ВКС-1305
Alloy SteelВКС-1305
Russian high-strength aircraft structural steel VKS-1305.
Chemical Composition (%)
| C | 0.25 |
|---|---|
| SI | 0.15 |
| MN | 0.5 |
| CR | 0.5 |
| NI | 1 |
| MO | 0.2 |
| V | 0.05 |
| P | 0.025 |
| S | 0.025 |
Applications
International high-end steel for aerospace, oil & gas, defense or engineering.
Available Forms
Bar, plate, sheet, tube, forgings, strip, wire, powder
Uses
Low-alloy engineering steel with enhanced hardenability and strength from alloying elements. Chromium (≈1.5%) improves hardenability, wear and corrosion resistance. Molybdenum (≈0.5%) raises high-temperature strength and prevents temper embrittlement. Nickel (≈3%) increases toughness and impact strength at low temperature. Vanadium (≈0.175%) refines grain and strengthens the tempered structure. Applied to gears, shafts, bolts, connecting rods, pressure parts and heavy forgings in automotive, energy and machinery sectors.
Heat Treatment
Austenitize at 820–870 °C (oil or water quench depending on section) and temper at 400–650 °C to the required strength/toughness balance.
Precautions
Preheat and control interpass temperature when welding; post-weld heat treatment or stress relief is recommended to avoid hard-zone cracking. Use low-hydrogen electrodes. Protect from decarburization during heating (controlled atmosphere or protective coating).
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