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Help CenterHigh Strength Aluminium Alloy Plate 7075 7050 T3 T4 T6 T651 3mm 5mm 6mm 15mm
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highest strength 7075 7050 T3 T4 T6 T651 3mm 5mm 6mm 15mm aluminium alloy plate for aerospace industry
7075 aluminium alloy plate is an aluminium alloy, with zinc as the primary alloying element. It is strong, with a strength comparable to many steels, and has goodfatigue strength and average machinability.
7075 alloy aluminum plate is made of one of the strongest of the aluminum alloys. Its use parallels that of 2024, with 7075 selected when higher mechanical properties are desired. 7075 aluminum is an aluminum-zinc alloy with 1%-8% zinc in addition to small amounts of magnesium and small quantities of copper and chromium.
7075-T6 Bare Aluminum alloy sheet | aluminium alloy Plate is primarily used in aerospace industry, often referred to as the Strongest Aluminum grade. Unlike the Clad, the Bare Sheet isn't coated with an additional aluminumlayer. Alloy 7075 has the strength of many steels, while retaining aluminum's lightweight qualities.
In terms of strength, 7075 Aluminum is near the top of the list among aluminum alloys manufactured for the needs of consumer and industrial markets. Among other 7XXX alloys, alloy 7075 exists as a standard with a solid mix of properties suitable for aircraft and aerospace applications. In particular, this alloy utilized in various forms, including as 7075 aluminum bar, is well-suited for use in parts that endure high stress levels. The strength properties of alloy 7075 are beneficial for the manufacture of items such as aircraft structures, military grade rifles, bicycle parts and equipment, and plastic industry molds.
| 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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