Highly stressed aircraft parts use aluminum sheet aerospace and
aviation 7075 aluminum plate supplier
Alloy 7075 aluminum plates are the outstanding member of the 7xxx
series and remains the baseline among the highest strength alloys
available. Zinc is the primary alloying element giving it strength
comparable to steel. Temper T651 possesses good fatigue strength,
fair machinability, resistance welding and corrosion resistance
ratings. Alloy 7075 in temper T7x51 has superior stress corrosion
resistance and replaces the 2xxx alloy in the most critical
applications. It is widely used by the aircraft industry with the
typical specifications of ASTM B209, AMS-QQ-A-250/4, as well as
many end users requirements.
One of the strongest of the aluminum alloys, 7075 aluminum plate
provides great performance and superior corrosion resistance for
our customers.
Zinc is the primary alloying element of 7075 with 1 to 8 percent of
the material composed of zinc. It is precipitation hardened to
strength levels comparable to steel. With 7075’s T651 temper, it
has been solution heat treated followed by a minimal stretching to
reduce stresses in the material. The material has also been
artificially aged to allow the alloying elements to precipitate out
of the material to give it immediate maximum strength
| 7075 aircraft aluminum plate aerospace plate aluminum mechanical
properties |
| Alloy|Temper | Tensile Strength(Mpa) | Yield Strength(Mpa) | Elongation |
| 7075 O | 280 | 140 | 9-10% |
| 7075 T6 | 510-540 | 430-480 | 5-11% |
| 7075 T651 | 570 | 500 | 3-9% |
| 7075 T7 | 505 | 435 | 13% |
XIAOXIAN RUIYI Can manufacture aluminum alloy plate sheet as
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.
Aluminium plate | aluminum alloy sheet | Aluminum tread plates |
Aluminum coils | Aluminum Foils| Aluminium diamond plate sheet |
Aluminum checker plates | Aluminium chequer plate sheet
| 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 |
