A high strength aerospace aluminium alloy with good resistance to stress-corrosion cracking.
SAE AMS 4050 Alloy 4050 |
|
---|---|
Chemical Element | % Present |
Aluminium (Al) | balance |
Chromium (Cr) | 0.04 max |
Other (Each) | 0.05 max |
Titanium (Ti) | 0.06 max |
Manganese (Mn) | 0.1 max |
Silicon (Si) | 0.12 max |
Iron (Fe) | 0.15 max |
Zirconium (Zr) | 0.08 - 0.15 |
Others (Total) | 0.15 max |
Copper (Cu) | 2 - 2.6 |
Magnesium (Mg) | 1.9 - 2.6 |
Zinc (Zn) | 5.7 - 6.7 |
Alloy AMS 4050 plate is supplied in temper T7451
Alloy AMS 4050 in temper T7451 is supplied as Plate
These Mechanical Properties are for AMS 4050 Plate in the T7451 temper
Thickness (mm) | Proof Strength (Min) | Tensile Strength (Min) | Elongation % (Min) |
Over 6.3 up to & incl. 51 | 441 | 510 | 9 |
Over 51 up to & incl. 76 | 434 | 503 | 8 |
Over 76 up to & incl. 102 | 427 | 496 | 6 |
Over 102 up to & incl. 127 | 421 | 490 | 5 |
Over 127 up to & incl. 152 | 414 | 483 | 4 |
Over 152 up to & incl. 178 | 407 | 476 | 4 |
Over 178 up to & incl. 203 | 400 | 469 | 4 |