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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</strong> promising alloy. <br> <strong>Good corrosion</strong> resistance, good weldability, good cold processing, and has moderate strength. <br> <strong>The main alloy </strong>element of 5083 is magnesium, which has good forming performance, corrosion resistance, weldability and medium strength.
<strong>5052 represents</strong> the brand of the product, and the word "5" indicates that the modified product belongs to the aluminum-magnesium alloy product.<br> <strong> According</strong> to the chemical composition, it can be seen that the magnesium alloy content of the product is between 2.2-2.8%, and the density is 2.68. <br> <strong>Generally, </strong> enterprises take the median value of 2.5% magnesium alloy content in the processing process, so this series of aluminum plate can become AlMG2.5.<br>
<strong>7075-T6 aluminum</strong> alloy hardness is 150HB, belongs to the high hardness aluminum alloy. <br> <strong>7075T6 aluminum</strong> alloy is precision machined aluminum in the United States, one of the most commercially available alloys. <br> <strong>The main alloying </strong> element of 7075 series is zinc, which has strong strength, good mechanical properties and anode reaction. <br>
7075 aluminum alloy is a high-strength, heat-treatable alloy primarily composed of zinc as the main alloying element, along with magnesium, copper, and chromium. Known for its exceptional strength-to-weight ratio, it is one of the strongest commercially available aluminum alloys, widely used in aerospace, military, and high-stress structural applications. It features ultra-high strength, excellent fatigue resistance, good machinability, heat treatability, and surface treatment compatibility. Limitations include poor corrosion resistance compared to other aluminum alloys, limited weldability, and sensitivity to stress corrosion cracking. Typical applications include aircraft structural components, high-performance automotive and racing parts, military and defense equipment, mold tools, and sporting goods.
<strong>6063 aluminum</strong> alloy material. <br> <strong>The main alloy </strong> elements are magnesium and silicon, with excellent machining performance, excellent weldability, extrusion and electroplating, good corrosion resistance, toughness, easy to polish, color film, excellent anodic oxidation effect, is a typical extrusion alloy.
<strong>6082</strong> is a heat-treatable alloy with good formability, weldability, machinability and corrosion resistance. <br> <strong>It also has </strong> moderate strength and can maintain good operability after annealing. <br> <strong>It is mainly used</strong> in mechanical structure, including bars, plates, pipes and profiles.
<strong>6061 alloy </strong>are magnesium and silicon, which have moderate strength, good corrosion resistance, weldability and good oxidation effect.<br> Widely used in various industrial structural parts requiring a certain strength and high antibiotic corrosion, its main chemical composition: Cu:0.15-0.4; Si: 0.4-0.8; Fe: 0.7 -; Mn: 0.15; Mg: 0.8-1.2; Zinc: 0.25; Cr: 0.04-0.35; Ti: 0.15 -; <strong>6061 aluminum plate</strong> its state T6 and T651 difference is that in general, T6 internal stress will be relatively large, processing will be deformed, the most suitable for processing state should be T651, he is on the basis of T6 tensile, eliminate internal stress.
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