Applications:
High strength fabricated or machined items in aircraft industries, general engineering, machinery, military equipment, truck wheels. Screw machine products. Structural applications. Rivets.
Characteristic Properties:
Heat treatable alloy. Very good machining characteristics. High strength alloy with a strength slightly higher than 2014(A) and 2017A and 2030. High fatigue strength. Suitable for welding only by resistance welding. Corrosion resistance only with cladding or other protection.
BS L110(1971) Alloy L110 |
|
---|---|
Chemical Element | % Present |
Aluminium (Al) | balance |
Lead (Pb) | 0.05 max |
Nickel (Ni) | 0.05 max |
Tin (Sn) | 0.05 max |
Chromium (Cr) | 0.1 max |
Titanium + Zirconium (Ti+Zr) | 0.2 max |
Zinc (Zn) | 0.2 max |
Iron (Fe) | 0.5 max |
Silicon (Si) | 0.5 max |
Manganese (Mn) | 0.3 - 0.9 |
Magnesium (Mg) | 1.2 - 1.8 |
Copper (Cu) | 3.8 - 4.9 |
Aluminium alloy L110 - 2024 clad 1050A is covered by standard BS L110 (1971)
The most common temper for L110 - 2024 clad 1050A aluminium is:
L110 - 2024 clad 1050A aluminium is supplied as sheet and strip
Physical Property | Value |
---|---|
Density | 2.79 g/cm³ |
Melting Point | 640 °C |
Thermal Expansion | 23.10 x10^-6 /K |
Modulus of Elasticity | 73 GPa |
Thermal Conductivity | 121-193 W/m.K |
BS L110(1971) Sheet - 0.4mm to 0.8mm |
|
---|---|
Mechanical Property | Value |
Elongation A50 mm | 12 Min % |
Tensile Strength | 390 Min N/mm2 |
0.2% Proof Stress | 235 Min N/mm2 |