Vertical Roller Mill Liner Weld Overlay Repair Technology

1. Definition and Technical Principles

Vertical Roller Mill (VRM) liner weld overlay repair technology refers to the application of hardfacing and weld overlay processes to restore, rebuild, and extend the service life of worn protective liners inside vertical roller mills used extensively in cement, coal, and mineral processing industries. The technology involves the controlled deposition of wear-resistant alloy layers onto the base metal surfaces of mill liners, grinding rings, and trunnion rollers to recover lost dimensions, restore geometric integrity, and impart enhanced abrasion and impact resistance.

The fundamental principle relies on the metallurgical bonding between the overlay alloy and the base substrate, achieved through thermal arc processes. During the overlay process, the heat-affected zone (HAZ) undergoes controlled melting and resolidification, creating a diffusion bond interface. The overlay alloy is selected to provide a hardness gradient — softer transition layers near the substrate for stress accommodation and harder wear-resistant layers on the surface for abrasion resistance. The dilution ratio between the overlay and base metal is a critical parameter that directly governs the final hardness, microstructure, and wear life of the repaired liner.

The metallurgical mechanism involves the formation of martensitic or austenitic microstructures in the overlay layer, depending on the alloy chemistry. Chromium-molybdenum (Cr-Mo), cobalt-chromium (Co-Cr), and manganese-nickel (Mn-Ni) alloy systems are commonly employed. The rapid cooling rates typical of multi-pass overlay welding promote fine-grained microstructures and retained carbides (Cr₇C₃, Mo₂C, WC) that provide superior wear resistance against the abrasive grinding media and material being processed.

2. Category and Business Positioning

This technology falls squarely within the company's TIG/MIG Weld Overlay technology route, which represents one of the three principal technology pillars alongside hydraulic explosive bonding and explosion welding. Within the weld overlay portfolio, VRM liner repair occupies a specialized niche focused on large-format, in-situ or ex-situ restoration of heavy industrial grinding equipment.

The business positioning of this capability is multi-dimensional:

3. Technical Purpose and Value

The primary technical purposes of VRM liner weld overlay repair include:

4. Key Process and Implementation Points

4.1 Pre-Repair Assessment and Preparation

Every VRM liner repair begins with a comprehensive condition assessment. The following steps are mandatory:

  1. Visual Inspection and Dimensional Survey: Map all wear patterns using laser scanning or coordinate measurement. Document the maximum, minimum, and average wear depth. Identify any cracks, spalling, or fatigue damage.
  2. Base Metal Identification: Confirm the substrate material composition through spark testing or optical emission spectrometry (OES). Common base metals include Q235, Q345, 16Mn, and low-alloy steels. Any unknown material must be confirmed before selecting the overlay alloy.
  3. Crack Detection: Perform magnetic particle testing (MT) or ultrasonic testing (UT) in accordance with GB/T 26905 or ASTM E1444 to detect subsurface cracks. All detected cracks must be ground out and re-tested before overlay work begins.
  4. Surface Preparation: Grind the entire repair area with a minimum overlap of 50 mm beyond the wear boundary. The surface must be free of rust, scale, paint, and contaminants. Achieve a surface roughness of Ra 6.3–12.5 μm for optimal weld bead adhesion.
  5. Pre-Heating: Apply pre-heat to the base metal to a temperature of 150–250°C (for low-carbon steels) or 250–350°C (for medium-carbon or high-hardness substrates). Pre-heat reduces thermal gradient and minimizes the risk of hydrogen-induced cracking (HIC) in the HAZ.

4.2 Overlay Alloy Selection

The selection of the overlay alloy system is the most critical engineering decision in VRM liner repair. The following table summarizes common alloy systems and their applicability:

Alloy System Typical Composition Hardness (HRC) Wear Mechanism Impact Resistance Recommended Application
Cr-Mo-C (Type I) 5–10% Cr, 3–6% Mo, 1–2% C 50–58 Abrasive (cement, limestone) Good Cement VRM liners, moderate impact
Cr-Mo-C (Type II) 8–12% Cr, 5–8% Mo, 1.5–2.5% C 55–63 Abrasive + erosive Moderate Coal VRM liners, high abrasion
Co-Cr (Stellite-type) 25–35% Cr, 5–10% Mo, 1–3% C 40–48 Erosive + corrosive Excellent Hot/corrosive service, trunnion rollers
Mn-Ni (Hadfield-type) 10–14% Mn, 0.5–2% Ni, 0.5–1% C 45–55 (work-hardened) Impact abrasion Outstanding High-impact zones, trunnion raceways
Transition Layer (309L) 22–25% Cr, 12–14% Ni 22–28 (as-welded) — (bonding layer) Excellent First pass on Cr-Mo substrates

4.3 Welding Process Parameters

The overlay process is typically executed using either TIG (GTAW) for precision transition layers and thin first passes, or MIG (GMAW) for bulk build-up passes. The following table presents typical parameters:

Parameter TIG (Transition Layer) MIG (Build-Up Passes) Notes
Shielding Gas Argon (99.99%) Argon + 5% CO₂ or 100% Ar Flow rate: 15–20 L/min
Wire/Rod Diameter φ3.2 mm or φ4.0 mm φ1.2 mm or φ1.6 mm Select per thickness per pass
Current 150–250 A (DCEN) 200–350 A (DC+) or DC- Pulse MIG for reduced dilution
Voltage 18–24 V 22–30 V Adjust per travel speed
Travel Speed 60–100 mm/min 150–300 mm/min Higher speed = lower dilution
Interpass Temperature ≤250°C ≤300°C Monitor with IR thermometer
Target Bead Height 3–5 mm 5–8 mm Flat or slightly convex profile
Dilution Target ≤30% ≤25% Verify by OES on completed overlay

