Xiaoxian Ruiyi Commercial Trade Co., Limited
Xiaoxian Ruiyi Commercial Trade Co., Limited
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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 |