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2618 ALUMINIUM - UNS A92618

2618 ALUMINIUM

2618 Aluminium (UNS A92618) is a high strength aluminium alloy which contains both copper and magnesium and can be used in higher temperature applications

Density

2.75g/cm3

Typical Applications

Related Specifications

Aerospace & Defence

Commonly used for pistons and rotating aircraft components due to it's high strength at elevated temperatures

UNS A92618

EN 573

EN AW-2618

BS H16

A-U2GN

Chemical Composition (Wt %)

   Al Si Fe Cu Mn Mg Ni Zn Ti Zr+Ti Pb+Sn
Min Bal - 0.90 1.80 - 1.20 0.80 - - - -
Max Bal 0.25 1.4 2.70 0.20 1.80 1.40 0.10 0.20 0.25 0.05

Typical Mechanical Properties

  0.2% Proof Stress Tensile Strength Elongation Reduction of area Typical Hardness (HBW)
Content 340 420 7 - -

Hardness after Heat Treatment

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