4.4 Multi-Pass Overlay Strategy

The overlay is built up in multiple passes following a structured strategy:

  1. Pass 1 — Transition/Bonding Layer: A single pass of 309L or equivalent austenitic stainless steel is deposited to create a metallurgical bridge between the base metal and the hardfacing alloy. This layer accommodates thermal expansion differences and prevents cracking at the interface. Bead width-to-height ratio should be ≤2.0:1.
  2. Passes 2–3 — Binder Layer: One to two passes of the selected hardfacing alloy are applied at controlled dilution to establish the alloy composition. Interpass grinding is performed between passes to remove any slag, oxidation, or undercut.
  3. Passes 4+ — Wear Layer: Additional passes of the hardfacing alloy are applied to achieve the required build-up thickness. The final pass should be directed such that the weld bead runs in the direction of material flow in the VRM, optimizing the wear surface profile.
  4. Post-Weld Heat Treatment (PWHT): For high-carbon overlay systems, a stress-relief anneal at 600–700°C for 2 hours is recommended to reduce residual stresses and prevent delayed cracking. The cooling rate from PWHT must be controlled (≤50°C/hour) to avoid temper embrittlement.

4.5 Post-Repair Finishing and Inspection

After overlay completion, the following finishing and inspection steps are performed:

5. Applicable Standards and Acceptance Criteria

5.1 Governing Standards

Standard Number Title / Scope Application in VRM Liner Repair
GB/T 12467 Welding — Welding procedure qualification WPS/PQR qualification for overlay processes
GB/T 985 Welding — Basic welding positions Positional welding qualification requirements
GB/T 26905 Magnetic particle testing of welds Surface defect detection acceptance
GB/T 11345 Ultrasonic testing of welds Subsurface defect detection for thick overlays
GB/T 19420 Welding procedure qualification for weld overlay Specific overlay qualification requirements
ASTM A396 Standard specification for carbon steel plate for pressure vessels Base metal material specification reference
ASTM A532 Standard specification for weld overlay materials Overlay alloy material qualification
ASTM E1444 Magnetic particle testing of welds NDT acceptance criteria
ASTM E2300 Ultrasonic testing of welds Subsurface NDT acceptance
ASTM E92 / E18 Vickers / Rockwell hardness testing Overlay hardness verification
ISO 9013 Welding procedure qualification — General principles International WPS qualification framework
NACE SP0287 Recommended practice for examination and qualification of welders Welder performance qualification
ASME IX Welding, Brazing, Fusing and Joining Qualifications WPS/PQR qualification (where applicable)

5.2 Acceptance Criteria Summary

6. Common Risks and Controls

Risk Root Cause Consequence Control Measures
Cracking in HAZ High carbon equivalent of base metal; insufficient pre-heat; rapid cooling Structural failure of liner; repair rejection Pre-heat to 200–300°C; use 309L transition layer; limit interpass temperature; apply PWHT; perform MT post-weld
Excessive Dilution Too-low travel speed; too-high current; inadequate bead profile control Reduced hardness; loss of wear resistance; overlay failure Use pulse MIG with optimized parameters; maintain flat bead geometry; verify dilution by OES after each critical pass
Spalling / Delamination High residual stress; hardness gradient too steep; thermal cycling in service Overlay material detachment during operation; equipment damage Apply PWHT; use graded hardness alloy system; limit single-pass thickness; design overlay to accommodate thermal expansion
Porosity Moisture contamination of wire/rod; inadequate shielding gas; oil on base metal Reduced overlay integrity; potential crack initiation site Store electrodes in drying ovens (150°C for 2 hours); ensure gas flow rate ≥15 L/min; degrease base metal with acetone
Undercut Excessive travel speed; incorrect torch angle; insufficient current Stress concentration; fatigue crack initiation Maintain travel speed within WPS range; use 75° torch angle for TIG; apply backing bar or filler to fill undercut before next pass
Field Welding Contamination Dust, debris, or moisture in field environment Poor weld quality; porosity; inconsistent hardness Set up windbreaks and welding tents; use IR pre-heat to evaporate moisture; perform witness tests on coupon before production welding

7. Application Across the Company's Three Technology Routes

7.1 TIG/MIG Weld Overlay (Primary Route for VRM Liner Repair)

VRM liner repair is the flagship application within the company's TIG/MIG weld overlay technology route. The company's established capabilities in this area include:

7.2 Hydraulic Explosive Bonding (Complementary Route)

While hydraulic explosive bonding is not directly applied to VRM liner repair, it contributes to the broader cladding ecosystem in the following ways:

7.3 Explosion Welding (Complementary Route)

Explosion welding serves a similar complementary role to hydraulic explosive bonding in the VRM ecosystem:

8. Contribution to Qualification Building, Product Delivery, and Customer Value

8.1 Qualification Building

The VRM liner weld overlay repair capability strengthens the company's qualification portfolio in several dimensions:

8.2 Product Delivery Enhancement

8.3 Customer Value Delivery

9. Conclusion

Vertical Roller Mill liner weld overlay repair technology represents a high-value, technically demanding capability that sits at the intersection of the company's weld overlay expertise and its industrial service orientation. By mastering the metallurgical, process, and quality control aspects of this technology — from alloy selection and multi-pass overlay strategy to NDT verification and post-repair performance tracking — the company positions itself as a comprehensive cladding and repair solutions provider rather than a pure fabrication shop. The synergy between this repair capability and the company's hydraulic explosive bonding and explosion welding routes creates a complete technology ecosystem that addresses the full lifecycle of cladded and overlay-protected industrial components, delivering measurable cost savings, availability improvements, and sustainability benefits to customers across the cement, power, and mineral processing sectors.