Plates
Sheets
Rod / Round Bar / Flat Bar
Tube / Extrusions / Profile
6262
AMS QQ-A-225/10 / AlMg1SiSn / 6262 / T9
Chemical Properties | % Value |
Silicon (Si) | 0,40 - 0,80 |
Chromium (Cr) | 0,04 - 0,14 |
Manganese (Mn) | 0,00 - 0,15 |
Magnesium (Mg) | 0,80 - 1,20 |
Copper (Cu) | 0,15 - 0,40 |
Titanium (Ti) | 0,00 - 0,15 |
Iron (Fe) | 0,00 - 0,70 |
Zinc (Zn) | 0,00 - 0,25 |
Aluminium (Al) | Balance |
Physical Properties | Value |
Density | 2,72 g/cm³ |
Melting Point | 582 °C |
Thermal Expansion | 21.8 x 10^-6 /K |
Modulus of Elasticity | 69 GPa |
Thermal Conductivity | 170 W/m.K |
Electrical Resistivity | %44 IACS |
Mechanical Properties | Value |
Proof Strength | 360 MPa |
Yield Strength | 390 MPa |
Elongation A50 mm | %6 |
Modulus of Elasticity | 69 GPa |
A medium strength aerospace aluminium alloy with, depending upon temper, Yield Strength of up to 35 ksi (240 MPa) and Tensile Strength of 42 ksi (290 MPa)
ALLOY DESIGNATIONS
Aluminium alloy QQ-A-250/11, 6061 has s imilarities to the following standard designations and specifications ;
Alloy 6061, UNS A96061, ASTM B209
AMS 4025, AMS 4026, AMS 4027
EN 4213, 3.3214
TEMPER TYPES
Alloy QQ-A-250/11, 6061 is supplied in a wide range of tempers:
- O - Soft
- T4 - Solution heat treated and naturaly aged to a substantially stable condition
- T42 - Solution heat treated and naturaly aged to a substantially stable condition
- T451 - Solution heat treated then stress relieved by stretching. Equivalent to T4.
- T6 - Solution heat treated and artificially aged
- T62 - Solution heat treated then artificially aged by the user
- T651 - Solution heat treated, stress relieved by stretching then artificially aged
SUPPLIED FORMS
6061 is supplied in plate, bar, round bar, tube, extrusıon and sheet.
- Plate
- Sheet
- Round Bar / Bar
- Tube / Extrusion
DELIVERY: