Aluminium Product

2024 aluminum is well suited for parts and structures requiring high strength to weight ratios.  It is predominantly used in aerospace, with some power and general industrial applications.  The key alloying element is copper, enhancing strength via response to thermal treatment.  For end use applications subject to aerodynamic heating, 2024 aluminum is suitable at temperatures up to approximately 300°F.  2024 Aluminum has good machining characteristics and high surface finishes are possible.  

Extruded bar is solution heat treated (910°F – 930°F), cold worked, then naturally aged.  Stress relief is provided by stretching a nominal permanent set of 2%.  The effect of cold work and straightening are included in mechanical property limits.  Cold finishing of bar imparts exceptional dimensional uniformity and internal properties.

Temper
T351

Specifications
AMS 4120, AMS-QQ-A-225/6B, ASTM B211 

Features
Machinability
Superior resistance to fatigue
High strength-to-weight ratio

Applications

Aircraft Structures
Screw Machine Products
Housings
Hydraulic Parts
Automotive

6061 aluminum is one of the most versatile heat-treatable aluminum alloys, with good formability and high resistance to corrosion. Containing magnesium and silicon additions, alloy 6061 features medium strength relative to 2000 or 7000 series aluminum alloys. 6061 is one of the most common alloys of aluminum for general-purpose use, and is highly-weldable using MIG or TIG methods. The response to anodization of 6061 aluminum is among the highest in class.

Extruded Bar is solution heat treated (960-1075°F) and quenched, then stretched a nominal 2% for stress relieving purposes before artificially aging (340-360°F). This combination of solution treatment, water quenching, and artificial aging imparts high strength.

Temper
T6511

Specifications
AMS-QQ-A-200/8, ASME SB-221, ASTM B221

Features
Excellent corrosion resistance, including sea water applications
Weldability
High strength-to-weight ratio

Applications
Automotive
Marine
Aircraft parts
Chemical equipment
Paper and Textile
Electrical fittings and components

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.

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.

Chemical Composition

Aluminum: Remainder
Chromium: 0.1% max
Copper: 3.9% - 5%
Iron: 0.7% max
Magnesium: 0.2% - 0.8%
Manganese: 0.4 - 1.2%
Remainder: Each 0.05% max
Remainder: Total 0.15% max
Silicon: 0.5% - 1.2%
Titanium: 0.15% max
Titanium + Zinc: 0.2% max
Zinc: 0.25% max

2219 aluminium alloy is an alloy in the wrought aluminium-copper family (2000 or 2xxx series). It can be heat-treated to produce tempers with higher strength but lower ductility. The aluminium-copper alloys have high strength, but are generally less corrosion resistant and harder to weld than other types of aluminium alloys. To compensate for the lower corrosion resistance, 2219 aluminium can be clad in a commercially pure alloy such as 1050 or painted. This alloy is commonly formed by both extrusion and forging, but is not used in casting.

The 2219 aluminium alloy in particular has high fracture toughness, is weld-able and resistant to stress corrosion cracking, therefore it is widely used in supersonic aircraft skin and structural members. The Space Shuttle Standard Weight Tank was also fabricated from the 2219 alloy.Aluminium Alloy 2219 is a high strength alloy which combines good machinability and good mechanical properties. 2219 is useful over a temperature range of -452°F to 600°F, is readily weldable and has good fracture toughness. In the T8 condition it is resistant to stress corrosion cracking.
Aluminium 2219 is typically used in a range of aerospace applications such as high temperature structural applications including space booster and fuel tanks.

Aluminum 3003 is a commercially pure aluminum with the addition of manganese. 3003 is the most widely used aluminum alloy due to it's excellent characteristics. The addition of manganese increases the strength and 3003 is 20% stronger than 1100 . As with 1100, 3003 has excellent corrosion resistance and workability. It is commonly used in Chemical equipment, Cooking and Kitchen equipment, decorative trim and storage tanks

Aluminum Alloy 4047

Aluminum / aluminum is widely used in several commercial, transportation and building applications. One of the key benefits of this silverfish white metal is its excellent corrosion resistance. Aluminum is also light weight, relatively strong, and has good thermal and electrical conduction.

Aluminium Alloy 7075 Sheets

Doshi Impex India is one of the leading Aluminium Alloy 7075 Sheets based suppliers, carrying an extensive stock and providing professional Aluminium Alloy 7075 Sheets 7075 processing services.

Aluminium Alloy 7075 Sheets 7075 is stocked, processed and supplied from a Thickness of 1 mm to 25 mm.

7075 aluminum is a heat-treatable Zinc alloy commonly used for structural parts subject to high stresses.  7075 offers one of the highest strengths available from an aluminum alloy. Fabricated parts offer dimensional stability as well as fair resistance to corrosion. Further performance characteristics include high hardness, excellent surface quality, and good response to anodization.

Extruded bar receives cold work, solution heat treatment (915°F) and stretching (nominal 2%) before artificially aging (250°F).  Cold finishing of bar imparts exceptional dimensional uniformity and internal properties.   

Temper
T651

Specifications
AMS 4123, AMS-QQ-A225/9, ASTM B211

Features
Best in class strength
Dimensional stability
Good anodization response
Applications
Aircraft Structures
Screw Machine Products
Housings
Hydraulic Parts
Automotive

7075 Aluminium Plate
7075 Aluminium Flat Bar

1100 aluminum alloy is an aluminum-based alloy in the "commercially pure" wrought family (1000 or 1xxx series). With a minimum of 99.0% aluminum, it is the most heavily alloyed of the 1000 series. It is also the mechanically strongest alloy in the series, and is the only 1000-series alloy commonly used in rivets. At the same time, it keeps the benefits of being relatively lightly alloyed (compared to other series), such as high electrical conductivity, thermal conductivity, corrosion resistance, and workability. It can be strengthened by cold working, but not by heat treatment

Availability
Aluminum 1100 is available in Sheet &  Plate.

Chemical Composition

Aluminium: 99.0–99.95%
Copper: 0.05–0.20%
Iron: 0.95% max
Manganese: 0.05% max
Silicon: 0.95% max
Zinc: 0.1% max
Residuals: 0.15% max