Aluminum
Aluminum 2018
Aging Procedure
Age hardening is accomplished starting with the alloy in the solution treated, T4, condition (950 F and water quenched). Age at 340 F for 10 hours followed by air cool for T61 temper . Age at 450 F for 6 hours and air cool for T71 temper.
Annealing Procedure
Annealing ("O" temper) is done at 775 F for 3 hours and then controlled cooling at 50 F per hour down to 500 F, followed by air cooling.
Applications
Commonly used in the manufacture of aircraft engine cylinders and in heads and pistons.
Cold Workability
This alloy is primarily intended for fabrication by forging and/or hot working. However it may be cold worked by conventional means but this should be done with the alloy in the annealed condition.
Forgeability
Forging should be done in the temperature range of 900 to 970 F, finishing at 500 F before reheating to 970 F if necessary.
Formability
This is primarily a forging, or hot working, alloy. However cold working can be done with the alloy on the annealed condition.
Hardening Procedure
Hardens by heat treatment and aging and/or cold working.
Heat Treatability
Solution heat treatment is done at 950 F for sufficient time to allow uniform heating throughout, then water quench. For heavy section size parts the water quench should be done using water at approximately 200 F.
Hot Workability
The alloy may be hot worked readily in the temperature range of 500 to 970 F.
Machinability
The alloy is readily machined, especially in the aged condition for smooth finishing. In the T4 condition (solution heat treated) the alloy is softer and may tend to build up during lathe turning or milling. Use of lubricating oils is recommended.
Other Mechanical Properties
Shear strength T61 temper 39 ksi.
Other Physical Properties
Electrical conductivity 40% of copper.
Principle Design Features
This is a high strength, age hardening, forging alloy.
Tempering Procedure
Not applicable.
Weldability
Welding of this alloy by conventional methods is NOT recommended. It may be arc or resistance welded by special techniques
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
B247,A-367Chemical Elements
| Aluminum | Balance |
| Chromium | 0.1 max |
| Copper | 3.5 - 4.5 |
| Iron | 1 max |
| Magnesium | 0.45 - 0.9 |
| Manganese | 0.2 max |
| Nickel | 1.7 - 2.3 |
| Remainder Each | 0.05 max |
| Remainder Total | 0.15 max |
| Silicon | 0.9 max |
| Zinc | 0.25 max |
Physical Properties
Density: 0.102lb/in³
Melting Point: 950°F
Poissons Ratio: 0.33
Specific Gravity: 2.82
Mechanical Properties
Modulus of Elasticity – Tension: 10.8MSI
Modulus of Elasticity – Torsion: 4.1MSI