Hot Rolling Process Effects on Weld Microstructure and Residual Stress in Stainless Steel Clad Plates

1. Definition and Fundamental Principles

The interaction between hot rolling processes and the weld zone of stainless steel clad plates represents a critical metallurgical phenomenon that directly governs the mechanical performance, fatigue resistance, and service life of composite materials. When a stainless steel clad plate—fabricated through weld overlay, explosion welding, or hydraulic explosive bonding—undergoes subsequent hot rolling operations (such as pipe forming, ring rolling, or plate re-rolling), the weld interface and heat-affected zone (HAZ) are subjected to severe thermomechanical cycling that fundamentally alters the microstructural evolution and residual stress state established during the initial cladding process.

The fundamental metallurgical principles at play include:

2. Category and Business Positioning

This technical competency falls squarely within the post-cladding thermomechanical processing domain, serving as a critical knowledge bridge between the initial cladding fabrication process and the final product geometry. Within Cladding Technology Shanxi Co., Ltd.'s capability matrix, this understanding is essential for:

From a business perspective, mastery of this subject area enables the company to deliver fully rolled and formed clad products (pipes, rings, rolled sections) with confidence in interface integrity, thereby expanding the addressable market beyond flat clad plate into high-value pipe and ring applications.

3. Technical Purpose and Value

The systematic study and application of hot rolling effects on clad plate weld microstructure and residual stress serves multiple strategic purposes:

3.1 Technical Purposes

  1. Microstructural Control: Predict and control the grain size, phase distribution, and precipitate state at the clad interface after hot rolling to ensure compliance with code requirements for toughness, ductility, and corrosion resistance.
  2. Residual Stress Management: Quantify the net residual stress state (thermal + mechanical) after hot rolling to assess risk of SCC, fatigue failure, and dimensional instability during downstream welding or machining.
  3. Process Window Definition: Establish the allowable hot rolling temperature, reduction ratio, cooling rate, and interpass temperature ranges that maintain clad interface integrity without inducing detrimental microstructural changes.
  4. WPS/PQR Qualification Support: Provide metallurgical data to support welding procedure qualifications where clad products are subsequently joined by welding in the field or in fabrication shops.

3.2 Business Value

4. Key Process and Implementation Points

4.1 Critical Hot Rolling Parameters

Parameter Typical Range Effect on Weld Microstructure Effect on Residual Stress
Starting Rolling Temperature 1000–1150°C (austenitic SS); 1050–1200°C (duplex SS) Above recrystallization temperature: full grain refinement; below: partial recrystallization with retained elongated grains Higher temperatures promote greater thermal stress relaxation via creep
Total Reduction Ratio 10–30% per pass; cumulative 40–70% Higher reductions increase stored energy, driving more complete recrystallization; excessive reduction may cause edge cracking Higher reductions introduce greater mechanical residual stress due to differential strain
Rolling Speed 0.5–3.0 m/s Higher speeds increase adiabatic heating, potentially causing local overheating and grain coarsening in the weld zone Higher speeds reduce time for stress relaxation during deformation
Interpass Temperature 800–1050°C (maintained above recrystallization onset) Too low: strain accumulation without recovery leads to brittle microstructure; too high: grain coarsening Lower interpass temperatures preserve more mechanical residual stress
Cooling Rate After Rolling Controlled (furnace cool) or air cool; avoid water quench Slow cool: allows precipitate coarsening and possible σ-phase formation in susceptible alloys; rapid cool: retains fine grains but may increase residual stress Faster cooling rates increase thermal residual stress gradients
Number of Rolling Passes 2–6 passes depending on final geometry Multiple passes with adequate interpass recovery produce more uniform grain structure Multi-pass rolling with high interpass temperatures reduces net residual stress

