Aluminum Threaded Rods
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Grand Metal Corporation is acknowledged as a manufacturer, exporter & suppliers of Aluminium Threaded Rods, available in a variety or grades, materials, and finishes, in metric and inch sizes. We have a full range available always, with unrivalled lead times, superior quality and exemplary customer service, leading Aluminium Threaded Rods. manufacturing, supplying and exporting a commendable range of Aluminium Round Bar. Having good strength, machining and anodizing characteristics, these round bars are available customized threading with Aluminium 2219, This material is commonly used to secure parts together in applications such as manufacturing, automotive and construction.
, our offered products are closely inspected to avoid defects.
Grand Metal Corporation carries a variety of Aluminium Threaded Rods and supply at Best suitable price.
Useful Information of Aluminium Threaded Rods
Specifications: 2011-T3; 2014-T4, -T6; 2017-4 2024-T3, -T351, -T3511; 2219-T31, -T8511; 5052, 5083, 5086 - All Tempers. 6061-T6, T651, - T6511; 7075-T6, -T651, -T6511, -T7351 Tempers Special Aluminum Alloys and Sizes are available on request.
Material: Aluminum and Alloys of Aluminum
Form : Round ,Square , Hex , Bush , Rectangle , Flat
Standard: ASTM B429 / B429M
Type: Rods Solid.
Sizes: |
5 mm X 12' Long |
6 mm X 12' Long |
10 mm X 12' Long |
12 mm X 12' Long |
15 mm X 12' Long |
19 mm X 12' Long |
25 mm X 12' Long |
30 mm X 12' Long |
38 mm X 12' Long |
50 mm X 12' Long |
60 mm X 12' Long |
100 mm X 12' Long |
110 MM |
120 MM |
130 MM |
140 MM |
150 MM TO 203 MM ( HINDALCO & JINDAL ) |
210MM TO 400MM ( IMPORTED MATERIAL ) |
Additional Information: |
Minimum Order Quantity: 250 Kilogram(s) |
Pay Mode Terms: T/T (Bank Transfer),Other |
Port of Dispatch: EX - BHIWANDI |
Delivery Time: READY STOCK |
Packaging Details: AS PER YOUR REQUIREMENT . |
Aluminium Detailed Guide
2011 Aluminium
2011 is the most machinable of the commonly available aluminium alloys. Machining this alloy can produce excellent surface finishes on your product, and small, broken chips.
Weldability, strength, and anodizing response are all rated as average at best, and this alloy does not have a high degree of corrosion resistance.
If the ability to make your part quickly is important to you, and strength is not the primary desire, 2011 represents a good choice if you're using aluminium.
2011-T3 Aluminium |
Minimum Properties |
Ultimate Tensile Strength, psi |
55,000 |
Yield Strength, psi |
43,000 |
Brinell Hardness |
95 |
Rockwell Hardness |
B60 |
Chemistry |
Aluminium (Al) |
91.2 - 94.6% |
Bismuth (Bi) |
0.2 - 0.6% |
Copper (Cu) |
5.0 - 6.0% |
Iron (Fe) |
0.7% max |
Magnesium (Mg) |
2.1 - 2.9% |
Lead (Pb) |
0.2 - 0.6% |
Silicon (Si) |
0.4% max |
2024 Aluminium
Copper is the main alloying ingredient in 2024. It is very strong compared to most aluminium alloys, and has average machinability, but the copper component of this alloy makes it susceptible to corrosion (many items in this alloy are produced with a clad surface to protect the underlying material.) In addition, 2024 is not considered to be weldable.
Finally, the fatigue resistance of 2024 make it a primary choice when the application is expected to be under stress or strain for prolonged periods. It is commonly used in aerospace applications
2024-T3 Aluminium |
Minimum Properties |
Ultimate Tensile Strength, psi |
70,000 |
Yield Strength, psi |
50,000 |
Brinell Hardness |
120 |
Rockwell Hardness |
B75 |
Chemistry |
Aluminium (Al) |
90.7 - 94.7% |
Chromium (Cr) |
0.1% max |
Copper (Cu) |
3.8 - 4.9% |
Iron (Fe) |
0.5% max |
Magnesium (Mg) |
1.2 - 1.8% |
Manganese (Mn) |
0.3 - 0.9% |
Silicon (Si) |
0.5% max |
5052 Aluminium
5052 is the alloy most suited to forming operations, with good workability and higher strength than that of the 1100 or 3003 alloys that are commercially available.
5052 is not heat-treatable, but is stronger than most of the 5xxx series of alloys. It has very good corrosion resistance, and can be easily welded. 5052 is not a good choice for extensive machining operations, as it has only a fair machinability rating.
