Wear parts and dies account for approximately 15% of cemented carbide consumption globally. Unlike cutting tools (replaced frequently) or mining buttons (catastrophic failure acceptable), die applications demand predictable, gradual wear with consistent dimensional output over millions of cycles. Grade selection must match the specific wear mechanism—abrasive, adhesive, erosive, or fatigue—to maximize service life.
Master Specification Table
| Application | FSSS (μm) | Co % | HRA | TRS (MPa) | Wear Type | Die Life (typical) | Surface Finish |
|---|---|---|---|---|---|---|---|
| Wire drawing (fine wire) | 0.5-0.8 | 3-4 | 93.5-94.5 | 2600-3000 | Abrasive | 5-20M meters | Ra <0.1 μm |
| Wire drawing (medium) | 0.8-1.5 | 4-6 | 92.5-93.5 | 2800-3200 | Abrasive | 10-50M meters | Ra <0.2 μm |
| Wire drawing (heavy) | 1.0-2.0 | 6-8 | 91.5-92.5 | 3200-3600 | Abrasive + impact | 20-100M meters | Ra <0.4 μm |
| Progressive stamping | 0.8-1.5 | 10-12 | 90.5-91.5 | 3800-4200 | Impact + adhesive | 1-5M strokes | Ra 0.2-0.8 μm |
| Fine blanking | 0.6-1.0 | 8-10 | 91.5-92.5 | 3600-4000 | Abrasive + fatigue | 0.5-2M strokes | Ra <0.2 μm |
| Hot extrusion | 1.5-3.0 | 10-14 | 88.5-90.5 | 3600-4000 | Thermal + adhesive | 10K-100K cycles | Ra 0.4-1.6 μm |
| Cold extrusion | 1.0-2.0 | 8-12 | 90.0-91.5 | 3400-3800 | Abrasive + fatigue | 50K-500K cycles | Ra 0.2-0.8 μm |
| Cold heading | 1.5-4.0 | 12-16 | 87.5-90.0 | 4000-4600 | Impact + fatigue | 0.2-2M strokes | Ra 0.4-1.6 μm |
| Powder compaction | 0.8-1.5 | 8-10 | 91.0-92.5 | 3400-3800 | Abrasive | 0.5-5M cycles | Ra <0.4 μm |
| Seal rings | 1.0-2.0 | 6-8 | 91.5-92.5 | 3200-3600 | Sliding + erosive | 2-10 years | Ra <0.1 μm |
| Spray nozzles | 0.8-1.5 | 6-10 | 91.0-92.5 | 3200-3800 | Erosive | 0.5-5 years | Ra <0.4 μm |
| Guide bushings | 1.5-3.0 | 10-12 | 89.5-91.0 | 3600-4000 | Sliding + adhesive | 1-10 years | Ra 0.2-0.8 μm |
This table spans the entire range of wear part applications—notice how dramatically different they are from each other. Wire drawing dies face pure abrasion and use very low cobalt (3-6%) for maximum hardness. Cold heading dies face repeated violent impacts and use high cobalt (12-16%) or even higher for toughness; some cold heading applications use up to 25% cobalt. The "Wear Type" column tells you the dominant mechanism, which drives the grade selection. The "Die Life" column gives you realistic expectations—wire drawing life is measured in millions of meters of wire; stamping in millions of strokes. Use this table to find your application and see what specifications you should be targeting.
Understanding Wear Mechanisms
Grade selection starts with identifying the dominant wear mechanism:
Abrasive Wear
What happens: Hard particles or asperities plow grooves into the carbide surface, removing material.
Archard wear equation: Q = K × W × L / H
Where:
- Q = wear volume
- K = wear coefficient (10⁻⁸ for mild, 10⁻² for severe)
- W = normal load
- L = sliding distance
- H = hardness
Key insight: Wear is inversely proportional to hardness. For abrasive wear, maximize hardness with fine grain and low cobalt.
Grade recommendation: 0.5-1.5 μm grain, 3-8% Co, HRA >92
Adhesive Wear
What happens: Workpiece material bonds to die surface at asperity contacts, then tears away, removing carbide particles.
Common in: Stamping dies, forming dies, cold heading (especially with soft metals like aluminum or copper).
Key insight: Surface chemistry matters as much as hardness. Coatings (TiN, TiAlN) often more effective than grade changes.
