Availability: | |
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Quantity: | |
2024
HONESTY-AL
76061200
▍ Product Features
Alloy with copper as the main alloying element (Al-Cu alloy). The highest content of copper is about 3-5%.
Can be hardened heat treatment, high strength, commonly known as duralumin (typical 2A12)
Good heat resistance, good processability, good cutting performance
Poor corrosion resistance easy to be corroded (high CU content)
2××× series aluminum plate belongs to aviation aluminum material, which is not often used in conventional industry.
▍ Technical Parameters
Item | Aluminum Sheet / Plate |
Standard | GB/T3190-2008, GB/T3880-2006, ASTM B209, JIS H4000-2006 etc |
Grade | 2012, 2017, 2024 |
Temper | T3-T8/T351-T851 |
Tolerance | ±1% |
Surface Treatment | Mirrored, Brushed |
Processing Service | Bending, Punching,Cutting etc |
Edge | Mill edge, Cut edge |
Thickness | 0.1-200mm |
Width | 10-2200mm |
Customized | Yes |
Certificate | ISO9001 |
Package | Standard Seaworthy Wooden Pallet Packing |
MOQ | 6 Ton |
Sample | Available |
Delivery Time | 7-15 Working Days |
▍ Chemical Performance
Grade | Temper | Thickness (mm) | Tensile Strength (R/Mpa) | Yield Strength (R/MPa) | Elongation(%) | |
A50mm | A | |||||
2024 | O | >0.40~1.50 | ≤220 | ≤140 | 12 | |
>1.50~3.00 | 13 | |||||
>3.00~6.00 | ||||||
>6.00~9.00 | ||||||
>9.00~12.50 | ||||||
>12.50~25.00 | - | - | 11 | |||
T3 | >0.40~1.50 | 435 | 290 | 12 | 11 | |
>1.50~3.00 | 14 | - | ||||
>3.00~6.00 | 440 | 14 | - | |||
>6.00~12.50 | 13 | - | ||||
>12.50~40.00 | 430 | - | 11 | |||
>40.00~80.00 | 420 | - | 8 | |||
>80.00~100.00 | 400 | 285 | - | 7 | ||
>100.00~120.00 | 380 | 270 | - | 5 | ||
>120.00~150.00 | 360 | 250 | - | 5 | ||
T4 | >0.40~1.50 | 425 | 275 | 12 | - | |
>1.50~6.0 | 14 | - | ||||
T8 | >0.40~1.50 | 460 | 400 | 5 | - | |
>1.50~6.00 | 6 | - | ||||
>6.00~12.50 | 5 | - | ||||
>12.50~25.00 | 455 | - | 4 | |||
>25.00~40.00 | 395 | - | 4 | |||
F | >4.50~80.00 | - |
▍ Product Uses
2 series aluminum belongs to aviation aluminum, aluminum plate is mainly used in aircraft structure (such as skin, etc.), aerospace, weapons, engines, pistons, automobile body, ship hull and stress components.
▍ Product Features
Alloy with copper as the main alloying element (Al-Cu alloy). The highest content of copper is about 3-5%.
Can be hardened heat treatment, high strength, commonly known as duralumin (typical 2A12)
Good heat resistance, good processability, good cutting performance
Poor corrosion resistance easy to be corroded (high CU content)
2××× series aluminum plate belongs to aviation aluminum material, which is not often used in conventional industry.
▍ Technical Parameters
Item | Aluminum Sheet / Plate |
Standard | GB/T3190-2008, GB/T3880-2006, ASTM B209, JIS H4000-2006 etc |
Grade | 2012, 2017, 2024 |
Temper | T3-T8/T351-T851 |
Tolerance | ±1% |
Surface Treatment | Mirrored, Brushed |
Processing Service | Bending, Punching,Cutting etc |
Edge | Mill edge, Cut edge |
Thickness | 0.1-200mm |
Width | 10-2200mm |
Customized | Yes |
Certificate | ISO9001 |
Package | Standard Seaworthy Wooden Pallet Packing |
MOQ | 6 Ton |
Sample | Available |
Delivery Time | 7-15 Working Days |
▍ Chemical Performance
Grade | Temper | Thickness (mm) | Tensile Strength (R/Mpa) | Yield Strength (R/MPa) | Elongation(%) | |
A50mm | A | |||||
2024 | O | >0.40~1.50 | ≤220 | ≤140 | 12 | |
>1.50~3.00 | 13 | |||||
>3.00~6.00 | ||||||
>6.00~9.00 | ||||||
>9.00~12.50 | ||||||
>12.50~25.00 | - | - | 11 | |||
T3 | >0.40~1.50 | 435 | 290 | 12 | 11 | |
>1.50~3.00 | 14 | - | ||||
>3.00~6.00 | 440 | 14 | - | |||
>6.00~12.50 | 13 | - | ||||
>12.50~40.00 | 430 | - | 11 | |||
>40.00~80.00 | 420 | - | 8 | |||
>80.00~100.00 | 400 | 285 | - | 7 | ||
>100.00~120.00 | 380 | 270 | - | 5 | ||
>120.00~150.00 | 360 | 250 | - | 5 | ||
T4 | >0.40~1.50 | 425 | 275 | 12 | - | |
>1.50~6.0 | 14 | - | ||||
T8 | >0.40~1.50 | 460 | 400 | 5 | - | |
>1.50~6.00 | 6 | - | ||||
>6.00~12.50 | 5 | - | ||||
>12.50~25.00 | 455 | - | 4 | |||
>25.00~40.00 | 395 | - | 4 | |||
F | >4.50~80.00 | - |
▍ Product Uses
2 series aluminum belongs to aviation aluminum, aluminum plate is mainly used in aircraft structure (such as skin, etc.), aerospace, weapons, engines, pistons, automobile body, ship hull and stress components.