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Aluminium Alloys

Alloy code

ALUMINIUM Alloy 2014,2024,6061,7075 etc

1xxx Series

Contains no alloying elements. The proportion of aluminium is 99.3 – 99.9% and the rest is formed by tiny impurities. The combination of material properties, especially superior conductivity makes these alloys suitable for applications mainly in electrical and heat-power industry. Materials of this series are considered non-hardenable alloys and have tensile strengths of 40 – 60 MPa.

2xxx Series

The alloying element is copper. Alloys of this series are high strength alloys. The strength is achieved by the heat treatment process. The tensile strength is about 400 MPa on completion of hardening. Alloys of this series are considered not suitable for surface treatments and poor forwelding.

5xxx Series

The alloying element is magnesium. Alloys of this series are moderate in strength (200 – 350 MPa). The strength is achieved by the heat treatmentprocessing or forming. Alloys of this series have excellent resistance to corrosion in aggressive atmosphere and seawater.

6xxx Series

The alloying elements are magnesium and silicon. Alloys of this series are moderate in strength (200 – 350 MPa). The strength is achieved by the heat treatmentprocessing or forming. Alloys of 6xxx series can be easily anodized.

7xxx Series

The alloying element is zinc. Alloys of this series have the highest strength among all series. The tensile strengths ranging between 450 – 500 MPa may exceed 600 MPa in some cases. These alloys prone to stress corrosion, especially when welded.

Aluminium Alloy 2024 T3511

Aluminium Alloy 2024 T3511
  • Aluminium Alloy 2024 T3511
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Approx. Price: Rs 466 / Kilogram
Aluminium Alloy 2024 T3511
Technical Data Sheet
Chemical Composition Limits
Weight%SiFeCuMnMgCrZnTiOther EachOther TotalAl
2024 USA0.50 max0.50 max3.8-4.90.3-0.91.2-1.80.10 max0.25 max0.15 max0.05 max0.15 maxRem
2024A France0.15 max0.20 max3.7-4.50.15-0.81.2-1.50.10 max0.25 max0.15 max0.05 max0.15 maxRem

Aluminium 2024 (2024A) is one of the most popular high strength Aluminium alloys when it is the heat treated condition. Due to 2024 (2024A) high strength and excellent fatigue resistance it is commonly used on structures and components in the aircraft and transportation industries.

Availability DIA 20 MM TO 300 MM
Aluminum Alloy 2024 (2024A) is available in Bar ( Flat, Round, Hexagon, Square), Sheet, Plate, Rod, Shapes and Tube. Aluminum 2024A (2024) Foil (Shim) is available in various thicknesses. View stock list for further information. Foil Stock List , Sheet Stock List, Plate Stock List. For all stock availability for Alloy 2024 contact Sales.

AMS 4033 Plate T351
AMS 4034 Plate Clad T351
AMS 4035 Sheet T0
AMS 4036 Sheet T3 Clad One Side, Plate T351
AMS 4037 Sheet T3, Plate T351
AMS 4041 Sheet T3
AMS 4088 Tube T3 Drawn
AMS 4112 Wire rod / Bar Cold Finished T6
AMS 4119 Wire rod / Bar Cold Finished T351
AMS 4120 Wire rod / Bar Cold Finished T4
AMS 4152 Extruded Wire / Rod / Bar / Shapes T3
AMS 4165 Extruded Wire / Rod / Bar / Shapes T3511

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Aluminium 7075 T651 AMS 4045 ASTM B209 AMS QQA 250/12

Aluminium 7075 T651 AMS 4045 ASTM B209 AMS QQA 250/12
  • Aluminium 7075 T651 AMS 4045 ASTM B209 AMS QQA 250/12
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Approx. Price: Rs 456 / Kilogram
7075 T651 AMS 4045 ASTM B209 AMS QQA 250/12
ALUMINUM PLATES
Aluminium Alloy // BS-L // L95 T651 Plate

Alloy 7075 aluminum plates are the outstanding member of the 7xxx series and remains the baseline among the highest strength alloys available. Zinc is the primary alloying element giving it strength comparable to steel. Temper T651 possesses good fatigue strength, fair machinability, resistance welding and corrosion resistance ratings. Alloy 7075 in temper T7x51 has superior stress corrosion resistance and replaces the 2xxx alloy in the most critical applications. It is widely used by the aircraft industry with the typical specifications of ASTM B209, AMS-QQ-A-250/4, as well as many end users requirements.

Applications:
  • Air-frame structures
  • Highly stressed aircraft parts
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  • Item Code: aluminium
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Aluminium Alloy 2014 T651 Plates

Aluminium Alloy 2014 T651 Plates
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Approx. Price: Rs 540 / Kilogram(s)
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.

Availability
Aluminium Alloy 2014 (2014A) is available in Bar, Sheet, Strip, Plate, Wire, Tube, Drawn Tube, Forging Stock and Rivet Stock. For all stock availability of Aluminium 2014 contact Sales.

