- Specifications of 7050 Aluminium Alloy(Aluminum alloy 7050)
1. Type: Sheet/Plate, Coil, Tube, Extension, Parts
2. Grade:7050
3. Tempers: T7651, T7451, T74511
4. Thickness: 4-260 mm
5. Width: 1200-3800 mm
6. Standard: AMS 4201, AMS 4050, AMS 4342
7. Delivery Time: 15 – 30 Days
Aluminum alloy 7075 Features
High fracture toughness
High strength
Hgh resistance to corrosion
Fatigue resistance.
Chemical Composition Limits
Weight% Al Zr Si Fe Cu Mn Mg Cr Zn Ti Other Each Others Total Alloy 7050 min 87.3 0.08 - - 2 - 1.9 - 5.7 - - - Alloy 7050 max 90.3 0.15 0.12 0.15 2.6 0.1 2.6 0.04 6.7 0.06 0.05 0.15
Aluminium Alloy 7050 Physical Properties
Material Temper Thickness Tensile Strength (ksi) Yield Strength (ksi) Elongation in 2" % Alloy 7050 Plate (longitudinal) T7451 <2.0 74 64 10 Alloy 7050 Plate (longitudinal) T7451 2.0 -3.0 73 63 9 Alloy 7050 Plate (longitudinal) T7451 3.0 - 4.0 72 62 9 Alloy 7050 Plate (longitudinal) T7451 4.0 - 5.0 71 61 9 Alloy 7050 Plate (longitudinal) T7651 0.25 - 1.0 76 66 9 Alloy 7050 Plate (longitudinal) T7651 1.0 - 1.5 77 67 9 Alloy 7050 Plate (longitudinal) T7651 1.5 - 2.0 76 66 9 Alloy 7050 Plate (longitudinal) T7651 2.0 - 3.0 76 66 8
Aluminum alloy 7050 is used in a wide range of aerospaceMaterial Temper Tensile Strength (ksi) Yield Strength (ksi) Elongation in 2" % Alloy 7050 Bar (AMS 4340) T76511 79 69 7 Alloy 7050 Bar (AMS 4340) T73511 70 60 8 Alloy 7050 Bar (AMS 4342) T74511 73 63 7
Fuselage frames
Bulkheads
Wing skins
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7050 Aluminium Alloy 7050 Aluminum Bar
7050 Aluminium alloy is widely used for aircraft structure applications like fuselage frames, bulkheads, and wing skins. Which featured with high fracture toughness,high strength, high resistance to corrosion and fatigue resistance.
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