Aluminum 7475

Aging Procedure

Proprietary data. Consult Alcoa.

Annealing Procedure

Proprietary data. Consult Alcoa.

Applications

Commonly used in the manufacture of shell casings, aircraft, and other structures.

Cold Workability

The alloy in the annealed condition is readily cold worked using conventional means. In the heat treated tempers it is more difficult to form because of it greater strength. See also "Forming".

Forgeability

No data available.

Formability

This alloy may be formed by conventional methods. However forming is easier in the annealed condition because in the heat treated (hardened) condition the alloy has more springback due to its strength. Use of warming at 250 F will assist in forming, especially for spinning. Optimum formability is with the material in the W (quenched) condition.

Hardening Procedure

Proprietary data. Consult Alcoa.

Heat Treatability

Heat treatment may be done. However the parameters of the treatment are proprietary to Alcoa. Heat treat information is available from Alcoa on a non-disclosure agreement basis.

Hot Workability

No hot work data available. However use of warming at 250 F for annealed stock is conducive to forming operations such as spinning.

Machinability

Machining characteristics are very good in the annealed condition. Use of oil base lubricants for all machining operations is recommended.

Principle Design Features

This is a high strength alloy of very good toughness. It is a derivative of AL 7075 alloy and the AL 7475 version is available in sheet and plate product forms.

Tempering Procedure

Not applicable to this alloy.

Weldability

Not normally done to this alloy and no data on techniques available at this time.

Known Forms

Angle

Angle

Channel

Channel

Coil

Coil

Disc

Disc

Flat Bar

Flat Bar

Foil

Foil

Hollow Bar

Hollow Bar

Pipe

Pipe

Plate

Plate

Rectangle Tube

Rectangle Tube

Ring

Ring

Rod

Rod

Round Bar

Round Bar

Round Tube

Round Tube

Sheet

Sheet

Square Bar

Square Bar

Square Tube

Square Tube

Strip

Strip

Tee

Tee

Additional Data

Specifications

4084,4085,4089,4090,4202,A97475

Chemical Elements

AluminumBalance
Chromium0.18 - 0.25
Copper1.2 - 1.9
Iron0.12 max
Magnesium1.9 - 2.6
Manganese0.06 max
Remainder Each0.05 max
Remainder Total0.15 max
Silicon0.1 max
Titanium0.06 max
Zinc5.2 - 6.2

Physical Properties

Density: 0.101lb/in³Density

Melting Point: 1015°FMelting Point

Poissons Ratio: 0.33Poissons Ratio

Specific Gravity: 2.81Specific Gravity

Mechanical Properties

Modulus of Elasticity – Tension: 10.2MSIModulus of Elasticity – Tension

Modulus of Elasticity – Torsion: 3.9MSIModulus of Elasticity – Torsion

Thermal Conductivity

ConditionTemperatureConductivity
T65177 °F8.2 BTU/hr·ft·°F

Thermal Expansion

ConditionMinMaxExpansion Coefficient
Annealed68 °F212 °F13 μin/in·°F