EP998 Nickel Alloy (Alloy Х20Н73ЮМ)
No foreign analogues
The alloy is used to make turbine working parts.
No foreign analogues
The alloy is used to make turbine working parts.
Standard | Fe, % | Si, % | Mn, % | Cr, % | Ni, % | Al, % | Mo, % |
---|---|---|---|---|---|---|---|
GOST 5632-14 | 1.3–2 | < 0.2 | < 0.2 | 19–21 | 71.2–75.3 | 3.1–3.6 | 1.3–1.8 |
Rolling | Standard | Size, mm | Tension | Classifiers | $$\sigma _{U}$$, $$MPa$$ | $$\sigma_{Y}$$, $$MPa$$ | d5, % | Treatment |
---|---|---|---|---|---|---|---|---|
Sheet | GOST 24982-81 | <5.0 | Transverse | raw, rolling, thin, Transverse | 880–920 | 400 | 35 |
Rolling | Standard | Classifiers | Value, HBW |
---|---|---|---|
Sheet | GOST 24982-81 | raw, rolling, thin, Transverse | 230 |
Standard | Description |
---|---|
GOST 5632-14 |
Parameter | Units of measurement | Description |
---|---|---|
no limits | Welding is performed without heating and without subsequent heat treatment | |
Boundedly welded | Welding is possible with heating up to 100–120 °C and subsequent heat treatment | |
Difficult to weld | For obtaining quality welded joints, additional operations are required: heating up to 200–300 °C for welding, heat treatment after welding — annealing | |
Not applicable for welded structures |