Specifications
UNS A92014
Werkstoff Nr. 3.1255
Werkstoff Nr. 3.1254
AMS 4028 Sheet and Plate - Alloy 2014 T0
AMS 4029 Sheet and Plate - Alloy 2014 T651
AMS 4121 Bars, Rods, Wire (rolled or cold finished) - Alloy 2014 T6
AMS 4133 Forgings, Rolled Rings - Alloy 2014 T6
AMS 4134 Die Forgings - Alloy 2014 T4
AMS 4135 Superseded by 4133 Forgings, Rolled Rings - Alloy 2014 T6
AMS 4153 Extrusions - Alloy 2014 T6
BS 7L37 Rivet Stock
BS 3L63 Tube

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Aluminium Alloy 6061 T6 Round Bars

Aluminium Alloy 6061 T6 Round Bars
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Approx. Price: Rs 276 / Kilogram(s)
Aluminum Alloy 6061 combines most of the good qualities of aluminum. It possesses high strength, high resistance to corrosion, good workability, and a wide range of mechanical properties. It is the least expensive.
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  • Item Code: alloys
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Aluminium Alloy 6061 T6 Plate

Aluminium Alloy 6061 T6 Plate
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Approx. Price: Rs 280 / Kilogram
Aluminum Alloy 6061 combines most of the good qualities of aluminum. It possesses high strength, high resistance to corrosion, good workability, and a wide range of mechanical properties. It is the least expensive.
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  • Item Code: alloy
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Aluminium Alloy 7075 T651 Round Bars

Aluminium Alloy 7075 T651 Round Bars
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Approx. Price: Rs 445 / Kilogram
7075 AEROSPACE ALUMINUM BAR

7075 (UNS A97075) is an aerospace aluminum bar with cold finished or extruded aluminum wrought alloy with high strength, adequate machinability and improved stress corrosion control. Fine grain control results in good tool wear.

7075 is one of the highest strength aluminum alloys. It has good fatigue strength and average machinability. Often used where parts are highly stressed. It is not weld able and has less corrosion resistance than other aluminum alloys. The mechanical properties depend on the temper of the material. Commonly used in the bicycle industry, aircraft structures, and in rifles for the American military. We stock 7075-T651, 7075-T6511, 7075-T7351, 7075-T3511 and 7075-T76511

Available shapes: Flats, squares and rounds

Tempers: T6, T651, T73, T7351

Specifications: ASTM B211, AMS 4122, AMS 4123, AMS 4124, AMS4186, AMS-QQ-A-225/9, ASTM B221, AMS 4154, AMS 4166, AMS 4167, AMS-QQ-A-200/11

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Aluminium Alloy 2014 T651 Round Bars

Aluminium Alloy 2014 T651 Round Bars
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Approx. Price: Rs 376 / Kilogram

Availability
Aluminium Alloy 2014 (2014A) is available in Bar, Sheet, Strip, Plate, Wire, Tube, Drawn Tube, Forging Stock and Rivet Stock. For all stock availability of Aluminium 2014 contact Sales.

Specifications
UNS A92014
Werkstoff Nr. 3.1255
Werkstoff Nr. 3.1254
AMS 4028 Sheet and Plate - Alloy 2014 T0
AMS 4029 Sheet and Plate - Alloy 2014 T651
AMS 4121 Bars, Rods, Wire (rolled or cold finished) - Alloy 2014 T6
AMS 4133 Forgings, Rolled Rings - Alloy 2014 T6
AMS 4134 Die Forgings - Alloy 2014 T4
AMS 4135 Superseded by 4133 Forgings, Rolled Rings - Alloy 2014 T6
AMS 4153 Extrusions - Alloy 2014 T6
BS 7L37 Rivet Stock
BS 3L63 Tube

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Aluminium Alloy 6061 T651 Sheet

Aluminium Alloy 6061 T651 Sheet
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Approx. Price: Rs 450 / Kilogram(s)
6061-T6 Aluminum Properties

 

Aluminum alloys are divided into casting alloys and wrought alloys, and are best suited for different applications. Wrought aluminum alloys, such as the 6061 alloy, are worked by extruding, rolling or forging them into specified shapes. Some alloys can be heat-treated or cold-worked by different methods to increase their strength and hardness, corrosion resistance, ease of fabrication and other advantages.

Wrought and cast alloys are first graded by a 4-digit number which identifies their major alloying element. For example, 2XXX includes copper, 4XXX includes silicon, and 6XXX includes magnesium and silicon.

The alpha-numeric suffixes attached to alloys, such as 6061-T6, represent the temper, or degree of hardness. They also represent the method by which the hardness was obtained. In the case of 6061-T6 aluminum alloy, the “T6” indicates that it was solution heat-treated and artificially aged. The suffixes may include additional numbers. For instance, -T6511 would indicate that the alloy was solution heat-treated, stress-relieved by stretching, and artificially aged to reduce the possibility of distortion in machined parts.

The common grades of commercial 6061 aluminum are 6061-0, 6061-T4, and 6061-T6; however, tempers up to -T9 are produced. At Sapa Extrusions, we produce 6061 aluminum in a wide selection of tempers for use in standard and custom solid and hollow shapes, rod and bar products and seamless and structural pipe and tube, for use in an extensive variety of applications.

6061-T6 Aluminum Properties

6061-T6 aluminum properties include its structural strength and toughness. It is also offers good finishing characteristics and responds well to anodizing, including clear, clear and color dye, and hardcoat. 6061 aluminum alloy is also easily welded and joined. However, in its –T6 condition the welds may lose some strength, which can be restored by re-heat-treating and artificially aging.

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Applications for 6061-T6 Aluminum

Aluminum in its purest form is too soft and reactive to be of structural use. However, its alloys, such as 6061-T6 alloy, make it structurally stronger and more useful in the manufacturing of durable products.

6061-T6 aluminum is commonly used in aircraft construction. Although primarily used in private rather than commercial aircraft, its strength-to-weight ratio is very high, making it ideal for large parts that need to be very light, such as the plane’s fuselage and wings. This light weight also made 6061-T6 aluminum the best choice for the famous gold-anodized plaques that were mounted on board the 1972 Pioneer 10 and 1973 Pioneer 11 spacecraft.

6061-T6 aluminum properties make it a material of choice for builders of boats and watercraft because it’s strong and lightweight. It is ideal for sailboat masts and for hulls of larger yachts that cannot be made from fiberglass. Small, flat-bottom canoes are almost entirely fabricated from 6061-T6, although the bare aluminum is often coated with protective epoxy to improve its resistance to corrosion.