5052-H32 Aluminium |
Minimum Properties |
Ultimate Tensile Strength, psi |
33,000 |
Yield Strength, psi |
28,000 |
Brinell Hardness |
60 |
Chemistry |
Aluminium (Al) |
95.7 - 97.7% |
Chromium (Cr) |
0.15 - 0.35% |
Copper (Cu) |
0.1% max |
Iron (Fe) |
0.4% max |
Magnesium (Mg) |
2.2 - 2.8% |
Manganese (Mn) |
0.1% max |
Silicon (Si) |
0.25% max |
6061 Aluminium
6061 Aluminium is, by most any measure, the most commonly used aluminium alloy. It is specified in most any application due to its strength, heat treatability, comparatively easy machining, and weldability. If that were not enough, it is also capable of being anodized, adding a layer of protection for finished parts.
The main alloy ingredients of 6061 aluminium are magnesium and silicon.
6061-T6 Aluminium |
Physical and Mechanical Properties |
Ultimate Tensile Strength, psi |
45,000 |
Yield Strength, psi |
40,000 |
Brinell Hardness |
95 |
Rockwell Hardness |
B60 |
Chemistry |
Aluminium (Al) |
95.8 - 98.6% |
Chromium (Cr) |
0.04 - 0.35% |
Copper (Cu) |
0.15 - 0.40% |
Iron (Fe) |
0.70% |
Magnesium (Mg) |
0.8 - 1.2% |
Manganese (Mn) |
0.15% max |
Silicon (Si) |
0.4 - 0.8% |
Zinc (Zn) |
0.25% |
6063 Aluminium
6063 is often called architectural aluminium for two reasons - first, it has a surface finish that is far smoother than the other commercially available alloys, and second, its strength is significantly less (roughly half the strength of 6061), making it suited for applications where strength is not the foremost consideration.
6063 is rated as "Good" for forming and cold working operations, "Excellent" for anodizing, and "Fair" for machining.
6063-T52 Aluminium |
Minimum Properties |
Ultimate Tensile Strength, psi |
27,000 |
Yield Strength, psi |
21,000 |
Brinell Hardness |
60 |
Chemistry |
Aluminium (Al) |
97.5% max |
Chromium (Cr) |
0.1% max |
Copper (Cu) |
0.1% max |
Iron (Fe) |
0.35% max |
Magnesium (Mg) |
0.45 - 0.90% |
Manganese (Mn) |
0.1% max |
Silicon (Si) |
0.2 - 0.6% |
6101 Aluminium
6101 is best suited for applications involving moderate strength and maximum electrical conductivity. It is similar to alloy 6063, but with minor chemistry changes which enhance electrical conductivity. Although slightly lower in conductivity than alloy 1350, it offers greater strength. Its most typical application is bus bar.
6101-T6 Aluminium |
Physical and Mechanical Properties |
Ultimate Tensile Strength, psi |
32,000 |
Yield Strength, psi |
28,000 |
Brinell Hardness |
71 |
Electrical Conductivity |
57% IACS |
Chemistry |
Aluminium (Al) |
97.6% |
Chromium (Cr) |
0.03% |
Copper (Cu) |
0.10% |
Iron (Fe) |
0.50% |
Magnesium (Mg) |
0.35 - 0.80% |
Manganese (Mn) |
0.03% max |
Silicon (Si) |
0.3 - 0.7% |
Boron (Si) |
0.06% |
6262 Aluminium
6262 was designed as an aluminium alloy for operations where significant machining is required. It contains lead and bismuth to help with chip creation and breakage, as well as to partially lubricate the cutting tool. It is generally regarded as having good strength and corrosion resistance. Finished parts can be produced with a high level of polishing.
6262-T6511 Aluminium |
Minimum Properties |
Ultimate Tensile Strength, psi |
31,900 |
Yield Strength, psi |
27,600 |
Brinell Hardness |
71 |
Chemistry |
Aluminium (Al) |
94.6 - 97.8% |
Chromium (Cr) |
0.04 - 0.14% |
Copper (Cu) |
0.15 - 0.40% |
Iron (Fe) |
0.7% max |
Magnesium (Mg) |
0.8 - 1.2% |
Manganese (Mn) |
0.15% Max |
Bismuth (Bi) |
0.4 - 0.7% |
Silicon (Si) |
0.4 - 0.8% |
Lead (Pb) |
0.4 - 0.7% |
7075 Aluminium
7075 is the other "aircraft grade" aluminium that is carried by Grand Metal Corporation. Its principal alloying ingredients are zinc and copper, which make it one of the highest-strength aluminium alloys that are available. In fact, its typical strength in the T6 temper is higher than mildest steels.
7075 also has average-to-good ratings for machinability, corrosion resistance, and anodizing response. Like 2024, however, it is not considered to be weldable.
7075-T6 Aluminium |
Physical and Mechanical Properties |
Ultimate Tensile Strength, psi |
83,000 |
Yield Strength, psi |
73,000 |
Brinell Hardness |
150 |
Rockwell Hardness |
B87 |
Chemistry |
Aluminium (Al) |
87.1 - 91.4% |
Zinc (Zn) |
5.1 - 6.1% max |
Copper (Cu) |
1.2 - 2.0% |
Chromium (Cr) |
0.18 - 0.28% |
Iron (Fe) |
0.5 max |
Magnesium (Mg) |
2.1 - 2.9% |
Manganese (Mn) |
0.3% max |
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