4.2 Microstructural Assessment Protocol

  1. Sample Preparation: Extract longitudinal and transverse specimens from the weld zone, HAZ, and base metal of both clad and base layers. Metallographic preparation following ASTM E3 with final polish to 0.05 µm alumina.
  2. Optical Microscopy (OM): Examine grain size, phase distribution, inclusion morphology, and any signs of intergranular attack or cracking at the clad interface. Etch with appropriate reagents (e.g., Beraha's reagent for austenitic SS, Vilella's reagent for duplex SS).
  3. Scanning Electron Microscopy (SEM) with EDS: Characterize precipitate phases, segregation at grain boundaries, and elemental distribution across the weld interface. Perform line scans across the clad/base boundary.
  4. X-Ray Diffraction (XRD): Identify phase fractions (austenite, ferrite, martensite, precipitates) and quantify lattice strain as an indicator of localized residual stress.
  5. Hardness Mapping: Perform Vickers hardness traverses (HV0.5) across the clad thickness at 0.5 mm intervals to identify soft zones, hard zones, and microstructural transitions.

4.3 Residual Stress Measurement Methods

Method Standard Spatial Resolution Depth Sensitivity Applicability to Clad Plates
X-ray Diffraction (sin²ψ method) ASTM E975 ~0.1–0.5 mm Surface to ~100 µm Excellent for surface residual stress mapping across clad thickness
Hole Drilling ASTM E837 ~1–3 mm Surface to ~1 mm Good for bulk residual stress; requires sufficient material thickness
Neutron Diffraction ASTM E1482 ~0.5–1 mm Up to 15–30 mm (material dependent) Best for through-thickness residual stress profiles in thick clad plates
Slitting/Sectioning ASTM E2228 ~1 mm Full thickness Destructive; provides complete through-thickness residual stress profile
Contour Cracking ASTM E3975 ~0.5 mm Full thickness Useful for stress distribution mapping; semi-destructive

4.4 Process Optimization Strategy

The following decision logic should guide hot rolling parameter selection for clad plates:

  1. Assess the initial clad interface condition: Determine the as-welded (or as-bonded) microstructure, residual stress state, and any pre-existing defects through NDT and metallurgical examination.
  2. Define the target post-rolling condition: Based on the applicable product standard and end-use requirements, specify target grain size, phase fraction, hardness range, and maximum allowable residual stress.
  3. Select the rolling temperature window: Ensure the rolling temperature is above the recrystallization temperature of both the base and cladding materials to achieve complete microstructural homogenization. Avoid temperatures that promote σ-phase or other brittle intermetallic precipitation.
  4. Control the reduction schedule: Distribute total reduction across multiple passes with adequate interpass recovery to minimize mechanical residual stress buildup and ensure uniform deformation.
  5. Specify the cooling protocol: Match cooling rate to the alloy's precipitation kinetics to avoid detrimental phase formation while achieving target hardness and toughness.
  6. Validate through post-rolling inspection: Perform full metallurgical examination and residual stress measurement to confirm compliance with target specifications.

5. Applicable Standards and Acceptance Criteria

5.1 Product Standards

5.2 Residual Stress Acceptance Criteria

Application Category Standard Reference Maximum Allowable Residual Stress Measurement Location
Pressure vessels (general) ASME BPVC Section VIII Div. 1, UW-44 Not explicitly specified; stress relief recommended per UW-44 Weld zone and HAZ
Pressure vessels (SS clad) ASME BPVC Section VIII Div. 1, UCS-66 Stress relief required when specified; residual stress <0.5 σ_y recommended Clad interface and surface
Oil & gas pipelines API 5L / ASME B31.4 Longitudinal residual stress <0.4 σ_y for SCC-sensitive applications Full circumference and longitudinal
Nuclear components NB/T 20310 / RCC-E Strict limits per specific component design; typically <0.3 σ_y Full thickness profile
General industrial equipment GB/T 24511 / GB/T 17748 No explicit residual stress limit; stress relief recommended for SCC-prone environments Surface and clad interface

