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Master Bond adhesives

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Alclad Aluminum 2024-T4, T351
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 Has largely superseded 2017 for structural applications.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. Intrinsic corrosion resistance of 2024 is low for an aluminum alloy, so the clad version is used where needed.

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

Composition Notes: Composition for AA 2024 (not Alclad 2024).
Composition information provided by the Aluminum Association and is not for design.

Key Words: UNS A82024; Alclad 2024-T4, T351; Alclad 2024-T4, T351; Al2024-T4
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Physical PropertiesOriginal ValueComments
Density 2.78 g/ccFor AA2024 (Not Alclad)
 
Mechanical PropertiesOriginal ValueComments
Tensile Strength, Ultimate 64.0 ksiAA; Typical
 >= 395 MPa
@Thickness 76.23 - 102 mm
Plate; T351
 >= 400 MPa
@Thickness 0.254 - 1.52 mm
Coiled sheet
 >= 415 MPa
@Thickness 50.83 - 76.2 mm
Plate; T351
 >= 420 MPa
@Thickness 1.60 - 3.25 mm
Coiled sheet
 >= 425 MPa
@Thickness 6.35 - 12.7 mm
Plate; T351
 >= 425 MPa
@Thickness 25.43 - 50.8 mm
Plate; T351
 >= 435 MPa
@Thickness 12.7 - 25.4 mm
Plate; T351
Tensile Strength, Yield 42.0 ksiAA; Typical
 >= 250 MPa
@Thickness 0.254 - 1.52 mm
Coiled sheet
 >= 260 MPa
@Thickness 1.60 - 3.25 mm
Coiled sheet
 >= 275 MPa
@Thickness 6.35 - 12.7 mm
Plate; T351
 >= 285 MPa
@Thickness 76.23 - 102 mm
Plate; T351
 >= 290 MPa
@Thickness 12.7 - 25.4 mm
Plate; T351
 >= 290 MPa
@Thickness 25.43 - 50.8 mm
Plate; T351
 >= 290 MPa
@Thickness 50.83 - 76.2 mm
Plate; T351
Elongation at Break >= 4.0 %
@Thickness 50.83 - 76.2 mm
Plate; T351
 >= 4.0 %
@Thickness 76.23 - 102 mm
Plate; T351
 6.0 - 7.0 %
@Thickness 25.43 - 50.8 mm
Plate; T351
 >= 8.0 %
@Thickness 12.7 - 25.4 mm
Plate; T351
 >= 12 %
@Thickness 6.35 - 12.7 mm
Plate; T351
 12 - 15 %
@Thickness 0.254 - 1.52 mm
Coiled sheet
 >= 15 %
@Thickness 1.60 - 3.25 mm
Coiled sheet
 19 %
@Thickness 1.59 mm
AA; Typical
Modulus of Elasticity 10600 ksiAA; Typical; Average of tension and compression. Compression modulus is about 2% greater than tensile modulus.
Shear Strength 40.0 ksiAA; Typical
 
Processing PropertiesOriginal ValueComments
Annealing Temperature 775 °F
Solution Temperature 493 °C
 
Component Elements PropertiesOriginal ValueComments
Aluminum, Al 90.7 - 94.7 %As remainder
Chromium, Cr <= 0.10 %
Copper, Cu 3.8 - 4.9 %
Iron, Fe <= 0.50 %
Magnesium, Mg 1.2 - 1.8 %
Manganese, Mn 0.30 - 0.90 %
Other, each <= 0.05 %
Other, total <= 0.15 %
Silicon, Si <= 0.50 %
Titanium, Ti <= 0.15 %
Zinc, Zn <= 0.25 %

References for this datasheet.

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MA2024AT4 / 8861

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