Aluminium Alloy DTD 5014a 2618-T6511 Bar
Technical Data Sheet
| Chemical Composition Limits | ||||||||||
| Weight% | Al | Si | Fe | Cu | Mn | Mg | Ni | Zn | Other | Ti |
| DTD 5014A | Rem | 0.25 | 0.9-1.4 | 1.8-2.7 | 0.2 | 1.2-1.8 | 0.8-1.4 | 0.1 | Pb 0.05 Sn 0.05 Ti + Zr 0.2 |
0.2 |
Aluminium Alloy 2618 (2618 A) is a high strength aluminium alloy which contains both copper and magnesium. Alloy 2618 (2618A) has good machinability and is fair resistance to atmospheric attack. Aluminium Alloy 2618 (2618A) is typically used in aerospace and defence components. It is commonly used for pistons and rotating aircraft parts due to it's ability to work in higher temperature applications. 2618 is also used in high performance autosport applications.
Typical Mechanical Properties
| Material | Thickness | 0.2% Proof Stress min N/mm² | Tensile Strength min (N/mm²) | Elongation on 50mm min% | Elongation on 5.65v (min%) |
| DTD 5014A | up to and incl 10mm | 320 | 400 | 5 | - |
| DTD 5014A | 10-100mm | 340 | 420 | 7 | 8 |
Availability
Aluminium Alloy DTD 5014A is available in Bar and Section. For all stock availability of Aluminium DTD 5014A contact Sales
Specifications
Similar Specifications
2618a
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Disclaimer
Every effort is made to ensure that technical specifications are accurate. However, technical specifications included herein should be used as a guideline only. All specifications are subject to change without notice.
