Special Metals are the provider of expansive reach 7075 Aluminum Alloy Rods, and we give our customers the most satisfiable regard list for Aluminum Alloy.
How Aluminum Alloy 7075 Rods are made:
Aluminum Alloy 7075 Rods is an aluminum-zinc composite with 1%-8% zinc, in any case, little proportions of magnesium, and little measures of copper and chromium. In light of its high disintegration assurance properties, 7075 Rods are regularly used as a piece of marine and aeronautics applications. In addition, these Rods are used as a piece of airframe structures and others particularly centered around portions because of its excellent levels.
Table Of Content
- What is Aluminium Alloy 7075 Rod
- Aluminium Alloy 7075 Rod Specifications
- ASTM B211 Aluminium Alloy 7075 Rod Equivalent Grades
- Aluminium Alloy 7075 Rod Types
- Aluminium Alloy 7075 Extruded Rod
- Aluminium Alloy 7075 Hex Rod
- Aluminium Alloy 7075 Threaded rod
- Aluminium Alloy 7075 Square Rod
- Aluminium Alloy 7075 Rectangular Rod
- Aluminium Alloy 7075 Forged Rod
- Aluminium Alloy 7075 Rod Sizes
- Chemical Composition of Aluminium Alloy 7075 Rods
- Mechanical Properties of Aluminium Alloy 7075 Rods
- Ready Stock of Aluminium Alloy 7075 Rod in India
- Aluminium Alloy 7075 Rod Application Industries
- People Also Searched for
Elements of Aluminum Alloy 7075 Rods:
Aluminum Alloy 7075 Rods offer the most extraordinary strength of the normal screw machine composites. The better pressure consumption obstruction of the T173 and T7351 tempers makes combination 7075 a consistent substitution for 2024, 2014, and 2017 in a considerable lot of the most basic applications. With gigantic data and experience, we are occupied with giving assortments of Aluminum 7075 Rods to our clients throughout the nation. This alloy is similarly present in numerous determinations and broadly valued by our customers.
Why would this compound one say one is of the most normally utilized aluminum combination?
The high opposition of these 7075 Alloy Rods against exhaustion, notwithstanding its consumption obstruction properties, is the motivation behind why this amalgam is quite possibly the most normally utilized aluminum combination, especially for applications that include exceptionally focused on underlying conditions.
Why Aluminum Alloy 7075 is utilized in Aircraft and Ordnance businesses?
Compound 7075 is ready to give superior grade as made by heat treating. This is an extremely high-strength airplane compound, which likewise has superb properties at low temperatures. Ordinarily utilized in assembling the airplane and other aviation applications, not needing the erosion obstruction of Clad 7075. Great machinability and hardness and not intended for welding and stress-erosion breaking. Because of its overall strength, Alloy 7075 is vigorously used by the airplane and weapons businesses.
Specifications : ASTM B211, ASME SB 211 / ASTM B221, ASME SB221
Dimensions : EN, DIN, JIS, ASTM, BS, ASME, AISI, ASTM, ASME
Size : 5 mm To 500 mm
Length : 9 – 12 metres
Form : Round, Square, Hex (A/F), Rectangle, Billet, Ingot, Forging Etc.
Finish : Cold drawn, Bright drawn, Centreless ground, Cold finished, Peeled and turned, Smooth turned, Slit rolled edge, Hot finished, Hot rolled, Rough turned/peeled, Peeled and reeled
Temper : T3, T4, T5, T6, T651, T6511
UNS | EN | DIN,WNr | ISO |
A97075 | EN3982 | 3.4144 | AlZn6CuMgZr |
Size in Inches | Approx. Weight per Foot in Lbs. | Est. Weight 12′ Bar |
---|---|---|
1/8 | .0144 | .1728 |
3/16 | .0325 | .3900 |
1/4 | .0577 | .6924 |
5/16 | .0902 | 1.082 |
3/8 | .1299 | 1.559 |
7/16 | .1768 | 2.122 |
1/2 | .2309 | 2.771 |
9/16 | .2922 | 3.506 |
5/8 | .3608 | 4.330 |
3/4 | .5195 | 6.234 |
7/8 | .7071 | 8.485 |
1 | .9236 | 11.08 |
1 – 1/8 | 1.169 | 14.03 |
1 – 1/4 | 1.443 | 17.32 |
1 – 3/8 | 1.746 | 20.95 |
1 – 1/2 | 2.078 | 24.94 |
1 – 5/8 | 2.439 | 29.27 |
1 – 3/4 | 2.829 | 33.95 |
2 | 3.694 | 44.33 |
2 – 1/4 | 4.676 | 56.11 |
2 – 1/2 | 5.773 | 69.28 |
2 – 3/4 | 6.985 | 83.82 |
3 | 8.312 | 99.74 |
3 – 1/4 | 9.756 | 117.1 |
3 – 1/2 | 11.31 | 135.7 |
3 – 3/4 | 12.99 | 155.9 |
4 | 14.78 | 177.4 |
4 – 1/2 | 18.70 | 224.40 |
5 | 23.09 | 277.1 |
6 | 33.25 | 399.0 |
10 | 92.36 | 1108.32 |
Weight % | Zn | Cu | Mg | Zr | Fe | Si | Mn | Ti | Cr | Others (total) |
Minimum | 5.7 | 2.0 | 1.9 | 0.08 | – | – | – | – | – | – |
Maximum | 6.7 | 2.6 | 2.6 | 0.15 | 0.15 | 0.12 | 0.10 | 0.06 | 0.04 | 0.15 |
Material | Temper | Tensile Strength (ksi) | Yield Strength (ksi) | Elongation in 2″ % |
Aluminium Alloy 7075 Angle (AMS 4340) | T76511 | 79 | 69 | 7 |
Aluminium Alloy 7075 Angle (AMS 4340) | T73511 | 70 | 60 | 8 |
Aluminium Alloy 7075 Angle (AMS 4342) | T74511 | 73 | 63 | 7 |
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