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.
2024-O Alclad aluminum alloy sheet is a high-strength aluminum alloy with excellent ductility and corrosion resistance, widely used in the aerospace field, particularly for aircraft structural components and external skins.
2024 T3 Alclad aluminum plate is a special material that combines the strength and corrosion resistance of aluminum alloys with advanced surface treatment to enhance its performance in various applications.
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.
7010 aluminum alloy is a high-strength, good fatigue strength, and excellent stress corrosion resistance forged aluminum alloy.
7010 aluminum has better tensile strength and shear strength, making it more suitable for high-stress applications, while 7050 aluminum offers excellent fatigue strength and resistance to stress corrosion cracking, making it an ideal choice for critical aerospace structures.
Both 7010 and 7475 aluminum alloys are high-performance materials specifically designed for aerospace applications, but their selection should be based on specific performance requirements.
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.
6082-O aluminum alloy is a type of 6082 series aluminum alloy in the annealed state ("O" represents the annealed state), which has high ductility and good formability.
6082 aluminum alloy is a commonly used medium-strength aluminum alloy, widely applied in various fields. The performance characteristics of 6082 aluminum alloy vary significantly based on different heat treatment conditions.
6082-T6151 aluminum alloy is a special heat-treated aluminum alloy with excellent strength, corrosion resistance, and formability. Its heat treatment process and corresponding properties make it an ideal material for environments with high strength and corrosion resistance requirements.
6082 T6151 aluminum alloy performs excellently in high-strength and high-toughness applications, while 6082-T651 aluminum alloy, due to its more economical and stable performance, is widely used in conventional engineering.
6082-T62 aluminum is an aluminum alloy that has been subjected to solution heat treatment and artificial aging. It is a specific temper of the 6082 aluminum alloy, offering excellent fatigue strength and good mechanical properties.
6082-T6 aluminum alloy is suitable for high-strength structural components subjected to higher shear forces, while 6082-T62 aluminum alloy is more suitable for applications that require resistance to repeated loads and high fatigue performance.
6082 T4 aluminum alloy is a high-strength aluminum alloy that is widely used in the manufacture of structural components, especially for applications requiring good mechanical properties and corrosion resistance.
6082-T5 aluminum alloy is an aluminum alloy with good strength, good corrosion resistance, and good machinability, primarily used for structural applications.
2618 Aluminum is suitable for professional applications that require high strength and high-temperature performance, while 6061 Aluminum performs better in terms of versatility, corrosion resistance, and formability, making it a more widely used choice.
2618 is favored for its high-temperature elasticity and machinability, while 7075 is known for its excellent strength and structural capabilities in demanding applications.
2618 aluminum is well-suited for applications that require high strength and ductility, particularly under extreme thermal and mechanical stresses, while 4032 aluminum is better suited for high-performance applications where durability and high-temperature resistance are the primary considerations.
2618 T61 Aluminum Alloy is a high-strength aluminum-copper alloy, particularly suitable for applications that work in high temperature and high pressure environments, with widespread use in aerospace and high-performance racing fields.
2017 aluminum alloy is more suitable for applications that require higher corrosion resistance but do not require extreme strength, while 2024 aluminum alloy is suitable for applications where high strength and fatigue resistance are crucial.
2017 aluminum alloy and 6061 aluminum alloy have significant differences in performance, making them suitable for different application scenarios.
The choice between 2017-T4 and 2017-T451 aluminum alloys depends on the specific requirements of the application: whether the focus is on ductility, tensile strength, and the subsequent processing needs.
2017-T351 Aluminum is the form of 2017 aluminum alloy in the T351 temper. This state of the alloy is obtained through specific heat treatment and aging processes, which significantly improve its strength, hardness, and durability.
2017-T42 aluminum is suitable for applications that require high strength but less strict requirements for ductility, particularly in the aerospace and high-strength structural fields.
2219 T3 aluminum alloy is an aluminum alloy that has undergone solution heat treatment, strain hardening, and natural aging. It has high mechanical strength, excellent weldability, outstanding corrosion resistance, and anodizing capabilities.
2219-T31 aluminum alloy is a heat-treated state of 2219 aluminum alloy, where "T31" indicates that the metal has undergone a specific heat treatment process, including solution heat treatment, strain hardening, and natural aging.
