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7050 Aluminium Alloy Plate T7351 Temper for Aircraft Structural Parts

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7050 Aluminium Alloy Plate T7351 Temper for Aircraft Structural Parts

Brand Name : zhuxia
Model Number : 7050 T7351
Certification : MTC,AS9100,ISO9001,NADCAP
Place of Origin : CHINA
MOQ : 3MTS
Price : NEGOTIABLE
Payment Terms : L/C, T/T
Supply Ability : 15000tons/month
Delivery Time : 20-30days
Packaging Details : plastic film/craft paper, wooden case/pallet, 25 tons per container
Alloy : 7050
Temper : T651,T6,T73,T76,T74,T7351
Surface : Mill finish
Thickness : 0.5-250mm
Width : 800-3800mm
Elongation : 10%
Standard : SAE AMS 4243
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7050 Aluminium Alloy Plate T651 Temper for Aircraft Structural Parts


Aluminum alloys have high strength at subzero temperatures. However, their strength can be reduced at high temperatures.


Aluminium / Aluminum 7050 alloy is a heat treatable alloy. which has high toughness, strong mechanical strength, and good stress corrosion cracking resistance. The following gives an overview of Aluminium / Aluminum 7050 alloy.


1.Description

Specification
ItemTypical Thickness / mmTensile StrengthYield StrengthElongation / %Standard
7050 sheet T760.5-6.053548510SAE AMS 4243
7050 plate T74516.0-225.053046010SAE AMS 4050
7050 palte T76516.0-100.055048010SAE AMS 4201

Chemical Composition
SiFeCuMnMgCrZnZrTiStandard
0.120.152.0-2.60.101.9-2.60.0045.7-6.70.08-0.150.16En573

2.Features

Forming: can be formed in O temper or heat treated conditions.

Welding: should not be welded in order to prevent cracking and development of porosity. The weld joint produced will be weaker than the parent metal. Gas tungsten or gas metal arc welding methods are not preferred for welding this alloy.

Heat Treatment: Aluminium / Aluminum 7050 alloy can be heat treated at 477°C (890°F). The time taken for this process is based upon the thickness of the section.

Cold Working: can be cold worked using conventional methods.

Aging: is aged using two-stage heat treatment. It is heated at 122°C (250°F) for 3 to 6 h. It is again heated at 163°C (325°F) for 15 h followed by cooling in air.

Hardening: Aluminium / Aluminum 7050 alloy can be hardened by precipitation heat treatment.

Applications: Aluminium / Aluminum 7050 alloy is mainly used in manufacturing aircraft and other structures.


3.Application

Aluminium alloy 7050 is an aerospace grade of aluminium combining high strength, stress corrosion cracking resistance and toughness. It is particularly suited for heavy plate applications (3" to 6" thick) due to it's lower quench sensitivity and retention of strength in thicker sections. Aluminium 7050 therefore is the premium choice aerospace aluminium for applications such as fuselage frames, bulkheads and wing skins.



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