Grade recommendation: 1.0-2.0 μm grain, 8-12% Co, HRA 90-92; consider coating
Erosive Wear
What happens: Particles impact surface at angle, causing material removal through repeated impacts.
Impact angle effect:
- 15-30°: Maximum erosion for ductile carbide
- 90°: Maximum erosion for brittle materials
- Carbide behaves between ductile and brittle depending on Co content
Grade recommendation: 0.8-2.0 μm grain, 6-10% Co, balance hardness and toughness
Fatigue Wear
What happens: Cyclic loading creates subsurface cracks that propagate and cause spalling/pitting.
Common in: Cold heading dies, stamping dies, powder compaction tooling.
Key insight: Fatigue resistance correlates with TRS. Higher cobalt and cleaner microstructure (low porosity) improve fatigue life.
Grade recommendation: 1.0-3.0 μm grain, 10-15% Co, TRS >3800 MPa, porosity A00-A02
Thermal Wear
What happens: Temperature cycling causes thermal fatigue cracking; high temperatures reduce hot hardness.
Common in: Hot extrusion, die casting, forging dies.
Grade recommendation: 1.5-4.0 μm grain, 10-14% Co, consider TiC/TaC additions for hot hardness
Wire Drawing Die Design
Wire drawing dies have specific geometry requirements:
Die Profile Zones
| Zone | Function | Geometry |
|---|---|---|
| Entrance cone | Guide wire, hold lubricant | 60° included angle (typical) |
| Approach cone | Main reduction zone | 6-15° included angle (2α) |
| Bearing | Size wire, burnish surface | Parallel, L = 20-50% of wire Ø |
| Back relief | Exit clearance | 30-60° included angle |
A wire drawing die isn't just a hole—it has four distinct zones, each with a specific job. The entrance cone catches the wire and holds lubricant for smooth drawing. The approach cone does the actual size reduction—this is where most wear happens as the wire is compressed through the narrowing passage. The bearing zone sizes the wire precisely and burnishes the surface to final quality. The back relief lets the wire exit cleanly without scraping. Understanding these zones helps you diagnose wear problems: if the entrance wears prematurely, your wire is misaligned or you have lubricant issues; if the bearing wears, that's normal operation. Each zone can be optimized separately during die design.
Approach Angle Selection
| Wire Material | Drawing Reduction | Approach Angle (2α) |
|---|---|---|
| Soft (copper, aluminum) | 15-25% | 12-16° |
| Medium (low carbon steel) | 15-20% | 10-14° |
| Hard (high carbon steel) | 10-15% | 8-12° |
| Stainless steel | 10-15% | 8-10° |
The approach angle (also called the reduction angle or drawing cone) determines how aggressively you reduce the wire diameter. The angle is usually expressed as the included angle (2α), though some references use the half-angle (α). Soft metals like copper and aluminum can handle steeper angles (12-16°) because they flow easily under pressure and don't work-harden excessively. Hard metals like high-carbon steel and stainless steel need gentler angles (8-12°) to avoid work hardening, surface cracking, and excessive drawing force. The rule is straightforward: harder material = narrower angle; larger area reduction per pass = wider angle. Getting this wrong causes excessive die wear, surface defects on the wire, or even wire breakage during drawing.
Rule: Harder wire → narrower angle. Larger reduction → wider angle.
Bearing Length
| Wire Diameter | Bearing Length (L) |
|---|---|
| <0.5 mm | 20-30% of Ø |
| 0.5-2 mm | 30-40% of Ø |
| 2-5 mm | 40-50% of Ø |
| >5 mm | 50-75% of Ø |
Bearing length is the parallel section that determines the final wire diameter and surface quality. It's expressed as a percentage of the wire diameter. Finer wire needs proportionally shorter bearing because there's less contact area and friction heat builds up faster in a confined space—a bearing that's too long on fine wire causes overheating and potential wire breakage. Coarser wire can handle longer bearing, which gives better size control and longer die life because the wear is distributed over more surface area. Too short a bearing results in inconsistent sizing and poor surface finish. Too long causes excessive friction, heat buildup, and potential wire breakage. The percentages shown are starting points; fine-tune based on your specific wire material and drawing speed.
Trade-off: Longer bearing = better size control, longer die life, but more friction and heat.
