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High seawater proof 6061 T6 aircraft grade aluminum plate sheets manufacturer
6061 t6 aircraft grade aluminum plate sheets is an aluminium alloy with magnesium and traces of manganese and chromium.
It is highly resistant to attack by seawater and industrial chemicals.Alloy 5083 retains exceptional strength after welding.
It has the highest strength of the non-heat treatable alloys, but is notrecommended for use in temperatures in excess of 65°C.
6061 is commonly used for the following:
Name | 6061 t6 aircraft grade aluminum plate sheets |
Usage | Shipping building, aircraft, train body and etc |
Material | 6082 t6 5083-h116 / 5083-h321 2000X8000 MM 2000x6000mm 2-300mm thick |
Thickness | 2.5-300mm |
Length | 5.8-12M |
T6 temper 6061 has an ultimate tensile strength of at least 290 MPa (42,000 psi) and yield strength of at least 240 MPa (35,000 psi
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 |