Other common applications of 6061-T6 aluminum include bicycle frames, applications where heat transfer is required, such as heat exchangers, air coolers and heat-sinks, and applications where 6061-T6’s non-corrosive characteristics are important, such as water, air and hydraulic piping and tubing.

Aluminum 6061-T6 alloy conducts and dissipates heat well. Since it can be extruded, it can be formed into almost any imaginable shape. With our advanced processing and heat-treating equipment, Sapa has developed an improved machinability 6061 formulation used in the ECON-O-ROD®, ECON-O-HEX®, ACC-U-ROD®, ECON-O-PLATE®, ACC-U-BAR™ and ACC-U-PLATE® products, which conforms to industry specifications.

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Aluminium-Alloy-6061-T6 Plates

Aluminium-Alloy-6061-T6 Plates
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Approx. Price: Rs 420 / Kilogram(s)
6061 - T6 PLATE

Aluminium alloy 6061 is a medium to high strength heat-treatable alloy with a strength higher than 6005A. It has very good corrosion resistance and very good weldability although reduced strength in the weld zone. It has medium fatigue strength. It has good cold formability in the temper T4, but limited formability in T6 temper. Not suitable for very complex cross sections.

Applications
Alloy 6061 is typically used for heavy duty structures in:
~ Rail coaches
~ Truck frames
~ Ship building
~ Bridges and Military bridges
~ Aerospace applications including helicopter rotor skins
~ Tube
~ Pylons and Towers
~ Transport
~ Boilermaking
~ Motorboats
~ Rivets

Chemical CompositionSpec: BS EN 573-3:2009Alloy 6061
Chemical Element% Present
Manganese (Mn)0.0 - 0.15
Iron (Fe)0.0 - 0.70
Magnesium (Mg)0.80 - 1.20
Silicon (Si)0.40 - 0.80
Copper (Cu)0.15 - 0.40
Zinc (Zn)0.0 - 0.25
Titanium (Ti)0.0 - 0.15
Chromium (Cr)0.04 - 0.35
Other (Each)0.0 - 0.05
Others (Total)0.0 - 0.15
Aluminium (Al)Balance
Properties
Physical PropertyValue
Density2.70 g/cm³
Melting Point650 °C
Thermal Expansion23.4 x10^-6 /K
Modulus of Elasticity70 GPa
Thermal Conductivity166 W/m.K
Electrical Resistivity0.040 x10^-6 Ω .m
Spec: BS EN 755-2:2008Extrusions - Up to 200mm Dia. & A/F, 5mm WT for Tube and Prof
Mechanical PropertyValue
Proof Stress240 Min MPa
Tensile Strength260 Min MPa
Hardness Brinell95 HB
Temper Types

The most common temper for 6061 aluminium is:

  • T6 - Solution heat treated and artificially aged
Supplied Forms

Alloy 6061 is typically supplied as

  • PLATE
Weldability

Weldability – Gas: Good

Weldability – Arc: Very Good

Weldability – Resistance: Good

Brazability: Good

Solderability: Good

 

Fabrication

Workability – Cold: Good

Machinability: Acceptable

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Aluminium Plate 7075 T651 AMS QQA 250/12

Aluminium Plate 7075 T651 AMS QQA 250/12
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Approx. Price: Rs 580 / Kilogram(s)
7075 ALUMINUM PLATES

Alloy 7075 aluminum plates are the outstanding member of the 7xxx series and remains the baseline among the highest strength alloys available. Zinc is the primary alloying element giving it strength comparable to steel. Temper T651 possesses good fatigue strength, fair machinability, resistance welding and corrosion resistance ratings. Alloy 7075 in temper T7x51 has superior stress corrosion resistance and replaces the 2xxx alloy in the most critical applications. It is widely used by the aircraft industry with the typical specifications of ASTM B209, AMS-QQ-A-250/4, as well as many end users requirements.

Applications:
  • Air-frame structures
  • Highly stressed aircraft parts
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Aluminium Alloy 7075 T6511 Round Bars

Aluminium Alloy 7075 T6511 Round Bars
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7075 AEROSPACE ALUMINUM BAR
Aluminium Alloy // BS-L // L170 T6511 Bar

7075 (UNS A97075) is an aerospace aluminum bar with cold finished or extruded aluminum wrought alloy with high strength, adequate machinability and improved stress corrosion control. Fine grain control results in good tool wear.

7075 is one of the highest strength aluminum alloys. It has good fatigue strength and average machinability. Often used where parts are highly stressed. It is not weld able and has less corrosion resistance than other aluminum alloys. The mechanical properties depend on the temper of the material. Commonly used in the bicycle industry, aircraft structures, and in rifles for the American military. We stock 7075-T651, 7075-T6511, 7075-T7351, 7075-T3511 and 7075-T76511

Available shapes: Flats, squares and rounds

Tempers: T6, T651, T73, T7351

Specifications: ASTM B211, AMS 4122, AMS 4123, AMS 4124, AMS4186, AMS-QQ-A-225/9, ASTM B221, AMS 4154, AMS 4166, AMS 4167, AMS-QQ-A-200/11

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Aluminium Alloy 2014 T651 Plates

Aluminium Alloy 2014 T651 Plates
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Approx. Price: Rs 466 / Kilogram(s)
Aluminium Alloy 2014 (2014 A)Aluminium Alloy // BS-L // L93 (AMS 4029) Plate 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.


Aluminium Alloy 2014 (2014A) is available in Bar, Sheet, Strip, Plate, Wire, Tube, Drawn Tube, Forging Stock and Rivet Stock. For all stock availability of Aluminium 2014 contact Sales.

