Our
product range
Quality 1.5924.3
General Product Description
Material number 1.5924.3
Short name according to EN 1.5924.3
Applicable standards WL 1.5924
Treatment annealed
Variations
| Quality | Treatment | Shape | Dimension (mm) |
|---|---|---|---|
| 1.5924.3 | annealed | 25 - 40 |
Tim Weber
Purchasing / Aviation Sales / Authorized Representative
+49 (0) 23 31 - 387 115
weber@remystahl.de
Download business card (vcf)
Pierre Hermsdorf
Authorized Officer / Head of Procurement & Sales
+49 (0) 23 31 - 387 124
hermsdorf@remystahl.de
Download business card (vcf)
Description
The material 1.5924.3 is an alloyed engineering steel and belongs to the Cr-Ni steels with > 1.5 < 2.0% Cr
Chemical composition (in %)
| C | Mn | P | S | Cr | Ni | Si | |
|---|---|---|---|---|---|---|---|
| Min | 0,14 | 0,4 | - | - | 1,4 | 1,4 | - |
| Max | 0,19 | 0,6 | 0,035 | 0,035 | 1,7 | 1,7 | 0,4 |
| Element | Min | Max |
|---|---|---|
| C | 0,14 | 0,19 |
| Mn | 0,4 | 0,6 |
| P | - | 0,035 |
| S | - | 0,035 |
| Cr | 1,4 | 1,7 |
| Ni | 1,4 | 1,7 |
| Si | - | 0,4 |
Mechanical properties (annealed)
Tensile strength Rm 600–750 N/mm2
0.2% proof stress Rp0.2 ≥ 250 N/mm2
Elongation at break A5 ≥ 40 %
Notched impact energy (ISO-V) ≥ 40 %
Hardness ~200 HB
Magnetizability No
Typical areas of application
aircraft components
Mechanical engineering
precision components
General properties (annealed)
Corrosion Resistance
Weldability
Forgeability
Tensionability
Note
All information in this data sheet has been compiled to the best of our knowledge and belief. It is for information purposes only and does not constitute a assured property or guarantee. For the suitability of the material in specific applications, we recommend carrying out appropriate inspections and tests. Any liability for damage or errors is excluded.

