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-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.
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.
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.
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.
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-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 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.
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 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.