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Aluminium Alloys

Aluminium 1050 / 19500

SPECIFICATIONS:-

Aluminum alloy 1050A also corresponds to the following standard designations and specifications but may not be a direct equivalent:

AA1050

S1B

A91050

IS 737 DESIGNATION 19500

 

CHEMISTRY :- UNLESS AND UNTIL SPECIFIED CUSTOMER NEED 99.50% PURE ALUMINUM.

MAJOR USE IN FORM OF SHEETS AND PLATES.

 

 

Aluminium 1060 / 19600

Aluminium Alloy 6351

Aluminium Alloy 6061

Key Words: al6061, UNS A96061; ISO AlMg1SiCu; Aluminum 6061-T6, AD-33 (Russia); AA6061-T6; 6061T6, UNS A96061; ISO AlMg1SiCu; Aluminum 6061-T651, AD-33 (Russia); AA6061-T651

 

Aluminum 6061 Commonly used in the manufacture of heavy-duty structures requiring good corrosion resistance, truck and marine components, railroad cars, furniture, tank fittings, general structural and high pressure applications, wire products, and in pipelines.

 

Chemical Composition Limits :-
Weight% Al Si Fe Cu Mn Mg Cr Zn Ti Other Each Others Total
ALLOY 6061 Bal 0.40 – 0.80 0.70 max 0.15-0.40 0.15 0.8-1.2 0.04-0.35 0.25 max 0.15 max 0.05 max 0.15 max

 

Mechanical Properties

 

Material Thickness (in) Tensile Strength (KSI) Yield Strength (KSI) Elongation
Alloy 6061 Sheet T6 0.020-0.500 42 35 10
Alloy 6061 Sheet T6 0.500-1.000 42 35 9
Alloy 6061 Sheet T6 1.00-2.00 42 35 8
Alloy 6061 Sheet T6 2.00-4.00 42 35 6
Alloy 6061 Sheet T6 4.00-6.00 40 35 6
Material Temper Diameter (in) Tensile Strength (ksi) Yield Strength (ksi) Elongation
Alloy 6061 Bar
Cold Finished
T651 All 42 35 10
Alloy 6061 Bar
Cold Finished
T6511 <0.25″ 38 35 8
Alloy 6061 Bar
Cold Finished
T6511 >0.25″ 38 35 10
Alloy 6061 Bar – T651 / T6 condition and extruded T6511/T6

 

 

Aluminium Alloy 6101-T6

Get High Conductivity 6101-T6 Aluminium from Bharat Aerospace Metals

 

6101-T6 is a high electrical conductivity Aluminum Alloy which has good mechanical properties, machinability, formability and weld-ability. It is commonly used for electrical bus bar conductor applications in enclosed bus electrical installations.

 

6101-T6 Aluminium is available in only flat forms:-

Thickness 0.25” (6.35 mm) to 1.5” (38.10 mm)

Width 0.50” (12.70 mm) to 12” (304.80 mm)

Length 40” (1016 mm)  to 144” (3657.60 mm)

WITH RADIUS AND NON-RADIUS CORNER.

Aluminium Alloy 5754

Aluminium Alloy 5056 / 55000

Aluminium Alloy 5052 / 52000

Aluminium Alloy 2007

Aluminium Alloy 2014 / 24345

Aluminium 2014A /2014 Aluminum


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

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.

Typical Mechanical Properties

Material Temper Thickness (mm) Tensile Strength min (N/mm²) Yield Strength min (N/mm²) Elongation in 50 mm
0.5 mm 0.8 mm 1.3 mm 2.6 mm 3.0 mm
2014 Sheet T4 Bare 0.2-6.0 400 225 13 14 14 14 14
2014 Sheet T6 Bare 0.2-6.0 440 380 6 6 7 7 8
2014 Sheet T4 Clad 0.2-1.6 385 240 13 14 14
2014 Sheet T4 Clad 1.6-6.0 395 245 14 14
2014 Sheet T6 Clad 0.2-1.6 420 345 7 7 8
2014 Sheet T6 Clad 1.6-6.0 420 355 9 9
Material Temper Diameter (mm) Tensile Strength min ((N/mm²) Yield Strength (min) (N/mm²) Elongation on 5.65 V (min)
2014 Bar T4 <20 370 230 11
2014 Bar T4 20-75 390 250 11
2014 Bar T4 75-150 390 250 9
2014 Bar T4 150-200 370 230 8
2014 Bar T6510 20-75 480 435 7
2014 Bar T6510 75-150 465 420 7
2014 Bar T6510 150-200 435 390 7

