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7475 T651 T7651 T7351 Aircraft Aluminum Sheet Plate For Fuselage Bulkheads

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7475 T651 T7651 T7351 Aircraft Aluminum Sheet Plate For Fuselage Bulkheads

China 7475 T651 T7651 T7351 Aircraft Aluminum Sheet Plate For Fuselage Bulkheads supplier
7475 T651 T7651 T7351 Aircraft Aluminum Sheet Plate For Fuselage Bulkheads supplier 7475 T651 T7651 T7351 Aircraft Aluminum Sheet Plate For Fuselage Bulkheads supplier

Large Image :  7475 T651 T7651 T7351 Aircraft Aluminum Sheet Plate For Fuselage Bulkheads

Product Details:

Place of Origin: China
Brand Name: RUIYI
Certification: CCS, LR, DNV, ISO
Model Number: 7475

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: 7475 Aluminum Sheet Alloy: 7475
Temper: T7651, T7351, T651 Thickness: 0.2-300mm
Width: 500mm-2800mm Type: Sheet Plate

7475 T651 T7651 T7351 aircraft aluminum alloy sheet for Fuselage bulkheads

 

Alloy 7475 aluminum plates are a controlled toughness alloy whose values are 40 percent greater than alloy 7075 in the same tempers. This alloy’s corrosion resistance and fatigue behavior are also equal to, or better than, many of the other high strength aerospace alloys, and is for those applications that require a combination of high strength, superior fracture toughness and resistance to fatigue crack propagation.

Application:

  • Wings spars
  • Fuselage bulkheads


The strength and corrosion resistance of the 7475 alloy are equivalent to those of the 7075 alloy at the same state, while the fracture toughness is higher than that of the existing aluminum alloy with equal strength. Its strength and fracture toughness match best.

The 7475 aluminum alloy sheet is supplied with O, T6 and T76, and the thick plate is supplied with T651, T7651 and T7351. Compared with the state of T76 and T6, the corrosion resistance, especially the anti peeling corrosion resistance, was improved, but the strength was reduced. Compared with the state of T7651 and T651, the resistance to peeling corrosion and stress corrosion resistance is improved, and the fracture toughness is improved, but the strength is reduced.

The technical standard of 7475 alloy not only stipulates the tensile properties at room temperature, but also stipulates the fracture toughness index. The 7475 T651 T7651 T7351 aluminum alloy sheet is mainly used for manufacturing high strength, medium fatigue strength and high fracture toughness structure, such as wing skin, fuselage skin and spacer. Using 7475 alloy can improve the safety, reliability and service life of the aircraft. As 7475 is a high strength aluminum alloy at room temperature, the strength properties of the alloy will be reduced with the increase of the temperature, and the long-term use temperature should not exceed 125 ℃.

 

7475 T651 T7651 T7351 Aircraft Aluminum Sheet Plate For Fuselage Bulkheads

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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