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What is the difference between 4032 and 2618 aluminum?

The main difference between 4032 and 2618 aluminum alloys lies in their composition, mechanical properties, and suitability for specific applications, especially in high-performance fields such as motorsports and aerospace.

2618 aluminum is well-suited for applications that require high strength and ductility, particularly under extreme thermal and mechanical stresses, while 4032 aluminum is better suited for high-performance applications where durability and high-temperature resistance are the primary considerations.

Differences between 4032 and 2618 Aluminum Alloys

Property 2618 Aluminum Alloy 4032 Aluminum Alloy
Ductility More ductile, capable of absorbing high-impact stresses Due to higher silicon content, it is harder and more durable, with lower ductility
Heat Resistance Suitable for applications that require heat resistance but have lower thermal stability Performs better in high-temperature environments, with strength maintained above 300°C
Strength Has a better strength-to-weight ratio, suitable for high-stress, heavy-load applications Generally stronger, especially in high-temperature applications
Applications Suitable for high-stress, heavy-load applications requiring flexibility (e.g., racing pistons, aerospace engine components) Suitable for applications requiring exceptional wear resistance and high-temperature performance (e.g., high-performance engine components, racing pistons)

4032 and 2618 Aluminum Alloys Applications

2618 Aluminum Applications

  • Common Uses: Primarily used for high-performance engine components, particularly in motorsports and aerospace applications. Its ability to withstand high temperatures and mechanical stress makes it an ideal choice for jet engine parts, structural components, and high-performance racing pistons.
  • Advantages: 2618 aluminum is more flexible, with better impact resistance, making it suitable for high-load applications that involve thermal cycling and high stress.

4032 Aluminum Applications

  • Common Uses: 4032 is widely used in motorsports, especially for high-performance pistons, engine parts, and chassis components. It is typically used in applications that require exceptional performance at high temperatures, such as racing engines and aerospace components.
  • Advantages: The higher silicon content in 4032 provides better thermal stability and wear resistance, making it suitable for parts exposed to high temperatures and mechanical stresses over extended periods.

4032 and 2618 Aluminum Alloys Processing and Machinability

2618 Aluminum Machinability and Workability

Machinability: It has good machinability, but due to its lower silicon content, it is less wear-resistant compared to 4032. Lubrication is required during the machining process to achieve optimal results.

Welding: It can be welded using arc welding or inert gas welding methods, but care must be taken to prevent damage from overheating.

4032 Aluminum Machinability and Workability

Machinability: 4032 is more difficult to machine than 2618 because it has a higher silicon content, making it harder and less ductile. However, it provides excellent durability for the finished product.

Welding: Like 2618, it can also be welded using arc or inert gas methods, but care must be taken to avoid cracking.

2618 Aluminum vs. 4032 Aluminum Mechanical Properties

2618 Aluminum Mechanical Properties

  • Strength and Durability: 2618 is known for its excellent strength-to-weight ratio, making it the preferred choice for components that need to withstand extreme high temperatures, such as pistons and engine parts in aerospace and automotive applications.
  • Ductility: The low silicon content makes 2618 more ductile, allowing it to absorb significant thermal and mechanical stresses without failure.
  • Heat Resistance: It has good heat resistance, especially in high-load, high-stress applications, such as jet engines and high-performance automotive parts.

4032 Aluminum Mechanical Properties

  • Strength and Durability: 4032 is designed to withstand high-performance environments, particularly when temperature stability is critical. It retains mechanical strength at temperatures up to around 200°C, with a maximum operating temperature of up to 300°C. This makes it ideal for components that operate at higher temperatures for extended periods.
  • Lower Ductility: Due to its higher silicon content, 4032 has lower ductility compared to 2618. While this makes it more wear-resistant, it also limits its ability to absorb high impacts.
  • Heat Resistance: Due to its higher silicon content, 4032 shows greater stability at higher temperatures, making it particularly suitable for applications such as racing pistons and high-performance engine components.
Property 2618 Aluminum 4032 Aluminum
Brinell Hardness 120 120
Elastic (Young's, Tensile) Modulus, GPa 71 73
Elongation at Break, % 5.8 6.7
Fatigue Strength, MPa 110 110
Poisson's Ratio 0.33 0.33
Shear Modulus, GPa 27 28
Shear Strength, MPa 260 260
Tensile Strength: Ultimate (UTS), MPa 420 390
Tensile Strength: Yield (Proof), MPa 350 320

2618 Aluminum vs. 4032 Aluminum Thermal Properties

Property 2618 Aluminum 4032 Aluminum
Latent Heat of Fusion, J/g 390 570
Maximum Temperature: Mechanical, °C 210 180
Melting Completion (Liquidus), °C 640 570
Melting Onset (Solidus), °C 550 530
Specific Heat Capacity, J/kg-K 880 900
Thermal Conductivity, W/m-K 160 140
Thermal Expansion, µm/m-K 22 19

2618 Aluminum vs. 4032 Aluminum Electrical Properties

Property 2618 Aluminum 4032 Aluminum
Electrical Conductivity: Equal Volume, % IACS 37 34
Electrical Conductivity: Equal Weight (Specific), % IACS 110 120

2618 Aluminum vs. 4032 Aluminum Alloy Composition

2618 Aluminum Composition and Alloy Elements

Composition: 2618 aluminum has a lower silicon content, which enhances its ductility. This makes it more flexible and able to absorb high thermal stresses. It typically contains copper, iron, and small amounts of nickel and manganese.

Silicon Content: Compared to 4032, it has a lower silicon content, making it more ductile and flexible, making it very suitable for high-load, high-stress applications.

4032 Aluminum Composition and Alloy Elements

Composition: 4032 aluminum has a higher silicon content (around 12%), which significantly improves its strength but reduces its ductility. The silicon increases the material's resistance to thermal expansion and enhances its performance under high-temperature conditions.

Silicon Content: The high silicon content makes the structure stronger, reduces its ductility, but makes it more durable for high-performance components that need to withstand extreme conditions.

Element 2618 Aluminum 4032 Aluminum
Aluminum (Al), % 92.4 to 94.9 81.1 to 87.2
Chromium (Cr), % 0 0 to 0.1
Copper (Cu), % 1.9 to 2.7 0.5 to 1.3
Iron (Fe), % 0.9 to 1.3 0 to 1.0
Magnesium (Mg), % 1.3 to 1.8 0.8 to 1.3
Nickel (Ni), % 0.9 to 1.2 0.5 to 1.3
Silicon (Si), % 0.1 to 0.25 11 to 13.5
Titanium (Ti), % 0.040 to 0.1 0
Zinc (Zn), % 0 to 0.1 0 to 0.25
Residuals, % 0 0 to 0.15