A high strength aerospace aluminium alloy offering good corrosion resistance.
SAE AMS QQ-A-225/9 Alloy QQ A 225/9 |
|
---|---|
Chemical Element | % Present |
Aluminium (Al) | balance |
Other (Each) | 0.05 max |
Others (Total) | 0.15 max |
Titanium (Ti) | 0.2 max |
Chromium (Cr) | 0.18 - 0.28 |
Manganese (Mn) | 0.3 max |
Silicon (Si) | 0.4 max |
Iron (Fe) | 0.5 max |
Copper (Cu) | 1.2 - 2 |
Magnesium (Mg) | 2.1 - 2.9 |
Zinc (Zn) | 5.1 - 6.1 |
Alloy QQ-A-225/9 is supplied in a range of tempers:
Alloy QQ-A-225/9 T6511 is supplied in bar/rod
Physical Property | Value |
---|---|
Density | 2.81 g/cm³ |
Melting Point | 635 °C |
Thermal Expansion | 23.5 x10^-6 /K |
Modulus of Elasticity | 72 GPa |
Thermal Conductivity | 134-160 W/m.K |
Electrical Resistivity | 40 % IACS |
SAE AMS QQ-A-225/9 Bar - 12.7mm to 101.6mm |
|
---|---|
Mechanical Property | Value |
Proof Stress | 455 Min MPa |
Tensile Strength | 531 Min MPa |
Elongation A50 mm | 7 Min % |
Mechanical Properties are for T651 temper Bar in diameters 12.7mm to 101mm