Aluminum
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
Channel
Coil
Disc
Flat Bar
Foil
Hollow Bar
Pipe
Plate
Rectangle Tube
Ring
Rod
Round Bar
Round Tube
Sheet
Square Bar
Square Tube
Strip
Tee
Additional Data
Specifications
4084,4085,4089,4090,4202,A97475Chemical Elements
| Aluminum | Balance |
| Chromium | 0.18 - 0.25 |
| Copper | 1.2 - 1.9 |
| Iron | 0.12 max |
| Magnesium | 1.9 - 2.6 |
| Manganese | 0.06 max |
| Remainder Each | 0.05 max |
| Remainder Total | 0.15 max |
| Silicon | 0.1 max |
| Titanium | 0.06 max |
| Zinc | 5.2 - 6.2 |
Physical Properties
Density: 0.101lb/in³
Melting Point: 1015°F
Poissons Ratio: 0.33
Specific Gravity: 2.81
Mechanical Properties
Modulus of Elasticity – Tension: 10.2MSI
Modulus of Elasticity – Torsion: 3.9MSI
Thermal Conductivity
| Condition | Temperature | Conductivity |
|---|---|---|
| T651 | 77 °F | 8.2 BTU/hr·ft·°F |
Thermal Expansion
| Condition | Min | Max | Expansion Coefficient |
|---|---|---|---|
| Annealed | 68 °F | 212 °F | 13 μin/in·°F |