Specifications
UNS A92014
Werkstoff Nr. 3.1255
Werkstoff Nr. 3.1254
AMS 4028 Sheet and Plate - Alloy 2014 T0
AMS 4029 Sheet and Plate - Alloy 2014 T651
AMS 4121 Bars, Rods, Wire (rolled or cold finished) - Alloy 2014 T6
AMS 4133 Forgings, Rolled Rings - Alloy 2014 T6
AMS 4134 Die Forgings - Alloy 2014 T4
AMS 4135 Superseded by 4133 Forgings, Rolled Rings - Alloy 2014 T6
AMS 4153 Extrusions - Alloy 2014 T6
BS 7L37 Rivet Stock
BS 3L63 Tube

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Aluminium Alloy 2014 T651 Round Bars

Aluminium Alloy 2014 T651 Round Bars
  • Aluminium Alloy 2014 T651 Round Bars
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Approx. Price: Rs 366 / Kilogram(s)

Availability
Aluminium Alloy 2014 (2014A) is available in Bar, Sheet, Strip, Plate, Wire, Tube, Drawn Tube, Forging Stock and Rivet Stock. For all stock availability of Aluminium 2014 contact Sales.

Specifications
UNS A92014
Werkstoff Nr. 3.1255
Werkstoff Nr. 3.1254
AMS 4028 Sheet and Plate - Alloy 2014 T0
AMS 4029 Sheet and Plate - Alloy 2014 T651
AMS 4121 Bars, Rods, Wire (rolled or cold finished) - Alloy 2014 T6
AMS 4133 Forgings, Rolled Rings - Alloy 2014 T6
AMS 4134 Die Forgings - Alloy 2014 T4
AMS 4135 Superseded by 4133 Forgings, Rolled Rings - Alloy 2014 T6
AMS 4153 Extrusions - Alloy 2014 T6
BS 7L37 Rivet Stock
BS 3L63 Tube

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Aluminium Alloy Plates 2014-t651

Aluminium Alloy Plates 2014-t651
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Approx. Price: Rs 406 / Kilogram(s)
pecifications
UNS A92014
Werkstoff Nr. 3.1255
Werkstoff Nr. 3.1254
AMS 4028 Sheet and Plate - Alloy 2014 T0
AMS 4029 Sheet and Plate - Alloy 2014 T651
AMS 4121 Bars, Rods, Wire (rolled or cold finished) - Alloy 2014 T6
AMS 4133 Forgings, Rolled Rings - Alloy 2014 T6
AMS 4134 Die Forgings - Alloy 2014 T4
AMS 4135 Superseded by 4133 Forgings, Rolled Rings - Alloy 2014 T6
AMS 4153 Extrusions - Alloy 2014 T6

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BS 7L37 Rivet Stock
BS 3L63 Tube
BS 2L77 Forging Stock T6 Temper
BS 2L87 Bars and Sections T6 Temper
BS 2L93 Plate Alloy 2014A
BS L102 Bars and Sections T4 Temper
BS L103 Forging Stock T4 Temper
BS L105 Tube T4 Temper S07-1011, S07-1012
BS L156 Sheet and Strip T4 Temper
BS L157 Sheet and Strip T6 Temper
BS L158 Sheet and Strip T4 Temper Close Tolerance.
BS L159 Sheet and Strip T6 Temper Close Tolerance.
BS L163 Clad Sheet and Strip T3 Temper
BS L163 Clad Sheet and Strip T4 Temper
BS L164 Clad Sheet and Strip
BS L165 Clad Sheet and Strip T6 Temper
BS L166 Clad Sheet and Strip T4 Temper Close Tolerance.
BS L167 Clad Sheet and Strip T6 Temper close Tolerance.
BS L168 Bars and Sections T6, T6510 and T6511
BS H15, HS15, HP15, HT15, HE15.
AlCu4SiMg
A-U4SG
QQ-A-200/2
QQ-A-225/4
QQ-A-250/3
DTD 5010, Alloy 2014A
DTD 5030, DTD 5040
EN 2087
EN 2088
EN 2089 SHEET
EN 2395 SHEET
EN 2100 BAR T4511, EN 2634 BAR T4511
EN 2324 BAR, EN 2639 BAR, EN 2384, EN2635 T6, T6511
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Aluminum Alloy 7075 t6

Aluminum Alloy 7075 t6
  • Aluminum Alloy 7075 t6
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Approx. Price: Rs 486 / Kilogram
Aluminum Alloy 7075 t651
7075 AEROSPACE ALUMINUM BAR

7075 (UNS A97075) is an aerospace aluminum bar with cold finished or extruded aluminum wrought alloy with high strength, adequate machinability and improved stress corrosion control. Fine grain control results in good tool wear.

7075 is one of the highest strength aluminum alloys. It has good fatigue strength and average machinability. Often used where parts are highly stressed. It is not weld able and has less corrosion resistance than other aluminum alloys. The mechanical properties depend on the temper of the material. Commonly used in the bicycle industry, aircraft structures, and in rifles for the Indian military. We stock 7075-T651, 7075-T6511, 7075-T7351, 7075-T3511 and 7075-T76511

Available shapes: Flats, squares and rounds

Tempers: T6, T651, T73, T7351

Specifications: ASTM B211, AMS 4122, AMS 4123, AMS 4124, AMS4186, AMS-QQ-A-225/9, ASTM B221, AMS 4154, AMS 4166, AMS 4167, AMS-QQ-A-200/11

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Aluminium Alloy 5083

Aluminium Alloy 5083
  • Aluminium Alloy 5083
Approx. Rs 380 / Kilogram(s)
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Aluminum Alloy 2014

