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Ensinger PEI

Aluminum 2024-T361
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 Has largely superseded 2017 for structural applications.

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-T361; UNS A92024; ISO AlCu4Mg1; NF A-U4G1 (France); DIN AlCuMg2, ASME SB211; CSA CG42 (Canada); AA2024-T361; Al2024-T361
Vendors: Click here to view all available suppliers 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 130130AA; Typical; 500 g load; 10 mm ball
Hardness, Knoop 163163Converted from Brinell Hardness Value
Hardness, Rockwell A 49.549.5Converted from Brinell Hardness Value
Hardness, Rockwell B 8080Converted from Brinell Hardness Value
Hardness, Vickers 149149Converted from Brinell Hardness Value
Tensile Strength, Ultimate 496 MPa72000 psiAA; Typical
 >= 455 MPa
@Thickness 6.35 - 12.7 mm
>= 66000 psi
@Thickness 0.250 - 0.500 in
Sheet and plate
 >= 460 MPa
@Thickness 0.508 - 1.57 mm
>= 66700 psi
@Thickness 0.0200 - 0.0620 in
Sheet and plate
 >= 470 MPa
@Thickness 1.60 - 6.32 mm
>= 68200 psi
@Thickness 0.0630 - 0.249 in
Sheet and plate
Tensile Strength, Yield 393 MPa57000 psiAA; Typical
 >= 340 MPa
@Thickness 6.35 - 12.7 mm
>= 49300 psi
@Thickness 0.250 - 0.500 in
Sheet and plate
 >= 345 MPa
@Thickness 0.508 - 1.57 mm
>= 50000 psi
@Thickness 0.0200 - 0.0620 in
Sheet and plate
 >= 350 MPa
@Thickness 1.60 - 6.32 mm
>= 50800 psi
@Thickness 0.0630 - 0.249 in
Sheet and plate
Elongation at Break  >= 8.0 %
@Thickness 0.508 - 1.57 mm
>= 8.0 %
@Thickness 0.0200 - 0.0620 in
Sheet and plate
 >= 9.0 %
@Thickness 1.60 - 6.32 mm
>= 9.0 %
@Thickness 0.0630 - 0.249 in
Sheet and plate
 9.0 - 10 %
@Thickness 6.35 - 12.7 mm
9.0 - 10 %
@Thickness 0.250 - 0.500 in
Sheet and plate
 13 %
@Thickness 1.59 mm
13 %
@Thickness 0.0625 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.
Poissons Ratio 0.330.33
Fatigue Strength 124 MPa
@# of Cycles 5.00e+8
18000 psi
@# of Cycles 5.00e+8
completely reversed stress; RR Moore machine/specimen
Machinability 70 %70 %0-100 Scale of Aluminum Alloys
Shear Modulus 28.0 GPa4060 ksi
Shear Strength 290 MPa42000 psiAA; Typical
 
Electrical PropertiesMetricEnglishComments
Electrical Resistivity 0.00000582 ohm-cm
@Temperature 20.0 °C
0.00000582 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 121 W/m-K840 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
Aging Temperature 191 °C375 °F8 to 16 hr at temperature
 
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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MA2024T361 / 8866

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