Swipe or use the arrows to view product images.
7075 T6/T62/T7351 Aircraft Aerospace Aviation Aluminum Alloy Sheet Plate
| Price | $2800.00 |
|---|---|
| Min Order | 1 Ton |
| Availability | In Stock |
| Shipping From | Henan, China |
| Popularity | 345 people viewed |
Model NO.:
7075
Application:
Transportation Tools, Aviation
Certification:
ISO9001, JIS, GB, EN
Technique:
Hot Rolled
Grade:
7000 Series
Temper:
O/T6/T62/T73/T7351/T76
Surface Treatment:
Mill Finish
Alloy:
Alloy
Deep Process:
CNC, Drilling, Milling, Cutting, Welding
Trade Term:
Fob CIF CFR CNF EXW, etc
Tolerance:
1%
Sample:
Available
Lead Time:
According to Order Quantity
Test:
Factory Inspection List
Trademark:
Chalco Aluminum
Transport Package:
Export Standard Wooden Pallet
Specification:
According to Customer Requirement
Origin:
Henan China
HS Code:
7606125900
Product Description
7075 T6 T62 T7351 aluminum alloy sheet plate
7075 T6 T62 T7351 aluminum alloy sheet plate is currently the most widely used 7 * * * aviation Aluminum Alloy, main supply varieties of aluminum or aluminum, heat treatment condition of O, T6, T73, T76. The static strength of T6 is the highest, the ductility is the lowest and the fatigue is the worst. It is sensitive to stress corrosion cracking, and toughness decreases with the decrease of temperature. So the T6 state is not applied to cryogenic working parts. T73 has the lowest state strength, but has high fracture toughness and excellent resistance to stress corrosion cracking and denudation. The performance of T76 is between T6 and T73. Compared with T6 state, it has low strength but good resistance to stress corrosion. Compared with T73 state, its strength is high, but its stress corrosion resistance is poor.
7075 T6 T62 T7351 aluminum alloy sheet plate is currently the most widely used 7 * * * aviation Aluminum Alloy, main supply varieties of aluminum or aluminum, heat treatment condition of O, T6, T73, T76. The static strength of T6 is the highest, the ductility is the lowest and the fatigue is the worst. It is sensitive to stress corrosion cracking, and toughness decreases with the decrease of temperature. So the T6 state is not applied to cryogenic working parts. T73 has the lowest state strength, but has high fracture toughness and excellent resistance to stress corrosion cracking and denudation. The performance of T76 is between T6 and T73. Compared with T6 state, it has low strength but good resistance to stress corrosion. Compared with T73 state, its strength is high, but its stress corrosion resistance is poor.
| Chemical Composition of 7075 alloy | |||||||||||||
| Alloy | Si | Fe | Cu | Mn | Mg | Cr | Ni | Zn | Ti | Zr | Others | Al | |
| Each | Total | ||||||||||||
| 7075 | 0.40 | 0.50 | 1.2~2.0 | 0.3 | 2.1~2.9 | 0.18~0.28 | ~ | 5.1~6.1 | 0.20 | ~ | 0.05 | 0.15 | Remainder |
| Alloy | Alloy Series | Main features | σb Value/MPa | Working Temperature/ºC |
