| Payment Type: | L/C,T/T |
| Incoterm: | FOB,CFR,CIF,EXW |
| Min. Order: | 5 Ton |
| Transportation: | Ocean |
| Port: | Tianjin Port,Qingdao Port,Shanghai Port |
Place Of Origin: China
Whether Alloy: Is Alloy
Material: 7000 Series
Surface Treatment: Coated
Annealed State: O - H112
Tolerance: ±1%
Processing Service: Bending, Decoiling, Welding, Punching, Cutting
Model NO.: 7 series, 7475
Surface Treatment: Powder Coating
Technique: Cold Drawn
Customized: Yes
Application: Transportation Tools, Door & Window, Glass Wall, Heat Sink, Decorations
| Selling Units | : | Ton |
| Package Type | : | Wood Package, Transportion by Container |
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7475 aluminum alloy (Adirium) is a wrought alloy with high zinc weight percentage. It also contains magnesium, silicon and chromium.[1]
7475 alloy can not be welded. It has more spring back because of its strength. It has high machinability.
The 7475 aluminum alloy coil is a high-strength aluminum alloy that is commonly used in aerospace applications. It is a precipitation-hardened alloy that contains Copper, magnesium, and zinc as its primary alloying elements.
7475 aluminum coil is a form of this alloy that is produced by rolling the alloy into thin sheets or coils. It is typically used in applications that require high strength and toughness, such as aircraft structures, missile components, and spacecraft parts.
Some of the key features of 7475 aluminum coil include its high strength-to-weight ratio, excellent fatigue resistance, and good corrosion resistance. It is also relatively easy to weld and has good machinability.
Overall, 7475 aluminum coil is a versatile and reliable material that is well-suited for a wide range of aerospace and other high-performance applications.
| No. | Alloy States | |||||||||||||||
| Chemical composition.% | ||||||||||||||||
| Si | Fe | Cu | Mn | Mg | Cr | Ni | Zn |
| Ti | Zr | Other | AI | ||||
|
| Single | Total | ||||||||||||||
| 1 | 3003 | 0.6 | 0.7 | 0.05-0.20 | 1.0-1.5 | - | - | - | 0.1 | - | - | - | 0.05 | 0.15 | Rem | - |
| 2 | 4032 | 11.0-13.5 | 1 | 0.50-1.30 | - | 0.8-1.3 | 0.1 | 0.50-1.30 | 0.25 | - | - | - | 0.05 | 0.15 | Rem | - |
| 3 | 4043 | 4.5-6.0 | 0.8 | 0.3 | 0.05 | 0.05 | - | - | 0.1 | - | 0.2 | - | 0.05 | 0.15 | Rem | - |
| 4 | 4047 | 11.0-13.0 | 0.8 | 0.3 | 0.15 | 0.1 | - | - | 0.2 | - | - | - | 0.05 | 0.15 | Rem | - |
| 5 | 5052 | 0.25 | 0.4 | 0.1 | 0.1 | 2.2-2.8 | 0.15-0.35 | - | 0.1 | - | - | - | 0.05 | 0.15 | Rem | - |
| 6 | 5754 | 0.4 | 0.4 | 0.1 | 0.5 | 2.6-3.6 | 0.3 | - | 0.2 | Mn+Cr:0.1-0.6 | 0.15 | - | 0.05 | 0.15 | Rem | - |
| 7 | 5182 | 0.2 | 0.35 | 0.15 | 0.20-0.50 | 4.0-5.0 | 0.1 | - | 0.25 | - | 0.1 | - | 0.05 | 0.15 | Rem | - |
| 8 | 5083 | 0.4 | 0.4 | 0.1 | 0.40-1.0 | 4.0-4.9 | 0.05-0.25 | - | 0.25 | - | 0.15 | - | 0.05 | 0.15 | Rem | LF4 |
| 9 | 6061 | 0.40-0.8 | 0.7 | 0.15-0.40 | 0.15 | 0.8-1.2 | 0.04-0.35 | - | 0.25 | - | 0.15 | - | 0.05 | 0.15 | Rem | LD30 |
| Alloy States | Thickness (mm) | Tensile strenght (Rm/Mpa) | Yield Strength (Rp0.2 Mpa) | Elongation A50(%) | Bending Radius |
| 5052 H32 | >0.20-0.50 | 210-260 | 130 | 5 | 0.5t |
| >0.50-1.50 | 6 | 1.0t | |||
| >1.50-3.00 | 7 | 1.5t | |||
| >3.00-6.00 | 10 | 1.5t | |||
| 5052 H34 | >0.20-0.50 | 230-280 | 150 | 4 | 0.5t |
| >0.50-1.50 | 5 | 1.5t | |||
| >1.50-3.00 | 6 | 2.0t | |||
| >3.00-6.00 | 7 | 2.5t | |||
| 5052 H36 | >0.20-0.50 | 250-300 | 180 | 3 | 1.5t |
| >0.50-1.50 | 4 | 2.0t | |||
| >1.50-3.00 | 5 | 3.0t | |||
| >3.00-6.00 | 6 | 3.5t | |||
| 5052 H38 | >0.20-0.50 | 270 | 210 | 3 | - |
| >0.50-1.50 | 3 | - | |||
| >1.50-3.00 | 4 | - |
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