5.3 Metallurgical Acceptance Criteria

6. Common Risks and Controls

6.1 Microstructural Risks

Risk Mechanism Consequence Control Measures
σ-Phase Precipitation Rolling in the 600–850°C range promotes σ-phase nucleation in Cr-rich austenitic and duplex grades Severe embrittlement, loss of ductility, SCC susceptibility Maintain rolling temperature >900°C; avoid prolonged exposure in the σ-phase precipitation window; apply post-rolling solution heat treatment if necessary
Grain Coarsening Excessive rolling temperature or slow cooling allows grain growth beyond target specification Reduced toughness, lower fatigue strength Limit rolling temperature to minimum required for recrystallization; control cooling rate; verify grain size per ASTM E112
Partial Recrystallization Rolling temperature below recrystallization onset or insufficient strain per pass Retained elongated grains, anisotropic properties, incomplete stress relief Ensure rolling temperature ≥ T_rx + 50°C; maintain adequate reduction per pass (>15%); monitor interpass temperature
Carbon Segregation Non-equilibrium cooling after rolling allows carbon to segregate to grain boundaries Intergranular corrosion susceptibility, sensitization Control cooling rate; apply stabilizing heat treatment (620–650°C for Ti-stabilized grades); verify via ASTM A262 Practice 1E or 5A
Phase Transformation (Duplex SS) Excessive temperature or slow cooling shifts ferrite/austenite balance outside acceptable range Loss of duplex characteristics, reduced pitting resistance Monitor phase fraction via ASTM A240 requirements; control cooling rate; consider post-rolling solution treatment

6.2 Residual Stress Risks

Risk Mechanism Consequence Control Measures
Incomplete Stress Relief Rolling temperature insufficient for full stress relaxation; rapid cooling re-introduces thermal stresses SCC initiation at clad interface; fatigue cracking Verify residual stress via XRD or neutron diffraction; apply supplementary stress relief anneal (ASME UW-44) if required
Over-Stress Relief (Softening) Excessive temperature or prolonged hold time causes grain growth and hardness reduction Failure to meet minimum hardness or strength requirements Limit stress relief temperature and duration; verify hardness after treatment
Non-Uniform Stress Distribution Differential deformation between base and clad layers due to mismatch in flow stress Localized high-stress concentrations at the clad interface; distortion Use multi-pass rolling with controlled reduction per pass; model stress distribution using FEA; measure through-thickness stress profile
Hydrogen-Induced Cracking (HIC) Residual tensile stress combined with hydrogen pickup during rolling (from moisture, lubricants) Sub-surface cracking, particularly in high-strength base steels Control rolling atmosphere; use dry lubricants; apply post-rolling bake-out per NACE MR0175; monitor residual stress

6.3 Process Control Checklist

  1. Confirm hot rolling temperature is within the validated range for the specific alloy combination (base steel + cladding material).
  2. Verify that rolling lubricants are compatible with the clad material and will not introduce hydrogen contamination.
  3. Monitor and record rolling temperature, reduction ratio, and speed at each pass.
  4. Ensure interpass temperature remains above the minimum recrystallization temperature throughout the rolling sequence.
  5. Implement controlled cooling (furnace cool or air cool) to prevent re-introduction of high thermal residual stresses.
  6. Conduct post-rolling metallurgical examination: grain size, phase fraction, hardness profile, and precipitate assessment.
  7. Perform residual stress measurement at defined locations (surface, clad interface, mid-thickness) using validated methods.
  8. Apply supplementary stress relief treatment if measured residual stresses exceed acceptance criteria.
  9. Document all process parameters and inspection results in the product traceability record.

7. Application Across the Three Technology Routes

7.1 TIG/MIG Weld Overlay Route

In the TIG (Gas Tungsten Arc Welding) and MIG (Gas Metal Arc Welding) weld overlay process, the clad plate is built up by depositing successive layers of stainless steel filler metal onto a carbon or low-alloy steel base. The resulting weld structure exhibits a characteristic multi-pass weld with a fusion line at the base/weld interface and multiple interpass boundaries within the overlay.