Grade Selection by Wire Type
| Wire Material | FSSS (μm) | Co % | HRA | Notes |
|---|---|---|---|---|
| Fine copper (<0.5mm) | 0.5-0.6 | 3-4 | 94.0-94.5 | Maximum hardness for fine wire |
| Copper/aluminum | 0.6-1.0 | 4-6 | 93.0-94.0 | Adhesion resistant |
| Low carbon steel | 0.8-1.5 | 4-6 | 92.5-93.5 | Balance wear/toughness |
| High carbon steel | 1.0-1.5 | 6-8 | 92.0-93.0 | More toughness for hard wire |
| Stainless steel | 1.0-2.0 | 6-8 | 91.5-92.5 | Work hardening resistance |
| Tungsten/molybdenum | 0.6-1.0 | 3-5 | 93.5-94.5 | Extreme hardness required |
Different wire materials create different demands on the die grade. Soft metals like copper and aluminum tend to stick (adhesive wear), so you need smooth polished surfaces and sometimes coatings to prevent material transfer. Steel wires cause more abrasive wear, so you need harder grades. Stainless steel work-hardens during drawing, increasing the drawing force progressively and causing more wear—use slightly tougher grades with more cobalt to handle the increased stress. Refractory metals (tungsten, molybdenum) are extremely hard and will wear through soft dies quickly—use the hardest grades available (94+ HRA). Fine copper wire is a special case requiring ultra-fine grain (0.5-0.6 μm) because the die bore is so small that even minor wear causes significant dimensional variation.
Stamping Die Selection
Progressive Die Requirements
| Component | FSSS (μm) | Co % | HRA | TRS (MPa) | Key Requirement |
|---|---|---|---|---|---|
| Punch (blanking) | 0.8-1.2 | 10-12 | 91.0-92.0 | 3800-4200 | Impact resistance |
| Die (blanking) | 0.8-1.5 | 8-10 | 91.5-92.5 | 3600-4000 | Wear resistance |
| Stripper | 1.0-2.0 | 10-12 | 90.5-91.5 | 3800-4200 | Fatigue resistance |
| Pilot | 0.6-1.0 | 8-10 | 92.0-93.0 | 3400-3800 | Precision + wear |
Progressive stamping dies have multiple components, each with different requirements—don't use the same grade for everything. Punches take the brunt of impact when blanking (cutting through the sheet metal), so they need higher cobalt for toughness. The die (female part) experiences more sliding wear as the blank is pushed through, so it prioritizes wear resistance with slightly lower cobalt. Strippers face repeated fatigue loading as they push the strip off the punch millions of times—they need high TRS. Pilots require precision first (to locate the strip accurately) and wear resistance second. Optimizing each component separately can significantly extend overall tool life compared to using one grade for the entire die set.
Work Material Effects
| Workpiece | Die Challenge | Grade Adjustment |
|---|---|---|
| Mild steel | Moderate adhesion | Standard grade |
| Stainless steel | High adhesion, work hardening | Higher Co (10-12%), consider TiN coating |
| Aluminum | Severe adhesion (galling) | Coating essential, TiAlN or DLC |
| Copper/brass | Adhesion + smearing | Lower Co (6-8%), polished surface |
| High-strength steel | Impact + abrasion | Higher Co (12-14%), coarser grain |
The material you're stamping determines how your dies will fail, so adjust your grade selection accordingly. Stainless steel work-hardens and sticks aggressively to uncoated carbide—you'll likely need TiN or TiAlN coatings. Aluminum is notorious for galling (severe material transfer)—coatings are essential, not optional; uncoated carbide dies stamping aluminum will fail quickly from buildup. High-strength steel (AHSS, UHSS) hits harder and abrades more aggressively than mild steel—you need both toughness (more cobalt, coarser grain) and possibly coating for the combined challenge. Copper and brass smear rather than gall, so polished surfaces help more than coatings. Always adjust your grade to the specific workpiece material, not just the operation type.
Cold Heading Die Selection
Cold heading involves severe impact—each stroke compresses metal at high speed.
