![]() | Poly Metal India
Ganesh Peth, Pune, Maharashtra GST No. 27AAEHJ4083Q1ZN |
Approx. 390 / Kg Get Latest Price
Specifications of Aluminum Checker Plate (Aluminum chequer plate,Aluminum checkered plate)Aluminum Checker Plate aslo named as Aluminum chequer plate,Aluminum checkered plate.It is easy to fabricate and its raised diamond ,bar,pointer,lug pattern provides good slip resistance.Which has good forming, drilling and welding abilityis and widely used in decorative, shipbuilding and architectural applications.Approx. 190 / Kilogram(s) Get Latest Price
In line with clients' diverse requirements across the country, we are offering an excellent range of Aluminum HE 9. Extensively used for architecture, particularly window frames, door frames, roofs, and sign frames, it is typically produced with very smooth surfaces fit for anodizing. This alloy is manufactured using superior quality raw material and the latest technology by our skilled professionals. Being a quality-oriented organization, we assure our clients that this alloy is excellent on counts of durability and quality.Approx. 210 Get Latest Price
Introduction Aluminum alloys tend to lose their strength when they are exposed to temperatures of about 200-250°C. However, their strength increases at subzero temperatures. They have high corrosion resistance.Approx. 300 / Kilogram(s) Get Latest Price
High strength alloys with excellent machinability widely used in aircraft. Have limited formability and only fair corrosion resistant in the heat treated condition. Not recommended for fusion welding. Used for high strength parts in aircraft and machinery, including gears and bolts and for security vans where strength ids critical. It has a tendency to allow the removal of a greater volume of metal in a single operation for an equipment standard of finish than 6082. Durability, however, is lower and needs a protection coating. Machines better in solution treated condition than fully heat treated. Used for machined parts where these characteristics are critical.Data Sheet: | Aluminium Alloy H15 HE 15 |
Chemical Composition Limits | ||||||||||
Weight % | Si | Fe | Cu | Mn | Cr | Mg | Ni | Zn | Ti + Zr | Ti |
H15 HE 15 | 0.50-0.90 | 0.50 max | 3.9-5.0 | 0.4-1.2 | 0.10 max | 0.2-0.8 | 0.10 max | 0.25 max | 0.20 max | 0.15 max |
Aluminum Alloy H15 is available in Bar, Sheet and Plate.
Approx. 300 Get Latest Price
High strength alloys with excellent machinability widely used in aircraft. Have limited formability and only fair corrosion resistant in the heat treated condition. Not recommended for fusion welding. Used for high strength parts in aircraft and machinery, including gears and bolts and for security vans where strength ids critical. It has a tendency to allow the removal of a greater volume of metal in a single operation for an equipment standard of finish than 6082. Durability, however, is lower and needs a protection coating. Machines better in solution treated condition than fully heat treated. Used for machined parts where these characteristics are critical.Data Sheet: | Aluminium Alloy HE 14 |
Chemical Composition Limits | ||||||||||
Weight % | Si | Fe | Cu | Mn | Cr | Mg | OTHER |
| ||
HE 14 | 0.20-0.70 | 0.70 max | 3.5-4.7 | 0.4-1.2 | 0.10 max | 0.4-1.2 | 0.50 max |
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Aluminum Alloy HE 14 is available in Bar, Sheet and Plate.
Approx. 300 / Kilogram(s) Get Latest Price
While climbing on the success ladder, it has become increasingly important for us to deliver precisely tested and high grade assortment of Aluminum 24345. It is used for high strength parts in aircraft and machinery, including gears and bolts and for security vans where strength is critical. The offered range is manufactured using high grade raw material and contemporary technology. We assure our clients that our range is quality tested on predefined parameters, in order to meet industry set standards. Apart from this our prestigious clients can avail these alloys, as per their needs, at highly competitive price.Weight % | Si | Fe | Cu | Mn | Cr | Mg | Ni | Zn | Ti + Zr | Ti |
IS 24345 | 0.50-0.90 | 0.50 max | 3.9-5.0 | 0.4-1.2 | 0.10 max | 0.2-0.8 | 0.10 max | 0.25 max | 0.20 max | 0.15 max |
Approx. 200 / Kilogram(s) Get Latest Price
With sincere intentions to preserve and uplift our reputation in the market, we bring forth a distinguished assortment of Aluminum 6063. It is an aluminum alloy, with magnesium and silicon as the alloying elements. Our offered alloy is manufactured using utmost-grade raw material and cutting-edge technology in compliance with defined quality standards. The offered alloy is extensively used in various industrial applications. Keeping in mind the diverse requirements of our clients, we provide this alloy in various sizes and designs and at affordable prices.Approx. 210 / Kilogram(s) Get Latest Price
With the endorsement of our adept and seasoned professionals, we are engaged in offering a commendable range of Aluminum 63400. It is mostly used in extruded shapes for architecture, particularly window frames, door frames, roofs, and sign frames. It is typically produced with very smooth surfaces fit for anodizing. The offered alloy is manufactured by making use of high grade raw material and leading technology in synchronization with the set industrial norms. In line with clients' variegated requirements, we offer the entire range in various customized options. Moreover, clients can avail the entire range from us at industrial leading prices.Approx. 210 Get Latest Price
IntroductionAluminum alloys tend to lose their strength when they are exposed to temperatures of about 200-250°C. However, their strength increases at subzero temperatures. They have high corrosion resistance.
