12H17G9AN4 (EI878, H17G9AN4)
Used in the aviation industry.
for products operating under atmospheric conditions at temperatures up to 350 degrees C; austenitic steel
Classification
| Country | Section | Category |
|---|---|---|
| CIS, Russia, Ukraine | Corrosion-resistant alloys and steels | Corrosion-resistant ordinary steel |
Chemical composition
| Standard | Fe, % | Si, % | Mn, % | Cr, % | Ni, % | P, % | C, % | S, % | N, % |
|---|---|---|---|---|---|---|---|---|---|
| GOST 5632-72 | 65.775–72.35 | < 0.8 | 8–10.5 | 16–18 | 3.5–4.5 | < 0.035 | < 0.12 | < 0.02 | 0.15–0.25 |
Information on suppliers
Mechanical properties at 20 °C
| Rolling | Standard | Size, mm | Tension | Classifiers | $$\sigma _{U}$$, $$MPa$$ | $$\sigma_{P}$$, $$MPa$$ | $$\epsilon_L$$, % | $$\psi$$, % | Treatment |
|---|---|---|---|---|---|---|---|---|---|
| Rod | GOST 5949-75 | 690 | 345 | 45 | 55 | Hardening of 1050-1100 ° C, air | |||
| The plates | GOST 7350-77 | 690 | 345 | 40 | hardening | ||||
| Sheet | GOST 5582-75 | 690 | 40 | Hardening of 1050-1080 ° C, cooling water | |||||
| The sheet is thin and hardened. | GOST 5582-75 | 980 | 15 | ||||||
| Sheet | GOST 4986-79 | 640 | 20–40 | Hardening of 1050-1080 ° C |
Analogues
| Germany | USA |
|---|---|
| X8CrMnNi188 | 202 |
Standards
| Standard | Description |
|---|---|
| GOST 5632-72 | |
| TU 14-1-377-72 |
Description of chemical elements
| Element | Units of measurement | Description |
|---|---|---|
| Fe | % | Iron |
| Si | % | Silicon |
| Mn | % | Manganese |
| Cr | % | Chrome |
| Ni | % | Nickel |
| P | % | Phosphorus |
| C | % | Carbon |
| S | % | Sulfur |
| N | % | Nitrogen |
Description of mechanical properties
| Parameter | Units of measurement | Description |
|---|---|---|
| $$\sigma _{U}$$ | $$MPa$$ | Ultimate tensile strength |
| $$\sigma_{P}$$ | $$MPa$$ | Proportionality limit |
| $$\epsilon_L$$ | % | Elongation at break (longitudinal) |
| $$\psi$$ | % | Reduction in cross section on fracture |