2219-T37 aluminum alloy is a specially treated aluminum alloy, which undergoes solution heat treatment, 7% strain hardening, and natural aging to form the T37 state.
2219-T31 Aluminum and 2219-T37 Aluminum are two different processing states of the same aluminum alloy. Although they have the same alloy composition and many physical properties, their mechanical properties differ due to the different processing treatments.
2219-T351 aluminum alloy is a high-strength aluminum alloy typically used in aerospace applications as well as other high-performance applications, such as rocket, spacecraft, and aircraft structural components.
If better ductility is needed, 2219 T351 might be a better choice. However, when higher strength and fatigue resistance are required, 2219 T851 is more suitable.
2219-T6 aluminum is a high-strength aluminum alloy, particularly suitable for aerospace and other high-stress, weight-critical applications.
2219-T62 aluminum alloy is a 2219 aluminum alloy that has been treated through a specific heat treatment process, which mainly includes solution heat treatment and artificial aging.
2219 T6 aluminum provides high strength and rigidity, making it suitable for high-stress applications, while 2219-T62 aluminum offers better ductility and resistance to deformation, making it suitable for complex structures that require significant deformation.
2219-T81 is a heat treatment state of 2219 aluminum alloy, which enhances its strength while maintaining good machinability.
Its different heat treatment states significantly affect its properties, with 2219-T62 and 2219-T81 being two common heat treatment states.
Both 2219-T81 and 2219-T851 aluminum alloys are variants of the same 2219 aluminum, but their mechanical properties differ due to the distinct processing methods used.
2219-T37 aluminum has higher fatigue strength, making it suitable for medium-strength and high-fatigue environments, while 2219-T87 aluminum has higher tensile strength, yield strength, and shear strength, making it suitable for high-load applications.
6061 aluminum is a versatile, medium-strength alloy with excellent corrosion resistance, while 2219 aluminum is a high-strength, heat-resistant alloy commonly used in aerospace applications.
2011-T3 aluminum alloy is a specific temper of 2011 aluminum alloy that achieves excellent performance characteristics after undergoing T3 heat treatment. The T3 temper involves a solution heat treatment, strain hardening, and natural aging process.
2011-T6 aluminum alloy excels in strength and hardness, making it suitable for applications that require withstanding high mechanical loads.
2011-T3 aluminum alloy has better ductility and fatigue resistance, making it suitable for applications that require good formability; while 2011-T6 aluminum alloy offers higher strength and thermal conductivity, making it suitable for applications with high strength and heat dissipation requirements.
2011-T4 aluminum alloy is an aluminum alloy that has undergone solution heat treatment and natural aging, belonging to the T4 temper of the 2011 series aluminum alloys.
2011-T3 aluminum alloy and 2024-T4 aluminum alloy are both high-strength aluminum alloys, widely used in aerospace and other structural applications.
2011-T451 Aluminum is a high-strength aluminum alloy that has undergone heat treatment and aging treatment, offering good mechanical properties, moderate ductility, fatigue resistance, and shear strength.
2011 aluminum alloy is known for its excellent machinability and high strength, and is commonly used in various aerospace, automotive, and engineering applications. The mechanical properties of 2011 aluminum vary depending on the heat treatment state, with T3 and T451 being two different conditions.
2011-T4511 aluminum alloy is a high-strength aluminum alloy enhanced by the T4511 heat treatment state, widely used in aerospace, precision machinery, and other fields, particularly suitable for components that require high-precision machining and complex shapes.
2011 T4511 aluminum and 2030-T4511 aluminum are two different alloy series, and although both are in the T4511 temper, their compositions, properties, and applications differ.
2011-T651 aluminum alloy is a high-strength aluminum alloy with good machinability, widely used in aerospace, automotive, and other industrial fields.
2011 T3 T651, due to the differences in aging treatment and hardening processes, the T3 alloy has higher ductility and electrical conductivity, while the T651 alloy has higher strength, making it suitable for more demanding structural applications.
2011-T8 aluminum has excellent strength characteristics, making it suitable for applications with high strength requirements, but it is slightly inferior in terms of ductility.
2011-T3 aluminum is very suitable for applications that require good machinability and medium strength, while 2011-T8 aluminum is suitable for high-strength, high-stress applications.