A

Aluminium Alloy 2024

Aluminium, 2024 Bar

This grade is a heat treatable Alloy with good strength higher than AA 2014 and 2017a which gives very good machining characteristics and high fatigue strength. The applications are Aerospace machined parts, general engineering and other military equipment.
Chemical Composition (Weight %)
Si Fe Cu Mn Mg Cr Zn Ti Other each Other total Al
Min 3.8 0.30 1.20
Max 0.50 0.50 4.9 0.90 1.80 0.10 0.25 0.15 0.05 0.15 Bal
Typical Mechanical Properties (Min)
Diameter or minor sectional dimension mm Tensile Strength, MPa Yield Strength 0.2%, MPa  Elongation %
0-12.7 427 310 10
12.7-114.30 427 290 10
114.30-165.1 427 276 10
165.1-203.2 400 262 10

Aluminium Alloy 2017

Aluminium Alloy 2017A is Equivalent to IS 733 Grade 24534 and available in Bars and Sheet form.

Aluminium Alloy 2014A

Aluminium Alloy 2011

Aluminium Alloy 3003

Aluminium Alloy 5083 / 54300

Aluminium Alloy 5086 / 53000

Aluminium Alloy 6082

Aluminium Alloy 7050

Aluminium Alloy 7475

Aluminium Alloy 7075 / DTD 5124


7075 is an aluminum alloy with zinc as the primary alloying element. It is strong, with a strength comparable to many steels, and has good fatigue strength and average machinability, but has less resistance to corrosion than many other Al alloys. Due to its high strength, low density, thermal properties and its ability to be highly polished, 7075 is widely used in mold tool manufacture.

Related Specifications :-

GOST V95 (B95)
AA7075
JIS 7075
USA A97075
W.Nr.3.4365
AlZnMgCu1.5
BS L95
BS L96
EN AW-7075
AlZnMgCu

Key Words :-

Aluminium 7075 T6
Aluminium 7075 T651
BS 2 L95 Alloy 7075-T651 Plate
BS 2 L88 Alloy 7075-T6 Clad Sheet and Strip
BS L160 Alloy 7075-T73511 Bars and Sections
BS L161 Alloy 7075 Forging Stock and Forgings
BS L162 Alloy 7075 Forging Stock and Forgings
BS L170 Alloy 7075-T6511 Bars and Sections
DTD 5110 7075 Clad Plate
DTD 5124 7075 Bars and Sections
AMS 4038 7075-T651 Superseded by AMS 4045
AMS 4039 7075-T651 Superseded by AMS 4049
AMS 4044 7075 -0 Sheet and Plate
AMS 4045 7075-T6 Sheet and T651 Plate
AMS 4046 7075-T6 Alclad one side Sheet, T651 Plate
AMS 4048 7075-T0 Alclad Sheet and Plate
AMS 4049 7075 -T6 Alclad Sheet and T651 Plate
AMS 4078 7075-T351 Plate
AMS 4122 7075-T6 Cold finished rod, bar, wire
AMS 4123 7075-T651 Cold finished bar, rod
AMS 4124 7075-T7351 Cold finished bar, rod, wire
AMS 4126 7075-T6 Forgings
AMS 4131 7075-T74 Forgings
AMS 4139 7075 Forgings (Non-Current)
AMS 4154 7075-T6 Extrusions
AMS 4166 7075-T73 Extusion
AMS 4167 7075-T73511 Extrusions
AMS 4168 7075-T6511 Extrusions Unstraightened
AMS 4169 7075-T6511 Extrusions Straightened
AMS 4174 7075-T73 Flash Welded Rings
QQ-A-250/13 7075-0 Alclad sheet and plate
QQ-A-250/13 7075-T6 Alclad sheet and plate
QQ-A-250/18 7075-0 Clad one side, sheet and plate
QQ-A-250/18 7075-T6 Clad one side, sheet and plate
QQ-A-250/24 7075-T7651 Plate
QQ-A-250/25 7075 Sheet, clad with7072-T76
QQ-A-250/26 7075 Sheet, clad with7011-T76
QQ-A-367 Alloy 7075-T6 Forgings
MIL-A-22771
AIR 9048.690 7075-T7351 Plate
AIR 9048.700 7075-T7351 Plate
AIR 9048.710 7075-T7351 Plate
AIR 9049
Aluminium 7075 materials supply’s in form of Round Bars, Sheet, Plates, Flats, Forgings and Rings.
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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, Peru

Aluminium Alloy 8011

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