• 7075 T6/T62/T7351 Aircraft Aerospace Aviation Aluminum Alloy Sheet Plate
  • 7075 T6/T62/T7351 Aircraft Aerospace Aviation Aluminum Alloy Sheet Plate
  • 7075 T6/T62/T7351 Aircraft Aerospace Aviation Aluminum Alloy Sheet Plate
  • 7075 T6/T62/T7351 Aircraft Aerospace Aviation Aluminum Alloy Sheet Plate
  • 7075 T6/T62/T7351 Aircraft Aerospace Aviation Aluminum Alloy Sheet Plate
  • 7075 T6/T62/T7351 Aircraft Aerospace Aviation Aluminum Alloy Sheet Plate

7075 T6/T62/T7351 Aircraft Aerospace Aviation Aluminum Alloy Sheet Plate

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
Samples:
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Basic Info.

Model NO.
7075
Alloy
Alloy
Transport Package
Export Standard Wooden Pallet
Specification
According to Customer Requirement
Trademark
Chalco Aluminum
Origin
Henan China
HS Code
7606125900
Production Capacity
15000mt/Month

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.
 
                                                           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.






 

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Registered Capital
3000000 RMB
Plant Area
101~500 square meters