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 |
