2011 T4 Aluminum
2011-T4 aluminum alloy is an aluminum alloy that has undergone solution heat treatment and natural aging, belonging to the T4 temper of the 2011 series aluminum alloys. Specifically, the T4 temper indicates that the aluminum alloy has been solution heat-treated and then naturally aged at room temperature to achieve certain strength and hardness characteristics.
2011-T4 aluminum alloy is widely used in many applications that require high precision and strength due to its high strength, excellent machinability, and good mechanical properties. However, due to its relatively low corrosion resistance and ductility, it is typically used for more precise mechanical components or structural parts, and needs to be paired with appropriate surface treatments to enhance its corrosion resistance.
2011 T4 Aluminum Properties
2011 aluminum alloy is primarily composed of aluminum (Al) and copper (Cu), making it a high-strength aluminum alloy, commonly used in applications that require good mechanical properties, machinability, and corrosion resistance.
-
High Strength: 2011 aluminum alloy has relatively high strength due to its higher copper content.
-
Excellent Machinability: Due to the presence of copper, 2011 aluminum alloy is very easy to machine, making it an ideal material for manufacturing precision parts.
-
Corrosion Resistance: Although it has a higher copper content, 2011 aluminum alloy still has some corrosion resistance, making it suitable for various environments. However, compared to other aluminum alloys like 2024 or 7075, 2011 alloy has slightly inferior corrosion resistance.
-
Lower Ductility: Due to its high strength, 2011 aluminum alloy has relatively low ductility, making it prone to fracture during deformation. Therefore, it is typically not suitable for large-scale plastic forming operations.
T4 Temper 2011 Aluminum
-
Solution Heat Treatment: In the T4 temper, 2011 aluminum alloy is first subjected to solution heat treatment (typically heated to around 450°C and held for a period of time). During this process, the alloying elements (primarily copper) are fully dissolved into the aluminum matrix, forming a uniform solution.
-
Natural Aging: After the solution treatment, the aluminum alloy undergoes natural aging at room temperature, where some elements (such as copper) gradually precipitate out, enhancing the metal's strength and hardness. The natural aging process typically takes a few days to a few weeks, depending on the alloy's composition and environmental conditions.
-
Mechanical Properties: After solution heat treatment and natural aging, 2011-T4 aluminum alloy has good mechanical properties. Compared to the 2011-O state aluminum alloy (which is not aged), the T4 temper alloy has higher strength, but its ductility and toughness are relatively lower.
2011-T4 Aluminum Applications
-
Aerospace: Used for manufacturing aircraft structural parts and high-strength components. 2011-T4 aluminum alloy has excellent machinability, making it suitable for producing complex parts.
-
Precision Machining: In automotive and mechanical manufacturing, 2011-T4 aluminum alloy is commonly used for producing precision machined parts such as machine tool components, bolts, gears, etc., due to its high strength and ease of machining.
-
Electronic Products: The excellent machinability of 2011 aluminum alloy makes it suitable for producing enclosures and components for some electronic products, especially in applications requiring high-precision cutting.
-
Other Industrial Applications: Due to its high strength, 2011-T4 aluminum alloy is also commonly used for manufacturing structural components such as brackets, fasteners, and connectors.
Limitations of 2011-T4 Aluminum Alloy
-
Lower Corrosion Resistance: Compared to some other aluminum alloys (such as 2024-T3 or 7075 series), 2011-T4 aluminum alloy has weaker corrosion resistance, especially in harsh environments where localized corrosion may occur. To enhance its corrosion resistance, surface treatments such as anodizing are often required.
-
Lower Ductility: The low ductility of 2011 aluminum alloy makes it unsuitable for applications requiring large-scale forming or complex plastic deformation.
2011 T4 Aluminum Mechanical Properties
Property
|
2024-T4 Aluminum
|
Brinell Hardness
|
120
|
Elastic (Young's, Tensile) Modulus (GPa)
|
71
|
Elongation at Break (%)
|
16
|
Fatigue Strength (MPa)
|
140
|
Poisson's Ratio
|
0.33
|
Shear Modulus (GPa)
|
27
|
Shear Strength (MPa)
|
290
|
Tensile Strength: Ultimate (UTS) (MPa)
|
480
|
Tensile Strength: Yield (Proof) (MPa)
|
310
|
2011 T4 Aluminum Thermal Properties
Property
|
2024-T4 Aluminum
|
Latent Heat of Fusion (J/g)
|
390
|
Maximum Temperature: Mechanical (°C)
|
200
|
Melting Completion (Liquidus) (°C)
|
640
|
Melting Onset (Solidus) (°C)
|
500
|
Specific Heat Capacity (J/kg-K)
|
880
|
Thermal Conductivity (W/m-K)
|
120
|
Thermal Expansion (µm/m-K)
|
23
|
2011 T4 Aluminum Electrical Properties
Property
|
2024-T4 Aluminum
|
Electrical Conductivity: Equal Volume (% IACS)
|
30
|
Electrical Conductivity: Equal Weight (% IACS)
|
90
|
2011 T4 Aluminum Alloy Composition
Element
|
2024-T4 Aluminum
|
Aluminum (Al) (%)
|
90.7 to 94.7
|
Bismuth (Bi) (%)
|
0
|
Chromium (Cr) (%)
|
0 to 0.1
|
Copper (Cu) (%)
|
3.8 to 4.9
|
Iron (Fe) (%)
|
0 to 0.5
|
Lead (Pb) (%)
|
0
|
Magnesium (Mg) (%)
|
1.2 to 1.8
|
Manganese (Mn) (%)
|
0.3 to 0.9
|
Silicon (Si) (%)
|
0 to 0.5
|
Titanium (Ti) (%)
|
0 to 0.15
|
Zinc (Zn) (%)
|
0 to 0.25
|
Zirconium (Zr) (%)
|
0 to 0.2
|
Residuals (%)
|
0 to 0.15
|