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7A55 Aerospace Transportation aluminium sheet 7075/7475/7050/7B50/7A55 aircraft Aluminum Alloy Sheet
Item | 7xxx aluminum plate |
series | 7xxx |
character | high strength ,good toughness,good corrosion resistance,good cutting performance and easy surface treatment etc |
Applications | aerospace,marine,automotive,railway transportation,oil and chemical industries etc |
processing technic | stretching,quenched,cold rolled |
Surface | Degreased, anodized, mill finis,laminating,etc |
MOQ | 2 tons |
Delivery time | 15-20 days after confirming order |
payment | 15~ 30% TT as deposit , the balance after you checked the quality before shippment |
Packing | Export standard packing : PP bag , wooden box or other packing according clients request |
alloy | Si | Fe | Cu | Mn | Mg | Cr | Zn | Zr | Ti | standard |
7075 | 0.4 | 0.5 | 1.2-2.0 | 0.3 | 2.1-2.9 | 0.18-0.28/ | 5.1-6.1 | 0.05 | 0.2 | AMS |
7475 | 0.1 | 0.12 | 1.2-1.9 | 0.06 | 1.9-2.6 | 0.18-0.25 | 5.2-6.2 | 0.05 | 0.06 | |
7050 | 0.12 | 0.15 | 2.0-2.6 | 0.1 | 1.9-2.6 | 0.04 | 5.7-6.7 | 0.08-0.15 | 0.06 | |
7B50 | 0.12 | 0.15 | 1.8-206 | 0.1 | 2.0-2.8 | 0.04 | 6.0-7.0 | 0.08-0.16 | 0.10-0.25 | |
7A55 | 0.1 | 0.1 | 1.8-2.5 | 0.05 | 1.8-2.8 | 0.04 | 7.5-8.5 | 0.08-0.20 | 0.10-0.25 |
specification:
alloy | temper | thickness(mm) | width(mm) |
7075 | T73,T76,T74,T6 | 0.5-3.5 | 800-2600 |
7475 | |||
7050 | 3.5-6.0 | 800-2900 | |
7B50 | |||
7075 | T651,T7351,T7651,T7451,T7751 | 6-12 | 800-2900 |
7475 | |||
7050 | |||
7B50 | 12-250 | 800-3800 | |
7A55 |
Mechanical properties:
alloy | temper | thickness(mm) | tensile strength (Mpa) | yield strength(Mpa) | elongation(%) | standard |
7075 | T6 | 0.5-0.6 | 580 | 500 | 12 | SAE AMS-QQ-A-250/12 |
T73 | 0.5-0.6 | 480 | 405 | 12 | SAE AMS-QQ-A-250/12 | |
T76 | 0.5-0.6 | 490 | 410 | 12 | SAE AMS-QQ-A-250/12 | |
7475 | T61 | 0.5-0.6 | 540 | 460 | 12 | SAE AMS 4084 |
T761 | 0.5-0.6 | 510 | 435 | 12 | SAE AMS 4085 | |
7050 | T76 | 0.5-0.6 | 535 | 485 | 10 | SAE AMS 4243 |
7075 | T651 | 6.0-225 | 570 | 495 | 10 | SAE AMS 4045 |
7075 | T7351 | 6.0-150 | 550 | 420 | 10 | SAE AMS 4078 |
7475 | T7651 | 6.0-50 | 510 | 435 | 10 | SAE AMS 4089 |
7050 | T7451 | 6.0-225 | 530 | 460 | 10 | SAE AMS 4050 |
7050 | T7651 | 6.0-100 | 550 | 480 | 10 | SAE AMS 4201 |
7B50 | T6151 | 6.0-50 | 600 | 550 | 12 | / |
7B50 | T7751 | 6.0-100 | 590 | 540 | 10 | / |
7A55 | T7751 | 6.0-50 | 635 | 605 | 10 | / |
Aluminium Sheet, the most widely used form of aluminum, is found in all of the aluminum industry’s major markets.
Aluminum alloy can be tempered to get hardness. Aluminum alloy also can be color-anodized other colors. It can be etched to a matte finish, polished to a sparkling brightness or coated to resemble wood and painted. Aluminium alloy can be laminated with other materials, such as paper, plastic, other metals to achieve super advantages. Aluminum has penetrative into your every corner of your life. We believe that aluminium has unlimited potential and the use of aluminum in a wide variety of applications continues to grow.
XIAOXIAN RUIYI Can manufacture aluminum alloy plate sheet as
Alloy: 1050 1060 1100 3003, 3105, 5052, 5005, 5754 5083 5182, 6061 6063 6082, 7075, 8011…
Temper: HO, H111,H12, H14, H24,H 32, H112, T4, T6, T5,T651
Surface:Mill/Emboss/Diamond/2bar/3bars/Bright
Thickness: 0.2mm to 300mm
Width: 30mm to 2300mm
Length:1000mm to 10000mm.
Aluminium plate | aluminum alloy sheet | Aluminum tread plates | Aluminum coils | Aluminum Foils| Aluminium diamond plate sheet | Aluminum checker plates | Aluminium chequer plate sheet
Chemical Analysis of aluminum alloy Plate | ||||||||||
Alloy | Si | Fe | Cu | Mn | Mg | Cr | Ni | Zn | Ti | Al |
1050 | 0.25 | 0.4 | 0.05 | 0.05 | 0.05 | - | - | 0.05 | 0.03 | Remains |
1060 | 0.25 | 0.35 | 0.05 | 0.03 | - | - | - | - | - | Remains |
1070 | 0.2 | 0.25 | 0.04 | 0.03 | 0.03 | - | - | - | - | Remains |
1100 | 0.95 | 0.95 | 0.05-0.2 | 0.05 | - | - | 0.1 | - | - | Remains |
1200 | 1 | 1 | 0.05 | 0.05 | - | - | - | 0.1 | 0.05 | Remains |
3003 | 0.6 | 0.7 | 0.05-0.2 | 1.0-1.5 | - | - | - | 0.1 | - | Remains |
5005 | 0.3 | 0.7 | 0.2 | 0.2 | 0.5-1.1 | 0.1 | - | 0.25 | - | Remains |
5042 | 0.2 | 0.35 | 0.15 | 0.2--.5 | 3.0-4.0 | 0.1 | - | 0.25 | 0.1 | Remains |
5052 | 0.25 | 0.4 | 0.1 | 0.1 | 2.2-2.8 | 0.15-0.35 | - | 0.1 | - | Remains |
5083 | 0.4 | 0.4 | 0.1 | 0.4-1.0 | 4.0-4.9 | 0.05-0.25 | - | 0.25 | - | Remains |
5754 | 0.4 | 0.4 | 0.1 | 0.5 | 2.6-3.6 | 0.3 | - | 0.2 | - | Remains |
6061 | 0.4-0.8 | 0.7 | 0.15-0.4 | 0.15 | 0.8-1.2 | 0.04-0.35 | - | 0.25 | - | Remains |
6063 | 0.2-0.6 | 0.35 | 0.1 | 0.1 | 0.45 | 0.1 | - | 0.1 | - | Remains |
6082 | 0.7-1.3 | 0.5 | 0.1 | 0.4-1.0 | 0.6-1.2 | 0.25 | - | 0.2 | - | Remains |
7050 | 0.12 | 0.15 | 2.0-2.6 | 0.1 | 1.9-2.6 | 0.04 | - | 5.7-6.7 | 0.06 | Remains |
7075 | 0.4 | 0.5 | 1.2-2.0 | 0.3 | 2.1-2.9 | 0.18-0.28 | - | 5.1-6.1 | 0.2 | Remains |