This specification covers a premium aircraft-quality, low-alloy Ni-Cr-Mo steel in the form of bars, forgings and forging stock requiring high tensile and toughness values, particular in large cross sections in the hardened and tempered condition. The molybdenum addition prevents the steel from being susceptible to temper brittleness.
These products have been used typically for parts requiring a through-hardening capability up to 6 inches (152,4 mm) in nominal thickness at time of heat treatment but usage is not limited to such applications.
Acier de traitement au Ni-Mo-Cr pour exigences élevées en matière de résistance et de ténacité, avec de grandes sections transversales de traitement.
Insensible à la fragilisation de recuit grâce à la teneur en Mo.
| SEL | Market grade |
|---|---|
| 1.6745 | S98 |
| BS | BS |
|---|---|
| S98 | S99 |
| C | Si | Mn | P | S | Cr | Mo | Al | |
|---|---|---|---|---|---|---|---|---|
| 0.36 to 0.44 | 0.10 to 0.35 | 0.45 to 0.7 | max. 0.025 | max. 0.015 | 0.5 to 0.8 | 0.45 to 0.65 | 0.015 to 0.050 |
Merci de patienter. Votre demande est en cours de traitement.
