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 |