Die Components
| Component | FSSS (μm) | Co % | HRA | TRS (MPa) | Life Expectancy |
|---|---|---|---|---|---|
| Header die (1st blow) | 2.0-4.0 | 14-18 | 87.0-89.0 | 4200-4600 | 0.3-1M parts |
| Punch (heading) | 2.0-3.0 | 12-16 | 88.0-90.0 | 4000-4400 | 0.2-0.8M parts |
| Point die (trimming) | 1.0-2.0 | 10-12 | 90.0-91.5 | 3800-4200 | 0.5-2M parts |
| Extrusion insert | 1.5-2.5 | 12-15 | 88.5-90.5 | 4000-4400 | 0.1-0.5M parts |
| Knock-out pin | 1.5-3.0 | 10-12 | 89.5-91.0 | 3600-4000 | 0.5-2M parts |
Cold heading is brutal on tooling—each stroke is essentially a controlled explosion of force that compresses a metal blank into a fastener head or complex shape. The header die (first blow die) takes the worst abuse and uses the highest cobalt content (14-18% or even higher—some applications use up to 25% cobalt). Punches need slightly less toughness but still face severe impact. Point dies and extrusion inserts have more controlled loading but still require high TRS. The "Life Expectancy" column sets realistic expectations: even the best grades only last 0.1-2M parts depending on the component and fastener material. Don't expect cutting tool life from cold heading dies—the loading is fundamentally different.
Part Material Effects
| Heading Material | Grade Adjustment |
|---|---|
| Low carbon steel | Standard grades |
| Medium carbon steel | Increase Co 2%, coarser grain |
| Alloy steel | Higher Co (16-20%), coarsest practical grain |
| Stainless steel | Highest Co (18-25%), may need coating |
| Non-ferrous | Lower Co acceptable, watch for galling |
Harder materials hit harder—this is the fundamental reality of cold heading. Low carbon steel is the baseline that standard grades can handle. As you move to medium carbon, alloy steel, and especially stainless steel, you need progressively more cobalt and coarser grain to survive the increased impact forces. Stainless steel is particularly challenging because it work-hardens during heading, meaning each subsequent blow is harder than the last as the material becomes stiffer. Grades with 18-25% cobalt are common for stainless heading. Non-ferrous metals (aluminum, copper) are easier on the carbide in terms of impact, but watch for galling—material transfer that builds up and ruins dimensional accuracy.
Hot Extrusion Die Selection
Hot extrusion dies operate at 400-1200°C depending on material being extruded.
Temperature vs Grade
| Extrusion Temp | FSSS (μm) | Co % | HRA (room) | Notes |
|---|---|---|---|---|
| <500°C | 1.5-2.5 | 10-12 | 89.5-91.0 | Standard grade |
| 500-800°C | 2.0-3.0 | 12-14 | 88.5-90.0 | Higher Co for thermal shock |
| >800°C | 2.5-4.0 | 12-16 | 87.0-89.0 | Consider TiC additions |
Hot extrusion presents a unique challenge: the die softens significantly at operating temperature. A grade that measures 91 HRA at room temperature might only be 78-80 HRA at 800°C—a dramatic drop in wear resistance. Higher temperatures require more cobalt to handle thermal shock (the temperature swings as each billet enters and exits), but more cobalt also means more softening at temperature. Above 800°C, consider adding TiC (titanium carbide) to the formulation—TiC maintains hardness at elevated temperatures better than pure WC-Co. The room temperature HRA values shown are just the starting point; what matters is the hot hardness at your actual operating temperature.
Hot hardness: At 800°C, WC-Co loses ~10-15 HRA compared to room temperature. Adding 5-15% TiC maintains hardness at elevated temperatures.
Failure Modes and Diagnostics
| Failure Mode | Appearance | Cause | Prevention |
|---|---|---|---|
| Uniform wear | Gradual dimensional change | Normal operation | Accept, plan regrind schedule |
| Galling | Material transfer, scoring | Adhesive wear | Coating, surface treatment, lubricant |
| Chipping | Edge fractures | Grade too brittle | Increase Co 2-4% |
| Cracking | Thermal or fatigue cracks | Thermal shock or cyclic stress | Coarser grain, higher Co, preheat die |
| Spalling | Surface layer detachment | Subsurface fatigue | Cleaner grade (lower porosity), higher TRS |
| Erosion | Localized material loss | Particle impingement | Adjust angle, consider harder grade |
| Corrosion | Pitting, discoloration | Chemical attack on Co | Nickel binder, coating |
| Deformation | Dimensional drift without wear | Die too soft at operating temp | Harder grade, lower temp, TiC addition |
This diagnostic table helps you identify what went wrong when a die fails. Uniform wear is normal and expected—plan your regrind schedule around it. Galling (material transfer/scoring) is an adhesion problem indicating workpiece material is bonding to and tearing from the die surface—the solution is usually a coating (TiN, TiAlN, DLC), not a grade change. Chipping means the grade is too brittle for the loading—add cobalt. Cracking patterns tell you whether the problem is thermal (radial cracks from center) or fatigue (circumferential cracks)—both benefit from tougher grades. Spalling (surface layers peeling off) indicates subsurface fatigue crack propagation—demand cleaner material with lower porosity. Look at your failed die, match the symptom, and apply the prevention strategy for your next die.
