• 7010 A320 Aircraft Aerospace Aviation Aluminum Alloy Plate Sheet
  • 7010 A320 Aircraft Aerospace Aviation Aluminum Alloy Plate Sheet
  • 7010 A320 Aircraft Aerospace Aviation Aluminum Alloy Plate Sheet
  • 7010 A320 Aircraft Aerospace Aviation Aluminum Alloy Plate Sheet
  • 7010 A320 Aircraft Aerospace Aviation Aluminum Alloy Plate Sheet
  • 7010 A320 Aircraft Aerospace Aviation Aluminum Alloy Plate Sheet

7010 A320 Aircraft Aerospace Aviation Aluminum Alloy Plate Sheet

Application: Transportation Tools, Aviation
Certification: ISO9001, JIS, GB, EN
Technique: Hot Rolled
Grade: 7000 Series
Temper: T7351/T7451/T7651
Surface Treatment: Mill Finish
Samples:
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Basic Info.

Model NO.
7010
Alloy
Alloy
Transport Package
Export Standard Wooden Pallet
Specification
According to Customer Requirement
Trademark
Chalco Aluminum
Origin
Henan China
HS Code
7606125900
Production Capacity
20000mt/Month

Product Description

7010 A320 Aircraft Aerospace Aviation Aluminum Alloy Plate Sheet

7010 and 7050 basic properties of the alloy, the main varieties of thick plate, use T7351, T7451, T7651.7010 T7351 T7451 T7651 aluminum alloy plate is mainly done by the main structure of high load of a thick section, such as the manufacture of fuselage frame and bulkhead, wing skin, extrusion reinforcing rod, stringers and ribs, forging parts, gear support member and beam to strengthen the wall, flanges, important joints etc..
Chemical Composition of 7010 Alloy
Alloy Si Fe Cu Mn Mg Cr Ni Zn Ti Zr Others Al
Each Total
7010 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 sereis Main features σb  Value/MPa Working Temperature/ºC
7010 7050 series 7010 and 7050 basic properties of the alloy, the main varieties of thick plate, use T7351, T7451, T7651.
414~524
<125
Physical Property of 7010 Alloy
Alloy Type Temper /mm Direction σb/MPa σp 0.2/MPa δ % KIC or KC
7010 Aluminum plate T7651 ~.50.80 L 524 455 8 δ25~51MM:
L -T: 27.5;
T-L: 25.3;
>δ51~76MM
L -T: 26.4;
T - L: 24.2;
S-T: 22.0
>δ76~126MM
L -T: 24.0;
T - L: 22.0;
S-T:19.8
>δ127~140MM
L -T: 22.0;
T - L: 19.8;
S-T:18.7




 
LT 524 455 6
>δ50.80~63.50 L 517 448 8
LT 517 448 6
ST 490 407 2.5
>δ63.50~76.20 L 503 441 7
LT 510 441 5
ST 483 400 2.5
>δ76.20~101.60 L 496 441 7
LT 503 434 5
ST 476 386 2
>δ101.60~127.0 L 496 434 7
LT 496 427 5
ST 469 379 2
>δ127.0~139.7 L 490 427 6
LT 496 421 4
ST 455 365 2
Aluminum plate T7451 ~.50.80 L 490 427 9
LT 496 427 6
>δ50.80~63.50 L 490 427 9
LT 496 427 6
ST 462 393 2.5
>δ63.50~101.60 L 483 421 9
LT 490 421 6
ST 455 386 2
>δ101.60~127.0 L 469 407 9
LT 476 407 5
ST 448 372 2
>δ127.0~139.7 L 455 393 8
LT 462 393 5
    ST 434 365 2
7010 Aluminum plate T7351 ~.50.80 L 462 379 9  
LT 469 379 7
>δ50.80~76.0 L 462 379 9
L -T: 31.9;
T - L: 28.6;
S-T:25.3
LT 469 379 7
ST 434 338 3
>δ76.0~101.60 L 445 372 9
LT 462 372 7
ST 427 331 3
>δ101.60~127.0 L 448 365 9 L -T: 28.6;
T - L: 26.4;
S-T: 24.2
LT 455 365 6
ST 420 324 3
>δ127.0~139.7 L 440 358 9
LT 448 358 5
ST 414 317 3
                   
 
Alloy Temper Aircraft model Application parts and typical parts
7010 Aluminum plate:  T7651,T7451,T7351 A320 The thick section of the main structure of high load, such as the manufacture of fuselage frame and bulkhead, wing skin, extrusion reinforcing rod, stringers and ribs, forging parts, gear support member, beams, strengthening panels, flanges, important joints etc..

 

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Registered Capital
3000000 RMB
Plant Area
101~500 square meters