7050 ALUMINUM SHEET
Zinc is the main alloying element of 7050 series aluminum alloys, and the addition of magnesium to alloys containing 3%-75% of zinc results in the formation of reinforced alloys. The remarkable effect of MgZn2 makes the heat treatment effect of this alloy far better than that of Al-Zn binary alloy. Increase the content of zinc and magnesium in the alloy, the tensile hardness will have to be further improved, but its resistance to stress corrosion and corrosion resistance to peeling will be It decreases with age. After heat treatment, very high strength characteristics can be achieved. Small amounts of copper-chromium and other alloys are usually added to this series. The 7050-T7451 aluminum alloy is the best of the aluminum alloys in this series and is considered to be the strongest. Mild steel. This alloy has good mechanical properties and anodic reaction. Mainly used in aerospace, mold processing, machinery and equipment, jigs and fixtures, especially for aircraft structures and other high stress structures requiring high strength and corrosion resistance. It is especially used in aircraft manufacturing structures and other high stress structures that require high strength and corrosion resistance.
7050 aluminum sheet is primarily used in the aerospace industry, but can also be used in other applications where high strength aluminum is required.
Aircraft structural components. For extrusion, free forging and die forging of heavy plate. Can also be used in a variety of dies, fixtures, machinery and high-end aluminum bike frames.