Audited Supplier
7050
Metal
Hot Forging
Gravity Casting
Aviation
Aluminium
Quenching
Zinc/Chrome Plating,Anodizing
+/-0.2mm
ANSI
CE, ISO 9001:2008
OEM ODM
Chalco Aluminum
Export Standard Wooden Pallet or as Your Requsts
According to Customer Requirement
Henan China
7218100000
Product Description
7050 T7452 Aircraft Aerospace Aviation Aluminum Alloy Forgings
7050 Alloy increased the content of zinc and copper, increased the ratio of zinc to magnesium, and replaced chromium with zirconium as a grain refiner, and greatly reduced the content of iron and silicon. These improvements and over aging treatment make the 7050 type alloys have good comprehensive properties such as good toughness, high fatigue strength and good corrosion resistance at high strength level. Another outstanding advantage of type 7050 Alloy is good hardenability, especially for the manufacture of heavy section parts such as forgings.
The 7050 aluminum alloy plate profile forgings is mainly used for aircraft structure parts, such as fuselage frames, partitions, wing panels, wing beams, wing ribs, landing gear support parts and rivets, which require high light, high stress corrosion and peeling corrosion resistance and good fracture toughness. When the temperature rises, the strength of the alloy will be reduced, and the long-term use temperature can not exceed 125ºC.
The force components of different state materials were used for different use conditions: T76 State General requirements for the structure exfoliation corrosion resistance and high strength; T74 state for high strength and anti stress corrosion structure, especially the structure of a thick section; the T73 state is mainly used for rivet wire of high strength, corrosion resistance.
| Chemical Composition of 7050 Alloy | |||||||||||||
| Alloy | Si | Fe | Cu | Mn | Mg | Cr | Ni | Zn | Ti | Zr | Others | Al | |
| Each | Total | ||||||||||||
| 7050 | 0.12 | 0.15 | 2.0~2.6 | 0.1 | 1.9~2.6 | 0.04 | ~ | 5.7~6.7 | 0.06 | 0.08~0.15 | 0.05 | 0.15 | Remainder |
| Alloy | Alloy series | Main features | Σb Value/MPa | Working temperatue/ºC |
| 7050 | 7050 series | 7050, it is one of the most widely used and comprehensive high strength aluminum alloys. It has high strength, high resistance to stress corrosion cracking and good fracture toughness. The main varieties are thick plates, profiles and forgings. The 7050 thick plate has two kinds of use state T7651 and T7451. T7651 has good anti peeling corrosion performance and medium stress corrosion resistance, and has high static strength. T7451 has the best anti stripping corrosion ability, and the ability to resist stress corrosion is also better than T7651, but the strength is slightly lower. At present, the short transverse properties of the 7050 Alloy thick plate have been further improved. | 495~530 | <125 |
| Physical Properties of 7050 Alloy | ||||||||
| Alloy | Type | Temper | Specification/mm | Direction | σb/MPa | σp 0.2/MPa | ||
| A | B | A | B | |||||
| 7050 | Aluminum sheet | T7451 | δ6.35~38.1 | L | 217.6 | 524.4 | 448.5 | 462.3 |
| LT | 510.6 | 524.4 | 441.6 | 455.4 | ||||
| δ38.125~76.2 | L | 510.6 | 524.4 | 448.5 | 455.4 | |||
| LT | 517.5 | 524.4 | 441.6 | 455.4 | ||||
| δ76.225~101.6 | L | 510.6 | 517.5 | 448.5 | 455.4 | |||
| LT | 510.6 | 517.5 | 441.6 | 455.4 | ||||
| ST | 469.2 | 496.8 | 407.1 | 414.0 | ||||
| δ101.625~127 | L | 496.8 | 503.7 | 427.8 | 448.5 | |||
| LT | 496.8 | 510.6 | 420.9 | 441.6 | ||||
| ST | 462.3 | 476.1 | 400.2 | 414.0 | ||||
| δ127.025~152.4 | L | 489.9 | 496.8 | 414.0 | 434.7 | |||
| LT | 483.0 | 503.7 | 414.0 | 427.8 | ||||
| ST | 455.4 | 476.1 | 393.3 | 393.3 | ||||
| T7651 | δ25.425~38.1 | L | 531.3 | 552.0 | 462.3 | 489.9 | ||
| LT | 524.4 | 545.1 | 455.4 | 483.0 | ||||
| δ38.125~50.8 | L | 524.4 | 538.2 | 455.4 | 483.0 | |||
| LT | 517.5 | 538.2 | 448.5 | 476.1 | ||||
| ST | 496.8 | 517.5 | 407.1 | 434.7 | ||||
| δ50.825~63.5 | L | 517.5 | 538.2 | 455.4 | 483.0 | |||
| LT | 517.5 | 538.2 | 448.5 | 476.1 | ||||
| ST | 483.0 | 503.7 | 414.0 | 427.8 | ||||
| Aluminum profile | T76511 | δ≤12.675 | L | 531.3 | 545.1 | 469.2 | 489.9 | |
| LT | 524.4 | 538.2 | 462.3 | 476.1 | ||||
| Free aluminum forgings | T7452 | δ152.425~177.8 | L | 469.2 | 489.9 | 386.4 | 420.9 | |
| LT | 462.3 | 483 | 386.4 | 407.1 | ||||
| ST | 448.5 | 476.1 | 358.8 | 386.4 | ||||
| Alloy | Temper | Aircraft models | Application parts and typical parts |
| 7050 | Aluminum plate: T7651,T7451 Aluminum profile: T76511 Free aluminum forgings:7452 | Widely used abroad, domestic ARJ21 and so on | For thick section of main structure of high load, such as the manufacture of fuselage frame and bulkhead, wing skin stiffener, extrusion, Stringer, reinforcing rib, forging parts, gear parts, supporting beam, wall, flange, important joints etc.. |
