The 7010 T7651 aluminum alloy offers high strength, durability, and excellent mechanical properties. Belonging to the aluminum-zinc alloy class, this material is especially used in aerospace, aviation, and structural applications requiring high performance. The T7651 temper provides the alloy with high durability, stress resistance, and hardness through specialized heat treatments, while also allowing the material to be machinable. These features make the 7010 T7651 alloy ideal for heavy-duty components used in demanding conditions.

The suitability of the 7010 T7651 aluminum alloy for anodizing is limited. Its high zinc content inhibits the formation of an effective oxide layer during the anodizing process, making it difficult to protect the alloy through anodization. Instead, other coating methods are generally preferred to protect the alloy. In terms of weldability, 7010 T7651 requires careful processing during welding. The high zinc content can increase the risk of cracking during welding, so specialized welding techniques and appropriate filler materials should be used to minimize this risk.

In terms of bending and forming, 7010 T7651 requires careful handling due to its high strength. However, with proper processing techniques, bending and forming operations can be successfully carried out. Additionally, the 7010 T7651 alloy can be used in high-vibration environments. Its high elastic modulus and durability make it suitable for engine parts, chassis, and other components in the automotive and aerospace sectors.

Regarding corrosion resistance, the 7010 T7651 aluminum alloy may have some limitations compared to other aluminum alloys due to its high zinc content. However, these limitations can be overcome, and the corrosion resistance of the alloy can be enhanced with proper surface treatments and coatings. Advantages of the 7010 T7651 alloy include high strength, durability, and light weight, while its disadvantages include limited corrosion resistance and welding difficulties.

MATERIAL COMPOSITION STANDARDS

The 7010 T7651 alloy can be produced according to the following standards:
• 7010 T7651 Sheet/Plate; AMS 4204, ISO AlZn6MgCu, WNR 3.4394, UNS A97010, EN 2684, DTD 5120, ASTM B209
 

Characteristic Properties of 7010 T7651: 

• Strength: Very good
• Machinability: Good
• Weldability: Poor
• Formability: Poor
• Corrosion Resistance: Very good
• Heat Treatment: Yes
   

Common Applications of 7010 T7651: 
Used in mold and model making,
Structural components in aircraft fuselages,
Used in aircraft wings and structural parts.
 

STOCK
We provide 7010 T7651 in sheet form.

• Sheet/Plate