Professional Plain Aluminum Sheet 2024 Aluminum Sheet For Aircraft Tank
High quality cheap price 2024 Plain aluminium alloy plate suppliers 2024 aluminum sheet
2024 aluminum panels are widely used in aircraft structures (skin, skeleton, rib beams, bulkheads, etc.), rivets, missile components, truck hubs, propeller components and other structural components.2024 aluminium alloy is an aluminium alloy, with copper as the primary alloying element. It is used inapplications requiring high strength to weight ratio, aswell as good fatigue resistance. It is weldable onlythrough friction welding, and has averagemachinability.
The 2024 alloy aluminum plate is a typical hard aluminum alloy in the aluminum-copper-magnesium system, and its composition is reasonable and the comprehensive performance is good. This alloy is produced in many countries and is the most used in hard aluminum
Chemical composition of 2024 aluminum alloy plate
Silicon: 0.5%
Iron: 0.5%
Copper: 3.8-4.9
Manganese: 0.3-0.9
Magnesium: 1.2-1.8
Chromium: 0.10
Nickel:-
Zinc: 0.25
Titanium: 0.15
Other: 0.15
Aluminum: the rest
2024 aluminum alloy plate panels are widely used in aircraft structures (skin, skeleton, rib beams, bulkheads, etc.), rivets, missile components, truck hubs, propeller components and other structural components.
Hardness of 2024 aluminum plate alloy in different temper
2024-H112 hardness: about HB85
2024-T4 hardness: HB120~145
2024-T351 hardness: HB120~145
2024-0 hardness: about HB40
We can supply
Alloy: 1050 1060 1100 3003, 3105, 5052, 5005, 5754 5083 5182, 6061 6063 6082, 7075, 8011…
Temper: HO, H111,H12, H14, H24,H 32, H112, T4, T6, T5,T651
Surface:Mill/Emboss/Diamond/2bar/3bars/Bright
Thickness: 0.2mm to 300mm
Width: 30mm to 2300mm
Length:1000mm to 10000mm.
| Chemical Analysis of aluminum alloy Plate | ||||||||||
| Alloy | Si | Fe | Cu | Mn | Mg | Cr | Ni | Zn | Ti | Al |
| 1050 | 0.25 | 0.4 | 0.05 | 0.05 | 0.05 | - | - | 0.05 | 0.03 | Remains |
| 1060 | 0.25 | 0.35 | 0.05 | 0.03 | - | - | - | - | - | Remains |
| 1070 | 0.2 | 0.25 | 0.04 | 0.03 | 0.03 | - | - | - | - | Remains |
| 1100 | 0.95 | 0.95 | 0.05-0.2 | 0.05 | - | - | 0.1 | - | - | Remains |
| 1200 | 1 | 1 | 0.05 | 0.05 | - | - | - | 0.1 | 0.05 | Remains |
| 3003 | 0.6 | 0.7 | 0.05-0.2 | 1.0-1.5 | - | - | - | 0.1 | - | Remains |
| 5005 | 0.3 | 0.7 | 0.2 | 0.2 | 0.5-1.1 | 0.1 | - | 0.25 | - | Remains |
| 5042 | 0.2 | 0.35 | 0.15 | 0.2--.5 | 3.0-4.0 | 0.1 | - | 0.25 | 0.1 | Remains |
| 5052 | 0.25 | 0.4 | 0.1 | 0.1 | 2.2-2.8 | 0.15-0.35 | - | 0.1 | - | Remains |
| 5083 | 0.4 | 0.4 | 0.1 | 0.4-1.0 | 4.0-4.9 | 0.05-0.25 | - | 0.25 | - | Remains |
| 5754 | 0.4 | 0.4 | 0.1 | 0.5 | 2.6-3.6 | 0.3 | - | 0.2 | - | Remains |
| 6061 | 0.4-0.8 | 0.7 | 0.15-0.4 | 0.15 | 0.8-1.2 | 0.04-0.35 | - | 0.25 | - | Remains |
| 6063 | 0.2-0.6 | 0.35 | 0.1 | 0.1 | 0.45 | 0.1 | - | 0.1 | - | Remains |
| 6082 | 0.7-1.3 | 0.5 | 0.1 | 0.4-1.0 | 0.6-1.2 | 0.25 | - | 0.2 | - | Remains |
| 7050 | 0.12 | 0.15 | 2.0-2.6 | 0.1 | 1.9-2.6 | 0.04 | - | 5.7-6.7 | 0.06 | Remains |
| 7075 | 0.4 | 0.5 | 1.2-2.0 | 0.3 | 2.1-2.9 | 0.18-0.28 | - | 5.1-6.1 | 0.2 | Remains |
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