Aluminum 2017-T4; 2017-T451
Subcategory: 2000 Series Aluminum Alloy; Aluminum Alloy; Metal; Nonferrous Metal
Close Analogs: 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 or producer and the purchaser have mutually so agreed. Agreement may be indicated, for example, by reference to a standard, by letter, by order note, or other means which allow the Zr + Ti limit. Aluminum content reported is calculated as remainder. Composition information provided by the Aluminum Association and is not for design.
Key Words: Aluminium 2017-T4; UNS A92017; ISO AlCuMgSi; AA2017-T4, Aluminium 2017-T451; QQ-A-4300; QQ-A-222/5; CM41 (Canada); NF A-U46 (France); MIL-R-430; AA2017-T451
Component | Wt. % | | | Al | 91.5 - 95.5 | | Cr | Max 0.1 | | Cu | 3.5 - 4.5 | | Fe | Max 0.7 | |
| Component | Wt. % | | | Mg | 0.4 - 0.8 | | Mn | 0.4 - 1 | | Other, each | Max 0.05 | | Other, total | Max 0.15 | |
| Component | Wt. % | | | Si | 0.2 - 0.8 | | Ti | Max 0.15 | | Zn | Max 0.25 | |
|
Material Notes: Data points with the AA note have been provided by the Aluminum Association, Inc. and are NOT FOR DESIGN.
Physical Properties | Metric | English | Comments |
|
Density | 2.79 g/cc | 0.101 lb/in³ | AA; Typical |
Mechanical Properties |
|
Hardness, Brinell | 105 | 105 | AA; Typical; 500 g load; 10 mm ball |
Hardness, Knoop | 132 | 132 | Converted from Brinell Hardness Value |
Hardness, Rockwell A | 42.5 | 42.5 | Converted from Brinell Hardness Value |
Hardness, Rockwell B | 66 | 66 | Converted from Brinell Hardness Value |
Hardness, Vickers | 118 | 118 | Converted from Brinell Hardness Value |
Ultimate Tensile Strength | 427 MPa | 62000 psi | AA; Typical |
Tensile Yield Strength | 276 MPa | 40000 psi | AA; Typical |
Elongation at Break | 22 % | 22 % | AA; Typical; 1/2 in. (12.7 mm) Diameter |
Modulus of Elasticity | 72.4 GPa | 10500 ksi | AA; Typical; Average of tension and compression. Compression modulus is about 2% greater than tensile modulus. |
Poisson's Ratio | 0.33 | 0.33 | Estimated from trends in similar Al alloys. |
Fatigue Strength | 124 MPa | 18000 psi | AA; 500,000,000 cycles completely reversed stress; RR Moore machine/specimen |
Machinability | 70 % | 70 % | 0-100 Scale of Aluminum Alloys |
Shear Modulus | 27 GPa | 3920 ksi | Estimated from similar Al alloys. |
Shear Strength | 262 MPa | 38000 psi | AA; Typical |
Electrical Properties |
|
Electrical Resistivity | 5.15e-006 ohm-cm | 5.15e-006 ohm-cm | AA; Typical at 68°F |
Thermal Properties |
|
CTE, linear 68°F | 23.6 µm/m-°C | 13.1 µin/in-°F | AA; Typical; Average over 68-212°F range. |
CTE, linear 250°C | 25.4 µm/m-°C | 14.1 µin/in-°F | Estimated from trends in similar Al alloys. 20-300°C. |
Specific Heat Capacity | 0.88 J/g-°C | 0.21 BTU/lb-°F | Estimated from trends in similar Al alloys. |
Thermal Conductivity | 134 W/m-K | 930 BTU-in/hr-ft²-°F | AA; Typical at 77°F |
Melting Point | 513 - 641 °C | 955 - 1185 °F | AA; Typical range based on typical composition for wrought products 1/4 inch thickness or greater. Eutectic melting is not eliminated by homogenization. |
Solidus | 513 °C | 955 °F | AA; Typical |
Liquidus | 641 °C | 1185 °F | AA; Typical |
Processing Properties |
|
Annealing Temperature | 338 - 349 °C | 640 - 660 °F | cold-work anneal |
Annealing Temperature | 413 °C | 775 °F | heat treated anneal |
Solution Temperature | 499 - 510 °C | 930 - 950 °F | |
Aging Temperature | 22.2 °C | 72 °F | |
References for this datasheet.
Some of the values displayed above may have been converted from their original units and/or rounded in
order to display the information in a consistant format. Users requiring more precise data for scientific or
engineering calculations can click on the property value to see the original value as well as raw conversions
to equivalent units. We advise that you only use the original value or one of its raw conversions in your
calculations to minimize rounding error. We also ask that you refer to MatWeb's disclaimer and terms of use
regarding this information. MatWeb data and tools provided by MatWeb, LLC.
|