The following datasheet will discuss in detail about the aluminum 6351 alloy.
Chemical CompositionThe chemical composition of the aluminum 6351 alloy is tabulated below.
Element | Content (%) |
---|---|
Aluminum, Al | 97.8 |
Silicon, Si | 1 |
Manganese, Mn | 0.6 |
Magnesium, Mg | 0.6 |
The following table shows the physical properties of the aluminum 6351 alloy.
Properties | Metric | Imperial |
---|---|---|
Density | 2.6-2.8 g/cc | 0.0939- 0.101 lb/in3 |
The mechanical properties of the aluminum 6351 alloy are outlined in the following table.
Properties | Metric | Imperial |
---|---|---|
Tensile strength | 250 MPa | 36260 psi |
Yield strength | 150 MPa | 21756 psi |
Shear strength | 200 MPa | 29008 psi |
Fatigue strength | 90 MPa | 13054 psi |
Elastic modulus | 70-80 GPa | 10153-11603 ksi |
Poisson's ratio | 0.033 | 0.033 |
Elongation | 20% | 20% |
Hardness | 95 | 95 |
The thermal properties of the aluminum 6351 alloy are given in the following table.
Properties | Conditions | ||
---|---|---|---|
T (ºC) | Treatment | ||
Thermal conductivity | 176 W/m-K | 25 | T6 |
Other designations equivalent to the aluminum 6351 alloy include ASTM B221.
Approx. 210 Get Latest Price
Introduction Aluminum alloys tend to lose their strength when they are exposed to temperatures of about 200-250°C. However, their strength increases at subzero temperatures. They have high corrosion resistance.Approx. 300 Get Latest Price
High strength alloys with excellent machinability widely used in aircraft. Have limited formability and only fair corrosion resistant in the heat treated condition. Not recommended for fusion welding. Used for high strength parts in aircraft and machinery, including gears and bolts and for security vans where strength ids critical. It has a tendency to allow the removal of a greater volume of metal in a single operation for an equipment standard of finish than 6082. Durability, however, is lower and needs a protection coating. Machines better in solution treated condition than fully heat treated. Used for machined parts where these characteristics are critical.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.
Approx. 300 Get Latest Price
High strength alloys with excellent machinability widely used in aircraft. Have limited formability and only fair corrosion resistant in the heat treated condition. Not recommended for fusion welding. Used for high strength parts in aircraft and machinery, including gears and bolts and for security vans where strength ids critical. It has a tendency to allow the removal of a greater volume of metal in a single operation for an equipment standard of finish than 6082. Durability, however, is lower and needs a protection coating. Machines better in solution treated condition than fully heat treated. Used for machined parts where these characteristics are critical.Data Sheet: | Aluminium Alloy 24534 |
Chemical Composition Limits | ||||||||||
Weight % | Si | Fe | Cu | Mn | Cr | Mg | OTHER |
| ||
24534 | 0.20-0.70 | 0.70 max | 3.5-4.7 | 0.4-1.2 | 0.10 max | 0.4-1.2 | 0.50 max |
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Aluminum Alloy 24534 is available in Bar, Sheet and Plate.
Approx. 650 Get Latest Price
7075 Aluminum Alloy Plate and SheetApprox. 190 / Kilogram(s) Get Latest Price
We are able to supply Aluminum Plate 6063 with the vast support of our team.Approx. 200 / Kilogram(s) Get Latest Price
We have been able to offer our clients a qualitative range of Aluminum Sheet 19000.