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Highly Stressed 7075 Aircraft Grade Aluminum Alloy 500mm-2800mm Width

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Highly Stressed 7075 Aircraft Grade Aluminum Alloy 500mm-2800mm Width

China Highly Stressed 7075 Aircraft Grade Aluminum Alloy 500mm-2800mm Width supplier
Highly Stressed 7075 Aircraft Grade Aluminum Alloy 500mm-2800mm Width supplier Highly Stressed 7075 Aircraft Grade Aluminum Alloy 500mm-2800mm Width supplier

Large Image :  Highly Stressed 7075 Aircraft Grade Aluminum Alloy 500mm-2800mm Width

Product Details:

Place of Origin: China
Brand Name: RUIYI
Certification: CCS, LR, DNV, ISO
Model Number: 7075

Payment & Shipping Terms:

Minimum Order Quantity: 5 Ton
Price: US$2300-US$3600 per ton
Packaging Details: pallets
Delivery Time: 35 days
Supply Ability: 1000 Ton Per Month
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Detailed Product Description
Product Name: Aircraft Aluminum Bare Sheet Alloy: 7075
Temper: T6, H321, T651 Thickness: 0.2-300mm
Width: 500mm-2800mm Type: Aluminum Sheet Plate

Highly stressed aircraft parts use aluminum sheet aerospace and aviation 7075 aluminum plate supplier

 

Alloy 7075 aluminum plates are the outstanding member of the 7xxx series and remains the baseline among the highest strength alloys available. Zinc is the primary alloying element giving it strength comparable to steel. Temper T651 possesses good fatigue strength, fair machinability, resistance welding and corrosion resistance ratings. Alloy 7075 in temper T7x51 has superior stress corrosion resistance and replaces the 2xxx alloy in the most critical applications. It is widely used by the aircraft industry with the typical specifications of ASTM B209, AMS-QQ-A-250/4, as well as many end users requirements.

 

One of the strongest of the aluminum alloys, 7075 aluminum plate provides great performance and superior corrosion resistance for our customers.

 

Zinc is the primary alloying element of 7075 with 1 to 8 percent of the material composed of zinc. It is precipitation hardened to strength levels comparable to steel. With 7075’s T651 temper, it has been solution heat treated followed by a minimal stretching to reduce stresses in the material. The material has also been artificially aged to allow the alloying elements to precipitate out of the material to give it immediate maximum strength

 

 

7075 aircraft aluminum plate aerospace plate aluminum mechanical properties
Alloy|Temper Tensile Strength(Mpa) Yield Strength(Mpa) Elongation
7075 O 280 140 9-10%
7075 T6 510-540 430-480 5-11%
7075 T651 570 500 3-9%
7075 T7 505 435 13%

 

 

Highly Stressed 7075 Aircraft Grade Aluminum Alloy 500mm-2800mm Width

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

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