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7050 aluminum material property data sheet

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Aluminum 7050

 


Specifications

The following specifications cover Aluminum 7050

  • AMS 4108 (Forging - Open Die)
  • AMS 4201 (Plate)
  • ASTM B247 (Forging - Open Die)
  • ASTM B316
  • QQ A-430
  • UNS A97050

 

 


Property Results

No Related Metal names.


Chemistry Data : [top]

Aluminum Balance
Chromium 0.04 max
Copper 2 - 2.6
Iron 0.15 max
Magnesium 1.9 - 2.6
Manganese 0.1 max
Remainder Each 0.05 max
Remainder Total 0.15 max
Silicon 0.12 max
Titanium 0.06 max
Zinc 5.7 - 6.7
Zirconium 0.08 - 0.15


Principal Design Features 7050 alloy is heat treatable so as to produce mechanical properties of high strength and toughness. It has very good resistance to stress corrosion cracking.

Applications Commonly used in the manufacture of aircraft and other structures.

Machinability No data available.

Forming The 7050 alloy may be readily formed in either the O temper or the heat treated condition.

Welding Welding of 7050 alloy is a problem and should be avoided. Gas tungsten or gas metal arc welding is NOT successful with this alloy. Weld cracking and porosity usually result and any weld joint that is made is much weaker than the parent metal.

Heat Treatment Solution heat treat at 890 F. Time at temperature is dependent upon section thickness and the producer of the alloy should be consulted on this as well as quenching rate.

Forging The alloy may be forged. However no data is available without consulting the alloy source.

Hot Working As with Forging the 7050 alloy may be hot worked but no data is available except from the alloy producer.

Cold Working The alloy may be cold formed by conventional means. However bend radii should be generous.

Annealing Not applicable to this alloy.

Aging A 2 stage heat treatment is used for aging this alloy. First heat to 250 F for 3 to 6 hours (depending on section size) and follow that with 325 F for 15 hours then air cool.

Tempering Not applicable.

Hardening Hardens only by precipitation heat treatment. See "Aging".

Other Physical Props Electrical conductivity 40% of copper.

Physical Data : [top]

Density (lb / cu. in.) 0.102
Specific Gravity 2.83
Melting Point (Deg F) 920
Poissons Ratio 0.33
Modulus of Elasticity Tension 10.3
Modulus of Elasticity Torsion 3.9


Mechanical Data : [top]

There is no Mechnical data available for this grade.


[top]
Nickel - www.nidi.org

Copper - www.copper.org

Titanium - www.titanium.org

Steel Lynx - www.mlc.lib.mi.us/~stewarca/steelynx.html


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