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 aerospace aluminum rod is a high-strength aluminum alloy material, mainly used in the aerospace field and other applications that require high strength and low weight.
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.
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.