Interaction with Hot Rolling:

Typical Application: Clad plates subsequently hot-rolled into pipe (per ASTM A335 or ASME SA-234) or formed into pressure vessel components. The weld overlay route offers flexibility in clad thickness (3–25 mm) and alloy selection, making it suitable for a wide range of hot-rolled product geometries.

7.2 Hydraulic Explosive Bonding (Hydrodynamic Explosive Welding) Route

Hydraulic explosive bonding (also known as hydrodynamic welding or hydraulic explosion welding) uses a shaped charge to generate a controlled detonation that propels the cladding material onto the base plate at high velocity (typically 300–700 m/s), achieving metallurgical bonding through jetting and plastic deformation at the interface.

Interaction with Hot Rolling:

Typical Application: Clad plates for hot-rolled pipe production where a thin, uniform cladding layer (0.5–3 mm) is required with minimal dilution. The hydraulic explosive bonding route is particularly suited for long-length products where weld overlay would be impractical.

7.3 Explosion Welding Route

Traditional explosion welding uses a high explosive charge to propel a cladding plate onto a base plate at supersonic velocities (typically 500–1000 m/s), achieving metallurgical bonding through intense plastic deformation, adiabatic shear, and jetting at the collision interface.

Interaction with Hot Rolling:

Typical Application: Thick clad plates (cladding thickness 1–10 mm) for pressure vessel and heat exchanger applications where the product is subsequently hot-rolled into pipe, ring, or formed shapes. The explosion welding route offers superior bond strength and minimal dilution, making it ideal for applications requiring high-performance cladding interfaces.

7.4 Comparative Summary

Characteristic TIG/MIG Weld Overlay Hydraulic Explosive Bonding Explosion Welding
Interface Morphology (As-Built) Flat fusion line with dilution zone Wavy/lobed with jetting zones Wavy with intense jetting and deformation
Interface Grain Size (As-Built) 10–100 µm (weld microstructure) 1–10 µm (deformation refined) 0.1–1 µm (ultrafine in jetting zones)
Post-Hot Rolling Interface Recrystallized weld grain structure; possible dilution zone homogenization Recrystallized; wavy morphology may be reduced Fully recrystallized; conventional grain size achieved
Residual Stress Relief by Hot Rolling Partial to significant relief (depends on temperature and cooling) Significant relief; new mechanical stresses possible Complete relief of welding residual stresses; new mechanical stresses introduced
Key Risk After Hot Rolling Incomplete stress relief; sensitization of dilution zone Interface flattening; potential bond weakening Loss of ultrafine grain benefits; interface homogenization
Supplementary Treatment Often Required Stress relief anneal (ASME UW-44) Usually not required if rolling parameters are optimized Usually not required; stress relief if code-specified

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

8.1 Qualification Building

8.2 Product Delivery

8.3 Customer Value

9. Conclusion

The systematic understanding of hot rolling process effects on stainless steel clad plate weld microstructure and residual stress represents a foundational technical competency for Cladding Technology Shanxi Co., Ltd. This knowledge bridges the gap between initial clad fabrication and final product performance, enabling the company to deliver metallurgically sound products across all three technology routes—TIG/MIG weld overlay, hydraulic explosive bonding, and explosion welding—regardless of subsequent hot rolling requirements.

By establishing validated process windows, comprehensive inspection protocols, and rigorous acceptance criteria aligned with international standards (GB, ASTM, ASME, API, NACE, ISO, NB/T), the company ensures that every clad product meets the highest standards of metallurgical integrity and residual stress control. This technical depth not only supports qualification building and code compliance but also delivers measurable value to customers through reduced risk, enhanced performance, and reliable long-term service in demanding industrial applications.

Continued investment in this technical area—through research, process optimization, and personnel training—will further strengthen the company's competitive position in the global clad materials market and ensure sustained growth in high-value applications across the oil & gas, power generation, chemical processing, and nuclear industries.