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ALUMINIUM
ALUMINIUM
Uses for the 6013 include primary structural applications, including body panels, leading and trailing edges, and engine hoods. It is a new medium strength aluminium alloy that provides improved corrosion resistance and formability for use in aerospace applications, including primary aircraft structures.
Alloy | Fe (%) | Mn (%) | Mg (%) | Cu (%) | Zn (%) | Ti (%) | Si (%) | Cr (%) | Al (%) |
---|---|---|---|---|---|---|---|---|---|
6013 | 0-0.50 | 0.20-0.80 | 0.80-1.20 | 0.60-1.10 | 0-0.25 | 0-0.10 | 0.60-1.00 | 0.00-0.10 | Balance |
Temper | Yield Strength (MPa) min-max | Tensile Strength (MPa) min-max | Elongation (50%) min-max | Hardness (brinel) min-max |
---|---|---|---|---|
T6 | 379 | 392 | 5 | 130 |