SPACE 2009
Quality Policy
AS 9120
لوحات/ طباقات
صاج
قضيب
أنابيب
6013
AMS 4347 / AlMg1Si0.8CuMn / 6013 / T4
| Chemical Properties | % Value |
| Silicon (Si) | 0,00 - 0,20 |
| Chromium (Cr) | 0,00 - 0,10 |
| Manganese (Mn) | 0,30 - 0,90 |
| Magnesium (Mg) | 1,20 - 1,80 |
| Copper (Cu) | 3,80 - 4,90 |
| Titanium (Ti) | 0,00 - 0,15 |
| Iron (Fe) | 0,00 - 0,30 |
| Zinc (Zn) | 0,00 - 0,25 |
| Aluminium (Al) | Balance |
| Physical Properties | Value |
| Density | 2,72 g/cm³ |
| Melting Point | 579 °C |
| Thermal Expansion | 21.7 x 10^-6 /K |
| Modulus of Elasticity | 71 GPa |
| Thermal Conductivity | 150 W/m.K |
| Electrical Resistivity | %38 IACS |
Alloy 6013 is a new medium strength aerospace alloy that provides improved corrosion resistance and formability for use in aerospace applications including primary aircraft structures.
ALLOY DESIGNATIONS
Aluminium alloy AMS 4347, 6013 has s imilarities to the following standard designations and specifications ;
Alloy 6013, UNS A96013, ASTM B209
TEMPER TYPES
6013 is supplied in a wide range of tempers:
- O - Soft
- T4 - Solution heat treated and naturaly aged to a substantially stable condition
- T6 - Solution heat treated and artificially aged
- T651 - Solution heat treated, stress relieved by stretching then artificially aged
SUPPLIED FORMS
6013 is supplied in plate, bar, round bar and sheet.
- Plate
- Sheet
- Round Bar / Bar
DELIVERY:
| Mechanical Properties | |||
| Thickness (mm) | Proof Strength (Min.) | Yield Strength (Min.) | Elongation A50 mm % |
| Over 38.1 up to & incl. 50.8 | 393 MPa | 455 MPa | %5 |
| Over 50,8 up to & incl. 76,2 | 393 MPa | 448 MPa | %4 |
| Over 76,2 up to & incl. 101,6 | 386 MPa | 448 MPa | %4 |
| Over 101,6 up to & incl. 127 | 379 MPa | 441 MPa | %4 |
| Over 127 up to & incl. 152,4 | 372 MPa | 434 MPa | %4 |
حساب الوزن