For aluminium alloy aviation plate products, new alloys and new sizes can be customized by Flat-Rolled Product Division of Nanshan Aluminium according to customers’ requirements. With the two (27m / 54m) roller hearth furnaces and the 80MN stretching machine, stable plate properties and low internal stress can be achieved; along with 27m aging furnaces, the production of plates in various sizes can be fulfilled. On requests of the customers, cuts convenient for taking arrival re-inspection coupons can be reserved on the plate products. In addition, Flat-Rolled Product Division of Nanshan Aluminium is endeavoring to develop various alloy products and making a good effort in meeting customers' requirements.

 Product Type and Specification

7050-T7451           6.35~177.8mm×800~3800mm×1000~14000mm

2024-T351             6.35~101.6mm×800~3800mm×1000~14000mm

7075-T651             6.35~200 mm×800~3800mm×1000~14000mm

7075-T7351           6.35~88.9mm×800~3800mm×1000~14000mm

Product Properties

Alloy Temper7050-T7451

Thickness

Sampling Orientation

Tensile Strength/MPa

Yield Strength/MPa

Elongation/%

6.3~51.0

L

510

440

10

LT

510

440

9

51.0~76.0

L

505

435

9

LT

505

435

8

76.0~102.0

L

495

425

9

LT

495

425

6

102.0~127.0

L

490

420

9

LT

490

420

5

127.0~152.0

L

485

415

8

LT

485

415

4

152.0~178.0

L

475

405

7

LT

475

405

4

Alloy Temper2024-T351

Thickness

Sampling Orientation

Tensile Strength/MPa

Yield Strength/MPa

Elongation/%

6.3~12.5

LT

440

290

12

12.5~25.0

LT

435

290

7

25.0~40.0

LT

425

290

6

40.0~50.0

LT

425

290

5

50.0~80.0

LT

415

290

4

80.0~100.0

LT

395

285

4

Alloy Temper7075-T651

Thickness

Sampling Orientation

Tensile Strength/MPa

Yield Strength/MPa

Elongation/%

6.3~12.5

LT

540

460

9

12.5~25.0

LT

540

470

7

25.0~50.0

LT

530

460

5

50.0~60.0

LT

525

440

4

60.0~80.0

LT

495

420

4

80.0~90.0

LT

490

400

4

90.0~100.0

LT

460

370

2

Alloy Temper: 7075-T7351

Thickness

Sampling Orientation

Tensile Strength/MPa

Yield Strength/MPa

Elongation/%

6.3~12.5

LT

475

390

7

12.5~25.0

LT

475

390

6

25.0~50.0

LT

475

390

5

50.0~60.0

LT

455

360

5

60.0~80.0

LT

440

340

5

Product Features

7050:with high strength, high toughness and high stress corrosion resistance properties.

7075: with high strength for 7075-T651 temper, relatively high fracture toughness for7075-T7351; with excellent stress corrosion resistance and exfoliation corrosion properties.

2024: with high tensile strength and yield strength under natural aging condition, along with good machinability properties.

Product Application

7050: mainly used for aircraft wing ribs, fuselage frames, structural beams, load-bearing structural parts and auxiliary panels.

7075: used for the main structural parts with thick and large sections and bearing high loads, such as beams, wing top skins, and fuselage bulkheads.

2024: mainly used for fuselage skins, bulkheads, wing bottom panels, wing ribs and other positions.

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