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Xar 400 500 Wear Resistant Steel Plate
XAR is available in various grades from
300 HBW to 600 HBW and plate thicknesses
from 1/6” to 4” (4 to 100 mm), tailored to particular applications, e.g.
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300 HBW to 600 HBW and plate thicknesses
from 1/6” to 4” (4 to 100 mm), tailored to particular applications, e.g.
Alloys 309 and 309S are austenitic chromium-nickel stainless steels that are often used for higher temperature applications. Owing to their high chromium and nickel content, Alloys 309 and 309S are highly corrosion resistant, have exceptional resistance to oxidation, and great heat resistance while offering good strength at room and elevated temperatures. The only significant difference between 309 and 309S is the carbon content, Alloy 309S has a much less carbon composition which minimizes carbide precipitation and improves weldability.
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6082 is a heat-treatable alloy with good formability, weldability, machinability and corrosion resistance.
It also has moderate strength and can maintain good operability after annealing.
It is mainly used in mechanical structure, including bars, plates, pipes and profiles.
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It also has moderate strength and can maintain good operability after annealing.
It is mainly used in mechanical structure, including bars, plates, pipes and profiles.
ASTM High yield strength steel plate A514 Grade K is used where a weldable, machinable, very high strength steel is required to save weight or meet ultimate strength requirements. Alloy steel plate A514GrK is normally used as a structural steel in building construction, cranes, or other large machines supporting high loads.
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The mechanical properties of 2024-T3 aluminum alloy can be significantly improved after heat treatment.
2024 is a typical duralumin alloy in the aluminum-copper-magnesium system.
It is a heat-treatable alloy with high strength, easy to work, easy to turn, and moderate corrosion resistance.
Main applications: aircraft structure, rivets, truck wheels, propeller components and other structural parts.
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2024 is a typical duralumin alloy in the aluminum-copper-magnesium system.
It is a heat-treatable alloy with high strength, easy to work, easy to turn, and moderate corrosion resistance.
Main applications: aircraft structure, rivets, truck wheels, propeller components and other structural parts.
The main alloying elements in 6061 alloy are magnesium and silicon, which have moderate strength, good corrosion resistance, weldability and good oxidation effect.
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 -; 6061 aluminum plate 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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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 -; 6061 aluminum plate 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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