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Alloy 800 Round bar ASTM B408
Alloy 800 Round bar ASTM B408
These Nichrome Base Alloysare used extensively in applications where heat resistance and/or corrosion resistance is required. In some members of the group, where conditions are less demanding, some nickel is replaced by iron to decrease the overall cost.
Metals fail at high temperatures by both oxidation (scaling) and through a loss in strength. Alloys in this class are designed to resist failure from both of these mechanisms. Nickel alloys are not suitable for high temperature sulphur rich environments.
Where corrosion resistance is significant, molybdenum is used as an alloying addition in nickel chromium based alloys.
The more recentnickel chromium base alloys in these groups also have a wide range of ancillary elements added to give special properties - some of these can be quite complicated and require very close control over composition and heat treatment.
Table 1. Compositions of some common nickel alloys.
UNS No | Al | Cr | Co | Fe | Mo | Ni | Nb+Ta | Ti | W |
N10276 |
| 15.5 |
| 5.5 | 16 | 57 |
|
| 3.8 |
N06600 |
| 15.5 |
| 8 |
| 76 |
|
|
|
N06625 |
| 21.5 |
|
| 9 | 61 | 3.6 |
|
|
N08800 |
| 21 |
| 46 |
| 32.5 |
|
|
|
N07718 | 0.5 | 19 |
| 18.5 | 3 | 52.5 | 5.1 |
|
|
N07090 | 1.5 | 19.5 | 16.5 |
|
| 60 |
| 2.5 |
|
Table 2. Typical properties of some common nickel alloys.
UNS No | Condition | UTS (MPa) | 0.2 Proof Stress (MPa) | Elong. On 5cm (%) | Hardness (HB) | 1000hr Ruptire Str. 750°C (MPa) |
N10276 | Annealed | 790 | 415 | 50 | 184 | N/a |
N06600 | Annealed | 550-690 | 210-430 | 55-35 | 120-170 | 38 |
N06625 | Annealed | 930 | 520 | 45 | 180 | 160 |
N08800 | Annealed | 520-690 | 210-410 | 60-30 | 120-184 | 70 (700°C) |
N07718 | Age Hardened | 1350 | 1180 | 17 | 382 | 170 |
Alloy 800 Round bar ASTM B408