2014 T6510 aluminum alloy is a high-strength wrought alloy belonging to the Al-Cu-Mg (Aluminum-Copper-Magnesium) system and is commonly preferred in aerospace and heavy engineering applications. This alloy stands out among the 2000 series aluminum alloys due to its high mechanical strength. The T6510 temper indicates that the material has been solution heat treated, stress relieved, and artificially aged to increase its strength. As a result, the material provides reliable performance especially in structural components subjected to high loads.

The strength of the 2014 T6510 alloy is very high, making it suitable for applications requiring high tensile strength. In this respect, it generally provides higher strength compared to the 2024 alloy, although it may exhibit slightly lower toughness. Compared with the 7075 alloy, it may offer better machinability in some cases, while 7075 typically provides higher maximum strength. Because of these characteristics, the 2014 alloy is often preferred in mechanical components operating under high loads.

In terms of corrosion resistance, the 2014 alloy does not offer as high resistance as pure aluminum or the 5000 and 6000 series alloys. For this reason, it is generally used with anodizing, painting, or protective surface coatings. For example, the 6061 alloy typically provides better natural corrosion resistance. However, when appropriate surface treatments are applied, the 2014 alloy can be safely used even in harsh environmental conditions.

In terms of machinability, the 2014 T6510 alloy demonstrates very good performance and offers advantages particularly in machining operations. In this respect, it may provide machinability similar to or sometimes better than the 2024 alloy. However, its bending capability is limited, and forming operations are usually performed in the annealed condition. In addition, the alloy is generally considered poor in weldability, and mechanical fastening or riveting is usually preferred in most applications.

Regarding vibration and fatigue behavior, the 2014 alloy performs well and can be used in components operating under dynamic loads. Therefore, it is widely used in the aerospace, defense, automotive, and heavy machinery industries. Aircraft structural components, structural fasteners, high-strength machine parts, and forged components are among the common applications of this alloy.

STANDARDS OF MATERIAL COMPOSITION

2014 T6510 can be supplied according to the following standards.
• 2014 T6510 Cold Drawn Tube; AMS 4121, ASTM B210, UNS A92014, ASTM B928, BS L 168, WNR 3.1255, ISO AlCu4SiMg
• 2014 T6510 Extruded Round Bar; ASTM B221, UNS A92014, EN 2635, WNR 3.1255, ISO AlCu4SiMg
• 2014 T6510 Extruded Flat Bar; ASTM B221, UNS A92014, EN 2635, WNR 3.1255, ISO AlCu4SiMg
• 2014 T6510 Extruded Wire Rod; ASTM B221, UNS A92014, EN 2635, WNR 3.1255, ISO AlCu4SiMg
 

Characteristic Properties of 2014 T6510:

• Strength: Very good
• Machinability: Medium to high
• Weldability: Low (Filler welding is the best option)
• Formability: Good
• Corrosion Resistance: Poor (Improves with coating)
• Heat Treatment: Yes

Some Well-Known Applications of 2014 T6510:
In weapon manufacturing and areas requiring high-strength materials,
In the defense industry and as armored vehicle equipment,
Additionally, it is mainly used in the aerospace industry.
 

STOCK
We manufacture and supply 2014 T6510 in round bar/flat bar and tube/profile forms.

• Round Bar / Flat Bar
• Tube / Profile