|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|
Aluminium Alloy 2014 (2014 A) is a copper based alloy with very high strength together with excellent machining characteristics. Alloy 2014 is commonly used in many aerospace structural applications due to its high strength. Other applications include military vehicles, bridges, weapons manufacture and structural applications.
|Material||Temper||Diameter (mm)||Tensile Strength min ((N/mm²)||Yield Strength (min) (N/mm²)||Elongation on 5.65 V (min)|
|Minimum Order Quantity||20 Kilogram|
|Size||200 to 2000 mm|
|Minimum Order Quantity||10 Kilogram|
|Dimensions (l x b x h)||45 x 1000 x 2000|
We are highlighting our supply of alloy 8090, a speciality Aluminum Lithium (Al Li) alloy.
Alloy 8090 has many uses including commercial and military aerospace applications, as well as space vehicles including commercial rocketry and satellite applications.
Our Alloy 8090 offers increased fatigue strength, cryogenic durability, high stiffness, reduced ductility, fracture toughness, and resistance to fatigue crack. Composition by weight (percentage) is: 2.5 Li, 0.12 Zr, 1.3 Cu, 0.95 Mg, and 95.13 Al.
Density: 2.55 G/cm
Elastic Modulus: 77 GPa
We have assorted bar stock, rounds, and sheets (meeting AMS 4259) on hand with the ability to create customized orders of additional sizes with reduced lead times for your manufacturing needs.
General Characteristics Of Aluminum 7475
Aluminum 7475 offers strength and fracture toughness while resisting fatigue crack propagation. It’s an ideal aircraft alloy appropriate for fuselage skins and bulkheads, and wing parts for commercial, fighter and transport airplanes.
Chemical Composition Of Aluminum 7475
Heat Treatment Of Aluminum 7475
Applications Of Aluminum 7475
· Upper and lower skins
· Center structures
Corrosion Resistance Of Aluminum 7475
Workability Of Aluminum 7475
Estonia, Portugal, Oman, Trinidad & Tobago,Tunisia, United Kingdom, Iran, Bhutan, United States, Vietnam, Chile, Iran, Azerbaijan, Taiwan, Poland, Italy, Mexico, Ireland, Chile, Gabon, Belgium, France, Ecuador, Lebanon, Canada, Namibia, Brazil, Germany, Norway, Angola, Pakistan, Turkey, Philippines, Nigeria, Belarus, New Zealand, Puerto Rico, Iraq, Hong Kong, Mongolia, Czech Republic, Mexico, Japan, Sri Lanka, Nepal, Finland, Malaysia, South Africa, Spain, Ukraine, Argentina, Afghanistan, Venezuela, Slovakia, Russia, Gambia, Singapore, Austria, Saudi Arabia, Bolivia, Israel, Netherlands, Switzerland, Greece, Indonesia, United Arab Emirates, China, Nigeria, Tibet, Croatia, Kuwait, Poland, Morocco, Kazakhstan, Libya, Romania, Colombia, Bahrain, Bulgaria, Yemen, Zimbabwe, Bangladesh, South Korea, Macau, Ghana, Jordan, Kenya, Australia, Qatar, Egypt, Denmark, Lithuania, Sweden, India, Costa Rica, Algeria, Hungary, Serbia, Thailand, PeruApplications/markets:
EN 6061 T6
AA 6061 T651
The alloy EN AW-6061 is a high strength alloy for highly loaded structural applications. Typical applications are scaffolding elements, rail coach parts, containers, machine building and aerospace parts. This alloy is equivalent to EN AW- 6082, however due to its higher Cu-content, the corrosion resistance is somewhat lower.
|Grade||L168 - 2014A|
Aluminum alloy L168 - 2014A is a very high mechanical strength alloy used for critical applications and is the most widely used aluminium bar alloy in the aerospace industry.
It has very good machinability and is thus used for the production of complex machined parts.
Aluminum alloy BS L168 - 2014A has similarities to the following standard designations and specificationsbut may not be a direct equivalent:
2014, AMS4121TEMPER TYPES
The most common tempers for L168 - 2014A aluminum are:
L168-2014A aluminum is supplied in Bar, Rod and Extruded Sections.
Aluminum Alloy 6061, sheet, bar, rod, plate, wire, tube, extrusions.
