NON-HEAT TREATABLE (COMMON) ALLOYS
3003 (UNS A93003) is alloyed with 1.2% manganese to provide a tensile strength range of 17 to 30 KSI. Excellent workability, weldability, and corrosion resistance. Used for drawing, spinning, fuel tanks, sheet metal work and other applications where slightly higher strength than 1100 is required. Conforms to AMS QQ_A_250/2 and ASTM B209.
5005 (UNS A95005) is alloyed with .8% manganese to provide a tensile strength range of 17 to 30 KSI. Excellent workability, weldability, and corrosion resistance. Specified for applications comparable to 1100 and 3003 – where anodizing is required. Anodized finish matches that of architectural alloy 6063. Conforms to ASTM B209.
5052 (UNS A95052) is alloyed with 2.5% magnesium. Tensile strength range 31 to 44 KSI. Very good corrosion resistance, good workability, weldability and strength. Used for aircraft fuel tanks, storm shutters, refrigerator liners, utensils, electronic mounting plates and panels, fan blades, etc. Conforms to ASTM B209.
HEAT TREATABLE (STRONG) ALLOYS
2024 (UNS A92024) is alloyed with 4.5% copper. Tensile strength range 30 to 63 KSI. Fair workability and corrosion resistance. Forming operations are limited. Used for high strength structural and aircraft applications. Also available as Alclad for improved corrosion resistance. 2024 conforms to ASTM B209.
6061 (UNS A96061) is alloyed with 1.0% magnesium and .6 silicon. Tensile strength range 20 to 41 KSI. Good formability, weldability, and corrosion resistance. Used for engineering and structural applications, boats, furniture, transportation equipment, etc. Conforms to ASTM B209.
7075 (UNS A97075) are heavily alloyed with zinc with lesser amounts of magnesium, copper, and chromium. One of the strongest aluminum alloys, it uses parallels that of 2024 with 7075 selected when higher mechanical properties are desired. Forming operations are limited. All 7075 flat products conform to ASTM B209.
|Dimensions||12 × 12 × 1 in|