
Add to Cart
High Strength Corrosion Resistance Aircraft Aluminum Sheet
Alloy: 7075-t7351 A7075 B95 76528 A97075
Temper : T7651 ,T7351,t651 t7651 O
Features of 7075 T7351 aluminum
7075-t7351 A7075 B95 76528 A97075 aluminum Mill Test Certificate (Standard:EN485-2008)
Chemical Composition | ||||||||||
Range | Si | Fe | Cu | Mn | Mg | Cr | Zn | each | total | Aluminum |
Min. | - | - | 1.2 | - | 2.1 | 0.18 | 5.1 | - | - | Allowance |
Max | 0.40 | 0.50 | 2.0 | 0.30 | 2.9 | 0.28 | 6.1 | 0.05 | 0.15 |
7075-t7351 A7075 B95 76528 A97075 aluminum Mechanical properties
Tensile Strength Rm(Mpa) | Yield Strength Rp0.2(Mpa) | Elongation A50mm(%) |
561-576 | 500-512 | 9.2-12.0 |
7075-t7351 A7075 B95 76528 A97075 Aluminum stretching plate specification
Alloy Series | TypIcial Alloy | Typcial Tempe | Thickness (MM) | Width (MM) | Length (MM) |
7××× | 7075-t7351 A7075 B95 76528 A97075 | T7651 T7251,T651 | 4~12 | 1000~2600 | 2000-24000 |
7xxx | 7075-t7351 A7075 B95 76528 A97075 | 12~260 | 1000~3800 | 2000~38000 |
The application of Aluminum 7075 in aerospace
Item | Grade | Temper | Application |
7 | 7075-t7351 A7075 B95 76528 A97075 | T651, T7651,O,T7351 | Airplane structure component required high strength, moderate toughness and moderate corrosion resistance. |
7075 aircraft aluminum plate
About JIMA Equipment
7075 aluminum standard package photos: