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We are engaged in offering a wide range of Aluminium Product. Our products are corrosion resistant, water repellent and are thermostatically approved. We have client centric approach and satisfy over clients in all respects. Copper alloy products offer wide application in electric motors, backing plate’s castings and welding applications. These also offers main tool in engineering accessories. The wide range offered by us includes copper pipes and cu tubes.
Aluminium Alloy Bars AA 2014 T651
Product Price: Rs 350 / KgGet Best Price
Minimum Order Quantity: 100 Kg
Product Details:
| Size | 2 mm onwards |
| Shape | Round |
| Weight | As per size |
| Temper | T651 |
| Diameter | 2 mm - 75 mm |
| Usage/Application | Aerospace |
| Material | Aluminium Alloy 2014 |
| Available Material Grade | Alloy 2014,Alloy 2024,Alloy 7075 |
One of the strongest heat-treatable alloys for screw machine applications. This alloy, while commonly found in forging applications, offers good machinability and high strength. Corrosion resistance is only fair; however, weldability is good with arc and resistance methods. In many applications this alloy can be substituted for 2024.
AluminumAlloy 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.
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.
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
Additional Information:
- Item Code: ALBAR
- Pay Mode Terms: L/C (Letter of Credit),T/T (Bank Transfer)
- Delivery Time: READY
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Aluminum Alloy Flat Rolled Plate
Product Price: Rs 400 / KgGet Best Price
Product Details:
| Thickness | 1-3 mm |
| Surface Finished | Polished |
| Available Material Grade | Alloy 2014,Alloy 2024,Alloy 6061,Alloy 6082,Alloy 7075 |
| Material Grade | Aluminium Alloy |
1100-O Aluminum Sheet / Plate:
- Aluminum Sheet 1100 O Bare, also referred to as commercially pure aluminum, is soft and ductile with excellent workability. Annealed aluminum 1100 sheet is ideal for applications involving intricate forming. It has the highest thermal conductivity of any aluminum alloy and excellent electrical conductivity.
2024-O Clad Aluminum Sheet / Plate:
- Aluminum Sheet 2024 O Clad , often referred to as aerospace grade aluminum, is an excellent choice when high strength capabilities, fatigue resistance and high corrosion resistance are needed. Aluminum 2024 O-temper sheet is found in aircraft siding and skins because of its high strength-to-weight ratio and clad aluminum or Alclad surface, further improving corrosion resistance.
5052-H32 Aluminum Sheet / Plate:
- 5052-H32 Aluminum Sheet is commonly used for the bodies of boats, buses, trucks, and trailers, as well as for chemical drums. It is nonmagnetic and not heat treatable.
- "PVC 1 SIDE?" That refers to a PVC coating the mill adds for protective purposes. It peels off after you get everything in place.
5086-H32 Aluminum Sheet / Plate:
- 5086-H32 Aluminum Sheet is frequently found in marine applications, with higher strength capacity than Aluminum Alloy 5052 or Aluminum Alloy 5083. Aluminum Alloy 5086 has superior corrosion resistance and good formability. Aluminum Alloy 5086 is non-magnetic and heat treatable
- "PVC 1 SIDE?" That refers to a PVC coating the mill adds for protective purposes. It peels off after you get everything in place.
6061-T6 Aluminum Sheet / Plate:
- 6061-T6 Aluminum Sheet / Plate are frequently found in aircraft construction. Alloy 6061-T6 is perhaps the most common grade of Aluminum because of its good machinability and weldability.
- PVC 1 SIDE?" That refers to a PVC coating the mill adds for protective purposes. It peels off after you get everything in place.
7075 Aluminum O Clad Sheet / Plate:
- Aluminum Sheet 7075 O Clad is an excellent choice for strength because of its high zirconium and titanium composition and annealed tempering. Aluminum 7075-O clad sheet is found where a superior weight to strength ratio is essential.
Applications:
- Aerospace Aircraft Industry.
- Electrical Industry
- Heavy Engineeirng Industry.
- Marine engineering Industry.
- Electrical Industry
- Telecommunications Industry
- Architectural Industry
- Antimicrobial Applications
Additional Information:
- Item Code: ALSHEET
- Pay Mode Terms: T/T (Bank Transfer)
- Packaging Details: PALLET
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Aluminium Alloy Bars AA 2024
Product Price: Rs 400 / KgGet Best Price
Product Details:
| Material | Aluminium |
| Grade | 2024 |
| Size | 2 mm onwards |
| Is It Anodised | Not Anodised |
| Weight | depends upon its size |
| Dimensions | 2 mm onwards in rounds 1 mm onwards in sheets |
| Usage/Application | Aerospace Industry |
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Aluminium Alloy 7075
Product Price: Rs 600 / KgGet Best Price
Product Details:
| Grade | Alloy 7075 |
| Thickness | 3 mm onwards |
| Material | Aluminiu. |
| Shape | Rounds and Plates. |
| Alloy | With Alloy |
| Dimensions | As per customer requirements |
| Weight | As per size |
| Model Name/Number | 7075 |
| Certification Of Conformity Coc | Available |
| Test Certificate | Available |
| Brand | European |
7075 aluminium alloy (AA7075) is an aluminium alloy, with zinc as the primary alloying element. It has excellent mechanical properties, and exhibits good ductility, high strength, toughness and good resistance to fatigue. It is more susceptible to embrittlement than many other aluminium alloys because of microsegregation, but has significantly better corrosion resistance than the 2000 alloys. It is one of the most commonly used aluminium alloy for highly stressed structural applications, and has been extensively utilized in aircraft structural parts. 7075 aluminium alloy's composition roughly includes 5.6 6.1% zinc, 2.1 2.5% magnesium, 1.2 1.6% copper, and less than a half percent of silicon, iron, manganese, titanium, chromium, and other metals. It is produced in many tempers, some of which are 7075-0, 7075-T6, 7075-T651.7075-0EditUn-heat-treated 7075 (7075-0 temper) has a maximum tensile strength of no more than 280 MPa (40,000 psi), and maximum yield strength of no more than 140 MPa (21,000 psi). The material has an elongation (stretch before ultimate failure) of 9 10%. As is the case for all 7075 aluminum alloys, 7075-0 is highly corrosion-resistant combined with generally acceptable strength profile.7075-T6EditT6 temper 7075 has an ultimate tensile strength of 510 540 MPa (74,000 78,000 psi) and yield strength of at least 430 480 MPa (63,000 69,000 psi). It has a failure elongation of 5 11%.[7]The T6 temper is usually achieved by homogenizing the cast 7075 at 450 ??C for several hours, quenching, and then ageing at 120 ??C for 24 hours. This yields the peak strength of the 7075 alloy. The strength is derived mainly from finely dispersed eta and eta' precipitates both within grains and along grain boundaries.[8]7075-T651EditT651 temper 7075 has an ultimate tensile strength of 570 MPa (83,000 psi) and yield strength of 500 MPa (73,000 psi). It has a failure elongation of 3 9%. These properties can change depending on the form of material used. Thicker plate may exhibit lower strengths and elongation than the numbers listed above.7075-T7EditT7 temper has an ultimate tensile strength of 505 MPa (73,200 psi) and a yield strength of 435 MPa (63,100 psi). It has a failure elongation of 13%.[9] T7 temper is achieved by overaging (meaning aging past the peak hardness) the material. This is often accomplished by aging at 100 120 C for several hours and then at 160 180 C for 24 hours or more. The T7 temper produces a micro-structure of mostly eta precipitates. In contrast to the T6 temper, these eta particles are much larger and prefer growth along the grain boundaries. This reduces the susceptibility to stress corrosion cracking. T7 temper is equivalent to T73 temper.7075-RRAEditThe retrogression and reage (RRA) temper is a multistage heat treatment temper. Starting with a sheet in the T6 temper, it involves overaging past peak hardness (T6 temper) to near the T7 temper. A subsequent reaging at 120 C for 24 hours returns the hardness and strength to or very nearly to T6 temper levels.RRA treatments can be accomplished with many different procedures. The general guidelines are retrogressing between 180 240 C for 15 min 10 s.
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