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7150 aluminum alloy sheet profile

7150 aluminum alloy sheet profile

The 7150 is the second generation modification of 7050 Alloy, the main varieties have thick plates and profiles, the use of the state of T7751 and T77511. Compared with other 7 * * * * system alloys, 7150 T77 alloys have obtained the best combination of strength and corrosion properties.

7075 aluminum tube

aluminum extrusion 7075

7085 aluminum plate

7075 t651 aluminum plate

The 7150 alloy is mainly supplied in the form of T7751 thick plate, T77511 extruded parts and T76511 extrusion parts. 7150 aluminum alloy sheet profile is used for the main stress parts of the upper wing structure and aircraft structure, such as wing upper wall panels, beams, edge strips and so on.

7075 t651 aluminum plate

7085 aluminum plate

aluminum extrusion 7075

7075 aluminum tube

                                                   Chemical Composition of 7150 alloy
Alloy Si Fe Cu Mn Mg Cr Ni Zn Ti Zr         Others Al
Each Total
7150 0.12 0.15 1.9~2.5 0.1 2.0~2.7 0.04 ~ 5.9~6.9 0.06 0.08~0.15 0.05 0.15 Remainder

Alloy Alloy series Main feature σb  Value/MPa Work Temperature/℃
7150 7050 series The 7150 is the second generation modification of 7050 Alloy, the main varieties have thick plates and profiles, the use of the state of T7751 and T77511. Compared with other 7 * * * * system alloys, 7150 T77 alloys have obtained the best combination of strength and corrosion properties.  
 
                579~622
 
 
<125

Physical Property of 7150 Alloy
Alloy Type Temper Size/mm Direction σb/MPa σp 0.2/MPa KIC oR KC δ %
7150 Aluminum sheet T7751 δ6.35~12.69 L 552 510  
8
LT 552 510
δ12.70~19.04 L 572 531 8
LT 572 524
δ19.05~25.40 L 579 538 L - T 22
T -L19.8
8
LT 579 531
δ25.41~38.10 L 579 53 L -T 24.2
T -L 22
8
LT 579 531
δ38.11~76.20 L 565 524 7
LT 565 517 6
ST 531 462 1
Aluminum profile T77511 δ1.0~6.34 L 594 545 7
LT 566 510
δ6.35~12.69 L 608 573 8
LT 573 531
δ12.70~19.04 ST 615 580 9
L 580 552
δ19.05~50.80 LT 622 587 L -T 23.1
T -L 18.7
8
ST 580 545
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