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High-performance mold steel SKD61: Core characteristics, engineering practices and practical guidelines
What is SKD61 Steel?
Internationally Recognized Equivalent Grades of SKD61 Steel
| Country/Organization Code | Grade |
|---|---|
| JIS | SKD 61 |
| DIN, EN | 1.2344 |
| ASTM/AISI | H13 |
| GB | 4Cr5MoSiV1 |
| ISC | T23353 |
| ISO | X40CrMoV5-1 |
Although these grades have similar overall performance, slight differences in chemical composition and heat treatment response may affect the die's performance under high-temperature operating conditions. For cross-border projects or alternative selections, it is recommended to conduct full verification based on specific process conditions.
Chemical Composition of SKD61 — JIS G 4404:2022
| Chemical Element | Composition Content (%) |
|---|---|
| C | 0.35~0.42 |
| Si | 0.80~1.20 |
| Mn | 0.25~0.50 |
| P | Maximum 0.03 |
| S | Maximum 0.02 |
| Cr | 4.80~5.50 |
| Mo | 1.00~1.50 |
| V | 0.80~1.15 |
Key Functions of Typical Elements:
C: Provides hardness and wear resistance through martensitic transformation; influences secondary hardening.
Si: Strengthens the ferrite matrix and helps resist temper softening.
Mn: Improves hardenability and contributes to overall toughness.
Cr: Enhances hardenability, corrosion resistance, and high-temperature strength.
Mo: Increases red hardness, secondary hardening capacity, and thermal fatigue resistance.
V: Forms fine carbides, improving wear resistance and grain refinement.
Engineering Significance:
The relatively high Cr and Mo contents ensure good dimensional stability and thermal fatigue resistance under repeated high-temperature cycles.
Vanadium carbides can improve wear resistance on critical die surfaces.
Silicon and manganese help optimize temper stability, reducing the risk of softening during long-term use.
Microstructure and Materials Science Analysis
Martensitic Structure and Carbide Distribution
M₆C: Main elements W and Mo; promotes secondary hardening and maintains high-temperature hardness.
MC: Main element V; refines grains and improves wear resistance.
M₂₃C₆: Main element Cr; enhances high-temperature strength and temper softening resistance.
ESR (Electroslag Remelting) and Purity
Reduced Inclusions: Minimizes non-metallic inclusions, which are common initiation sites for microcracks under thermal cycles.
Improved Fatigue Life: A cleaner microstructure supports enhanced resistance to thermal cracking and thermal fatigue.
Enhanced Polishing Performance: Fewer inclusions and uniform carbide distribution improve surface finish, which is particularly important for optical-grade or high-gloss dies.
Microstructural Evolution During Heat Treatment
Austenitization: Heating to 1020~1080℃ to dissolve alloy carbides and form a uniform austenitic matrix.
Quenching: Using air cooling, oil cooling, or vacuum cooling to transform austenite into martensite, thereby achieving high hardness and heat resistance. The retained austenite content is affected by cooling rate and section thickness.
Tempering: Usually performed 2~3 times to precipitate fine alloy carbides, relieve internal stress, enhance toughness, and reduce the formation of microcracks.
Multiple tempering cycles optimize the balance between hardness and toughness, which is crucial for dies subjected to thermal cycles and high mechanical loads.
Properly controlled heat treatment reduces the risk of soft spots caused by tempering and ensures dimensional stability, especially for complex or thick-walled section dies.
Mechanical Properties
Physical Properties
Density: ≈7.8g/cm³; affects handling, fixture design, and structural support.
Thermal Conductivity: 25~30W/m·K; influences heat dissipation and cycle time in high-speed forming.
Elastic Modulus: 210GPa; determines stiffness and resistance to load deformation.
Coefficient of Thermal Expansion: 11.5×10⁻⁶/℃; guides the allowable range for dimensional changes in thick-walled sections.
High-Temperature Strength
Red Hardness: Effectively retains hardness in the range of 600–650°C, ensuring dimensional stability and consistency in processing/forming performance.
Thermal Fatigue Resistance: The combination of tempered martensitic structure and fine alloy carbides can inhibit the initiation and propagation of thermal cracks during thermal cycles.
Fatigue and Failure Mechanisms
Thermal Cracking: Initiates from surface defects or inclusions during rapid heating.
Surface Spalling/Chipping: Localized detachment of the hardened layer due to repeated thermal cycles.
Oxidation/Scaling: Reduces surface integrity when exposed to high temperatures or corrosive environments for extended periods.
Control heat treatment and tempering to balance hardness and toughness.
Adopt ESR remelting to reduce thermal cracking caused by inclusions.
Design a reasonable cooling system to reduce local overheating and stress concentration.
Heat Treatment and Surface Enhancement
Standard Heat Treatment Processes:
Annealing: Furnace cooling at 780~820℃ to eliminate internal stress and improve machinability; hardness is approximately 220–250 HB.
Stress Relieving: Performed after rough machining to reduce the risk of subsequent heat treatment.
Austenitization: 1020~1080℃; heating should avoid overheating to prevent grain coarsening.
Quenching: Using oil cooling, air cooling, or gas cooling; the cooling rate must be controlled to prevent quenching cracks.
Tempering: Usually conducted 2~3 times at 540~560℃, resulting in a final hardness of 48~52 HRC.
Surface Hardening Technologies
Nitriding: Forms a high-hardness diffusion layer, significantly improving wear resistance; typical layer depth is 0.2~0.4mm with minimal dimensional deformation.
PVD/CVD Coating: Such as TiN and CrN, which can reduce friction, minimize adhesive wear, and enhance thermal cracking resistance.
Composite Treatment: Nitriding + PVD can exert synergistic advantages in high-cycle forging and die casting dies.
Deformation Control and Dimensional Stability
Reasonable fixture design to reduce warpage during heat treatment.
Reserve 0.3~0.5mm allowance for final grinding.
Use light grinding or polishing after heat treatment to achieve the final dimension.
Machining and Manufacturing Guidelines
CNC Machining Recommendations
Milling and Turning: Use coated cemented carbide or cermet tools; rough machining cutting speed is 80–120 m/min, and finish machining is 120~180m/min.
Cutting Depth Control: Avoid one-time heavy cutting; adopt multiple passes.
Grinding: Use CBN or alumina grinding wheels with sufficient cooling after heat treatment.
Cooling Method: High-pressure cooling or mist cooling helps dissipate heat and extend tool life.
Polishing and Surface Treatment
Gradually use sandpaper from P240~P400 to P800~P1200, and finally use 6~1μm diamond paste or colloidal silica.
Avoid local overheating to prevent orange peel or micro-scratches.
Repair and Re-machining
Welding: Use compatible nickel-based or stainless steel die steel welding wire; preheat to 200~300℃.
Post-weld Treatment: Perform stress relieving or tempering to restore performance.
Subsequent Grinding and Polishing: Restore dimensions and surface quality.
Typical Applications and Steel Grade Comparison
| Steel Grade | Red Hardness | Thermal Fatigue Resistance | Typical Applications |
|---|---|---|---|
| SKD61 | 50~52HRC | Excellent | Hot forging, die casting, extrusion |
| SKD6 | 48~50HRC | Medium | General hot work dies |
| H11 | 46~50HRC | Good | Forging, extrusion |
| H13 | 46~50HRC | Good | High-temperature industrial dies |
Engineering Cases:
Die service life increased by approximately 30%.
Thermal fatigue cracks were significantly reduced.
Dimensional accuracy was maintained over 500,000 cycles.
Conclusion
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