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 2L97(1971) Alloy L97 |
|
---|---|
Chemical Element | % Present |
Aluminium (Al) | balance |
Nickel (Ni) | 0.05 max |
Lead (Pb) | 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 L97 - 2024 is covered by standard BS 2L97 (1971)
The most common temper for L97 - 2024 aluminium plate is:
L97 - 2024 aluminium is supplied in the following forms:
Physical Property | Value |
---|---|
Density | 2790 g/cm³ |
Melting Point | 640 °C |
Thermal Expansion | 23.10 x10^-6 /K |
Modulus of Elasticity | 73000 GPa |
Thermal Conductivity | 121 W/m.K |
Thickness (mm) | Proof Strength (Min) | Tensile Strength (Min) | Elongation % (Min) |
Over 6 up to & incl. 12.5 | 280 | 430 | 10 |
Over 12.5 up to & incl. 25 | 280 | 430 | 10 |
Over 25 up to & incl. 40 | 280 | 420 | 9 |
Over 40 up to & incl. 63 | 270 | 410 | 9 |
Over 63 up to & incl. 90 | 270 | 410 | 8 |
Over 90 up to & incl. 115 | 270 | 400 | 8 |
Over 115 up to & incl. 140 | 260 | 390 | 7 |