2011 aluminum alloy and 6061 aluminum alloy are two common types of aluminum alloys, both widely used in various engineering applications.
2011 aluminum alloy has excellent machinability and high strength but poor corrosion resistance, while 6082 aluminum alloy offers better corrosion resistance, good weldability, and moderate strength.
In the fields of aerospace, automotive, and industrial machinery, 2014-T62 aluminum alloy, with its stable performance and processing advantages, has become one of the most favored materials.
2014-T6 aluminum alloy is a high-strength, high-temperature-resistant aluminum-copper alloy belonging to the 2xxx series. Due to its excellent mechanical properties, it is widely used in aerospace, automotive, and industrial equipment fields.
Both T6 and T62 tempers of the 2014 aluminum alloy undergo solution heat treatment and artificial aging to meet standard mechanical performance requirements.
2014 T4 aluminum alloy is a high-strength, high-hardness material with good machinability, widely used in aviation, military, and heavy machinery fields.
2014-T4 and 2024-T4 aluminum each have their unique strengths, and their selection mainly depends on the specific application requirements and environmental conditions.
2014-T651 aluminum is a high-strength aluminum alloy that has undergone solution heat treatment, stress relief, and artificial aging treatment, which gives it excellent strength and hardness.
Similar to 2014-T651 aluminum, 2014-T6511 aluminum is first heated to a specific temperature through solution heat treatment, allowing the elements such as copper, manganese, and silicon in the alloy to dissolve evenly, improving the overall uniformity of the aluminum alloy.
The elongation, shear strength, and ultimate tensile strength of 2014-T651 aluminum are slightly better, while the fatigue strength of 2014-T6511 aluminum is slightly higher.
2014-T42 aluminum alloy is processed through solution heat treatment and natural aging, offering good ductility, machinability, and moderate strength. It is widely used in fields that do not require ultra-high strength or fatigue resistance.
2014 T42 aluminum alloy and 2014-T62 aluminum alloy, although having the same alloy composition, exhibit significant differences in mechanical properties due to their different processing states.
2014-T6 is generally stronger and harder, while 2014-T4 has better ductility and fatigue strength. These differences make each temper more suitable for specific 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.
If high strength and fatigue resistance are needed, 7075 aluminum alloy is the better choice; while if machinability, weldability, and cost-effectiveness are more important, 6061 aluminum alloy is the better option.
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.
7050 aluminum alloy has higher strength and corrosion resistance, making it suitable for critical components in high-stress and high-corrosion environments, while 6061 aluminum alloy is more cost-effective with better machinability, suitable for general engineering and structural applications.
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.
2014 aluminum alloy is a member of the 2000 series, where the primary alloying element is copper. This gives the alloy several key properties that determine its range of applications.
Both 2014 and 2024 aluminum alloys belong to the 2000 series (aluminum-copper alloys), with many similarities. However, there are subtle but important differences in composition, processing, and performance, making each better suited for specific applications.
2014 aluminum and 6061 aluminum are widely used in aerospace, automotive, and industrial applications due to their excellent properties. However, they have distinct differences in composition, mechanical properties, and specific uses.
2014 aluminum alloy has good machinability and moderate strength, making it suitable for durable applications, while 7075 aluminum alloy offers higher strength and fatigue resistance, making it ideal for high-pressure and high-load environments.
7068 aluminum offers higher strength and better fatigue resistance than 7075, but with slightly reduced ductility and corrosion resistance.
7068 aluminum alloy has higher strength and hardness than 6061, but 6061 offers better workability 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.
Dive into a detailed comparison of Aluminum 7050 and 7075. Understand why 7075 excels in ultimate strength, while 7050 offers superior stress-corrosion cracking resistance for demanding environments.
The difference between 7075-T651 and 7075-T7351 aluminum alloys lies in their tempering processes and the resulting mechanical properties, particularly strength, stress corrosion resistance, and fracture toughness.
As a professional 7075 T6 aluminum alloy manufacturer, we provide aviation-grade aluminum blocks that meet AMS and ASTM standards, support customized sizes and bulk purchases, and ensure fast delivery and quality certification.
The difference between 7075-T73 and 7075-T73511 aluminum alloys lies in their heat treatment processes, mechanical properties, and intended applications.
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.