Diagnostic Approach
- Measure wear pattern: Uniform = normal. Localized = geometry or lubrication problem.
- Check failure location: Bearing wear (normal). Entrance wear (wrong angle). Exit cracking (thermal).
- Examine surface: Smooth wear = abrasive. Rough/pulled = adhesive. Pitted = fatigue or erosion.
- Temperature check: Discoloration indicates overheating—improve cooling or adjust grade.
Quality Requirements for Dies
| Parameter | Standard Grade | Premium Die Grade | Why Critical |
|---|---|---|---|
| Porosity | A02-B02 | A00-A02 | Pores initiate fatigue cracks, cause surface defects |
| Hardness variation | ±0.5 HRA | ±0.3 HRA | Uniform wear rate |
| Grain size uniformity | ±15% | ±10% | Consistent properties, polish quality |
| TRS variation | ±10% | ±5% | Predictable die life |
| Surface finish (ground) | Ra 0.8 | Ra 0.2-0.4 | Starting point for final polish |
| Concentricity | 0.02 mm | 0.01 mm | Uniform product dimensions |
Premium die grades have tighter specifications than standard grades—and the premium is justified for high-volume production where die failure is expensive. Porosity is especially critical: pores are stress concentrators where fatigue cracks initiate, and dies under cyclic loading are essentially doing fatigue testing on every pore in the material. Demand A00-A02 porosity rating (ISO 4505) for dies that will see millions of cycles. Hardness and grain size uniformity ensure consistent wear across the entire die face—if one area wears faster, your products go out of tolerance prematurely. TRS variation matters for predictable maintenance scheduling: you can't plan die changes effectively if some dies fail at 500K cycles and others at 2M cycles.
Cost-Benefit Analysis
Die Life vs Grade Cost
| Grade Type | Relative Cost | Typical Life Increase | Best For |
|---|---|---|---|
| Standard | 1.0× | Baseline | Low volume, prototyping |
| Premium (fine grain) | 1.3-1.5× | 1.5-2× | Medium-high volume |
| Ultra-fine | 2.0-2.5× | 2-3× | High precision, fine wire |
| Nano-grain | 3.0-4.0× | 3-5× | Ultra-high volume, critical applications |
This table reveals the economics of premium grades. The key insight is that cost increase often lags behind life increase: a grade that costs 30% more but lasts 50% longer is a good investment. Nano-grain grades cost 3-4× more but can last 3-5× longer—worth it for high-volume production where downtime for die changes is expensive. For prototyping or low-volume work, standard grades are fine because die life doesn't significantly affect total cost. Match your investment to your production volume: calculate the total cost per part including die cost, regrind cost, and downtime, then see which grade minimizes that total.
Total Cost of Ownership
Example: Wire drawing die for copper wire
- Standard grade: $200, 10M meters life → $20/M meters
- Premium grade: $260, 18M meters life → $14.4/M meters
- Ultra-fine: $450, 35M meters life → $12.9/M meters
Include in calculation:
- Die cost
- Regrind cost (× number of regrinds)
- Downtime for die change
- Scrap from worn dies
- Quality costs from out-of-tolerance product
Key Takeaways
Match wear mechanism to grade. Abrasive wear → maximize hardness. Impact/fatigue → maximize TRS. Adhesive → consider coatings.
Wire drawing dies need the hardest grades. 3-6% Co, 0.5-1.5 μm grain, HRA >92 for fine wire applications.
Cold heading requires maximum toughness. 12-25% Co (yes, up to 25%), 2-4 μm grain, TRS >4000 MPa to survive impact.
Hot work demands thermal shock resistance. Higher Co (10-14%), coarser grain, possibly TiC additions for hot hardness.
Porosity is critical for fatigue life. Demand A00-A02 for dies under cyclic loading.
Die life justifies premium grades. A 50% cost increase often yields 100%+ life increase—calculate total cost of ownership.
Surface finish determines starting grain size. Mirror finish requires <1 μm grain; Ra 0.8 μm tolerates 2-3 μm grain.
