Designation
| Name |
The value |
| Designation GOST Cyrillic |
20ХГСН2МФА |
| Designation GOST Latin |
20XGCH2MFA |
| Transliteration |
20HGSN2MFA |
| By chemical elements |
20CrGePbNi2CuP |
| Name |
The value |
| Designation GOST Cyrillic |
ДИ107 |
| Designation GOST Latin |
DI107 |
| Transliteration |
DI107 |
| By chemical elements |
ДIr107 |
Description
Alloy 20ХГСН2МФА used: for the manufacture of long products and forgings; loaded and the most critical parts of the aircraft.
Note
High-strength steel, structural, high quality, bromocinnamaldehyde.
Standards
| Name |
Code |
Standards |
| Classification, nomenclature and General rules |
В20 |
OST 1 90005-91 |
| Blanks. Of the workpiece. Slabs |
В31 |
TU 1-92-156-90 |
Mechanical properties
| Section, mm |
sT|s0,2, MPa |
σU, MPa |
d5, % |
y, % |
KCU, kJ/m2 |
HB, MPa |
HRC |
| Forgings. Quenching in oil with 890-910 °C + Vacation at 200-250 °C (extract 3 hours), air cooling |
|
≥1080 |
1320 |
≥10 |
≥50 |
≥735 |
- |
- |
| Gradation of performance properties of the finished heat-treated parts for OST 1 90005-91 |
| - |
- |
1230-1420 |
- |
- |
- |
353-401 |
38-43 |
| - |
- |
1230-1470 |
- |
- |
- |
- |
38-43.5 |
| - |
- |
1320-1520 |
- |
- |
- |
376-429 |
40-44 |
Description mechanical marks
| Name |
Description |
| sT|s0,2 |
Yield strength or limit of proportionality with a tolerance for residual deformation of 0.2% |
| σU |
Limit short-term strength |
| d5 |
Elongation after rupture |
| y |
The relative narrowing |
| KCU |
Toughness |
| HB |
Brinell hardness number |
| HRC |
Rockwell hardness (indenter diamond spheroconical) |