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2618 Aluminum

2618 aluminum alloy is a high-strength, high-temperature-resistant aluminum alloy, widely used in environments that require high stress and high temperature resistance. It combines excellent strength, high-temperature performance, good machinability, and limited ductility, making it an essential material in several industries. Although it is somewhat lacking in corrosion resistance, its other outstanding properties make it indispensable in aerospace, automotive, and high-temperature industrial applications.

2618 Aluminum Characteristics

Characteristics Description
Strength and High-Temperature Performance 2618 aluminum alloy has extremely high tensile strength and yield strength, much higher than many common aluminum alloys, making it suitable for high-stress and high-temperature environments. It is widely used in parts of jet engines, racing engine components, and other structural components that need to withstand extreme heat and load.
Ductility and Machinability Although ductility is low (with a smaller elongation before fracture), it maintains a good balance between strength and high-temperature performance. Its good machinability makes it suitable for high-load components in jet engines and racing engines, such as pistons.
Corrosion Resistance The corrosion resistance of 2618 aluminum alloy is relatively poor, mainly due to its higher copper and nickel content, which makes it more prone to oxidation in wet or corrosive environments. Additional surface treatments (such as coatings or anodizing) are usually required to improve corrosion resistance.

2618 Aluminum Applications

2618 aluminum alloy is a high-strength, high-temperature-resistant aluminum alloy with relatively low ductility. Although it does not have the same level of corrosion resistance as other aluminum alloys, its excellent mechanical properties make it widely used in aerospace, automotive, and high-temperature industrial fields. Whether in jet engines, racing pistons, or other high-temperature and high-stress environments, 2618 aluminum alloy provides unparalleled performance, making it the material of choice for critical component manufacturing.

2618 Aluminum Mechanical Properties

Property 2618 Aluminum
Elastic (Young's, Tensile) Modulus (GPa) 71
Elongation at Break (%) 5.8
Fatigue Strength (MPa) 110
Poisson's Ratio 0.33
Shear Modulus (GPa) 27
Shear Strength (MPa) 260
Tensile Strength: Ultimate (UTS) (MPa) 420
Tensile Strength: Yield (Proof) (MPa) 350

2618 Aluminum Thermal Properties

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

2618 Aluminum Electrical Properties

Property 2618 Aluminum
Electrical Conductivity: Equal Volume (% IACS) 37
Electrical Conductivity: Equal Weight (% IACS) 110

2618 Aluminum Alloy Composition (% by weight)

Element 2618 Aluminum
Aluminum (Al) 92.4 to 94.9
Chromium (Cr) 0
Copper (Cu) 1.9 to 2.7
Iron (Fe) 0.9 to 1.3
Magnesium (Mg) 1.3 to 1.8
Manganese (Mn) 0
Nickel (Ni) 0.9 to 1.2
Silicon (Si) 0.1 to 0.25
Titanium (Ti) 0.040 to 0.1
Zinc (Zn) 0 to 0.1
Residuals 0

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