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<strong>5083 belongs</strong> to Al-Mg-Si alloy, which is widely used, especially in the construction industry.<br> <strong>It is the most promising alloy. </strong>Good corrosion resistance, good weldability, good cold processing, and has moderate strength.<br> <strong>5083 is magnesium, </strong>which has good forming performance, corrosion resistance, weldability and medium strength. <br> <strong>5083 aluminum </strong>is one of the most widely used antirust<br>
<strong>7075 aluminum </strong>alloy is a cold - treated forging alloy, high strength, far better than mild steel. <br/> <strong>7075 </strong>is one of the strongest alloys commercially available. <br/> <strong>Under heat treatment</strong>, can achieve very high strength characteristics.<br/> <strong>The alloy </strong>also has good mechanical properties and anode reaction.<br/> <strong>Aluminum</strong> is a silver-white light metal, relatively soft, density 2.7g/cm3, melting point 660.4℃, boiling point 2467℃, aluminum and aluminum alloys have many excellent physical properties, has been very widely used.
<strong>6061</strong> is a common duralumin with good machinability and moderate strength. <br> <strong>6061</strong> is a heat-treatable alloy with good formability, weldability, machinability, and moderate strength.<br> <strong>It can still </strong>maintain good operation after annealing.<br> <strong>If there is a certain </strong> amount of manganese and chromium, the bad effect of iron can be neutralized.
The main alloying elements in 6161 alloy are magnesium and silicon, which provide moderate strength, good corrosion resistance, weldability, and oxidation resistance. It is widely used in various industrial structural parts requiring certain strength and high corrosion resistance. Its typical chemical composition is: Cu: 0.15–0.4%; Si: 0.4–0.8%; Fe: ≤0.7%; Mn: 0.15%; Mg: 0.8–1.2%; Zn: ≤0.25%; Cr: 0.04–0.35%; Ti: ≤0.15%. The difference between T6 and T651 tempers for 6161 aluminum plate is that T6 typically retains higher internal stress and may deform during machining, while T651—achieved by stretching after T6 treatment—effectively relieves internal stress, making it more suitable for precision machining.
<strong> 2024-T3aluminum </strong> alloy can be significantly improved after heat treatment. <br/> <strong>2024</strong> is a typical duralumin alloy in the aluminum-copper-magnesium system. <br/> <strong>It is a heat-treatable alloy </strong>with high strength, easy to work, easy to turn, and moderate corrosion resistance.<br/> Main applications: aircraft structure, rivets, truck wheels, propeller components and other structural parts.
<strong>6082</strong> is a heat-treatable alloy with good formability, weldability, machinability and corrosion resistance.<br/> <strong>It also</strong> has moderate strength and can maintain good operability after annealing. <br/> <strong>It is mainly</strong> used in mechanical structure, including bars, plates, pipes and profiles. <br/> <strong>This alloy</strong>has similar but not identical mechanical properties to alloy 6061, and its -T6 state has higher mechanical properties.
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