British Standard H20, HE20, HP20, HS20
L118 T6 Tube Hydraulically Tested
AMS 4009 6061T0 Foil
AMS 4021 AlClad 6061 T0 Temper Sheet and Plate
AMS 4022 AlClad 6061 T4 Temper Sheet and Plate
AMS 4023 AlClad 6061 T6 Temper Sheet and Plate
AMS 4025 6061 T0 Temper Sheet and Plate
AMS 4026 6061 T4 Temper Sheet and Plate
AMS 4027 6061 T6 Temper Sheet and Plate
AMS 4053 6061 T651 Plate
AMS 4079 6061 T0 Drawn Tube, Special Tolerances
AMS 4080 6061 T0 Drawn Tube Drawn Tube
AMS 4081 6061 T4 Drawn Hydraulic Tube
AMS 4082 6061 T6 Drawn Tube
AMS 4083 6061 T6 Drawn Hydraulic Tube
AMS 4113 6061 T6 Structural Shapes
AMS 4115 6061 T0 Rolled, Drawn or Cold Finish Wire Rod and Bar
AMS 4117 6061 T6 Rolled, Drawn or Cold Finish Wire Rod and Bar
AMS 4129 6061 T651 Rolled or Cold Finish Rod and Bar
AMS 4146 6061T4 Forgings QQ-A-367
AMS 4150 6061 T6 Extruded Wire Rod and Bar Shapes and Tube
AMS 4160 6061T0 Extrusion ASTM B221
AMS 4161 6061T4 Extrusion ASTM B221
AMS 4173 6061 T651 Extruded Wire Rod and Bar Shapes and Tube
MIL-T-7081 Hydraulic Tube
WW-T-700/6 Drawn Tube. Seamless
QQ-A-200/8 Extruded Bar, Rod, Shapes and Tube
QQ-A-200/16 Extruded Structural Shapes
QQ-A-225/8 Rolled, Drawn or Cold Finished Wire, Rod, Bar and Special shapes
QQ-A-250/11 Sheet and Plate
Germany 3.3211 AlMgSiCu
Key Words: Aluminium 2024-T351; AA2024-T351, Aluminium 2024-T4; UNS A92024; ISO AlCu4Mg1; NF A-U4G1 (France); DIN AlCuMg2; AA2024-T4, ASME SB211; CSA CG42 (Canada)
|1100||AMS-4001, 4003, QQ-A-250/1|
|2024-ALCLAD||AMS-4040, 41, QQ-A-250/5|
|2219||AMS-4031, 94, 95, QQ-A-250/30|
|3003||AMS-4006, 4008, QQ-A-250/2|
|5052||AMS-4015, 16, 17, QQ-A-250/8|
|6061||AMS-4025, 26, 27, QQ-A-250/11|
|7050||AMS-4050, 4201, BMS-7-194|
|7075-BARE||AMS-4044, 45, QQ-A-250/12|
|7075-ALCLAD||AMS-4048, 49, QQ-A-250/13|
Like 2011, this is also a general-purpose alloy for automatic screw machine work. It is stronger than 2011, but harder to machine and does not have the fine chip associated with 2011. It is recommended for heavy-duty parts because of its high strength. Workability is fair, with ductility and formability considered better that 2014. Arc and resistance weldability are satisfactory. Corrosion resistance is fair. It is used for rivets, fasteners and aircraft components.Technical Data Sheet
|Chemical Composition Limits|
|Weight%||Al||Si||Fe||Cu||Mn||Mg||Cr||Zn||Ti||Others Each||Other Total|
|2017 USA||Rem||0.20-0.8||0.7 max||3.5-4.5||0.40-1.0||0.40-0.8||0.10 max||0.25 max||0.15 max||0.05 max||0.15 max|
|Weight%||Al||Si||Fe||Cu||Mn||Mg||Cr||Zn||Zr + Ti||Others Each||Other Total|
|2017A EAA||Rem||0.20-0.8||0.7 max||3.5-4.5||0.40-1.0||0.40-1.0||0.10 max||0.25 max||0.25 max||0.05 max||0.15 max|
Aluminium Alloy 2017 (2017 A) has high strength with excellent fatigue strength. Alloy 2017 also has very good machining characteristics. It is suitable for welding only by resistance welding. Alloy 2017 (2017 A) is used for various applications from high strength structural components, aircraft, machine construction, military equipment, rivets.