Aluminum Alloy 2014
  • Aluminum Alloy 2014
Approx. Rs 456 / Kilogram(s)
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Aluminium Alloy 7075 T6511

Aluminium Alloy 7075 T6511
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Approx. Price: Rs 536 / Kilogram(s)
Aluminium Alloy 7075
 
Chemical Composition Limits
Weight%AlSiFeCuMnMgCrZnTiOther EachOthers Total
7075 minRem--1.2-2.10.185.1---
7075 maxRem0.400.502.00.302.90.286.10.200.050.15

Aluminium Alloy 7075 offers the highest strength of the common screw machine alloys. The superior stress corrosion resistance of the T173 and T7351 tempers makes alloy 7075 a logical replacement for 2024, 2014 and 2017 in many of the most critical applications. The T6 and T651 tempers have fair machinability. Alloy 7075 is heavily utilized by the aircraft and ordnance industries because of its superior strength.

Typical Mechanical Properties
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Aluminium 7075-T6511 AMS-QQ-A-200/11 AMS4169

Aluminium 7075-T6511 AMS-QQ-A-200/11 AMS4169
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Approx. Price: Rs 476 / Kilogram(s)
Aluminium Alloy 7075 T6511
Chemical Composition Limits
Weight%AlSiFeCuMnMgCrZnTiOther EachOthers Total
7075 minRem--1.2-2.10.185.1---
7075 maxRem0.400.502.00.302.90.286.10.200.050.15

Aluminium Alloy 7075 offers the highest strength of the common screw machine alloys. The superior stress corrosion resistance of the T173 and T7351 tempers makes alloy 7075 a logical replacement for 2024, 2014 and 2017 in many of the most critical applications. The T6 and T651 tempers have fair machinability. Alloy 7075 is heavily utilized by the aircraft and ordnance industries because of its superior strength.

MaterialTemperSize (")Tensile Strength (ksi)Yield Strength (ksi)Elongation in 2" %
Alloy 7075 BarT6511<0.2578707
Alloy 7075 BarT65110.25 - 0.581737

 

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Aerospace Aluminum 7050

Aerospace Aluminum 7050
  • Aerospace Aluminum 7050
Approx. Rs 550 / Kilogram(s)
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Aluminum Alloy 5052 Plate

Aluminum Alloy 5052  Plate
  • Aluminum Alloy 5052  Plate
Approx. Rs 375 / Kilogram(s)
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Aluminum Alloy 6082

Aluminum Alloy 6082
  • Aluminum Alloy 6082
Approx. Rs 375 / Kilogram(s)
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Aluminum Alloy 24345

Aluminum Alloy 24345
  • Aluminum Alloy 24345
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Approx. Price: Rs 386 / Kilogram(s)
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Aluminum 6061 T651

Aluminum 6061 T651
  • Aluminum 6061 T651
Approx. Rs 375 / Kilogram(s)
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Aluminum Alloy 2024 T3511

Aluminum Alloy 2024 T3511
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Approx. Price: Rs 496 / Kilogram(s)
Aluminium Alloy // ASTM & FED-QQ // QQ-A-200/3 T3511 Bar

A high strength alloy with, dependent upon temper, minimum Proof Stress up to 56 ksi / 385 Mpa and minimum Tensile Strength up to 70 ksi / 482 MPa.
Used in high strength applications where no welding is required.

ALLOY DESIGNATIONS

Aluminium alloy QQ-A-200/3 has similarities to the following standard designations and specifications but may not be a direct equivalent:

AMS 4164, AMS 4165

TEMPER TYPES

Alloy QQ-A-200/3 is supplied in a wide range of tempers:

  • O - Soft
  • T3 - Solution heat treated, cold worked and naturally aged
  • T3510 - Solution heat treated and stress-relieved by stretching. Equivalent to T4 condition.
  • T3511 - Solution heat treated and stress-relieved by stretching. Equivalent to T4 condition.
  • T42 - Solution heat treated and naturaly aged to a substantially stable condition
  • T81 - Solution heat treated, cold worked then artificially aged
  • T8510 - Solution heat treated, stress-relieved by stretching then artificially aged
  • T8511 - Solution heat treated, stress-relieved by stretching then artificially aged
SUPPLIED FORMS

Alloy QQ-A-200/3 is supplied in Bar, Rod, Wire, Tube and Extruded Sections.

  • Bar
  • Extrusions
  • Tube
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Aluminum Alloy 5052

Aluminum Alloy 5052
  • Aluminum Alloy 5052
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Approx. Price: Rs 300 / Kilogram(s)
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Aluminum Alloy Plates 2014 T651 Ams 4029L 150 mm Thickness

Aluminum Alloy Plates 2014 T651 Ams 4029L 150 mm Thickness
  • Aluminum Alloy Plates 2014 T651 Ams 4029L 150 mm Thickness
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Approx. Price: Rs 496 / Kilogram(s)
2014 T651 Sheet and Plate

A high strength 4 to 5% Copper alloy produced in extruded bar and profile form, in the fully heat-treated condition (solution heat-treated & artificially aged).Normally stocked in the T651 condition (stress relieved by controlled stretching) Except for sizes under 10mm diameter and over 203.2mm diameter. (T6 only). Over 203.mm diameter is manufactured to chemical composition Only.
Machinability of aluminium alloy 2014 is very good.
Typical applications of aluminium alloy 2014 are high strength componenets especially for use in the aerospace and defence industries.

