Hard Aircraft Aluminum Plate High Tensile Strength Alloy Type 2124 Grade
Hard Aircraft Aluminum Plate High Tensile Strength Alloy Type 2124 Grade
2124 Alloy is a typical hard aluminum alloy in the aluminum-copper-magnesium series. The characters of this material are with high strength and with certain heat resistance, it can be used as a working part below 150℃. The strength is higher than 7075 if the Working temperature above 125℃. The formability is better under hot, annealing and quenching conditions. And the effect of heat strengthened is significantly. The alloy 2124 are widely used in aircraft structures, rivets, truck hubs, propeller components and other structural components.
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Chemical Composition WT(%) |
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Silicon |
Iron |
Copper |
Magnesium |
Manganese |
Chromium |
Zinc |
Titanium |
Others |
Aluminum |
|
0.2 |
0.3 |
3.8~4.9 |
1.2~1.8 |
0.3~0.9 |
0.1 |
0.25 |
0.15 |
0.15 |
Balance |
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Typical Mechanical Properties |
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Thickness (mm) |
Tensile Strength (Mpa) |
Yield Strength (Mpa) |
Elongation (%) |
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0.3~350 |
345~425 |
245~275 |
≥7 |
Applications
Airplane Structurals
Precision Parts
Wing tension members
Automotive Parts
Our Advantage
Inventory and Delivery
We have enough product in stock, we can offer enough material to customers. The lead time can be within 7 days for stock materil.
Quality
All the product are from the biggest manufacturer, we can offer the MTC to you. And we can also offer Third-Party test report.
Custom
We have cutting machine, custom size are available.
