Applications:
High strength structural components: aircraft (e.g. fittings and wheels), military vehicles and bridges, forgings for trucks and machinery (hydraulic etc.). Weapons manufacture, structural applications.
Characteristic Properties:
Heat treatable alloy. High mechanical strength slightly higher than 2011 and 2017A.
BS 2L77(1971) Alloy 2L77 |
|
---|---|
Chemical Element | % Present |
Aluminium (Al) | balance |
Tin (Sn) | 0.05 max |
Lead (Pb) | 0.05 max |
Chromium (Cr) | 0.1 max |
Zinc (Zn) | 0.2 max |
Titanium + Zirconium (Ti+Zr) | 0.2 max |
Nickel (Ni) | 0.2 max |
Iron (Fe) | 0.5 max |
Magnesium (Mg) | 0.2 - 0.8 |
Silicon (Si) | 0.5 - 0.9 |
Manganese (Mn) | 0.4 - 1.2 |
Copper (Cu) | 3.9 - 5 |
Forging Stock: Cast billets and slabs for hot working and extruded bars, sections and hot-rolled plate for forging shall be supplied non-heat treated. Forgings: Unless otherwise agreed between the manufacturer and the purchaser and stated on the order, forgings shall be supplied solution treated and precipitation treated.
Aluminium alloy 2L77 - 2014A is covered by standard BS EN 4L77 (1971)
The most common temper for 2L77 - 2014A aluminium forging stock is:
2L77 - 2014A aluminium is supplied as forging stock made from cast billet, extruded stock or rolled plate.
Physical Property | Value |
---|---|
Density | 2.80 g/cm³ |
Melting Point | 640 °C |
Thermal Expansion | 22.8 x10^-6 /K |
Modulus of Elasticity | 73 GPa |
Thermal Conductivity | 134-155 W/m.K |
BS 2L77(1971) - |
|
---|---|
Mechanical Property | Value |
Elongation A50 mm | 6 Min % |
Hardness Brinell | 134 Min HB |
Proof Stress | 395 Min MPa |
Tensile Strength | 450 Min MPa |
This specification covers forging stock and forgings of aluminium-copper-magnesium-silicon-manganese alloy in the solution treated and precipitation treated condition. The values shown in the mechanical properties apply to test pieces prepared by forging covering extruded forging stock and forgings made from cast billets, hot-rolled plate and extruded stock in all sizes.