Chemical CompositionSpec: BS EN 573-3:2009Alloy 2014
Chemical Element% Present
Silicon (Si)0.50 - 0.90
Iron (Fe)0.0 - 0.50
Copper (Cu)3.90 - 5.00
Zinc (Zn)0.0 - 0.25
Manganese (Mn)0.40 - 1.20
Magnesium (Mg)0.20 - 0.80
Titanium (Ti)0.0 - 0.15
Others (Total)0.0 - 0.15
Chromium (Cr)0.0 - 0.10
Nickel (Ni)0.0 - 0.10
Other (Each)0.0 - 0.05
Titanium + Zirconium (Ti+Zr)0.0 - 0.20
Aluminium (Al)Balance
Properties
Physical PropertyValue
Density2.82 g/cm³
Modulus of Elasticity71 GPa
Electrical Resistivity0.045 x10^-6 Ω .m
Thermal Conductivity138 W/m.K
Thermal Expansion23 x10^-6 /K
Melting Point535 °C
Spec: BS EN 485-2:2008Sheet - 0.4mm to 6mm
Mechanical PropertyValue
Tensile Strength440 Min MPa
Proof Stress390 Min MPa
Hardness Brinell133 HB
Spec: BS EN 485-2:2008Plate - 6mm to 12.5mm
Mechanical PropertyValue
Proof Stress395 Min MPa
Tensile Strength450 Min MPa
Elongation A50 mm7 Min %
Hardness Brinell135 HB
Spec: BS EN 485-2:2008Plate - 12.5mm to 40mm
Mechanical PropertyValue
Proof Stress400 Min MPa
Tensile Strength460 Min MPa
Hardness Brinell138 HB
Elongation A6 Min %
Spec: BS EN 485-2:2008Plate - 40mm to 60mm
Mechanical PropertyValue
Proof Stress390 Min MPa
Tensile Strength450 Min MPa
Hardness Brinell135 HB
Elongation A5 Min %
Spec: BS EN 485-2:2008Plate - 60mm to 80mm
Mechanical PropertyValue
Proof Stress380 Min MPa
Tensile Strength435 Min MPa
Hardness Brinell131 HB
Elongation A4 Min %

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Aluminium Alloy Plates Aerospace 7075 T7351 (ASTM B 209 )

Aluminium Alloy Plates Aerospace 7075 T7351 (ASTM B 209 )
  • Aluminium Alloy Plates Aerospace 7075 T7351 (ASTM B 209 )
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Aluminium Alloy Plates Aerospace 7075 T7351 (ASTM B 209 )
7075 t7351 AEROSPACE ALUMINUM plate

7075 (UNS A97075) is an aerospace aluminum bar with cold finished or extruded aluminum wrought alloy with high strength, adequate machinability and improved stress corrosion control. Fine grain control results in good tool wear.

7075 is one of the highest strength aluminum alloys. It has good fatigue strength and average machinability. Often used where parts are highly stressed. It is not weld able and has less corrosion resistance than other aluminum alloys. The mechanical properties depend on the temper of the material. Commonly used in the bicycle industry, aircraft structures, and in rifles for the Indian military. We stock 7075-T651, 7075-T6511, 7075-T7351, 7075-T3511 and 7075-T76511

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Aluminium 2024 T3511 Extrusion

Aluminium 2024 T3511 Extrusion
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Approx. Price: Rs 556 / Kilogram
Aluminium 2024 t3511 in Extrusion, Sheet, Bar SPECIFICATIONS: GRADE ALUMINIUM 2024, UNS A92024

Chandan Steel World hold a wide range of Aluminium 2024 from their facilities in the India, stocking 2024 in Bars,plate, sheet, for commercial and defense aircraft.

Application

  • Aircraft structures
  • Wing structures
  • Fuselage structures
  • Couplings
  • Hydraulic valve bodies
  • Worm gears
  • Fasteners
  • Clock parts
Grade 2024 Bar Sizes & Specifications
GRADE
SHAPETEMPERSIZE RANGESPECIFICATION
2024
RoundsT3511/2" - 10"AMS 4120 / ASTM B-211
T43/16" -10"
Square

SquaresT3511/2" - 4"

1/4" - 8"
FlatsT3511/2" x 3/4" - 4" x 6"
T41/8" x 1" - 3/8" x 6"
Grade 2024 Bar Typical Mechanical Properties (Not For Design)
GRADETesnile-ksiYield-ksiElongation-%Brinell Hardness (BHN)
2024684719120



Grade 2024 Plate Sizes & Specifications
GRADESHAPETEMPERTHICKNESSSPECIFICATION
2024PlateT3511/4" - 4"AMS 4037 / ASTM B209

 

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Aluminium 7075 T6 AMS-QQ-A-200/11 AMS 4154

Aluminium 7075 T6 AMS-QQ-A-200/11 AMS 4154
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Aluminium 7075 in Plate, Sheet, Bar, Extrusion SPECIFICATIONS: GRADE ALUMINIUM 7075, UNS A97075

Chandan Steel World stocks a wide range of Aluminium 7075 in Plate, Sheet, Bar, Extrusion and Tube, available from inventory, from our facilities in the India, fully qualified to the highest industry standards. Combined with our large capacity cutting, profiling and CNC capabilities, we can meet requirements for the most demanding customers in aerospace and commercial industries:

 

Properties of 7075 / UNS A97075Applications
  • Aircraft skins
  • Aircraft cowls
  • Aircraft structures
  • Rock climbing equipment
  • Bicycle components
  • Hang glider airframes
  • Meter shafts and gears
  • Fuse parts
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Aluminium 2024 (2024A) Flats

Aluminium 2024 (2024A) Flats
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Approx. Price: Rs 666 / Kilogram
Aluminium Alloy 2024 (2024A) -Flats
Aluminium Alloy // BS-L // L97 T351 Plate
Technical Data Sheet
Chemical Composition Limits
Weight%SiFeCuMnMgCrZnTiOther EachOther TotalAl
2024 USA0.50 max0.50 max3.8-4.90.3-0.91.2-1.80.10 max0.25 max0.15 max0.05 max0.15 maxRem
2024A France0.15 max0.20 max3.7-4.50.15-0.81.2-1.50.10 max0.25 max0.15 max0.05 max0.15 maxRem

Aluminium 2024 (2024A) is one of the most popular high strength Aluminium alloys when it is the heat treated condition. Due to 2024 (2024A) high strength and excellent fatigue resistance it is commonly used on structures and components in the aircraft and transportation industries.

