecting the appropriate Aeronautical Aluminum Alloys according to different application needs is crucial for ensuring the safety and performance of aircraft structures.
Choosing the appropriate thickness of aircraft aluminum sheet is a critical step in the design and manufacturing process. The thickness of the aluminum sheet directly affects the structural strength, weight, cost, and performance of the 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.
The 2xxx series aluminum alloys are high-strength aluminum alloys with copper as the main alloying element, widely used in the aerospace field, particularly suited for high-stress and high-strength structures.
In aerospace applications, 7075 T6 and 2024 T3 are two commonly used high-strength aluminum alloys, each with distinct performance characteristics and application scenarios.
7475 and 7050 aluminum alloys are high-strength aerospace aluminum alloys widely used in the aerospace industry, especially in aircraft structures.
The 2219 aluminum alloy is well-suited for high-temperature environments, while the 7050 aluminum alloy is favored for its high strength and corrosion resistance.
Both alloys have their pros and cons; 7075 aluminum alloy performs better in terms of strength, while 2024 aluminum alloy has advantages in machining and welding.
In aircraft manufacturing, 6061 aluminum alloy is used for load-bearing and structural components due to its high strength and good corrosion resistance, while 6063 aluminum alloy is more often used for non-load-bearing decorative and interior components.
In aviation aluminum alloys, 7075 aluminum alloy is considered the strongest choice, suitable for aerospace applications that require high strength and lightweight materials.
2014-O aluminum alloy is a high-strength, heat-treatable alloy in the 2000 series, primarily composed of aluminum and copper, with small amounts of other elements like silicon, magnesium, and manganese.
Both 2014-T4 and 2014A-T451 aluminum alloys are variants of 2014 aluminum, renowned for their high strength and excellent machinability, making them ideal for heavy-duty structural applications.
Both 2014-T6 and 2014-T651 aluminum alloys belong to the 2014 series and are heat-treated alloys, but they differ in their heat treatment processes and resulting mechanical properties.
The T651 and T652 variants of 2014 aluminum are commonly used for high-strength applications, such as aerospace frames, military vehicles, and heavy-duty automotive components.
The 2014 T3 temper is achieved through solution heat treatment, strain hardening, and natural aging, which significantly improves the alloy's strength.
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.
2017-O aluminum alloy is in the annealed state (O state), meaning it has undergone high-temperature annealing during processing to improve its plasticity and formability.
2017-T4 aluminum alloy is the T4 form of 2017 aluminum alloy. To achieve this state, 2017 aluminum alloy is first subjected to solution heat treatment and then undergoes a natural aging process.
The T451 temper of 2017 aluminum alloy, due to the moderate stretching and natural aging treatment, ensures high strength while maintaining good dimensional stability and toughness.
2024-O aluminum is a variant of the 2024 aluminum alloy in the annealed condition. The "O" here stands for "annealed," which refers to the process of heating the aluminum alloy to a certain temperature and then slowly cooling it. This process relieves internal stresses and results in a lower hardness and enhanced workability.
2024 T3 aluminum is a specially processed aluminum alloy. To achieve the T3 temper, the 2024 aluminum alloy undergoes solution heat treatment, strain hardening, and a subsequent natural aging process.
2024-T851 aluminum alloy is a heat-treated state of 2024 aluminum alloy. To achieve the T851 condition, 2024 aluminum alloy undergoes a three-step process: solution heat treatment, stress relief, and artificial aging.
2024 T4 aluminum is a heat-treated condition of the 2024 aluminum alloy, where "T4" indicates that the alloy has undergone solution heat treatment followed by natural aging. 2024 T4 exhibits the best formability and good machinability.
2219 T87 is a specific temper of 2219 aluminum alloy, known for its high strength, excellent heat resistance, and superior mechanical properties. This alloy is primarily based on aluminum and copper, with small amounts of manganese and other elements.
2219-T851 is a high-performance aluminum alloy that has been specially heat-treated, suitable for demanding aerospace, military, and industrial applications, particularly in environments 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.
6063-T4 aluminum is a widely used aluminum alloy in aerospace, construction, and other industrial applications. It is obtained by solution heat treating the 6063 aluminum alloy and naturally aging it.
2124 O aluminum plate is a type of 2xxx series aluminum alloy, with aluminum-copper as the primary alloying element, belonging to high-strength aluminum alloys. This material has relatively high strength, excellent machinability, and certain heat resistance, making it suitable for various industrial applications, especially outstanding in the aerospace field.
2124 T851 aluminum plate is a high-strength aluminum alloy primarily composed of aluminum and copper, belonging to the 2000 series aluminum alloys.
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.
2024-T351 and 2124 aluminum alloys are both high-strength aluminum alloys, primarily used in aerospace and other demanding applications. However, their compositions, properties, and typical uses differ.
6063 T5 aluminum is an alloy with medium strength, excellent corrosion resistance, and good extrusion processing performance. Its chemical composition primarily includes silicon (Si) and magnesium (Mg), belonging to the heat treatable aluminum-magnesium-silicon series.
6061-T6 is suitable for high-strength and demanding applications, while 6063-T5 is more suitable for aesthetic, architectural, and lower-strength applications. Both alloys have similarities in welding, machinability, and extrudability, making them versatile across various industries.
6063 aluminum alloy is renowned for its excellent machinability, weldability, and surface treatment properties, and the T6 condition indicates that the alloy has undergone a specific heat treatment process to achieve higher strength and hardness.
6061-T6 and 6063-T6 are both part of the 6000 series of aluminum alloys, primarily composed of aluminum, magnesium, and silicon. However, they have different properties and are used in different applications.
6063 O aluminum alloy is an annealed state of the 6063 series, widely used in applications requiring good workability and high formability.
2024-T81 is a heat treatment condition of 2024 aluminum alloy. 2024 aluminum alloy is a high-strength alloy primarily used in aerospace, automotive, and military applications, known for its excellent strength and high-temperature resistance.
The heat treatment processes of 2024 T3 and 2024 T81 aluminum are different, resulting in differences in their mechanical properties.
2024-T351 aluminum plate is a high-strength, highly durable aluminum alloy sheet widely used in aerospace, transportation, and other structural components where high strength and resistance to metal fatigue are critical.
2024-T351 and 2024-T851 aluminum alloys have the same chemical composition, but due to differences in heat treatment and aging processes, they exhibit significant differences in mechanical properties.
6082-T6 aluminum alloy is an aluminum alloy that has been heat-treated with the T6 process (solution heat-treated, quenched, and artificially aged). It is commonly used in engineering fields that require high strength and good corrosion resistance.
6082 T651 aluminum alloy is an enhanced version of the 6082 alloy, which undergoes stress-relieving treatment based on the T6 heat treatment.
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.
2024-T3 aluminum alloy and 2124 aluminum alloy are both high-strength alloys commonly used in aerospace and other high-performance applications. They each have distinct advantages and are suited to specific application environments.
2024 T8 is still the preferred choice in high-performance aerospace applications due to its outstanding strength. On the other hand, 2124 offers more advantages in specific needs such as thermal performance, impact toughness, and electrical properties, making it suitable for a wider range of 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.