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Elmet Technologies

Aluminum 2014-T6; 2014-T651
Categories: Metal; Nonferrous Metal; Aluminum Alloy; 2000 Series Aluminum Alloy

Material Notes: Used in applications requiring high strength/hardness, including elevated temperature uses. Specific applications include heavy duty forgings, plate, and extrusions for aerospace fittings, wheels, tanks, and major structural components, heavy duty automotive frame and suspension componentry. 2014 exhibits poor corrosion resistance for an aluminum alloy.

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 2014-T651; UNS A92014; ISO AlCu4SiMg; BS H15 (UK); CSA CS41N (Canada); AA2014-T651, DIN AlCuSiMn; NF A-U4SG (France); Al2014-T6
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 2.80 g/cc0.101 lb/in³AA; Typical
 
Mechanical PropertiesMetricEnglishComments
Hardness, Brinell 135135AA; Typical; 500 g load; 10 mm ball
Hardness, Knoop 170170Converted from Brinell Hardness Value
Hardness, Rockwell A 50.550.5Converted from Rockwell B
Hardness, Rockwell B 8282
Hardness, Vickers 155155Converted from Brinell Hardness Value
Tensile Strength, Ultimate >= 415 MPa>= 60200 psiExtruded tube; T62
 >= 415 MPa>= 60200 psiExtruded wire, rod, bar, and shapes; T62
 >= 450 MPa>= 65300 psiRolled or cold finished wire (rod and bar); T6, T62, T651
 483 MPa70000 psiAA; Typical
 30.0 MPa
@Temperature 371 °C
4350 psi
@Temperature 700 °F
 45.0 MPa
@Temperature 316 °C
6530 psi
@Temperature 601 °F
 66.0 MPa
@Temperature 260 °C
9570 psi
@Temperature 500 °F
 110 MPa
@Temperature 204 °C
16000 psi
@Temperature 399 °F
 276 MPa
@Temperature 149 °C
40000 psi
@Temperature 300 °F
 439 MPa
@Temperature 100 °C
63700 psi
@Temperature 212 °F
 483 MPa
@Temperature 24.0 °C
70100 psi
@Temperature 75.2 °F
 496 MPa
@Temperature -28.0 °C
71900 psi
@Temperature -18.4 °F
 510 MPa
@Temperature -80.0 °C
74000 psi
@Temperature -112 °F
 579 MPa
@Temperature -196 °C
84000 psi
@Temperature -321 °F
Tensile Strength, Yield >= 365 MPa>= 52900 psiExtruded wire, rod, bar, and shapes; T62
 >= 365 MPa>= 52900 psiExtruded tube; T62
 >= 380 MPa>= 55100 psiRolled or cold finished wire (rod and bar); T6, T62, T651
 414 MPa60000 psiAA; Typical
 24.0 MPa
@Strain 0.2 %,
Temperature 371 °C
3480 psi
@Strain 0.2 %,
Temperature 700 °F
 34.0 MPa
@Strain 0.2 %,
Temperature 316 °C
4930 psi
@Strain 0.2 %,
Temperature 601 °F
 52.0 MPa
@Strain 0.2 %,
Temperature 260 °C
7540 psi
@Strain 0.2 %,
Temperature 500 °F
 90.0 MPa
@Strain 0.2 %,
Temperature 204 °C
13100 psi
@Strain 0.2 %,
Temperature 399 °F
 241 MPa
@Strain 0.2 %,
Temperature 149 °C
35000 psi
@Strain 0.2 %,
Temperature 300 °F
 393 MPa
@Strain 0.2 %,
Temperature 100 °C
57000 psi
@Strain 0.2 %,
Temperature 212 °F
 414 MPa
@Strain 0.2 %,
Temperature 24.0 °C
60000 psi
@Strain 0.2 %,
Temperature 75.2 °F
 427 MPa
@Strain 0.2 %,
Temperature -28.0 °C
61900 psi
@Strain 0.2 %,
Temperature -18.4 °F
 448 MPa
@Strain 0.2 %,
Temperature -80.0 °C
65000 psi
@Strain 0.2 %,
Temperature -112 °F
 496 MPa
@Strain 0.2 %,
Temperature -196 °C
71900 psi
@Strain 0.2 %,
Temperature -321 °F
Elongation at Break 7.0 %7.0 %Extruded wire, rod, bar, and shapes; T62
 7.0 %7.0 %Extruded tube; T62
 8.0 %8.0 %Rolled or cold finished wire (rod and bar); T6, T62, T651
 13 %
@Temperature -80.0 °C
13 %
@Temperature -112 °F
 13 %
@Temperature -28.0 °C
13 %
@Temperature -18.4 °F
 13 %
@Temperature 24.0 °C
13 %
@Temperature 75.2 °F
 14 %
@Temperature -196 °C
14 %
@Temperature -321 °F
 15 %
@Temperature 100 °C
15 %
@Temperature 212 °F
 20 %
@Temperature 149 °C
20 %
@Temperature 300 °F
 38 %
@Temperature 204 °C
38 %
@Temperature 399 °F
 52 %
@Temperature 260 °C
52 %
@Temperature 500 °F
 65 %
@Temperature 316 °C
65 %
@Temperature 601 °F
 72 %
@Temperature 371 °C
72 %
@Temperature 700 °F
 13 %
@Diameter 12.7 mm
13 %
@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.
Tensile Modulus 72.4 GPa10500 ksi
Compressive Strength 470 MPa68200 psi
Compressive Modulus 73.8 GPa10700 ksi
Notched Tensile Strength 414 MPa60000 psi2.5 cm width x 0.16 cm thick side-notched specimen, Kt = 17.
Ultimate Bearing Strength 889 MPa129000 psiEdge distance/pin diameter = 2.0
Bearing Yield Strength 662 MPa96000 psiEdge distance/pin diameter = 2.0
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
Fracture Toughness 19.0 MPa-m½17.3 ksi-in½KIC; TL orientation.
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 0.00000432 ohm-cm
@Temperature 20.0 °C
0.00000432 ohm-cm
@Temperature 68.0 °F
AA; Typical
 