Availability DIA 20 MM TO 300 MM
Aluminum Alloy 2024 (2024A) is available in Bar ( Flat, Round, Hexagon, Square), Sheet, Plate, Rod, Shapes and Tube. Aluminum 2024A (2024) Foil (Shim) is available in various thicknesses. View stock list for further information. Foil Stock List , Sheet Stock List, Plate Stock List. For all stock availability for Alloy 2024 contact Sales.

AMS 4033 Plate T351
AMS 4034 Plate Clad T351
AMS 4035 Sheet T0
AMS 4036 Sheet T3 Clad One Side, Plate T351
AMS 4037 Sheet T3, Plate T351
AMS 4041 Sheet T3
AMS 4088 Tube T3 Drawn
AMS 4112 Wire rod / Bar Cold Finished T6
AMS 4119 Wire rod / Bar Cold Finished T351
AMS 4120 Wire rod / Bar Cold Finished T4
AMS 4152 Extruded Wire / Rod / Bar / Shapes T3
AMS 4165 Extruded Wire / Rod / Bar / Shapes T3511

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2024 T3 ASM-QQ--A-200/3 AMS 4152 Aluminium Alloy Bar

2024 T3  ASM-QQ--A-200/3 AMS 4152 Aluminium Alloy Bar
  • 2024 T3  ASM-QQ--A-200/3 AMS 4152 Aluminium Alloy Bar
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AlloysTempersSpecifications



2024O, T3, T3511ASTM B221, B241; AMS 4152; ASME SB221; AMS-QQ-A-200/3
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2024 T3511 AMS-QQ-A-200/3 AMS4165 Aluminium Alloy Bar

2024 T3511 AMS-QQ-A-200/3 AMS4165 Aluminium Alloy Bar
  • 2024 T3511 AMS-QQ-A-200/3 AMS4165 Aluminium Alloy Bar
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2024 ALUMINUM BAR (Chandan STEEL WORLD)

AL-2024 (UNSA902404) is an aerospace aluminum bar with cold finished or extruded aluminum wrought product providing high to moderate strength, very good machinability and weld ability with improved stress corrosion cracking resistance.

2024 is known as the “aircraft alloy” in machining rod. It is one of the most popular alloys for cold heading and roll threading applications. It has high strength and excellent fatigue resistance. It is excellent on parts where good strength –to-weight ratio is needed. Machinability is good in heat treated and annealed condition. Commonly used in aircraft structural components, truck wheels, medical instruments, and screw machine products. We stock 2024-T351, 2024-T3511, and 2024-T4.

Available shapes: Flats, squares and rounds

Tempers: T351, T3511 & T4

Specifications: ASTM B211, AMS 4120, AMS 4339, AMS-QQ-A-225/6, ASTM B221, AMS 4152, AMS 4164, AMS 4165, AMS-QQ-A-200/3 

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Aluminium Alloy 2618 T6 Round Bar

Aluminium Alloy 2618 T6 Round Bar
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Aluminium Alloy 2618A (Aluminum 2618)
Technical Data Sheet
 
Chemical Composition Limits
Weight%AlSiFeCuMnMgNiZnTiZr + TiOther EachOthers Total
2618 USARem0.10-0.250.9-1.31.9-2.7-1.3-1.80.9-1.20.10 max0.04-0.10-0.05 max0.15 max
2618A EAARem0.15-0.250.9-1.41.8-2.70.25 max1.2-1.80.8-1.40.15 max0.20 max0.25 max0.05 max0.15 max

Aluminium Alloy 2618A (Aluminum 2618) 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 2618A (Aluminum 2618) 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
 
MaterialSizeDiameter (mm)Tensile Strength min (N/mm²)Yield Strength min (N/mm²)Elongation in 50 mm %
2618AExtruded Bar<104003205
2618Extruded Bar10-1004203407
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Aluminium 24345 Plate

Aluminium 24345 Plate
  • Aluminium 24345 Plate
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Approx. Price: Rs 506 / Kilogram

Chandan Steel World are among some of the most trusted names in the industry engaged in stocking and exporting a wide range of Aluminium 24345 Plates.

HOW ALLOYING ELEMENTS AFFECT ALUMINIUM

Series

Main Alloy

Effect on Alloying Elements

1000

Non (99% Alum.)

Unalloyed aluminium is highly corrosion resistant, low strength, workable, conductive, Non-heat-treatable.

2000

Copper Based

Gives strength, hardness, machinability, Heat-treatable

3000

Manganese Based

Adds moderate strength, good workability. Non-heat-treatable

5000

Magnesium Based

Moderate to high strength. Corrosion resistant. Non-heat-treatable

6000

Magnesium & Silicon Based

Increase strength, formability, corrosion resistant. Heat-treatable.

7000

Zinc Based

For greatest strength. Heat-treatable.

 

 

Chandan Steel World is a huge importer and stockist of Aluminium 24345 Plates in india.


