Aluminum
Aluminum 5454
Aging Procedure
Not applicable to this alloy.
Annealing Procedure
Annealing, if necessary to relieve cold working stress, may be done at 650 F, allowing sufficient time for thorough heating, followed by air cooling.
Applications
Commonly used in the manufacture of welded structures, pressure vessels, and in marine service.
Cold Workability
Cold working is easily accomplished with this alloy by conventional methods. It may be cold worked satisfactorily in either the annealed condition or any of the H-32, H-34, H-111 tempers..
Forgeability
This alloy may be hot forged, although no temperature range data is available. Consult the alloy supplier.
Formability
This alloy does posses good hot working and cold working characteristics. It may be readily cold worked in any of the temper, or annealed, conditions.
Hardening Procedure
Hardens by means of cold working only.
Heat Treatability
This alloy is not heat treatable, except for annealing to relieve cold working - see "Annealing".
Hot Workability
Hot working may be accomplished in the temperature range of 700 to 400 F.
Machinability
The machinability of Al 5454 is fair to poor. It is best to do machining operations with the alloy in the H-34 temper condition. Use of oil lubricants is recommended, except that very light cuts may be done dry.
Other Mechanical Properties
Shear strength varies slightly from 23 ksi in the annealed condition to 26 ksi in the H-34 temper.
Other Physical Properties
Electrical conductivity 32% of copper.
Principle Design Features
AL 5454 is a non-heat treatable alloy of aluminum and magnesium. It is a moderate strength alloy that may be hardened (strengthened) by cold working.
Tempering Procedure
Not applicable.
Weldability
All of the commercial welding methods will work satisfactorily with AL 5454. The TIG or MIG process, with AL 5554 or 5356 filler rod, works especially well.
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
B209,B221,B234,B241,B404,B547,B548,A-200/6,A250/10,J454,A95454Chemical Elements
| Aluminum | Balance |
| Chromium | 0.05 - 0.2 |
| Copper | 0.1 max |
| Magnesium | 2.4 - 3 |
| Manganese | 0.5 - 1 |
| Remainder Each | 0.05 max |
| Remainder Total | 0.15 max |
| Silicon + Iron | 0.4 max |
| Titanium | 0.2 max |
| Zinc | 0.25 max |
Physical Properties
Density: 0.097lb/in³
Melting Point: 1125°F
Specific Gravity: 2.69
Mechanical Properties
Modulus of Elasticity – Tension: 10.2MSI
Thermal Conductivity
| Condition | Temperature | Conductivity |
|---|---|---|
| Annealed | 77 °F | 93 BTU/hr·ft·°F |
Thermal Expansion
| Condition | Min | Max | Expansion Coefficient |
|---|---|---|---|
| Annealed | 68 °F | 212 °F | 13.1 μin/in·°F |
Mechanical Test Data
| Form | Sheet |
| Condition | H32 |
| Temperature | -320°F |
| Elongation | 32% |
| Tensile Strength | 59 KSI |
| Yield Strength | 36 KSI |
| Form | Sheet |
| Condition | H32 |
| Temperature | -112°F |
| Elongation | 23% |
| Tensile Strength | 42 KSI |
| Yield Strength | 31 KSI |
| Form | Sheet |
| Condition | H32 |
| Temperature | -18°F |
| Elongation | 20% |
| Tensile Strength | 41 KSI |
| Yield Strength | 30 KSI |
| Form | Sheet |
| Condition | H32 |
| Temperature | 75°F |
| Elongation | 18% |
| Tensile Strength | 40 KSI |
| Yield Strength | 30 KSI |
| Form | Sheet |
| Condition | H32 |
| Temperature | 212°F |
| Elongation | 20% |
| Tensile Strength | 39 KSI |
| Yield Strength | 29 KSI |
| Form | Sheet |
| Condition | H32 |
| Temperature | 300°F |
| Elongation | 37% |
| Tensile Strength | 32 KSI |
| Yield Strength | 26 KSI |
| Form | Sheet |
| Condition | H32 |
| Temperature | 400°F |
| Elongation | 45% |
| Tensile Strength | 25 KSI |
| Yield Strength | 19 KSI |
| Form | Sheet |
| Condition | H32 |
| Temperature | 500°F |
| Elongation | 80% |
| Tensile Strength | 17 KSI |
| Yield Strength | 11 KSI |
| Form | Sheet |
| Condition | H32 |
| Temperature | 600°F |
| Elongation | 110% |
| Tensile Strength | 11 KSI |
| Yield Strength | 7.5 KSI |
| Form | Sheet |
| Condition | H32 |
| Temperature | 700°F |
| Elongation | 130% |
| Tensile Strength | 6 KSI |
| Yield Strength | 4.2 KSI |
| Form | Sheet |
| Condition | H34 |
| Temperature | -320°F |
| Elongation | 30% |
| Tensile Strength | 63 KSI |
| Yield Strength | 41 KSI |
| Form | Sheet |
| Condition | H34 |
| Temperature | -112°F |
| Elongation | 21% |
| Tensile Strength | 46 KSI |
| Yield Strength | 36 KSI |
| Form | Sheet |
| Condition | H34 |
| Temperature | -18°F |
| Elongation | 18% |
| Tensile Strength | 44 KSI |
| Yield Strength | 35 KSI |
| Form | Sheet |
| Condition | H34 |
| Temperature | 75°F |
| Elongation | 16% |
| Tensile Strength | 44 KSI |
| Yield Strength | 35 KSI |
| Form | Sheet |
| Condition | H34 |
| Temperature | 212°F |
| Elongation | 18% |
| Tensile Strength | 43 KSI |
| Yield Strength | 34 KSI |
| Form | Sheet |
| Condition | H34 |
| Temperature | 300°F |
| Elongation | 32% |
| Tensile Strength | 34 KSI |
| Yield Strength | 28 KSI |
| Form | Sheet |
| Condition | H34 |
| Temperature | 400°F |
| Elongation | 45% |
| Tensile Strength | 26 KSI |
| Yield Strength | 19 KSI |
| Form | Sheet |
| Condition | H34 |
| Temperature | 500°F |
| Elongation | 80% |
| Tensile Strength | 17 KSI |
| Yield Strength | 11 KSI |
| Form | Sheet |
| Condition | H34 |
| Temperature | 600°F |
| Elongation | 110% |
| Tensile Strength | 11 KSI |
| Yield Strength | 7.5 KSI |
| Form | Sheet |
| Condition | H34 |
| Temperature | 700°F |
| Elongation | 130% |
| Tensile Strength | 6 KSI |
| Yield Strength | 4.2 KSI |