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Elmet Technologies

Aluminum 2024-O
Categories: Metal; Nonferrous Metal; Aluminum Alloy; 2000 Series Aluminum Alloy

Material Notes: General 2024 characteristics and uses (from Alcoa): Good machinability and surface finish capabilities. A high strength material of adequate workability. Has largely superseded 2017 for structural applications. Use of 2024-O not recommended unless subsequently heat treated.

Uses: Aircraft fittings, gears and shafts, bolts, clock parts, computer parts, couplings, fuse parts, hydraulic valve bodies, missile parts, munitions, nuts, pistons, rectifier parts, worm gears, fastening devices, veterinary and orthopedic equipment, structures.

Data points with the AA note have been provided by the Aluminum Association, Inc. and are NOT FOR DESIGN.

Composition Notes:
A Zr + Ti limit of 0.20 percent maximum may be used with this alloy designation for extruded and forged products only, but only when the supplier and the purchaser have mutually agreed.
Composition information provided by the Aluminum Association and is not for design.

Key Words: Aluminium 2024-O; UNS A92024; ISO AlCu4Mg1; NF A-U4G1 (France); DIN AlCuMg2; AA2024-O, ASME SB211; CSA CG42 (Canada); Al2024-O
Vendors: No vendors are listed for this material. Please click here if you are a supplier and would like information on how to add your listing to this material.
 
Physical PropertiesMetricEnglishComments
Density 2.78 g/cc0.100 lb/in³AA; Typical
 
Mechanical PropertiesMetricEnglishComments
Hardness, Brinell 4747AA; Typical; 500 g load; 10 mm ball
Tensile Strength, Ultimate 186 MPa27000 psiAA; Typical
 <= 220 MPa<= 31900 psiSheet and plate
 <= 220 MPa<= 31900 psiDrawn tube
 <= 240 MPa<= 34800 psiWire, rod, and bar (rolled or cold finished)
 <= 240 MPa<= 34800 psiWire, rod, bar and shapes (extruded)
 <= 240 MPa<= 34800 psiExtruded tube
 <= 240 MPa<= 34800 psiRivet and cold-heading wire and rod
Tensile Strength, Yield 75.8 MPa11000 psiAA; Typical
 <= 95.0 MPa<= 13800 psiSheet and plate
 <= 105 MPa<= 15200 psiDrawn tube
 <= 130 MPa<= 18900 psiWire, rod, bar and shapes (extruded)
 <= 130 MPa<= 18900 psiExtruded tube
Elongation at Break >= 12 %>= 12 %Sheet and plate
 >= 12 %>= 12 %Wire, rod, bar and shapes (extruded)
 >= 12 %>= 12 %Extruded tube
 >= 16 %>= 16 %Wire, rod, and bar (rolled or cold finished)
 20 %
@Thickness 1.59 mm
20 %
@Thickness 0.0625 in
AA; Typical
 22 %
@Diameter 12.7 mm
22 %
@Diameter 0.500 in
AA; Typical
Modulus of Elasticity 73.1 GPa10600 ksiAA; Typical; Average of tension and compression. Compression modulus is about 2% greater than tensile modulus.
Ultimate Bearing Strength 345 MPa50000 psiEdge distance/pin diameter = 2.0
Bearing Yield Strength 131 MPa19000 psiEdge distance/pin diameter = 2.0
Poissons Ratio 0.330.33
Fatigue Strength 89.6 MPa
@# of Cycles 5.00e+8
13000 psi
@# of Cycles 5.00e+8
completely reversed stress; RR Moore machine/specimen
Machinability 30 %30 %0-100 Scale of Aluminum Alloys
Shear Modulus 28.0 GPa4060 ksi
Shear Strength 124 MPa18000 psiAA; Typical
 
Electrical PropertiesMetricEnglishComments
Electrical Resistivity 0.00000349 ohm-cm
@Temperature 20.0 °C
0.00000349 ohm-cm
@Temperature 68.0 °F
AA; Typical
 
Thermal PropertiesMetricEnglishComments
CTE, linear  21.1 µm/m-°C
@Temperature -50.0 - 20.0 °C
11.7 µin/in-°F
@Temperature -58.0 - 68.0 °F
 22.9 µm/m-°C
@Temperature 20.0 - 100 °C
12.7 µin/in-°F
@Temperature 68.0 - 212 °F
 23.2 µm/m-°C
@Temperature 20.0 - 100 °C
12.9 µin/in-°F
@Temperature 68.0 - 212 °F
AA; Typical; average over range
 23.8 µm/m-°C
@Temperature 20.0 - 200 °C
13.2 µin/in-°F
@Temperature 68.0 - 392 °F
 24.7 µm/m-°C
@Temperature 20.0 - 300 °C
13.7 µin/in-°F
@Temperature 68.0 - 572 °F
Specific Heat Capacity 0.875 J/g-°C0.209 BTU/lb-°F
Thermal Conductivity 193 W/m-K1340 BTU-in/hr-ft²-°FAA; Typical at 77°F
Melting Point 502 - 638 °C935 - 1180 °FAA; Typical range based on typical composition for wrought products >= 1/4 in. thickness. Eutectic melting is not eliminated by homogenization.
Solidus 502 °C935 °FAA; Typical
Liquidus 638 °C1180 °FAA; Typical
 
Processing PropertiesMetricEnglishComments
Annealing Temperature 413 °C775 °F
Solution Temperature 493 °C919 °F
 
Component Elements PropertiesMetricEnglishComments
Aluminum, Al 90.7 - 94.7 %90.7 - 94.7 %As remainder
Chromium, Cr <= 0.10 %<= 0.10 %
Copper, Cu 3.8 - 4.9 %3.8 - 4.9 %
Iron, Fe <= 0.50 %<= 0.50 %
Magnesium, Mg 1.2 - 1.8 %1.2 - 1.8 %
Manganese, Mn 0.30 - 0.90 %0.30 - 0.90 %
Other, each <= 0.05 %<= 0.05 %
Other, total <= 0.15 %<= 0.15 %
Silicon, Si <= 0.50 %<= 0.50 %
Titanium, Ti <= 0.15 %<= 0.15 %
Zinc, Zn <= 0.25 %<= 0.25 %

References for this datasheet.

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