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.
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.
2024 aluminum bars and rods excel in high-strength, lightweight applications but require corrosion protection. Their performance varies significantly with temper, making them versatile for aerospace, automotive, and industrial uses.
2219 aluminum alloy is renowned for its excellent high-temperature resistance and high strength-to-weight ratio, making it particularly suitable for applications where structural strength and heat treatment performance are critical.
The 2017 aerospace aluminum bar is an alloy based on aluminum, with copper as the main alloying element, belonging to the aluminum-copper family of hard aluminum alloys.
2618 aerospace aluminum is a high-strength aluminum alloy belonging to the 2xxx series, with copper (Cu) as the primary alloying element, and often includes magnesium (Mg), silicon (Si), and a small amount of zirconium (Zr).
The 2014 aerospace aluminum rod is a widely used aluminum alloy material in the aerospace industry, belonging to the 2XXX series of aluminum alloys, which primarily consists of copper as the main alloying element.
2011 aerospace aluminum rod is a common aluminum alloy material primarily used for the manufacturing of structural components and parts in the aerospace industry.
Common forged products of 2014 aluminum alloy in the aerospace field include forged bars, forged balls, forged shafts, forged plates, and forged gears, which are primarily used for airfoil shapes, brackets, connectors, wheels, and flight control components.
2219 aerospace aluminum forgings are a high-strength, high-temperature-resistant aluminum alloy widely used in the aerospace field.
2618 aluminum forgings typically require heat treatment to achieve optimal mechanical performance. Common heat treatment methods include aging and quenching.
2A12 aluminum alloy is a superior aerospace material, suitable for high-strength and lightweight design requirements.
The main component of 2017 aluminum alloy is copper. After heat treatment, it can reach very high strength and is suitable for applications requiring strength and rigidity.
The aerospace sector also chooses forged 2024 aluminum alloy for its outstanding fatigue resistance, especially in structural components that must endure repeated loads.
2124 aluminum forgings are ideal materials for many high-demand engineering applications due to their high strength, good toughness, and excellent machinability.
Aluminum 2014 is a precipitation hardening alloy with good corrosion resistance, high conductivity and good machinability, used in the manufacture of aircraft and truck parts and forging.
In terms of processing, 2024 aluminum is typically formed through hot extrusion, making it suitable for manufacturing complex-shaped profiles such as frames, brackets, and components.
2219 aerospace aluminum profile is a high-strength aluminum alloy with a high copper content, which gives it excellent strength and toughness.
2011 CF aluminum bar is an aluminum alloy primarily composed of easy-to-machine elements (such as lead and bismuth), with the main features of excellent machinability and relatively low friction coefficient.
As a round bar form of 2011 aluminum alloy, it has the best machinability among all aluminum alloys, and its mechanical properties are also outstanding.
2011 Aluminum Hex Bar is a widely used aluminum alloy product for the manufacturing of precision mechanical parts. It has a range of excellent machining properties and physical characteristics, making it an ideal material for high-precision machining.
2024 Aluminum Round Bar is an aluminum alloy round bar with excellent strength and fatigue resistance, widely used in aerospace, automotive, machinery, and industrial fields.
2024 T851 aluminum round bar is a high-strength, medium-corrosion-resistant alloy, and its properties make it suitable for a wide range of applications, including construction, automotive, and aerospace industries.
2024 Aluminum Flat Bar is an aluminum material with a rectangular cross-section made from 2024 aluminum alloy. Compared to round aluminum bars, it has different mechanical properties and manufacturing advantages.
The 2024 T4 Aluminum Round Bar is a widely used aluminum alloy product, especially suitable for applications that require a good balance between strength and corrosion resistance.
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 cold rolled aluminum bar is an aluminum alloy product based on 2024 aluminum alloy, processed into shape through cold rolling.
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.
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2618 Aluminum Bar: The material of choice for applications requiring durability under high temperatures and pressures. Widely used in supersonic aircraft, engine forgings and tooling. Has unmatched high temperature performance. Meets AMS 4176/4180 standards.
Our 2618 aluminum alloy round bar products comply with AMS 4120 and ASTM B211 standards, provide a variety of diameters (5mm-300mm) and surface treatment options, support custom processing and global certification (AS9100/ISO 9001). Get fatigue-resistant and high-temperature resistant solutions now!
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.
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.
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.
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.
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.
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.
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-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.
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.