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Alumunium he-15

Alumunium he-15
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Approx. Price: Rs 506 / Kilogram
Aluminium HE15 (2014A /2014 Aluminum )
Technical Data Sheet
Chemical Composition Limits
Weight%AlSiFeCuMnCrMgNiZnTi+ZrTiOther EachOther Total
2014a AECMARem0.50 - 0.900.50 max3.9 - 5.00.4-1.20.10 max0.2-0.80.1 max0.25 max0.20 max0.15 max0.05 max0.15 max
2014 USARem0.50-1.200.7 max3.9 - 5.00.4 - 1.20.10 max0.2-0.8-0.25 max-0.15 max0.05 max0.15 max

Aluminium Alloy HE-15 ,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.

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Aluminium Alloy 74530 Wp

Aluminium Alloy 74530 Wp
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IS 74530
 
Chemical Composition
Elements
Alloy Designation
AAIS 74530
minmaxminmax
Cu
-0.20
Mn
0.200.70
Si
-0.40
Mg
1.001.50
Fe
-0.70
Zn
4.005.00
Ti
-0.20
Cr
-0.20
Ni
--
Others
0.030.10
AI
Remainder-

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Aluminium Alloy - L168 T6511 Bar

Aluminium Alloy - L168 T6511 Bar
  • Aluminium Alloy - L168 T6511 Bar
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Approx. Price: Rs 386 / Kilogram
SPECIFICATIONSAerospace L168 T6511Commercial 2014AAluminium alloy L168 - 2014A is a very highmechanical strength alloy used for critical applicationsand is the most widely used aluminium bar alloy in theaerospace industry.It has very good machinability and is thus used for theproduction of complex machined parts.CHEMICAL COMPOSITIONBS L168(1978)Alloy L168Element % PresentCopper (Cu) 3.90 - 5.00Manganese (Mn) 0.40 - 1.20Silicon (Si) 0.50 - 0.90Magnesium (Mg) 0.20 - 0.80Iron (Fe) 0.0 - 0.50Zinc (Zn) 0.0 - 0.25Titanium + Zirconium(Ti+Zr) 0.0 - 0.20Titanium (Ti) 0.0 - 0.15Others (Total) 0.0 - 0.15Chromium (Cr) 0.0 - 0.10Nickel (Ni) 0.0 - 0.10Other (Each) 0.0 - 0.05Aluminium (Al) BalanceALLOY DESIGNATIONSAluminium alloy BS L168 - 2014A has similarities tothe following standard designations and specifications
TEMPER TYPESThe most common tempers for L168 - 2014Aaluminium are:• T6 - Solution heat treated and artificially agedT6510 - Solution heat treated and stress-relieved bystretching then artificially aged with no straighteningafter aging - Equivalent to T4 condition•T6511 - Solution heat treated and stress-relieved bystretching then artificially aged with minorstraightening after aging - Equivalent to T4 condition•SUPPLIED FORMSL168-2014A aluminium is supplied in Bar, Rod andExtruded Sections.• Bar• Extrusions
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2011 T3 Aluminium Rod and Bar

2011 T3 Aluminium Rod and Bar
  • 2011 T3 Aluminium Rod and Bar
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2011 T3 Rod and Bar

Aluminium alloy 2011 is a high mechanical strength alloy that machines exceptionally well. Often called a Free Machining Alloy or ‘FMA’ it is well suited to use in automatic lathes.
Machining at high speeds produces fine chips that are easily removed. The excellent machining characteristics allow the production of complex and detailed parts. In some circumstances 2011 can replace free machining brass without the need for alterations to tooling.
It has poor corrosion resistance, which means parts made from 2011 tend to be anodised to provide additional surface protection.
When higher levels of corrosion resistance are required, 6262 T9 may be a suitable replacement.

Applications - 2011 is typically used in applications that require parts manufactured by repetition machining. These applications may include:
Appliance parts trim
Automotive trim
Fasteners and fittings
Ordnance

Alloy Designations

Aluminium alloy 2011 also corresponds to the following standard designations and specifications but may not be a direct equivalent :

AlCu6BiPb

FC1

A92011

CB60

3.1655  

AlCuBiPb:

Temper Types

The most common temper for 2011 aluminium bar - extruded and drawn - is:

  • T3 - Solution heat treated, cold worked and naturally aged
Supplied Forms

 

  • Bar
Weldability

Alloy 2011 has extremely poor weldability and thus welding is not recommended.  However, as it is used for machined parts there is rarely a need to weld this alloy.

 

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2017A Aluminium Round Extruded

2017A Aluminium Round Extruded
  • 2017A Aluminium Round Extruded
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Approx. Price: Rs 556 / Kilogram

Aluminum 2017 is a heat treatable wrought alloy that offers decent strength, ductility, and good machinability. Aluminum 2017 offers more strength than Aluminum 2011, and has fair workability and corrosion resistance.

As with many aluminum alloys, Aluminum 2017 should not be welded as it reduces the alloy’s corrosion resistance.

Because of its unique properties, Aluminum 2017 is popular for a number of different applications including:

  • Aerospace components
  • Rivets
  • General structural components
  • Transportation
  • Fasteners
  • Screw machine products
  • Gauges
  • Pulleys
  • Needles for knitting

To be called Aluminum 2017, an alloy must have a chemical composition that consists of:

  • Al 91.5-95.5%
  • Cu 3.5-4.5%
  • Mn 0.4-1%
  • Fe 0.7% max
  • Mg 0.4-0.8%
  • Zn 0.25% max
  • Ti 0.15%
  • Cr 0.1%

Chandan Steel World offers Aluminum 2017 in a variety of shapes and sizes including sheet, plate, wire, tube, rod, and bar.

All the Aluminum 2017 Chandan Steel World stocks and sells meets the most exacting standards including those from AMS, ASTM, QQ, SAE, and UNS. To discover if Aluminum 2017 is right for your next project, please contact an aluminum alloy expert at Chandan Steel World today.

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