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.
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.
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.
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-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 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.
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.