Components featuring elevated high temperature strength for use in thermal engines, such as turbine blades and turbine discs.
Creep resisting steel, hardened and tempered. Usual upper temperature limit for continuous operating 580°C.
| DIN | EN | Others |
|---|---|---|
| 1.4913 | X19CrMoNbVN11-1 | ≈ BS : S150 |
| C | Si | Mn | Cr | Mo | Ni | V | Nb | N | |
|---|---|---|---|---|---|---|---|---|---|
| 0.17 | 0.35 | 0.70 | 10.60 | 0.60 | 0.40 | 0.25 | 0.30 | 0.07 |
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