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

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

B247,A-367

Chemical Elements

AluminumBalance
Chromium0.1 max
Copper3.5 - 4.5
Iron1 max
Magnesium0.45 - 0.9
Manganese0.2 max
Nickel1.7 - 2.3
Remainder Each0.05 max
Remainder Total0.15 max
Silicon0.9 max
Zinc0.25 max

Physical Properties

Density: 0.102lb/in³Density

Melting Point: 950°FMelting Point

Poissons Ratio: 0.33Poissons Ratio

Specific Gravity: 2.82Specific Gravity

Mechanical Properties

Modulus of Elasticity – Tension: 10.8MSIModulus of Elasticity – Tension

Modulus of Elasticity – Torsion: 4.1MSIModulus of Elasticity – Torsion