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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. The 2014 aluminum alloy has significant advantages in high-stress environments due to its excellent strength and fatigue resistance.

Haomei Aluminum can produce AMS 4153 UNS A92014 QQA 200/2 2014 aerospace aluminum rod.

2014 Aerospace Aluminum Rod Bar

Characteristics of 2014 Aerospace Aluminum Rod Bar

  • 1. High Strength: The 2014 aluminum rod is known for its high strength, especially after heat treatment, which significantly enhances its strength, making it widely used in aerospace and military applications.
  • 2. Good Fatigue Strength: The material exhibits excellent fatigue strength under dynamic loads, making it suitable for long-term use.
  • 3. Machinability: The 2014 aluminum rod has good machinability, allowing for processes like cutting and drilling, while also possessing excellent thermal forming capabilities.
  • 4. Lower Corrosion Resistance: The corrosion resistance of 2014 aluminum alloy is relatively poor, especially when exposed to moisture or saltwater environments; therefore, surface treatment or coating is usually required to enhance its corrosion resistance.
  • 5. Heat Treatable: The 2014 aluminum alloy can further enhance its mechanical properties through heat treatment processes such as quenching and aging.
  • 6. Good Weldability: Although the weldability of the 2014 aluminum alloy is not as good as some other aluminum alloys, it can still be joined using suitable welding techniques.

Chemical composition of 2014 aerospace aluminum alloy

Element Composition %
Si 0.15-1.2
Fe 0.7
Cu 3.9-5.0
Mn 0.40-1.2
Mg 0.20-0.8
Ti 0.15
Cr 0.10
Zn 0.25
Other (Each) 0.0-0.05
Aluminium (Al) Balance

Mechanical properties of 2014 aerospace high quality rod bar

Mechanical property Value
Tensile strength 415MPa
Yield strength 370 Min MPa
Electrical conductivity 34%-50% IACS

2014 Aerospace Aluminum Rod Bar Heat Treatment Conditions

The typical heat treatment conditions for 2014 aluminum rods include T3, T4, and T6, each of which has different performance characteristics and applicable scenarios.

T3 and T4 conditions are suitable for applications requiring good toughness and medium strength.

T6 condition, on the other hand, is suitable for situations that require extremely high strength but relatively low toughness.

2014 T3 Aerospace Aluminum Rod Bar

The T3 condition refers to the state where the aluminum alloy undergoes solution treatment, is rapidly cooled, and is naturally aged at room temperature.

Characteristics of 2014 T3 Aluminum Rod Bar

  • Strength: The aluminum alloy in T3 condition has a high tensile strength, making it suitable for bearing significant mechanical loads.
  • Toughness: Compared to the T6 condition, the T3 condition has better toughness, maintaining certain performance under impact and deformation.

Application: Due to its good overall performance, the 2014 aluminum rod in T3 condition is commonly used in aircraft structural components, load-bearing parts, and applications requiring certain toughness.

2014 T4 Aerospace Aluminum Rod Bar

The T4 condition refers to the state where the aluminum alloy undergoes solution treatment and natural aging.

Characteristics of 2014 T4 Aluminum Rod Bar

  • Strength: The T4 condition provides medium strength, generally lower than T3 and T6 conditions, but still suitable for many medium-load applications.
  • Toughness: The T4 condition of the aluminum alloy exhibits good toughness, able to resist a certain degree of impact and deformation.

Application: Suitable for applications requiring good formability and subsequent processing, such as manufacturing complex-shaped components and structures.

2014 T6 Aerospace Aluminum Rod Bar

The T6 condition refers to the state where the aluminum alloy undergoes solution treatment followed by artificial aging to enhance hardness.

Characteristics of 2014 T6 Aluminum Rod Bar

  • Strength: The T6 condition of the aluminum alloy provides maximum strength, being the highest strength heat-treated state for 2014 aluminum alloy.
  • Toughness: Due to its high strength, the toughness of T6 condition is relatively lower, potentially exhibiting brittleness under high-stress concentrations or impact loads.

Application: T6 condition aluminum rods are widely used in structural and load-bearing components that require high strength, such as critical structural components in aerospace, racing, and high-performance mechanical parts.

2014 Aerospace Aluminum Rod Bar Applications

The 2014 aluminum rod is widely used in the aerospace field, especially because of its high strength, lightweight, and excellent machinability, making it very suitable for parts of aircraft structures that need to withstand high loads.

1. Airframe Structure

The 2014 aluminum rod is commonly used to manufacture the main load-bearing structural components of aircraft, such as fuselage frames and wing beams. These components need to bear immense mechanical stress while maintaining a low weight. The high strength and good fatigue performance of the 2014 aluminum rod provide long-term structural support.

  • Wing Main Beam: The main beam of the wing is the most crucial load-bearing component of an aircraft's wing, supporting lift, gravity, and aerodynamic loads generated during flight. After undergoing T6 heat treatment, the 2014 aluminum rod provides extremely high tensile strength and fatigue strength, ensuring the safety and durability of the wing.
  • Fuselage Frame: In the frame structure of the aircraft fuselage, the 2014 aluminum rod is commonly used for the ribs and stringers. These structures need to withstand deformation and stress during flight, requiring extremely high material strength. The strength and rigidity of 2014 aluminum make it an ideal choice.

2. Aircraft Landing Gear

The landing gear is one of the most critical components of an aircraft, as it must not only support the aircraft's weight but also withstand the strong impact during landing. The high strength and fatigue resistance of 2014 aluminum alloy make it applicable in certain parts of the landing gear, particularly in structural components such as support arms, bearings, and joints.

  • Landing Gear Strut: The strut is the core component of the landing gear, directly supporting the weight of the aircraft. The high tensile strength and rigidity of the 2014 aluminum rod ensure the stability of the strut during prolonged use.
  • Joints and Hinges: These components play a critical role in the extension and retraction of the landing gear, requiring materials that not only have high strength but also good wear resistance. The 2014 aluminum rod meets these requirements.

3. Aircraft Fuselage Panel Connectors

Although the 2014 aluminum rod is not directly used for thin sheet manufacturing, its high strength makes it an important material in certain thick plate structures and connection points, especially in the connections between skin and support structures.

These connectors need to possess good machinability and high strength to withstand tensile and shear stresses generated during flight. The 2014 aluminum rod performs excellently in processing and connection.

4. Aircraft Engine Components

Although the 2014 aluminum rod is not suitable for high-temperature environments, it is still applicable in certain non-high-temperature bearing components, due to its strength and lightweight characteristics.

Connecting Shafts and Brackets: Certain brackets and connecting components in the engine require high strength and fatigue resistance, making the 2014 aluminum rod a suitable choice.

5. Solar Panel Brackets

These brackets need to maintain an extremely lightweight to reduce impact on launch weight, and the lightweight and high-strength characteristics of the 2014 aluminum rod give it a competitive advantage in this field.

The 2014 aluminum rod, with its exceptional strength, rigidity, and fatigue resistance, is widely used in the aerospace field for manufacturing various high-stress components such as airframe structures and landing gear. Although its corrosion resistance is poor, surface treatments or the use of composite materials can effectively enhance its service life.

Limitations of 2014 Aerospace Aluminum Rod Bar

  • Poor Weldability: Due to the high copper content, the weldability of the 2014 aluminum alloy is inferior to that of other aluminum alloys, making it prone to hot cracking.
  • Poor Corrosion Resistance: Particularly in salt spray environments, it is prone to corrosion; thus, surface treatment or protective coatings are required.