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7085 aluminum alloy plate forgings
Chemical Composition of 7085Alloy | |||||||||||||
Alloy | Si | Fe | Cu | Mn | Mg | Cr | Ni | Zn | Ti | Zr | Others | Al | |
Each | Total | ||||||||||||
7085 | 0.12 | 0.15 | 1.5~2.0 | 0.1 | 2.1~2.6 | 0.05 | 0.05 | 5.7~6.7 | 0.05 | 0.10~0.16 | 0.05 | 0.15 | Remainder |
Alloy | Alloy series | Main features | Σb Value/MPa | Work Temperature/℃ |
7085 | New type alloy |
A kind of high strength and high hardenability forging aluminum alloy has been developed since 1990s. 7085 alloy heavy forgings can solve the contradiction between specification hardenability, performance and residual internal stress, and have excellent comprehensive properties, especially in fracture toughness, without the influence of thickness. |
510 |
<125 |
Physical Property of 7010 Alloy | ||||||||||
Alloy | Type | Temper | Size/mm | Direction | σb/MPa | σp 0.2/MPa | δ % | KIC OR KC | ||
7085 |
Aluminum plate |
T7651 | δ101.62~127.00 | L | 510 | 476 | 7 | - | ||
LT | 503 | 462 | 5 | |||||||
ST | 483 | 434 | 3 | |||||||
δ127.02~152.40 | L | 510 | 476 | 7 | ||||||
LT | 503 | 462 | 4 | |||||||
ST | 483 | 434 | 3 | |||||||
Δ152.42~177.80 | L | 503 | 469 | 6 | ||||||
LT | 503 | 448 | 3 | |||||||
ST | 476 | 434 | 3 | |||||||
Alloy | Temper | Aircraft models | Application parts and typical parts |
7085 |
Aluminum plate: T7651 Aluminum forgings:T7652 |
A380 | Wing beam |