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Strength in numbers

Aluminium Alloy   |   BS-L

L170 T6511 Bar

AerospaceL170 T6511 Commercial7075

Aluminium alloy L170 – 7075 is a very high strength alloy used for highly stressed components requiring maximum strength with low residual stress.
The standard specifying this grade has been superseded by BSEN 2127.


Chemical Composition

BS L170(1989)
Alloy L170
Chemical Element % Present
Aluminium (Al) balance
Other (Each) 0.05 max
Others (Total) 0.15 max
Titanium (Ti) 0.2 max
Titanium + Zirconium (Ti+Zr) 0.25 max
Chromium (Cr) 0.18 - 0.28
Manganese (Mn) 0.3 max
Silicon (Si) 0.4 max
Iron (Fe) 0.5 max
Copper (Cu) 1.2 - 2
Magnesium (Mg) 2.1 - 2.9
Zinc (Zn) 5.1 - 6.1

Alloy Designations

Aluminium alloy L160 has similarities to the following standard designations and specifications but may not be a direct equivalent:

7075


Temper Types

The most common temper for L160 – 7075 aluminium is:

  • T6511

Supplied Forms

L160 – 7075 aluminium is supplied in Bar and Extruded Sections.

  • Bar
  • Extrusions

Generic Physical Properties

Physical Property Value
Density 2.81 g/cm³
Melting Point 635 °C
Thermal Expansion 23.5 x10^-6 /K
Modulus of Elasticity 72 GPa
Thermal Conductivity 134-160 W/m.K
Electrical Resistivity 40 % IACS
'Typical' Physical Properties are given

Mechanical Properties

These Mechanical properties are for Bar in the T6511 temper

Diameter (mm) Proof Strength (Min) Tensile Strength (Min) Elongation % (Min)
Up to & incl. 10 480 540 4
Over 10 up to & incl. 100 520 580 4
Over 100 up to & incl. 150 490 550 4