| 7075 | 7075 series | 7075 T6 T62 T7351 aluminum alloy sheet plate is currently the most widely used 7 * * * aviation Aluminum Alloy, main supply varieties of aluminum or aluminum, heat treatment condition of O, T6, T73, T76. The static strength of T6 is the highest, the ductility is the lowest and the fatigue is the worst. It is sensitive to stress corrosion cracking, and toughness decreases with the decrease of temperature. So the T6 state is not applied to cryogenic working parts. T73 has the lowest state strength, but has high fracture toughness and excellent resistance to stress corrosion cracking and denudation. The performance of T76 is between T6 and T73. Compared with T6 state, it has low strength but good resistance to stress corrosion. Compared with T73 state, its strength is high, but its stress corrosion resistance is poor. | 421~538 | <125 |
| Alloy | Type | Temper | Size/mm | Direction | σb/MPa | σp 0.2/MPa | ||
| A | B | A | B | |||||
| 7075 | Aluminum sheet | T6 T62 | δ0.305~0.991 | L | 524.4 | 538.2 | 476.1 | 496.8 |
| LT | 524.4 | 538.2 | 462.3 | 483.0 | ||||
| δ1.016~3.175 | L | 538.2 | 552.0 | 483.0 | 496.8 | |||
| LT | 538.2 | 552.0 | 469.2 | 483.0 | ||||
| δ3.200~6.325 | L | 538.2 | 552.0 | 489.9 | 503.7 | |||
| LT | 538.2 | 552.0 | 476.1 | 489.9 | ||||
| δ6.35~12.675 | L | 510.6 | 524.4 | 448.5 | 462.3 | |||
| LT | 538.2 | 538.2 | 462.3 | 476.1 | ||||
| δ12.7~25.4 | L | 510.6 | 524.4 | 455.4 | 469.2 | |||
| LT | 538.2 | 552.0 | 469.2 | 483.0 | ||||
| δ25.425~50.8 | L | 503.7 | 517.5 | 441.6 | 448.5 | |||
| LT | 531.3 | 545.1 | 462.3 | 476.1 | ||||
| δ50.825~63.5 | L | 496.8 | 510.6 | 414.0 | 427.8 | |||
| LT | 524.4 | 538.2 | 441.6 | 455.4 | ||||
| ST | 483.0 | 489.9 | 407.1 | 420.9 | ||||
| δ63.525~76.2 | L | 476.1 | 489.9 | 386.4 | 400.2 | |||
| LT | 489.9 | 503.7 | 400.2 | 414 | ||||
| ST | 455.4 | 469.2 | 386.4 | 400.2 | ||||
| δ76.225~88.9 | L | 469.2 | 483.0 | 358.8 | 372.6 | |||
| LT | 489.9 | 503.7 | 400.2 | 414.0 | ||||
| ST | 448.5 | 462.3 | 372.6 | 379.5 | ||||
| δ88.9~101.6 | L | 441.6 | 455.4 | 331.2 | 338.1 | |||
| LT | 462.3 | 476.1 | 372.6 | 386.4 | ||||
| ST | 420.9 | 434.7 | 345.0 | 358.8 | ||||
| T7351 | δ12.7~25.4 | L | 469.2 | 483.0 | 393.3 | 407.1 | ||
| LT | 476.1 | 489.9 | 393.3 | 407.1 | ||||
| δ25.425~38.1 | L | 462.3 | 476.1 | 393.3 | 407.1 | |||
| LT | 469.2 | 483.0 | 393.3 | 407.1 | ||||
| δ38.125~50.8 | L | 455.4 | 469.2 | 379.5 | 393.3 | |||
| LT | 462.3 | 476.1 | 379.5 | 393.3 | ||||
| ST | 434.7 | 448.5 | 358.5 | 372.6 | ||||
| δ50.825~63.5 | L | 448.5 | 462.3 | 358.8 | 372.6 | |||
| LT | 455.4 | 469.2 | 365.7 | 379.5 | ||||
| ST | 427.8 | 441.6 | 338.1 | 358.8 | ||||
| δ63.525~76.2 | L | 437.7 | 448.5 | 338.1 | 365.7 | |||
| LT | 448.5 | 455.4 | 358.8 | 365.7 | ||||
| ST | 414.0 | 427.8 | 324.3 | 345.0 | ||||
| Alloy | Temper | Aircraft models | Application parts and typical parts |
| 7075 | Aluminum sheet: T6,T62,T7351 Aluminum plate: T6,T62,T7351 | Widely used | Panels, beams, frames, wing ribs, joints, etc. |
- Similar Products
$2800.00
1 Ton (MOQ)
5083 Aluminum Alloy Plate for Sale
Jiangsu Century Shunhang Metal Technology Co., Ltd