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.
2A12 aluminum alloy is a superior aerospace material, suitable for high-strength and lightweight design requirements.
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 cold rolled aluminum bar is an aluminum alloy product based on 2024 aluminum alloy, processed into shape through cold rolling.
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Durable 2017-T4 aluminum round bars with excellent fatigue resistance. ASTM B211 compliant, non-magnetic, and anodizing-ready. Shop now for certified material with guaranteed mechanical properties.
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!
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.
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-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.
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.
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.