Aluminum Alloy 7050 Data Sheet

ALUMINUM ALLOY 7050 GENERAL DESCRIPTION :

What is Alloy 7050?

The 7050 aluminum alloy is known for its high strength, toughness, and good stress corrosion resistance. It is widely used in aerospace for aircraft structures and other applications due to its excellent mechanical properties and corrosion resistance.

Main Alloy Chemistry Typical

Element

Si

Fe

Cu

Mn

Mg

Zn

Cr

Ti

Others 

Al

Maximum Content

0.12

0.15

2.0 - 2.6

0.10

1.9 - 2.6

5.7 - 6.7

0.04 - 0.15

0.06

0.15

Remainder

TYPICAL MECHANICAL DATA for 7050 ALUMINUM

Physical Performance Indicators

Tensile Strength (MPa)

Yield Strength (Mpa)

Elongation (%)

7050 - T7451

524

469

11

7050 - T7651

552

490

11

*LIMITATIONS OF LIABILITY AND DISCLAIMER: HDM shall not be liable for any damages arising from the use of the information contained in this document, or for the applicability of this document to the described “application”. The provided information and data are believed to be accurate to the best of our knowledge, but all data should be considered as typical values only. They are for reference and general information purposes, and are not recommended for specification, design, or engineering purposes. HDM does not provide any warranty, implied or expressed, regarding the creation or accuracy of the data provided in this document.

Product Capacities of Alloy 7050

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