aluminium 2014 roundbars

aluminium 2014 roundbars

aluminium 2014 roundbars   is a copper-alloy that typically contains between 4.0 and 5.0 % copper. It is a short-chipped alloy, which is suitable for treatment, and it has high strength and is thereby as EN AW-2011 and EN AW-2007. It is harder than an EN AW-2011. Typically, you use the alloy for military purposes and for the aviation industry. It is approved after the ROHS.

Category:

Aluminium Alloy 2014 (2014A)

Alloy 2014 (2014A) Sheet and Plate – Alloy 2014 (2014A) Bars, Rods, Wire (rolled or cold finished) – Alloy 2014 (2014A) Exporters & Supplier in Switzerland, New Zealand,Netherlands,Brazil,Colombia,Egypt, Iraq,Malaysia, Nigeria, Singapore.

2014 aluminium alloy (aluminum) is an aluminium-based alloy often used in the aerospace industry.

It is easily machined in certain tempers, and among the strongest available aluminium alloys, as well as having high hardness. However, it is difficult to weld, as it is subject to cracking.

2014 is the second most popular of the 2000-series aluminum alloys, after 2024 aluminum alloy. It is commonly extruded and forged. The corrosion resistance of this alloy is particularly poor. To combat this, it is often clad with pure aluminum. If unclad 2014 aluminum is to be exposed to the elements,
it should be painted as a corrosion protection measure.

available in on order with variety of Temper-Conditions.
2014-H111 Aluminum 2014-O Aluminum
2014-T3 Aluminum 2014-T351 Aluminum
2014-T3510 Aluminum 2014-T3511 Aluminum
2014-T4 Aluminum 2014-T42 Aluminum
2014-T451 Aluminum 2014-T4510 Aluminum
2014-T4511 Aluminum 2014-T6 Aluminum
2014-T62 Aluminum 2014-T651 Aluminum
2014-T6510 Aluminum 2014-T6511 Aluminum
2014-T652 Aluminum

Key phrases : Aluminium 2014-T651; UNS A92014; ISO AlCu4SiMg; BS H15 (UK); CSA CS41N (Canada);

AA2014-T651, DIN AlCuSiMn; NF A-U4SG (France)

Machining :  This alloy has high mechanical properties,

excellent resistance to fatigue, good attitude to forging and a fair machinability.

Application : Main applications: high structural resistance components for aircraft and defense.

According to EU directives:
2000/53/CE (ELV) – 2011/65/EU (RoHS II)

Technical Data Sheet
Chemical Composition Limits
Weight% Al Si Fe Cu Mn Cr Mg Ni Zn Ti+Zr Ti Other Each Other Total
2014a AECMA Rem 0.50 – 0.90 0.50 max 3.9 – 5.0 0.4-1.2 0.10 max 0.2-0.8 0.1 max 0.25 max 0.20 max 0.15 max 0.05 max 0.15 max
2014 USA Rem 0.50-1.20 0.7 max 3.9 – 5.0 0.4 – 1.2 0.10 max 0.2-0.8 0.25 max 0.15 max 0.05 max 0.15 max

MECHANICAL PROPERTIES 2014 ALUMINIUM ALLOY ROUND HEX BARS RODS SUPPLIERS TRADERS

Mechanical Property Value
Tensile Strength 440 Min MPa
Proof Stress 390 Min MPa
Hardness Brinell 133 HB

MECHANICAL PROPERTIES 2014 ALUMINIUM ALLOY ROUND HEX BARS RODS SUPPLIERS TRADERS

Mechanical Property Value
Proof Stress 395 Min MPa
Tensile Strength 450 Min MPa
Elongation A50 mm 7 Min %
Hardness Brinell 135 HB

PHYSICAL PROPERTIES OF 2014 ALUMINIUM ALLOY ROUND HEX BARS RODS SUPPLIERS TRADERS

Physical Property Value
Density 2.82 g/cm³
Modulus of Elasticity 71 GPa
Electrical Resistivity 0.045 x10^-6 Ω .m
Thermal Conductivity 138 W/m.K
Thermal Expansion 23 x10^-6 /K
Melting Point 535 °C