Thermal PropertiesMetricEnglishComments
CTE, linear  20.8 µm/m-°C
@Temperature -50.0 - 20.0 °C
11.6 µin/in-°F
@Temperature -58.0 - 68.0 °F
 22.5 µm/m-°C
@Temperature 20.0 - 100 °C
12.5 µin/in-°F
@Temperature 68.0 - 212 °F
 23.0 µm/m-°C
@Temperature 20.0 - 100 °C
12.8 µin/in-°F
@Temperature 68.0 - 212 °F
AA; Typical; average over range
 23.4 µm/m-°C
@Temperature 20.0 - 200 °C
13.0 µin/in-°F
@Temperature 68.0 - 392 °F
 24.4 µm/m-°C
@Temperature 20.0 - 300 °C
13.6 µin/in-°F
@Temperature 68.0 - 572 °F
 24.4 µm/m-°C
@Temperature 20.0 - 300 °C
13.6 µin/in-°F
@Temperature 68.0 - 572 °F
average
Specific Heat Capacity 0.880 J/g-°C0.210 BTU/lb-°FEstimated from trends in similar Al alloys.
Thermal Conductivity 154 W/m-K1070 BTU-in/hr-ft²-°FAA; Typical at 77°F
Melting Point 507 - 638 °C945 - 1180 °FAA; Typical range based on typical composition for wrought products >= 1/4 in. thickness. Eutectic melting is not eliminated by homogenization.
Solidus 507 °C945 °FAA; Typical
Liquidus 638 °C1180 °FAA; Typical
 
Processing PropertiesMetricEnglishComments
Annealing Temperature 413 °C775 °F
Solution Temperature 502 °C935 °F
Aging Temperature 160 °C320 °FSheet, plate, wire, rod, bar, shapes, tube; 18 hr at temperature
 171 °C340 °FForgings; 10 hr at temperature
 
Component Elements PropertiesMetricEnglishComments
Aluminum, Al 90.4 - 95 %90.4 - 95 %As remainder
Chromium, Cr <= 0.10 %<= 0.10 %
Copper, Cu 3.9 - 5.0 %3.9 - 5.0 %
Iron, Fe <= 0.70 %<= 0.70 %
Magnesium, Mg 0.20 - 0.80 %0.20 - 0.80 %
Manganese, Mn 0.40 - 1.2 %0.40 - 1.2 %
Other, each <= 0.05 %<= 0.05 %
Other, total <= 0.15 %<= 0.15 %
Silicon, Si 0.50 - 1.2 %0.50 - 1.2 %
Titanium, Ti <= 0.15 %<= 0.15 %
Zinc, Zn <= 0.25 %<= 0.25 %

References for this datasheet.

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MA2014T6 / 8847

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