7075 Aluminum Bar,Aluminum 7075 T6 T651 T6511 round bar,A97075 round bar
We are the professional manufacturer and exporter of 7075 Aluminum Bar,Aluminum 7075 T6 T651 T6511 round bar,A97075 round bar.
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 alloys from the 2000 series. It is one of the most commonly used aluminium alloys for highly stressed structural applications and has been extensively used 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.
Aerospace Defense Aluminum Temper T6 7075 Aluminum Round Bar
7075 T6 aluminum solid round bar
7075 T6 Aluminum Round Bar is one of the strongest material in aluminum alloys grade
Applications for 7075 T6 aluminum solid round bar include but are not limited to: Aerospace, Defense Applications, Shafts, Gears, and any application requiring a high strength to weight ratio material–Due to material handling and processing items may have light scratching.
SPECIFICATIONS
| Weight % | Si | Fe | Cu | Mn | Mg | Cr | Zn | Ti | Each | Total |
|---|---|---|---|---|---|---|---|---|---|---|
| Minimum | 1.20 | 2.10 | 0.18 | 5.10 | ||||||
| Maximum | 0.40 | 0.50 | 2.00 | 0.30 | 2.90 | 0.28 | 6.10 | 0.20 | 0.05 | 0.15 |
Remainder Aluminum
| Temper | Tensile | Hardness | ||||
|---|---|---|---|---|---|---|
| Ultimate | Yield | Elongation | Brinell | |||
| KSI | MPA | KSI | MPA | % | ||
| T6, T651 | 83 | 572 | 73 | 503 | 11 | 150 |
| T73, T7351 | 73 | 503 | 63 | 434 | 13 | N/A |
Typical Mechanical Properties
| Material | Temper | Size (“) | Tensile Strength (ksi) | Yield Strength (ksi) | Elongation in 2″ % |
| Alloy 7075 Bar | T651 | – | 77 | 66 | 7 |
| Alloy 7075 Bar | T7351 | <4″ | 68 | 56 | 10 |
| Alloy 7075 Bar | T73511 | <0.25 | 68 | 58 | 7 |
| Alloy 7075 Bar | T73511 | 0.25 – 1.5 | 70 | 61 | 8 |
| Alloy 7075 Bar | T73511 | 1.5 – 3.0 | 69 | 59 | 8 |
| Alloy 7075 Bar | T6511 | <0.25 | 78 | 70 | 7 |
| Alloy 7075 Bar | T6511 | 0.25 – 0.5 | 81 | 73 | 7 |
| Alloy 7075 Bar | T6511 | 0.5 – 3.0 | 81 | 72 | 7 |
7075 T6 aluminum rod is in artificial aging temper after solution heat treatment. If there is no precision requirement for dimensional stability and elastic margin, 7075 T6 aluminum rod can be used.
7075 T651 T6511 aluminum rods are stretched to eliminate the residual stress after solution treatment. For precision workpieces, 7075 T651 T6511 aluminum rods should be used to avoid elastic recovery after processing and unable to maintain dimensional stability.
