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2000 Series Aerospace Aluminum Bar

  • 2024 T3 T351 Aerospace Aluminum Rod Bar

    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 Aerospace Aluminum Bar

    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.

  • 2017 T4 T451 Aerospace Aluminum Bar Rod

    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 T6 T6511 T651 T61 Aircraft Aluminium Rod

    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).

  • 2014 T3 T6511 Aerospace Aluminum Rod Bar

    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 T3 T6 Aerospace Aluminum Bar Rod

    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 Aircraft Aluminum Bar

    2A12 aluminum alloy is a superior aerospace material, suitable for high-strength and lightweight design requirements.

  • 2017 O Aluminum

    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

    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.

  • 2017 T451 Aluminum

    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

    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 Plate Sheet

    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 Plate Sheet

    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 Plate Sheet

    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 Aluminum vs. 2124 Aluminum

    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.

  • A Comprehensive Comparison 2024-T3 and 2124 Aluminum Alloy Characteristics

    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.